airbus ac a320 jun2012
TRANSCRIPT
@AIRBUSA320
AIRCRAFT CHARACTERISTICSAIRPORT AND MAINTENANCE PLANNING
AC
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© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.Customer Services
Technical Data Support and Services31707 Blagnac Cedex
FRANCE
Issue: Sep 30/85 Rev: Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 27 - Jun 01/12
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 1 R
Section 1-1
Subject 1-1-0
Purpose R PURPOSE CHANGED DUE TO MERGE OFTHE MFP AND AC MANUALS.PART EFFECTIVITYADDED/REVISED/DELETED
Section 01-02 D
CHAPTER 2 R
Section 2-1 R
Subject 2-1-0 R
General Airplane Characteristics R WEIGHT DEFINITIONS UPDATED.PART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-1-1 R
General Airplane Characteristics Data R ADDED WV 0017 AND 0018. OEW ANDPAYLOAD DELETED.PART EFFECTIVITYADDED/REVISED/DELETED
Section 2-2 R
Subject 2-2-0 R
General Aircraft Dimensions R REPLACED ”AIRPLANE” BY ”AIRCRAFT”AND COMPLETED TITLE OFILLUSTRATIONS.DESCRIPTION TITLE UPDATED
FIGURE General Aircraft Dimensions -Wing Tip Fence
R ILLUSTRATION REVISED
Section 2-3
Subject 2-3-0
HIGHLIGHTSPage 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Ground Clearances R REVISED GROUND CLEARANCES TOSHOW THE DIMENSIONS FOR A LIGHTAND HEAVY WEIGHT VARIANT.DELETED THE TERM ”OWE”.PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Clearances R
FIGURE Ground Clearances - GroundClearances with Sharklets
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Flaps andFlap Track Fairings When Flaps FullyExtended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Flaps andFlap Track Fairings When Flaps FullyExtended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Flap TrackFairings Up
N ILLUSTRATION ADDED
FIGURE Ground Clearances - AileronDown
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Aileron Upand Spoilers 1 to 5 Extended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - SlatsExtended
N ILLUSTRATION ADDED
Section 2-4
Subject 2-4-0
Interior Arrangements R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-4-1
Typical Configuration R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Typical Configuration - TypicalConfiguration Single-Class, High Density
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Typical Configuration - TypicalConfiguration Two-Class
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Section 2-5
Subject 2-5-0
Passenger Compartment Cross-section R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Passenger Compartment Cross-section
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Passenger Compartment Cross-section - Economy Class, 6 Abreast -Wider Aisle
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Passenger Compartment Cross-section - Passenger Compartment Cross-section, First-class
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 2-6 R
Subject 2-6-0
Cargo Compartments R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Cargo Compartments -Locations, Dimensions and LoadingCombinations
N ILLUSTRATION ADDED
Subject 02-06-01 D
Section 2-7
Subject 2-7-0
Doors Clearances R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-1
Forward Passenger / Crew Doors R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - ForwardPassenger / Crew Doors
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-2
Emergency Exits R PART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Doors Clearances - EmergencyExits
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-3
Aft Passenger / Crew Doors R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - Aft Passenger/ Crew Doors
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-4
Forward Cargo Compartment Door R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - ForwardCargo Compartment Door
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-5
Aft Cargo Compartment Door R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - Aft CargoCompartment Door
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-6
Bulk Cargo Compartment Door R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - Bulk CargoCompartment Door
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-7
Main Landing Gear Doors R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - Main LandingGear Doors
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Doors Clearances - Main LandingGear Doors (Bogie)
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-8
Radome R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - Radome R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 2-7-9
APU and Nose Landing Gear Doors R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Doors Clearances - APU andNose Landing Gear Doors
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 2-8 N
Subject 2-8-0 N
Escape Slides N
FIGURE Escape Slides - Location N ILLUSTRATION ADDED
FIGURE Escape Slides - Dimensions N ILLUSTRATION ADDED
Section 2-9 N
Subject 2-9-0 N
Landing Gear N
FIGURE Landing Gear - Main LandingGear - Twin Wheel
N ILLUSTRATION ADDED
FIGURE Landing Gear - Main LandingGear Dimensions - Twin Wheel
N ILLUSTRATION ADDED
FIGURE Landing Gear - Main LandingGear - Four Wheels - Bogie
N ILLUSTRATION ADDED
FIGURE Landing Gear - Main LandingGear Dimensions - Four Wheels - Bogie
N ILLUSTRATION ADDED
FIGURE Landing Gear - Nose LandingGear
N ILLUSTRATION ADDED
HIGHLIGHTSPage 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Landing Gear - Nose LandingGear Dimensions
N ILLUSTRATION ADDED
Landing Gear Maintenance Pits N
FIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes
N ILLUSTRATION ADDED
FIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes
N ILLUSTRATION ADDED
Section 2-10 N
Subject 2-10-0 N
Exterior Lighting N
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
Section 2-11 N
Subject 2-11-0 N
Antennas and Probes Location N
FIGURE Antennas and Probes - Location N ILLUSTRATION ADDED
Section 2-12 N
Subject 2-12-0 N
Auxiliary Power Unit N
FIGURE Auxiliary Power Unit - AccessDoors
N ILLUSTRATION ADDED
FIGURE Auxiliary Power Unit - GeneralLayout
N ILLUSTRATION ADDED
Engine and Nacelle N
FIGURE Power Plant Handling - MajorDimensions - CFM56 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - MajorDimensions - CFM56 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - FanCowls - CFM56 Series Engine
N ILLUSTRATION ADDED
HIGHLIGHTSPage 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Power Plant Handling - ThrustReverser Cowls - CFM56 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - MajorDimensions - IAE V2500 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - MajorDimensions - IAE V2500 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - FanCowls - IAE V2500 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - ThrustReverser Halves - IAE V2500 SeriesEngine
N ILLUSTRATION ADDED
Section 2-13 N
Subject 2-13-0 N
Leveling, Symmetry and Alignment N
FIGURE Location of the Leveling Points N ILLUSTRATION ADDED
Section 2-14 N
Subject 2-14-0 N
Jacking for Maintenance N
FIGURE Jacking for Maintenance -Jacking Point Location
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Forward Jacking Point
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - WingJacking Points
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - SafetyStay
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Jacking Design
N ILLUSTRATION ADDED
FIGURE Loads at the Aircraft JackingPoints - Forward Fuselage Jacking Point -Twin Wheel/Bogie
N ILLUSTRATION ADDED
FIGURE Loads at the Aircraft JackingPoints - Wing Jacking Point Rib 8 - TwinWheel/Bogie
N ILLUSTRATION ADDED
HIGHLIGHTSPage 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Jacking for Maintenance -Location of Shoring Cradles
N ILLUSTRATION ADDED
Jacking for Wheel Change N
FIGURE Landing Gear Jacking for WheelChange - MLG Jacking Point Location -Twin Wheels
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - MLG Jacking with CantileverJack - Twin Wheels
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at MLG Jacking Points -Twin Wheels
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - MLG Jacking Point LocationBogie
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - MLG Jacking Point LocationBogie
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - MLG Jacking Point LocationBogie
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at MLG Jacking Points -Bogie Version
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at MLG Jacking Points -77 000 kg
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - NLG Jacking - Point Location
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at NLG Jacking Points
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at NLG Jacking Points -77 000 kg
N ILLUSTRATION ADDED
CHAPTER 3 R
HIGHLIGHTSPage 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Section 3-1
Subject 3-1-0
General Information R PART EFFECTIVITYADDED/REVISED/DELETED
Section 3-2
Subject 3-2-0
Payload / Range R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 3-2-1
ISA Conditions R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Payload / Range - CFM56-5Aseries engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Payload / Range - CFM56-5Bseries engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Payload / Range - IAE V2500-A1 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Payload / Range - IAE V2500-A5 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 3-3
Subject 3-3-0
FAR / JAR Take-off Weight Limitation R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 3-3-1
ISA Conditions R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE FAR / JAR Take-off WeightLimitation - ISA Conditions -- CFM56series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE FAR / JAR Take-off WeightLimitation - ISA Conditions -- IAE V2500series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 3-3-2
ISA +15˚C (+59˚F) Conditions R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE FAR / JAR Take-off WeightLimitation - ISA +15˚C (+59˚F)Conditions -- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE FAR / JAR Take-off WeightLimitation - ISA +15˚C (+59˚F)Conditions -- IAE V2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 3-4
Subject 3-4-0
FAR / JAR Landing Field Length R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 3-4-1
ISA Conditions R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE FAR / JAR Landing Field Length- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE FAR / JAR Landing Field Length- IAE V2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 3-5
Subject 3-5-0
Final Approach Speed R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Final Approach Speed - CFM56series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Final Approach Speed - IAEV2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
CHAPTER 4
Section 4-1
Subject 4-1-0
General Information R PART EFFECTIVITYADDED/REVISED/DELETED
Section 4-2
Subject 4-2-0
Turning Radii R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Turning Radii, No Slip Angle -Turning Radii -- Dual Landing Gear
R ILLUSTRATION REVISED
FIGURE Turning Radii, No Slip Angle -Turning Radii -- Dual Landing Gear
N ILLUSTRATION ADDED
FIGURE Turning Radii, No Slip Angle -Turning Radii -- Bogie Landing Gear
R ILLUSTRATION REVISED
FIGURE Turning Radii, No Slip Angle -Turning Radii -- Bogie Landing Gear
N ILLUSTRATION ADDED
Section 4-3
Subject 4-3-0
Minimum Turning Radii R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Minimum Turning Radii R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 4-4
Subject 4-4-0
Visibility from Cockpit in Static Position N
FIGURE Visibility from Cockpit in StaticPosition
N ILLUSTRATION ADDED
HIGHLIGHTSPage 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Binocular Visibility ThroughWindows from Captain Eye Position
N ILLUSTRATION ADDED
Section 4-5 R
Subject 4-5-0
Runway and Taxiway Turn Paths R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 4-5-1
135˚ Turn - Runway to Taxiway R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE 135˚ Turn - Runway to Taxiway- Cockpit Over Centerline Method
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE 135˚ Turn - Runway to Taxiway- Judgemental Oversteering Method
N ILLUSTRATION ADDED
Subject 4-5-2
90˚ Turn - Runway to Taxiway R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE 90˚ Turn - Runway to Taxiway -Cockpit Over Centerline Method
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE 90˚ Turn - Runway to Taxiway -Judgemental Oversteering Method
N ILLUSTRATION ADDED
Subject 4-5-3 N
180˚ Turn on a Runway N
FIGURE 180˚ Turn on a Runway - Edgeof Runway Method
N ILLUSTRATION ADDED
Subject 4-5-4 N
135˚ Turn - Taxiway to Taxiway N
FIGURE 135˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
N ILLUSTRATION ADDED
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway R PART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE 90˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 4-6
Subject 4-6-0
Runway Holding Bay (Apron) R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Runway Holding Bay (Apron) R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
CHAPTER 5 R
Section 5-0
Subject 5-0-0
Terminal Servicing R PART EFFECTIVITYADDED/REVISED/DELETED
Section 5-1 R
Subject 5-1-0 R
Airplane Servicing Arrangements R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-1-1
Symbols Used on Servicing Diagrams R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-1-2 R
Typical Ramp Layout - Open Apron R TITLE CHANGED FROM ”AIRCRAFT ATTHE GATE” TO ”TYPICAL RAMPLAYOUT - OPEN APRON”. ADDED”STAND SAFETY LINE” DEFINITION.DESCRIPTION TITLE UPDATED
FIGURE Typical Ramp Layout - OpenApron - Bulk Loading
R ILLUSTRATION REVISED
FIGURE Typical Ramp Layout - OpenApron - ULD Loading
N ILLUSTRATION ADDED
Subject 5-1-3 R
HIGHLIGHTSPage 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Typical Ramp Layout - Gate R TITLE CHANGED FROM ”AIRCRAFT ATAN OPEN APRON” TO ”TYPICAL RAMPLAYOUT - GATE”. ADDED ”STANDSAFETY LINE” DEFINITION.DESCRIPTION TITLE UPDATED
FIGURE Typical Ramp Layout - Gate R ILLUSTRATION REVISED
Section 5-2 R
Subject 5-2-0 R
Terminal Operations - Full Servicing TurnRound Time
N
FIGURE Turn Round Stations - FullServicing (43 Min.)
N ILLUSTRATION ADDED
Subject 05-02-01 D
Section 5-3 R
Subject 5-3-0 R
Terminal Operation - Minimum ServicingTurn Round Time
N
FIGURE Turn Round Stations - MinimumServicing (23 Min.)
N ILLUSTRATION ADDED
Subject 05-03-01 D
Section 5-4
Subject 5-4-0
Ground Service Connections R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-1
Ground Service Connections Layout R DELETED GROUND SERVICECONNECTIONS LAYOUT TABLE.PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Ground Service Connections Layout
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-2
HIGHLIGHTSPage 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Grounding Points R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Grounding Points
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Grounding Points
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-3
Hydraulic System R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Hydraulic System - Green SystemGround Service Panel
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Hydraulic System - Blue SystemGround Service Panel
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Hydraulic System - YellowSystem Ground Service Panel
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-4
Electrical System R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -External Power Receptacles
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-5
Oxygen System R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-6
Fuel System R PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
HIGHLIGHTSPage 15
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Service Connections -Refuel/Defuel Panel
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Refuel/Defuel Couplings
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Gravity Refuel Couplings
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Overpressure Protector and NACA FlameArrestor
N ADDED OVERPRESSURE PROTECTORAND NACA FLAME ARRESTORILLUSTRATION.ILLUSTRATION ADDED
Subject 5-4-7
Pneumatic System R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-8
Potable Water System R UPDATED ACCESS PANEL 133AL ASOPTIONAL FOR A320.UPDATED ACCESS PANEL 133AL ASOPTIONAL FOR A320.PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Ground Service Connections -Potable Water Ground Drain Panel
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-9
Oil System R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Engine Oil Tank -- CFM56 Series Engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -IDG Oil Tank -- CFM56 Series Engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 16
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Service Connections -Starter Oil Tank -- CFM56 Series Engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Engine Oil Tank -- IAE V2500 SeriesEngine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -IDG Oil Tank -- IAE V2500 Series Engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Starter Oil Tank -- IAE V2500 SeriesEngine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -APU Oil Tank
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-10
Vacuum Toilet System R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Service Connections -Waste Water Ground Service Panel
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 5-5
Subject 5-5-0
Engine Starting Pneumatic Requirements R PART EFFECTIVITYADDED/REVISED/DELETEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements
N ILLUSTRATION ADDED
Subject 5-5-1 R
Low Ambient Temperatures R DESCRIPTION TITLE UPDATEDPART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 17
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Engine Starting PneumaticRequirements - Low AmbientTemperature -40˚C (-40˚F) -- CFM56series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements - Low AmbientTemperature -40˚C (-40˚F) -- IAE V2500series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-5-2 R
Medium Ambient Temperatures R DESCRIPTION TITLE UPDATEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements - Medium AmbientTemperature +15˚C (+59˚F) -- CFM56series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements - Medium AmbientTemperature +15˚C (+59˚F) -- IAEV2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-5-3 R
High Ambient Temperatures R DESCRIPTION TITLE UPDATEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements - High AmbientTemperature +55˚C (+131˚F) -- CFM56series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements - High AmbientTemperature +50˚C (+122˚F) -- IAEV2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 5-6
Subject 5-6-0
HIGHLIGHTSPage 18
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Ground Pneumatic Power Requirements R DELETED THE AIRFLOW DATA TABLE.ADDED A NOTE FOR GROUNDPNEUMATIC POWER REQUIREMENTS.PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
Subject 5-6-1
Heating R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Pneumatic PowerRequirements - Heating
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-6-2
Cooling R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Pneumatic PowerRequirements - Cooling
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 5-7
Subject 5-7-0
Preconditioned Airflow Requirements R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Preconditioned AirflowRequirements
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 5-8
Subject 5-8-0
Ground Towing Requirements R SAE REFERENCES UPDATED ANDFIGURES CORRESPONDING TO TYPICALTOW BAR CONFIGURATION DELETEDPART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
HIGHLIGHTSPage 19
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Towing Requirements R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 5-9 N
Subject 5-9-0 N
De-Icing and External Cleaning N REVISED TABLES FOR DE-ICING ANDEXTERNAL CLEANING AREAS.
CHAPTER 6
Section 6-1
Subject 6-1-0
Engine Exhaust Velocities andTemperatures
R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-1-1
Engine Exhaust Velocities Contours -Ground Idle Power
R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Velocities -Ground Idle Power -- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Velocities -Ground Idle Power -- IAE V2500 seriesengine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-1-2
Engine Exhaust Temperatures Contours -Ground Idle Power
R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Temperatures -Ground Idle Power -- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Temperatures -Ground Idle Power -- IAE V2500 seriesengine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-1-3
Engine Exhaust Velocities Contours -Breakaway Power
R PART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 20
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Engine Exhaust Velocities -Breakaway Power -- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Velocities -Breakaway Power -- IAE V2500 seriesengine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-1-4
Engine Exhaust Temperatures Contours -Breakaway Power
R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Temperatures -Breakaway Power -- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Temperatures -Breakaway Power -- IAE V2500 seriesengine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-1-5
Engine Exhaust Velocities Contours -Takeoff Power
R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Velocities -Takeoff Power -- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Velocities -Takeoff Power -- IAE V2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-1-6
Engine Exhaust Temperatures Contours -Takeoff Power
R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Temperatures -Takeoff Power -- CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Engine Exhaust Temperatures -Takeoff Power -- IAE V2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 6-2
Subject 6-2-0
HIGHLIGHTSPage 21
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Airport and Community Noise R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-2-1
Noise Data R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Airport and Community Noise -CFM56-5A series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Airport and Community Noise -CFM56-5B series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Airport and Community Noise -IAE V2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 6-3
Subject 6-3-0
Danger Areas of Engines R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-3-1
Ground Idle Power R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Danger Areas of Engines -CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Danger Areas of Engines - IAEV2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-3-2
Takeoff Power R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Danger Areas of Engines -CFM56 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 22
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Danger Areas of Engines - IAEV2500 series engine
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 6-4
Subject 6-4-0
APU Exhaust Velocities and Temperatures R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 6-4-1
APU - APIC & GARRETT R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Exhaust Velocities andTemperatures - APU -- APIC &GARRETT
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
CHAPTER 7
Section 7-1
Subject 7-1-0
General Information R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Aircraft Codes R ILLUSTRATION REVISED
Section 7-2
Subject 7-2-0
Landing Gear Footprint R PART EFFECTIVITYADDED/REVISED/DELETEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Landing Gear Footprint R ILLUSTRATION REVISED
FIGURE Landing Gear Footprint R
FIGURE Landing Gear Footprint R
Section 7-3
Subject 7-3-0
Maximum Pavement Loads R PART EFFECTIVITYADDED/REVISED/DELETED
HIGHLIGHTSPage 23
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Maximum Pavement Loads R
FIGURE Maximum Pavement Loads R ILLUSTRATION REVISED
FIGURE Maximum Pavement Loads R
FIGURE Maximum Pavement Loads R
FIGURE Maximum Pavement Loads R
FIGURE Maximum Pavement Loads R
Section 7-4
Subject 7-4-0
Landing Gear Loading on Pavement R UPDATED TITLE FOR REFERENCESECTION 7-4-1 LANDING GEAR LOADINGON PAVEMENT.PART EFFECTIVITYADDED/REVISED/DELETED
Subject 7-4-1
Landing Gear Loading on Pavement R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
HIGHLIGHTSPage 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement
N ILLUSTRATION ADDED
Section 7-5
Subject 7-5-0
Flexible Pavement Requirements - U.S.Army Corps of Engineers Design Method
R UPDATED TITLE FOR REFERENCESECTION 7-5-1 FLEXIBLE PAVEMENTREQUIREMENTS.PART EFFECTIVITYADDED/REVISED/DELETED
Subject 7-5-1
Flexible Pavement Requirements - U.S.Army Corps of Engineers Design Method
R DELETED TWO FIGURES FOR THE A/CCODE ”P”.PART EFFECTIVITYADDED/REVISED/DELETEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
R
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements R
Section 7-6
Subject 7-6-0
HIGHLIGHTSPage 25
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Flexible Pavement Requirements - LCNConversion
R UPDATED TITLE FOR REFERENCESECTION 7-6-1 FLEXIBLE PAVEMENTREQUIREMENTS.PART EFFECTIVITYADDED/REVISED/DELETED
Subject 7-6-1
Flexible Pavement Requirements - LCNConversion
R DELETED TWO FIGURES FOR THE A/CCODE ”P”.PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Flexible Pavement Requirements- LCN Conversion
R
FIGURE Flexible Pavement Requirements- LCN Conversion
R
FIGURE Flexible Pavement Requirements- LCN Conversion
R ILLUSTRATION REVISED
FIGURE Flexible Pavement Requirements- LCN Conversion
R
FIGURE Flexible Pavement Requirements- LCN Conversion
R
FIGURE Flexible Pavement Requirements- LCN Conversion
R
Section 7-7
Subject 7-7-0
Rigid Pavement Requirements - PortlandCement Association Design Method
R UPDATED TITLE FOR REFERENCESECTION 07-07-01 RIGID PAVEMENTREQUIREMENTS (PCA).PART EFFECTIVITYADDED/REVISED/DELETED
Subject 7-7-1
HIGHLIGHTSPage 26
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Rigid Pavement Requirements - PortlandCement Association Design Method
R DELETED TWO FIGURES FOR THE A/CCODE ”P”.PART EFFECTIVITYADDED/REVISED/DELETEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Rigid Pavement Requirements(PCA)
R
FIGURE Rigid Pavement Requirements(PCA)
R
FIGURE Rigid Pavement Requirements(PCA)
R
FIGURE Rigid Pavement Requirements(PCA)
R
FIGURE Rigid Pavement Requirements(PCA)
R
FIGURE Rigid Pavement Requirements(PCA)
R
Section 7-8 R
Subject 07-08-00 D
Subject 7-8-1
Radius of Relative Stiffness R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Radius of Relative Stiffness -(Reference: Portland Cement Association)
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Subject 7-8-2
Rigid Pavement Requirements - LCNConversion
R MOVED THE TEXT FROM 7-8-0 TO 7-8-2.PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Rigid Pavement Requirements -LCN Conversion
R
FIGURE Rigid Pavement Requirements -LCN Conversion
R
HIGHLIGHTSPage 27
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Rigid Pavement Requirements -LCN Conversion
R
FIGURE Rigid Pavement Requirements -LCN Conversion
R
FIGURE Rigid Pavement Requirements -LCN Conversion
R
FIGURE Rigid Pavement Requirements -LCN Conversion
R ILLUSTRATION REVISED
FIGURE Rigid Pavement Requirements -LCN Conversion
R
FIGURE Rigid Pavement Requirements -LCN Conversion
R ILLUSTRATION REVISED
Subject 7-8-3
Radius of Relative Stiffness (Other valuesof ”E” and ”L”)
R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 7-8-4
Radius of Relative Stiffness R PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Radius of Relative Stiffness -(Effect E and µ on ”L” values)
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
Section 7-9
Subject 7-9-0
ACN/PCN Reporting System R UPDATED TITLE FOR REFERENCESECTION 7-9-1 AND 7-9-2.PART EFFECTIVITYADDED/REVISED/DELETED
Subject 7-9-1
Aircraft Classification Number - FlexiblePavement
R DELETED TWO FIGURES FOR THE A/CCODE ”P”.PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Aircraft Classification Number --Flexible Pavement
R
HIGHLIGHTSPage 28
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number --Flexible Pavement
R
FIGURE Aircraft Classification Number --Flexible Pavement
R
FIGURE Aircraft Classification Number --Flexible Pavement
R
FIGURE Aircraft Classification Number --Flexible Pavement
R
FIGURE Aircraft Classification Number --Flexible Pavement
R
FIGURE Aircraft Classification Number --Flexible Pavement
R
Subject 7-9-2
Aircraft Classification Number - RigidPavement
R DELETED TWO FIGURES FOR THE A/CCODE ”P”.PART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Aircraft Classification Number --Rigid Pavement
R
FIGURE Aircraft Classification Number --Rigid Pavement
R
FIGURE Aircraft Classification Number --Rigid Pavement
R
FIGURE Aircraft Classification Number --Rigid Pavement
R
FIGURE Aircraft Classification Number --Rigid Pavement
R
FIGURE Aircraft Classification Number --Rigid Pavement
R
CHAPTER 8 R
Section 8-0 N
Subject 8-0-0 N
Scaled Drawings N
FIGURE Scaled Drawing N ILLUSTRATION ADDED
HIGHLIGHTSPage 29
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Section 08-01 D
CHAPTER 10 N
Section 10-0 N
Subject 10-0-0 N
Aircraft Rescue and Fire Fighting N
FIGURE Front Page N ILLUSTRATION ADDED
FIGURE Highly Flammable and HazardousMaterials and Components
N ILLUSTRATION ADDED
FIGURE Wheel Safety Area N ILLUSTRATION ADDED
FIGURE Composite Materials N ILLUSTRATION ADDED
FIGURE LG Ground Lock Safety Devices N ILLUSTRATION ADDED
FIGURE Evacuation/Escape Slide/Raft N ILLUSTRATION ADDED
FIGURE Pax/Crew Doors N ILLUSTRATION ADDED
FIGURE Emergency Exit Hatch N ILLUSTRATION ADDED
FIGURE FWD and AFT Lower DeckCargo Doors
N ILLUSTRATION ADDED
FIGURE Control Panels N ILLUSTRATION ADDED
FIGURE APU Access Door N ILLUSTRATION ADDED
FIGURE Aircraft Ground Clearances N ILLUSTRATION ADDED
FIGURE Structural Break-in Points N ILLUSTRATION ADDED
HIGHLIGHTSPage 30
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 27 - Jun 01/12
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 1
Subject 1-1-0
Purpose R Jun 01/12
CHAPTER 2
Subject 2-1-0
General Airplane Characteristics R Jun 01/12
Subject 2-1-1
General Airplane Characteristics Data R Jun 01/12
Subject 2-2-0
General Aircraft Dimensions R Jun 01/12
FIGURE General Aircraft Dimensions - Wing Tip Fence R Jun 01/12
Subject 2-3-0
Ground Clearances R Jun 01/12
FIGURE Ground Clearances R Jun 01/12
FIGURE Ground Clearances - Ground Clearances with Sharklets N Jun 01/12
FIGURE Ground Clearances - Flaps and Flap Track Fairings WhenFlaps Fully Extended
N Jun 01/12
FIGURE Ground Clearances - Flaps and Flap Track Fairings WhenFlaps Fully Extended
N Jun 01/12
FIGURE Ground Clearances - Flap Track Fairings Up N Jun 01/12
FIGURE Ground Clearances - Aileron Down N Jun 01/12
FIGURE Ground Clearances - Aileron Up and Spoilers 1 to 5 Extended N Jun 01/12
FIGURE Ground Clearances - Slats Extended N Jun 01/12
Subject 2-4-0
Interior Arrangements R Jun 01/12
Subject 2-4-1
Typical Configuration R Jun 01/12
L.E.C.Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Typical Configuration - Typical Configuration Single-Class,High Density
R Jun 01/12
FIGURE Typical Configuration - Typical Configuration Two-Class R Jun 01/12
Subject 2-5-0
Passenger Compartment Cross-section R Jun 01/12
FIGURE Passenger Compartment Cross-section R Jun 01/12
FIGURE Passenger Compartment Cross-section - Economy Class, 6Abreast - Wider Aisle
R Jun 01/12
FIGURE Passenger Compartment Cross-section - PassengerCompartment Cross-section, First-class
R Jun 01/12
Subject 2-6-0
Cargo Compartments R Jun 01/12
FIGURE Cargo Compartments - Locations, Dimensions and LoadingCombinations
N Jun 01/12
Subject 2-7-0
Doors Clearances R Jun 01/12
Subject 2-7-1
Forward Passenger / Crew Doors R Jun 01/12
FIGURE Doors Clearances - Forward Passenger / Crew Doors R Jun 01/12
Subject 2-7-2
Emergency Exits R Jun 01/12
FIGURE Doors Clearances - Emergency Exits R Jun 01/12
Subject 2-7-3
Aft Passenger / Crew Doors R Jun 01/12
FIGURE Doors Clearances - Aft Passenger / Crew Doors R Jun 01/12
Subject 2-7-4
Forward Cargo Compartment Door R Jun 01/12
FIGURE Doors Clearances - Forward Cargo Compartment Door R Jun 01/12
Subject 2-7-5
Aft Cargo Compartment Door R Jun 01/12
L.E.C.Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Doors Clearances - Aft Cargo Compartment Door R Jun 01/12
Subject 2-7-6
Bulk Cargo Compartment Door R Jun 01/12
FIGURE Doors Clearances - Bulk Cargo Compartment Door R Jun 01/12
Subject 2-7-7
Main Landing Gear Doors R Jun 01/12
FIGURE Doors Clearances - Main Landing Gear Doors R Jun 01/12
FIGURE Doors Clearances - Main Landing Gear Doors (Bogie) R Jun 01/12
Subject 2-7-8
Radome R Jun 01/12
FIGURE Doors Clearances - Radome R Jun 01/12
Subject 2-7-9
APU and Nose Landing Gear Doors R Jun 01/12
FIGURE Doors Clearances - APU and Nose Landing Gear Doors R Jun 01/12
Subject 2-8-0
Escape Slides N Jun 01/12
FIGURE Escape Slides - Location N Jun 01/12
FIGURE Escape Slides - Dimensions N Jun 01/12
Subject 2-9-0
Landing Gear N Jun 01/12
FIGURE Landing Gear - Main Landing Gear - Twin Wheel N Jun 01/12
FIGURE Landing Gear - Main Landing Gear Dimensions - Twin Wheel N Jun 01/12
FIGURE Landing Gear - Main Landing Gear - Four Wheels - Bogie N Jun 01/12
FIGURE Landing Gear - Main Landing Gear Dimensions - FourWheels - Bogie
N Jun 01/12
FIGURE Landing Gear - Nose Landing Gear N Jun 01/12
FIGURE Landing Gear - Nose Landing Gear Dimensions N Jun 01/12
Landing Gear Maintenance Pits N Jun 01/12
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes N Jun 01/12
L.E.C.Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes N Jun 01/12
Subject 2-10-0
Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
Subject 2-11-0
Antennas and Probes Location N Jun 01/12
FIGURE Antennas and Probes - Location N Jun 01/12
Subject 2-12-0
Auxiliary Power Unit N Jun 01/12
FIGURE Auxiliary Power Unit - Access Doors N Jun 01/12
FIGURE Auxiliary Power Unit - General Layout N Jun 01/12
Engine and Nacelle N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - CFM56 SeriesEngine
N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - CFM56 SeriesEngine
N Jun 01/12
FIGURE Power Plant Handling - Fan Cowls - CFM56 Series Engine N Jun 01/12
FIGURE Power Plant Handling - Thrust Reverser Cowls - CFM56Series Engine
N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - IAE V2500Series Engine
N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - IAE V2500Series Engine
N Jun 01/12
FIGURE Power Plant Handling - Fan Cowls - IAE V2500 SeriesEngine
N Jun 01/12
FIGURE Power Plant Handling - Thrust Reverser Halves - IAE V2500Series Engine
N Jun 01/12
Subject 2-13-0
L.E.C.Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Leveling, Symmetry and Alignment N Jun 01/12
FIGURE Location of the Leveling Points N Jun 01/12
Subject 2-14-0
Jacking for Maintenance N Jun 01/12
FIGURE Jacking for Maintenance - Jacking Point Location N Jun 01/12
FIGURE Jacking for Maintenance - Forward Jacking Point N Jun 01/12
FIGURE Jacking for Maintenance - Wing Jacking Points N Jun 01/12
FIGURE Jacking for Maintenance - Safety Stay N Jun 01/12
FIGURE Jacking for Maintenance - Jacking Design N Jun 01/12
FIGURE Loads at the Aircraft Jacking Points - Forward FuselageJacking Point - Twin Wheel/Bogie
N Jun 01/12
FIGURE Loads at the Aircraft Jacking Points - Wing Jacking PointRib 8 - Twin Wheel/Bogie
N Jun 01/12
FIGURE Jacking for Maintenance - Location of Shoring Cradles N Jun 01/12
Jacking for Wheel Change N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - MLG JackingPoint Location - Twin Wheels
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - MLG Jacking withCantilever Jack - Twin Wheels
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at MLGJacking Points - Twin Wheels
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - MLG JackingPoint Location Bogie
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - MLG JackingPoint Location Bogie
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - MLG JackingPoint Location Bogie
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at MLGJacking Points - Bogie Version
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at MLGJacking Points - 77 000 kg
N Jun 01/12
L.E.C.Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Jacking for Wheel Change - NLG Jacking -Point Location
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at NLGJacking Points
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at NLGJacking Points - 77 000 kg
N Jun 01/12
CHAPTER 3
Subject 3-1-0
General Information R Jun 01/12
Subject 3-2-0
Payload / Range R Jun 01/12
Subject 3-2-1
ISA Conditions R Jun 01/12
FIGURE Payload / Range - CFM56-5A series engine R Jun 01/12
FIGURE Payload / Range - CFM56-5B series engine R Jun 01/12
FIGURE Payload / Range - IAE V2500-A1 series engine R Jun 01/12
FIGURE Payload / Range - IAE V2500-A5 series engine R Jun 01/12
Subject 3-3-0
FAR / JAR Take-off Weight Limitation R Jun 01/12
Subject 3-3-1
ISA Conditions R Jun 01/12
FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions --CFM56 series engine
R Jun 01/12
FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions --IAE V2500 series engine
R Jun 01/12
Subject 3-3-2
ISA +15˚C (+59˚F) Conditions R Jun 01/12
FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C(+59˚F) Conditions -- CFM56 series engine
R Jun 01/12
FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C(+59˚F) Conditions -- IAE V2500 series engine
R Jun 01/12
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Jun 01/12
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Subject 3-4-0
FAR / JAR Landing Field Length R Jun 01/12
Subject 3-4-1
ISA Conditions R Jun 01/12
FIGURE FAR / JAR Landing Field Length - CFM56 series engine R Jun 01/12
FIGURE FAR / JAR Landing Field Length - IAE V2500 series engine R Jun 01/12
Subject 3-5-0
Final Approach Speed R Jun 01/12
FIGURE Final Approach Speed - CFM56 series engine R Jun 01/12
FIGURE Final Approach Speed - IAE V2500 series engine R Jun 01/12
CHAPTER 4
Subject 4-1-0
General Information R Jun 01/12
Subject 4-2-0
Turning Radii R Jun 01/12
FIGURE Turning Radii, No Slip Angle - Turning Radii -- Dual LandingGear
R Jun 01/12
FIGURE Turning Radii, No Slip Angle - Turning Radii -- Dual LandingGear
N Jun 01/12
FIGURE Turning Radii, No Slip Angle - Turning Radii -- BogieLanding Gear
R Jun 01/12
FIGURE Turning Radii, No Slip Angle - Turning Radii -- BogieLanding Gear
N Jun 01/12
Subject 4-3-0
Minimum Turning Radii R Jun 01/12
FIGURE Minimum Turning Radii R Jun 01/12
Subject 4-4-0
Visibility from Cockpit in Static Position N Jun 01/12
FIGURE Visibility from Cockpit in Static Position N Jun 01/12
FIGURE Binocular Visibility Through Windows from Captain EyePosition
N Jun 01/12
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Subject 4-5-0
Runway and Taxiway Turn Paths R Jun 01/12
Subject 4-5-1
135˚ Turn - Runway to Taxiway R Jun 01/12
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
N Jun 01/12
Subject 4-5-2
90˚ Turn - Runway to Taxiway R Jun 01/12
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
N Jun 01/12
Subject 4-5-3
180˚ Turn on a Runway N Jun 01/12
FIGURE 180˚ Turn on a Runway - Edge of Runway Method N Jun 01/12
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway N Jun 01/12
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
N Jun 01/12
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway R Jun 01/12
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
Subject 4-6-0
Runway Holding Bay (Apron) R Jun 01/12
FIGURE Runway Holding Bay (Apron) R Jun 01/12
CHAPTER 5
Subject 5-0-0
Terminal Servicing R Jun 01/12
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Subject 5-1-0
Airplane Servicing Arrangements R Jun 01/12
Subject 5-1-1
Symbols Used on Servicing Diagrams R Jun 01/12
Subject 5-1-2
Typical Ramp Layout - Open Apron R Jun 01/12
FIGURE Typical Ramp Layout - Open Apron - Bulk Loading R Jun 01/12
FIGURE Typical Ramp Layout - Open Apron - ULD Loading N Jun 01/12
Subject 5-1-3
Typical Ramp Layout - Gate R Jun 01/12
FIGURE Typical Ramp Layout - Gate R Jun 01/12
Subject 5-2-0
Terminal Operations - Full Servicing Turn Round Time N Jun 01/12
FIGURE Turn Round Stations - Full Servicing (43 Min.) N Jun 01/12
Subject 5-3-0
Terminal Operation - Minimum Servicing Turn Round Time N Jun 01/12
FIGURE Turn Round Stations - Minimum Servicing (23 Min.) N Jun 01/12
Subject 5-4-0
Ground Service Connections R Jun 01/12
Subject 5-4-1
Ground Service Connections Layout R Jun 01/12
FIGURE Ground Service Connections - Ground Service ConnectionsLayout
R Jun 01/12
Subject 5-4-2
Grounding Points R Jun 01/12
FIGURE Ground Service Connections - Grounding Points R Jun 01/12
FIGURE Ground Service Connections - Grounding Points R Jun 01/12
Subject 5-4-3
Hydraulic System R Jun 01/12
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FIGURE Hydraulic System - Green System Ground Service Panel R Jun 01/12
FIGURE Hydraulic System - Blue System Ground Service Panel R Jun 01/12
FIGURE Hydraulic System - Yellow System Ground Service Panel R Jun 01/12
Subject 5-4-4
Electrical System R Jun 01/12
FIGURE Ground Service Connections - External Power Receptacles R Jun 01/12
Subject 5-4-5
Oxygen System R Jun 01/12
Subject 5-4-6
Fuel System R Jun 01/12
FIGURE Ground Service Connections - Refuel/Defuel Panel R Jun 01/12
FIGURE Ground Service Connections - Refuel/Defuel Couplings R Jun 01/12
FIGURE Ground Service Connections - Gravity Refuel Couplings R Jun 01/12
FIGURE Ground Service Connections - Overpressure Protector andNACA Flame Arrestor
N Jun 01/12
Subject 5-4-7
Pneumatic System R Jun 01/12
Subject 5-4-8
Potable Water System R Jun 01/12
FIGURE Ground Service Connections - Potable Water Ground DrainPanel
R Jun 01/12
Subject 5-4-9
Oil System R Jun 01/12
FIGURE Ground Service Connections - Engine Oil Tank -- CFM56Series Engine
R Jun 01/12
FIGURE Ground Service Connections - IDG Oil Tank -- CFM56 SeriesEngine
R Jun 01/12
FIGURE Ground Service Connections - Starter Oil Tank -- CFM56Series Engine
R Jun 01/12
FIGURE Ground Service Connections - Engine Oil Tank -- IAE V2500Series Engine
R Jun 01/12
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FIGURE Ground Service Connections - IDG Oil Tank -- IAE V2500Series Engine
R Jun 01/12
FIGURE Ground Service Connections - Starter Oil Tank -- IAE V2500Series Engine
R Jun 01/12
FIGURE Ground Service Connections - APU Oil Tank R Jun 01/12
Subject 5-4-10
Vacuum Toilet System R Jun 01/12
FIGURE Ground Service Connections - Waste Water Ground ServicePanel
R Jun 01/12
Subject 5-5-0
Engine Starting Pneumatic Requirements R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements N Jun 01/12
Subject 5-5-1
Low Ambient Temperatures R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Low AmbientTemperature -40˚C (-40˚F) -- CFM56 series engine
R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Low AmbientTemperature -40˚C (-40˚F) -- IAE V2500 series engine
R Jun 01/12
Subject 5-5-2
Medium Ambient Temperatures R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Medium AmbientTemperature +15˚C (+59˚F) -- CFM56 series engine
R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Medium AmbientTemperature +15˚C (+59˚F) -- IAE V2500 series engine
R Jun 01/12
Subject 5-5-3
High Ambient Temperatures R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - High AmbientTemperature +55˚C (+131˚F) -- CFM56 series engine
R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - High AmbientTemperature +50˚C (+122˚F) -- IAE V2500 series engine
R Jun 01/12
Subject 5-6-0
Ground Pneumatic Power Requirements R Jun 01/12
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Subject 5-6-1
Heating R Jun 01/12
FIGURE Ground Pneumatic Power Requirements - Heating R Jun 01/12
Subject 5-6-2
Cooling R Jun 01/12
FIGURE Ground Pneumatic Power Requirements - Cooling R Jun 01/12
Subject 5-7-0
Preconditioned Airflow Requirements R Jun 01/12
FIGURE Preconditioned Airflow Requirements R Jun 01/12
Subject 5-8-0
Ground Towing Requirements R Jun 01/12
FIGURE Ground Towing Requirements R Jun 01/12
Subject 5-9-0
De-Icing and External Cleaning N Jun 01/12
CHAPTER 6
Subject 6-1-0
Engine Exhaust Velocities and Temperatures R Jun 01/12
Subject 6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power R Jun 01/12
FIGURE Engine Exhaust Velocities - Ground Idle Power -- CFM56series engine
R Jun 01/12
FIGURE Engine Exhaust Velocities - Ground Idle Power -- IAE V2500series engine
R Jun 01/12
Subject 6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power R Jun 01/12
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- CFM56series engine
R Jun 01/12
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- IAEV2500 series engine
R Jun 01/12
Subject 6-1-3
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Engine Exhaust Velocities Contours - Breakaway Power R Jun 01/12
FIGURE Engine Exhaust Velocities - Breakaway Power -- CFM56series engine
R Jun 01/12
FIGURE Engine Exhaust Velocities - Breakaway Power -- IAE V2500series engine
R Jun 01/12
Subject 6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power R Jun 01/12
FIGURE Engine Exhaust Temperatures - Breakaway Power -- CFM56series engine
R Jun 01/12
FIGURE Engine Exhaust Temperatures - Breakaway Power -- IAEV2500 series engine
R Jun 01/12
Subject 6-1-5
Engine Exhaust Velocities Contours - Takeoff Power R Jun 01/12
FIGURE Engine Exhaust Velocities - Takeoff Power -- CFM56 seriesengine
R Jun 01/12
FIGURE Engine Exhaust Velocities - Takeoff Power -- IAE V2500series engine
R Jun 01/12
Subject 6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power R Jun 01/12
FIGURE Engine Exhaust Temperatures - Takeoff Power -- CFM56series engine
R Jun 01/12
FIGURE Engine Exhaust Temperatures - Takeoff Power -- IAE V2500series engine
R Jun 01/12
Subject 6-2-0
Airport and Community Noise R Jun 01/12
Subject 6-2-1
Noise Data R Jun 01/12
FIGURE Airport and Community Noise - CFM56-5A series engine R Jun 01/12
FIGURE Airport and Community Noise - CFM56-5B series engine R Jun 01/12
FIGURE Airport and Community Noise - IAE V2500 series engine R Jun 01/12
Subject 6-3-0
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Danger Areas of Engines R Jun 01/12
Subject 6-3-1
Ground Idle Power R Jun 01/12
FIGURE Danger Areas of Engines - CFM56 series engine R Jun 01/12
FIGURE Danger Areas of Engines - IAE V2500 series engine R Jun 01/12
Subject 6-3-2
Takeoff Power R Jun 01/12
FIGURE Danger Areas of Engines - CFM56 series engine R Jun 01/12
FIGURE Danger Areas of Engines - IAE V2500 series engine R Jun 01/12
Subject 6-4-0
APU Exhaust Velocities and Temperatures R Jun 01/12
Subject 6-4-1
APU - APIC & GARRETT R Jun 01/12
FIGURE Exhaust Velocities and Temperatures - APU -- APIC &GARRETT
R Jun 01/12
CHAPTER 7
Subject 7-1-0
General Information R Jun 01/12
FIGURE Aircraft Codes R Jun 01/12
Subject 7-2-0
Landing Gear Footprint R Jun 01/12
FIGURE Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint R Jun 01/12
FIGURE Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint R Jun 01/12
FIGURE Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint May 01/11
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FIGURE Landing Gear Footprint R Jun 01/12
FIGURE Landing Gear Footprint May 01/11
Subject 7-3-0
Maximum Pavement Loads R Jun 01/12
FIGURE Maximum Pavement Loads R Jun 01/12
FIGURE Maximum Pavement Loads R Jun 01/12
FIGURE Maximum Pavement Loads R Jun 01/12
FIGURE Maximum Pavement Loads R Jun 01/12
FIGURE Maximum Pavement Loads R Jun 01/12
FIGURE Maximum Pavement Loads R Jun 01/12
Subject 7-4-0
Landing Gear Loading on Pavement R Jun 01/12
Subject 7-4-1
Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement N Jun 01/12
FIGURE Landing Gear Loading on Pavement N Jun 01/12
Subject 7-5-0
Flexible Pavement Requirements - U.S. Army Corps of EngineersDesign Method
R Jun 01/12
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Subject 7-5-1
Flexible Pavement Requirements - U.S. Army Corps of EngineersDesign Method
R Jun 01/12
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
R Jun 01/12
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
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FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements R Jun 01/12
FIGURE Flexible Pavement Requirements R Jun 01/12
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion R Jun 01/12
Subject 7-6-1
Flexible Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion R Jun 01/12
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LAST REVISIONDATE
FIGURE Flexible Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Flexible Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Flexible Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Flexible Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
Subject 7-7-0
Rigid Pavement Requirements - Portland Cement Association DesignMethod
R Jun 01/12
Subject 7-7-1
Rigid Pavement Requirements - Portland Cement Association DesignMethod
R Jun 01/12
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
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FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) R Jun 01/12
FIGURE Rigid Pavement Requirements (PCA) R Jun 01/12
FIGURE Rigid Pavement Requirements (PCA) R Jun 01/12
FIGURE Rigid Pavement Requirements (PCA) R Jun 01/12
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) R Jun 01/12
FIGURE Rigid Pavement Requirements (PCA) R Jun 01/12
FIGURE Rigid Pavement Requirements (PCA) May 01/11
Subject 7-8-1
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Radius of Relative Stiffness R Jun 01/12
FIGURE Radius of Relative Stiffness - (Reference: Portland CementAssociation)
R Jun 01/12
Subject 7-8-2
Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
Subject 7-8-3
Radius of Relative Stiffness (Other values of ”E” and ”L”) R Jun 01/12
Subject 7-8-4
Radius of Relative Stiffness R Jun 01/12
FIGURE Radius of Relative Stiffness - (Effect E and µ on ”L” values) R Jun 01/12
Subject 7-9-0
ACN/PCN Reporting System R Jun 01/12
Subject 7-9-1
Aircraft Classification Number - Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
Subject 7-9-2
Aircraft Classification Number - Rigid Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
L.E.C.Page 22
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Rigid Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Rigid Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Rigid Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement R Jun 01/12
L.E.C.Page 23
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Rigid Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
CHAPTER 8
Subject 8-0-0
Scaled Drawings N Jun 01/12
FIGURE Scaled Drawing N Jun 01/12
CHAPTER 10
Subject 10-0-0
Aircraft Rescue and Fire Fighting N Jun 01/12
FIGURE Front Page N Jun 01/12
FIGURE Highly Flammable and Hazardous Materials and Components N Jun 01/12
FIGURE Wheel Safety Area N Jun 01/12
FIGURE Composite Materials N Jun 01/12
FIGURE LG Ground Lock Safety Devices N Jun 01/12
FIGURE Evacuation/Escape Slide/Raft N Jun 01/12
FIGURE Pax/Crew Doors N Jun 01/12
FIGURE Emergency Exit Hatch N Jun 01/12
FIGURE FWD and AFT Lower Deck Cargo Doors N Jun 01/12
FIGURE Control Panels N Jun 01/12
FIGURE APU Access Door N Jun 01/12
FIGURE Aircraft Ground Clearances N Jun 01/12
FIGURE Structural Break-in Points N Jun 01/12
L.E.C.Page 24
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TABLE OF CONTENTS
1 SCOPE
1-1-0 Purpose
2 AIRCRAFT DESCRIPTION
2-1-0 General Aircraft Characteristics
2-1-1 General Aircraft Characteristics Data
2-2-0 General Aircraft Dimensions
2-3-0 Ground Clearances
2-4-0 Interior Arrangements
2-4-1 Passenger Compartment Layout
2-5-0 Passenger Compartment Cross Section
2-6-0 Cargo Compartments
2-7-0 Door Clearances
2-7-1 Forward Passenger / Crew Doors
2-7-2 Emergency Exits
2-7-3 Aft Passenger / Crew Doors
2-7-4 Forward Cargo Compartment Doors
2-7-5 Aft Cargo Compartment Doors
2-7-6 Bulk Cargo Compartment Doors
2-7-7 Main Landing Gear Doors
2-7-8 Radome
2-7-9 APU and Nose Landing Gear Doors
2-8-0 Escape Slides
2-9-0 Landing Gear
2-10-0 Exterior Lighting
2-11-0 Antennas and Probes Location
2-12-0 Power Plant
2-13-0 Leveling, Symmetry and Alignment
2-14-0 Jacking
3 AIRCRAFT PERFORMANCE
3-1-0 General Information
3-2-0 Payload / Range
3-2-1 ISA Conditions
3-3-0 FAR / JAR Takeoff Weight Limitation
T.O.C.Page 1
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1 ISA Conditions
3-3-2 ISA +15˚C (+59˚F) Conditions
3-4-0 FAR / JAR Landing Field Length
3-4-1 ISA Conditions
3-5-0 Final Approach Speed
4 GROUND MANEUVERING
4-1-0 General Information
4-2-0 Turning Radii
4-3-0 Minimum Turning Radii
4-4-0 Visibility from Cockpit in Static Position
4-5-0 Runway and Taxiway Turn Paths
4-5-1 135˚ Turn - Runway to Taxiway
4-5-2 90˚ Turn - Runway to Taxiway
4-5-3 180˚ Turn on a Runway
4-5-4 135˚ Turn - Taxiway to Taxiway
4-5-5 90˚ Turn - Taxiway to Taxiway
4-6-0 Runway Holding Bay (Apron)
5 TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
5-1-0 Servicing Arrangements
5-1-1 Symbols Used on Servicing Diagrams
5-1-2 Typical Ramp Layout - Open Apron
5-1-3 Typical Ramp Layout - Gate
5-2-0 Terminal Operations - Full Servicing
5-3-0 Terminal Operation - Transit
5-4-0 Ground Service Connections
5-4-1 Ground Service Connections Layout
5-4-2 Grounding Points
5-4-3 Hydraulic System
5-4-4 Electrical System
5-4-5 Oxygen System
5-4-6 Fuel System
5-4-7 Pneumatic System
5-4-8 Potable Water System
5-4-9 Oil System
5-4-10 Vacuum Toilet System
T.O.C.Page 2
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
5-5-1 Low Ambient Temperatures
5-5-2 Medium Ambient Temperatures
5-5-3 High Ambient Temperatures
5-6-0 Ground Pneumatic Power Requirements
5-6-1 Heating
5-6-2 Cooling
5-7-0 Preconditioned Airflow Requirements
5-8-0 Ground Towing Requirements
5-9-0 De-Icing and External Cleaning
6 OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
6-2-0 Airport and Community Noise
6-2-1 Noise Data
6-3-0 Danger Areas of Engines
6-3-1 Ground Idle Power
6-3-2 Takeoff Power
6-4-0 APU Exhaust Velocities and Temperatures
6-4-1 APU
7 PAVEMENT DATA
7-1-0 General Information
7-2-0 Landing Gear Footprint
7-3-0 Maximum Pavement Loads
7-4-0 Landing Gear Loading on Pavement
7-4-1 Landing Gear Loading on Pavement
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-6-0 Flexible Pavement Requirements - LCN Conversion
7-6-1 Flexible Pavement Requirements - LCN Conversion
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-1 Radius of Relative Stiffness
7-8-2 Rigid Pavement Requirements - LCN Conversion
7-8-3 Radius of Relative Stiffness (Other values of E and L)
7-8-4 Radius of Relative Stiffness
7-9-0 ACN/PCN Reporting System
7-9-1 Aircraft Classification Number - Flexible Pavement
7-9-2 Aircraft Classification Number - Rigid Pavement
8 SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
10 AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0 Purpose
**ON A/C A320-200
Purpose
1. GeneralThe A320 AIRCRAFT CHARACTERISTICS -- AIRPORT AND MAINTENANCE PLANNING (AC)manual is issued for the A320-200 series aircraft, equipped with wing-tip fences or Sharklets toprovide necessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO)for airport and maintenance facilities planning.
This revision is now a merge of the Maintenance Facility planning (MFP) document and the AirplaneCharacteristics for Airport Planning (AC). This document has been renamed Aircraft Characteristics --Airport and Maintenance Planning (AC) to reflect this change.Additionally, a chapter 10 ”Aircraft Rescue and Fire Fighting” has been added to the AC. Thischapter contains the illustrations of the Aircraft Rescue and Fire fighting Charts poster and replacesthe PDF document that was available for download.
The data given in this issue of the A320-200 AC equipped with Sharklets can be subject to changepending completion of the flight test phase. It is given for guidance only and does not constitute acontractual commitment.
This non-customized document conforms to NAS 3601 specification.This document must not be used for training purposes.
The single aisle A320 Family is a short to medium range aircraft delivering superior fuel efficiency,passenger comfort, environmental characteristics and economics, with a global market coverage.With record number of operators and wide market approval, the A320 Family benefits fromcontinuous improvements such as:- Sharklets- New Engine Option (neo)The A320 Family wider fuselage, advanced troubleshooting and Cargo Loading System enable easyand cost effective ground handling, whilst minimizing aircraft turn round time.
This document does not include the A320neo which is under development.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services
1-1-0Page 1
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1, Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0Page 2
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-0 General Aircraft Characteristics
**ON A/C A320-200
General Airplane Characteristics
1. General Airplane CharacteristicsThe weight terms used throughout this manual are given below together with their respectivedefinitions.
Maximum Taxi Weight (MTW):Maximum weight for ground maneuver as limited by aircraft strength and airworthiness requirements.(It includes weight of run-up and taxi fuel). It is also called Maximum Ramp Weight (MRW).
Maximum Landing Weight (MLW):Maximum weight for landing as limited by aircraft strength and airworthiness requirements.
Maximum Takeoff Weight (MTOW):Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (This isthe maximum weight at start of the takeoff run).
Maximum Zero Fuel Weight (MZFW):Maximum operational weight of the aircraft without usable fuel.
Standard Seating Capacity:Number of passengers specifically certified or anticipated for certification.
Usable Volume:Usable volume available for cargo, pressurized fuselage, passenger compartment and cockpit.
Usable Fuel Capacity:Fuel available for aircraft propulsion.
Water Volume:Volume of cargo compartment.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-1-1 General Aircraft Characteristics Data
**ON A/C A320-200
General Airplane Characteristics Data
1. The following table provides characteristics of A320-200 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004
Kilograms 73 900 68 400 70 400 75 900 71 900Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds162 922 150 796 155 205 167 331 158 512
Kilograms 73 500 68 000 70 000 75 500 71 500Maximum TakeoffWeight (MTOW) Pounds 162 040 149 914 154 324 166 449 157 630
Kilograms 64 500 64 500 64 500 64 500 64 500Maximum LandingWeight (MLW) Pounds 142 198 142 198 142 198 142 198 142 198
Kilograms 60 500 60 500 60 500 60 500 60 500Maximum Zero FuelWeight (MZFW) Pounds 133 380 133 380 133 380 133 380 133 380
Aircraft CharacteristicsWV005 WV006 WV007 WV008 WV009
Kilograms 67 400 66 400 77 400 73 900 75 900Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds148 592 146 387 170 638 162 922 167 331
Kilograms 67 000 66 000 77 000 73 500 75 500Maximum TakeoffWeight (MTOW) Pounds 147 710 145 505 169 756 162 040 166 449
Kilograms 64 500 64 500 64 500 64 500 64 500Maximum LandingWeight (MLW) Pounds 142 198 142 198 142 198 142 198 142 198
Kilograms 60 500 60 500 60 500 61 000 61 000Maximum Zero FuelWeight (MZFW) Pounds 133 380 133 380 133 380 134 482 134 482
Aircraft CharacteristicsWV010 WV011 WV012 WV013 WV014
Kilograms 77 400 75 900 77 400 71 900 73 900Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds170 638 167 331 170 638 158 512 162 922
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsWV010 WV011 WV012 WV013 WV014
Kilograms 77 000 75 500 77 000 71 500 73 500Maximum TakeoffWeight (MTOW) Pounds 169 756 166 449 169 756 157 630 162 040
Kilograms 64 500 66 000 66 000 64 500 64 500Maximum LandingWeight (MLW) Pounds 142 198 145 505 145 505 142 198 142 198
Kilograms 61 000 62 500 62 500 61 000 61 500Maximum Zero FuelWeight (MZFW) Pounds 134 482 137 789 137 789 134 482 135 584
Aircraft CharacteristicsWV015 WV016 WV017 WV018
Kilograms 78 400 73 900 78 400 71 900Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds172 842 162 922 172 482 158 512
Kilograms 78 000 73 500 78 000 71 500Maximum Takeoff Weight(MTOW) Pounds 171 961 162 040 171 961 157 630
Kilograms 64 500 66 000 66 000 66 000Maximum Landing Weight(MLW) Pounds 142 198 145 505 145 505 145 505
Kilograms 61 000 62 500 62 500 62 500Maximum Zero Fuel Weight(MZFW) Pounds 134 482 137 789 137 789 137 789
2. The following table provides characteristics of A320-200 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard Seating Capacity Single-class 180
Liters 23 859 - 26 759* - 29 659**US gallons 6 303 - 7 069* - 7 835**
Kilograms (density= 0.785 kg/l) 18 729 - 21 005* - 23 282**
Usable Fuel Capacity
Pounds 41 290 - 46 308* - 51 328**Cubic meters 330Pressurized Fuselage Volume
(A/C non equipped) Cubic feet 11 654
Cubic meters 139Passenger Compartment VolumeCubic feet 4 909Cubic meters 9Cockpit VolumeCubic feet 318Cubic meters 13.28Usable Volume, FWD CCCubic feet 469
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsCubic meters 18.26Usable Volume, AFT CCCubic feet 645Cubic meters 5.88Usable Volume, Bulk CCCubic meters 208Cubic meters 15.56Water Volume, FWD CCCubic feet 549.5Cubic meters 20.77Water Volume, AFT CCCubic feet 733.5Cubic meters 7.76Water Volume, Bulk CCCubic feet 274
* OPTION: 1 ACT** OPTION: 2 ACT
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0 General Aircraft Dimensions
**ON A/C A320-200
General Aircraft Dimensions
1. This section provides General Aircraft Dimensions.
2-2-0Page 1
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
12.64 m(41.47 ft)
5.07 m
(16.63 ft)
4.14
m(1
3.58
ft)
5.87
m
(19.
26 ft
)
RELATED TO AIRCRAFT ATTITUDE AND WEIGHTN_AC_020200_1_0040101_01_03
12.45 m(40.85 ft)
34.10 m(111.88 ft)
7.59 m(24.90 ft)
0.93 m(3.05 ft)
0.50 m(1.64 ft)
8.95 m(29.36 ft)
General Aircraft DimensionsWing Tip Fence (Sheet 1 of 4)
FIGURE-2-2-0-991-004-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RELATED TO AIRCRAFT ATTITUDE AND WEIGHTN_AC_020200_1_0040104_01_00
37.57 m(123.26 ft)
5.75
m(1
8.86
ft)
11.9
1 m
(39.
07 ft
)
8.30
m(2
7.23
ft)
11.12 m(36.48 ft)
V2500
11.19 m(36.71 ft)
CFM56
3.95
m(1
2.96
ft)
4.87
m(1
5.98
ft)
General Aircraft DimensionsWing Tip Fence (Sheet 2 of 4)
FIGURE-2-2-0-991-004-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
12.64 m(41.47 ft)
5.07 m(16.63 ft)
4.14
m(1
3.58
ft)
5.87
m
(19.
26 ft
)
RELATED TO AIRCRAFT ATTITUDE AND WEIGHTN_AC_020200_1_0040103_01_01
7.59 m(24.90 ft)
0.93 m(3.05 ft)
0.50 m(1.64 ft)
12.45 m
(40.85 ft)
35.80 m
(117.45 ft)
8.95 m(29.36 ft)
3.79 m(12.43 ft)
2.43 m(7.97 ft)
General Aircraft DimensionsSharklet (Sheet 3 of 4)
FIGURE-2-2-0-991-004-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
37.57 m(123.26 ft)
5.75
m(1
8.86
ft)
11.9
1 m
(39.
07 ft
)
8.30
m(2
7.23
ft)
11.13 m(36.52 ft)
V2500
11.19 m(36.71 ft)
CFM56
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
3.95
m(1
2.96
ft)
4.87
m(1
5.98
ft)
16.2
9 m
(53.
44 ft
)
1.61 m(5.28 ft)
3.22 m(10.56 ft)
1.64 m(5.38 ft)
23.45 m(76.94 ft)
N_AC_020200_1_0040105_01_00
General Aircraft DimensionsSharklet (Sheet 4 of 4)
FIGURE-2-2-0-991-004-A01
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2-3-0 Ground Clearances
**ON A/C A320-200
Ground Clearances
1. This section gives the height of various points of the aircraft, above the ground, for different aircraftconfigurations.Dimensions in the tables are approximate and will vary with tire type, weight and balance and otherspecial conditions.
The dimensions are given for:- a light weight, for an A/C in maintenance configuration with a mid CG,- the MRW for a light weight variant with a FWD CG and a AFT CG,- the MRW for a heavy weight variant with a FWD CG and a AFT CG,- aircraft on jacks, FDL at 4.6 m (15.09 ft).
NOTE : Passenger and cargo door clearances are measured from the center of the door sill and fromfloor level.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
A
CG 26.5% FWD CG 17% FWD CG 17% AFT CG 36.8%
11.426.865.976.40
19.5919.982.202.795.648.9210.3311.457.28
BC1C2D1D2
E (CFM)E (IAE)
FF1F2F3G
11.096.535.686.10
19.2619.681.902.495.358.63
10.0411.156.99
11.426.765.875.87
19.4619.461.942.535.288.539.9511.026.79
11.326.695.775.87
19.3619.461.902.495.258.539.94
13.558.897.977.9721.5921.594.074.667.41
10.6612.07
12.14H 11.84 11.45
11.02 13.166.79 8.8911.48 13.55
39.63J 39.37 38.75 38.81 40.8512.76K1 12.47 12.27 12.27 14.3715.94K2 15.65 15.45 15.45 17.5518.24L 17.95 17.36 17.45 19.467.51M 7.22 6.92 6.92 9.02
13.06N 12.73 12.76 12.73 14.89
AFT CG 40%
14.04P 13.68 14.14 14.01 16.2715.88Q 15.62 14.96 15.06 17.06
11.096.505.646.0419.2319.651.872.465.318.5610.0111.126.9611.8139.3012.4015.6217.917.19
12.7013.6815.55
P B D1 E C2 M Q JC1 D2G
L F F1 F2 F3
K1 K2
3.482.091.821.955.976.090.670.851.722.723.153.492.223.70
12.083.894.865.562.293.984.284.84
3.381.991.731.865.876.000.580.761.632.633.063.402.133.61
12.003.804.775.472.203.884.174.76
3.482.061.791.795.935.930.590.771.612.603.033.362.073.4911.813.744.715.292.113.894.314.56
3.381.981.721.845.865.990.570.751.622.613.053.392.123.6011.983.784.765.462.193.874.174.74
3.452.041.761.795.905.930.580.761.602.603.033.362.073.5011.833.744.715.322.113.884.274.59
4.132.712.432.436.586.581.241.422.263.253.684.012.714.13
12.454.385.355.932.754.544.965.20
m ft m ft m ft m ft m ft m ft
NOTE:FROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
A/C JACKED FDLA/CCONFIG−URATION
41 t 74 tMRW
78 tMRW
= 4.60 m(15.09 ft)
A
N
N_AC_020300_1_0040101_01_05
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED
H
Ground ClearancesFIGURE-2-3-0-991-004-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_020300_1_0290101_01_00
A
CG 26.5% FWD CG 17% FWD CG 17% AFT CG 36.8%
11.426.865.976.40
19.5919.982.202.795.648.9210.3311.457.28
BC1C2D1D2
E (CFM)E (IAE)
FF1F2F3G
11.096.535.686.10
19.2619.681.902.495.358.63
10.0411.156.99
11.426.765.875.87
19.4619.461.942.535.288.539.9511.026.79
11.326.695.775.87
19.3619.461.902.495.258.539.94
13.558.897.977.97
21.5921.594.074.667.41
10.6612.07
12.14H 11.84 11.45
11.02 13.166.79 8.8911.48 13.55
39.63J 39.37 38.75 38.81 40.8513.65K1 13.35 13.16 13.16 15.2622.31K2 22.01 21.82 21.82 23.7918.24L 17.95 17.36 17.45 19.467.51M 7.22 6.92 6.92 9.02
13.06N 12.73 12.76 12.73 14.89
AFT CG 40%
14.04P 13.68 14.14 14.01 16.2715.88Q 15.62 14.96 15.06 17.06
11.096.505.646.0419.2319.651.872.465.318.5610.0111.126.9611.8139.3013.2921.9817.917.19
12.7013.6815.55
3.482.091.821.955.976.090.670.851.722.723.153.492.223.70
12.084.166.805.562.293.984.284.84
3.381.991.731.865.876.000.580.761.632.633.063.402.133.61
12.004.076.715.472.203.884.174.76
3.482.061.791.795.935.930.590.771.612.603.033.362.073.4911.814.016.655.292.113.894.314.56
3.381.981.721.845.865.990.570.751.622.613.053.392.123.6011.984.056.705.462.193.874.174.74
3.452.041.761.795.905.930.580.761.602.603.033.362.073.5011.834.016.655.322.113.884.274.59
4.132.712.432.436.586.581.241.422.263.253.684.012.714.13
12.454.657.255.932.754.544.965.20
m ft m ft m ft m ft m ft m ft
NOTE:PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
P A B C1 E C2 G M H Q
F3F2F1FL
JD1
K2
K1
42 tMRW74 t
MRW78 t
A/C JACKED
= 4.60 m(15.09 ft)
FDLA/CCONFIG−URATION
D2
N
Ground ClearancesGround Clearances with Sharklets
FIGURE-2-3-0-991-029-A01
2-3-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
m ft m ft m ft
A
B
C
D
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
2.09
2.82
2.86
3.68
1.99
2.71
2.75
3.56
1.96
2.69
2.72
3.52
6.86 6.53 6.43
11.5511.6812.07
9.25
9.38
8.89
9.02
8.83
8.92
CFM 56 ENGINE
DCBA
N_AC_020300_1_0160101_01_00
2.18
2.66
3.10
7.15
8.73
10.17
2.08
2.55
2.99
6.82
8.37
9.81
2.05
2.52
2.95
6.73
8.27
9.68
E
F
G
E F G
Ground ClearancesFlaps and Flap Track Fairings When Flaps Fully Extended
FIGURE-2-3-0-991-016-A01
2-3-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
m ft
6.86
8.50
9.94
6.73
11.94
9.09
9.22
m ft m ft
A
B
C
D
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUNDIAE V2500 ENGINE
DCBA
2.09
2.59
3.03
1.98
2.48
2.92
6.49
8.14
9.58
1.95
2.44
2.88
6.40
8.01
9.45
E
F
G
E F G
N_AC_020300_1_0170101_01_00
2.05
2.77
2.81
3.64
1.94
2.66
2.70
3.53
1.92
2.64
2.68
3.49
6.37 6.30
11.4511.58
8.73
8.86
8.66
8.78
Ground ClearancesFlaps and Flap Track Fairings When Flaps Fully Extended
FIGURE-2-3-0-991-017-A01
2-3-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2.68
3.08
3.48
2.58
2.98
3.37
2.56
2.95
3.34
8.79 8.46 8.40
10.11
11.42
9.78
11.06
9.68
10.96
KJH
N_AC_020300_1_0180101_01_00
m ft m ft m ft
H
J
K
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
Ground ClearancesFlap Track Fairings Up
FIGURE-2-3-0-991-018-A01
2-3-0Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
4.17
3.83
4.06
3.72 12.21
13.32 4.01
3.68 12.07
13.1613.68
12.57
L M
N_AC_020300_1_0190101_01_00
m ft m ft m ft
L
M
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
Ground ClearancesAileron Down
FIGURE-2-3-0-991-019-A01
2-3-0Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
4.01
3.75
14.67
14.27
13.35
13.16
12.30
4.48
4.36
4.24
4.11
3.96
3.90
3.64
14.70
14.31
13.91
13.48
12.99
12.80
11.94
4.45
4.33
4.21
4.08
3.94
3.88
3.63
14.60
14.21
13.81
13.39
12.93
12.73
11.91
13.814.21
4.35
4.47
4.59 15.06
4.07
P R S T WU V
m ft m m
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
Q
R
N
P
ft ft
U
V
S
T
W
14.27
4.44
4.24
14.57
13.91
4.39
4.20
14.40
13.784.35
4.55 14.93
N Q
N_AC_020300_1_0200101_01_00
Ground ClearancesAileron Up and Spoilers 1 to 5 Extended
FIGURE-2-3-0-991-020-A01
2-3-0Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2.57
2.98
3.07
3.36
3.61
3.86
4.09 13.42
12.66
11.84
11.02
10.07
9.78
8.43 2.48
2.88
2.97
3.26
3.51
3.76
3.98 13.06 3.95 12.96
12.243.7312.34
11.52 3.50 11.48
10.703.2610.70
9.74 2.98 9.78
9.512.909.45
8.14 2.50 8.20
XA’ B’ C’ D’ E’ F’ G’Y Z
N_AC_020300_1_0210101_01_00
m ft m ft m ft
C’
D’
E’
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
F’
G’
A/C IN MAINTENANCECONFIGURATION MID CG
X
Y
Z
A’
B’
Ground ClearancesSlats Extended
FIGURE-2-3-0-991-021-A01
2-3-0Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-0 Interior Arrangements
**ON A/C A320-200
Interior Arrangements
1. This section gives the standard interior arrangements configuration.
2-4-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1 Passenger Compartment Layout
**ON A/C A320-200
Typical Configuration
1. This section gives the typical interior configuration.
2-4-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
S
EM
ER
GE
NC
Y E
XIT
S
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
180
SE
AT
S A
LL T
OU
RIS
T C
LAS
S
28/2
9 in
PIT
CH
. 6 A
BR
EA
ST
. 3.3
LA A
A A
G
G
LAL
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(3)
AA
TT
EN
DA
NT
SE
AT
(5)
N_AC_020401_1_0030101_01_02
Typical ConfigurationTypical Configuration Single-Class, High Density
FIGURE-2-4-1-991-003-A01
2-4-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
S
EM
ER
GE
NC
Y E
XIT
S
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
LA A
A
G
G
LAL
12 S
UP
ER
FIR
ST
CLA
SS
138
EC
ON
OM
Y C
LAS
S
PA
SS
EN
GE
R S
EA
TS
(15
0 T
OT
AL)
SE
AT
PIT
CH
ES
: F
IRS
T 3
6 in
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(3)
AA
TT
EN
DA
NT
SE
AT
(4)
N_AC_020401_1_0090101_01_00
EC
ON
OM
Y 3
2 in
Typical ConfigurationTypical Configuration Two-Class
FIGURE-2-4-1-991-009-A01
2-4-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0 Passenger Compartment Cross Section
**ON A/C A320-200
Passenger Compartment Cross-section
1. This section gives the typical passenger compartment cross-section configuration.
2-5-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
3.95(155.51)
Cargo CompartmentFloor
CABINFLOOR
Top of cargoCompartment
AircraftDatum
Windows
2.64
(103.94)
2.13(83.86)
1.60(62.99)
1.24(48.82)
NOTE: DIMENSIONS m (in)
0.49(19.29)
0.52(20.47)
N_AC_020500_1_0010101_01_01
3.45(135.83)
3.68
(144.88)
1.42(55.91)
Passenger Compartment Cross-sectionFIGURE-2-5-0-991-001-A01
2-5-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE: DIMENSIONS m (in)
1.24
(48.
9)2.
21(8
7)
6 ABREAST−WIDER AISLE
4.14
(163
)
3.95(155.5)
3.64(143)
1.50(59)
0.64(25)
1.50(59)
0.432(17)
N_AC_020500_1_0050101_01_00
Passenger Compartment Cross-sectionEconomy Class, 6 Abreast - Wider Aisle (Sheet 1 of 2)
FIGURE-2-5-0-991-005-A01
2-5-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE: DIMENSIONS m (in)
6 ABREAST−WIDER SEAT
3.95(155.5)
3.64(143)
1.58(62)
0.48(19)
1.58(62)
1.24
(48.
9)2.
21(8
7)
4.14
(163
)
0.457(18)
N_AC_020500_1_0050102_01_02
Passenger Compartment Cross-sectionEconomy Class, 6 Abreast - Wider Seat (Sheet 2 of 2)
FIGURE-2-5-0-991-005-A01
2-5-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE: DIMENSIONS m (in)
4 ABREAST−FIRST CLASS
3.95(155.5)
1.24
(48.
9)2.
21(8
7)
4.14
(163
)
3.59(141)
0.69(27)
1.45(57)
1.45(57)
(22.6)0.57
N_AC_020500_1_0060101_01_00
Passenger Compartment Cross-sectionPassenger Compartment Cross-section, First-class
FIGURE-2-5-0-991-006-A01
2-5-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-0 Cargo Compartments
**ON A/C A320-200
Cargo Compartments
1. This section gives the cargo compartments locations, dimensions and loading combinations.
2-6-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
9.8
m(3
85.8
3 in
)
4.95
m
(194
.88
in)
1.81
m(7
1.26
in)
1.81
m(7
1.26
in)
0.86
m(3
3.85
in)
FW
D C
AR
GO
CO
MP
AR
TM
EN
T(3
CO
NT
AIN
ER
S)
AF
T C
AR
GO
CO
MP
AR
TM
EN
T(4
CO
NT
AIN
ER
S)
BU
LK C
AR
GO
CO
MP
AR
TM
EN
T
FR
24A
FR
34F
R47
FR
59F
R65
N_AC_020600_1_0030101_01_00
Cargo CompartmentsLocations, Dimensions and Loading Combinations
FIGURE-2-6-0-991-003-A01
2-6-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0 Door Clearances
**ON A/C A320-200
Doors Clearances
1. This section gives doors clearances.
2-7-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-1 Forward Passenger / Crew Doors
**ON A/C A320-200
Forward Passenger / Crew Doors
1. This section gives forward passenger / crew doors clearances.
2-7-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
CRITICAL
CLEARANCE LIMIT
0.61 m(2 ft)
0.48 m(1 ft 6.88 in)
2.54 m(8 ft 3.99 in)
5.02 m(16 ft 5.62 in)
1.8 m(5 ft 10.8 in) 0.81 m
(2 ft 7.8 in)
1.85 m(6 ft 0.82 in)
SEECHAPTER
2.375 m(7 ft 9.48 in)
2−3
CL
CLCL
0.03 m(1.18 in)
N_AC_020701_1_0030101_01_00
Doors ClearancesForward Passenger / Crew Doors
FIGURE-2-7-1-991-003-A01
2-7-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-2 Emergency Exits
**ON A/C A320-200
Emergency Exits
1. This section gives emergency exits doors clearances.
2-7-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
(FRAME 47)
NOTE: ESCAPE SLIDE COMPARTMENT DOOROPENS ON WING UPPER SURFACE.
(FROM NOSE)
CL0.47 m
(1ft 6.49 in)
1.23 m(4 ft 0.42 in)
0.2 m(7.87 in)
FWD
0.9 m(2 ft 11.4 in)
0.495 m(1ft 7.48 in)
(TOP OF FLOOR)
0.12 m(4.72 in)
B B
A
A
B
B
CL
A A
SEESECTION
2−3
14.43 m(47 ft 4.1 in)
0.85 m
(2 ft 9.45 in)
0.5 m(1ft 7.68 in)
N_AC_020702_1_0040101_01_00
Doors ClearancesEmergency Exits
FIGURE-2-7-2-991-004-A01
2-7-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-3 Aft Passenger / Crew Doors
**ON A/C A320-200
Aft Passenger / Crew Doors
1. This section gives Aft passenger / crew doors clearances.
2-7-3Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
29.64 m(97 ft 2.9 in)
(FROM NOSE)
2.44 m(8 ft)
1.85 m(6 ft 0.82 in)
0.6 m(1 ft 11.6 in)
(1.18 in)0.03 m
SEE
2−3CHAPTER
A A
1.79 m(5 ft 10.46 in)
0.81 m(2 ft 7.88 in)
0.58 m(1 ft 10.8 in)
CRITICALCLEARANCE
LIMIT
FWD
A
A
N_AC_020703_1_0030101_01_00
Doors ClearancesAft Passenger / Crew DoorsFIGURE-2-7-3-991-003-A01
2-7-3Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-4 Forward Cargo Compartment Doors
**ON A/C A320-200
Forward Cargo Compartment Door
1. This section gives forward cargo compartment door clearances.
2-7-4Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1.24 m
3.945 m(12 ft 11.3 in)
1.495 m(4 ft 10.84 in)
A A
8.16 m
(26 ft 9.25 in)
1.82 m(5 ft 11.65 in)
CFM ENGINE = 2.29 m (7 ft 6.15 in)V2500 ENGINE = 2.04 m (6 ft 8.3 in)
(FROM NOSE)
2.71 m(8 ft 10.69 in)
A
A
FWD
2−3
SEECHAPTER(4 ft 0.81 in)
N_AC_020704_1_0030101_01_00
Doors ClearancesForward Cargo Compartment Door
FIGURE-2-7-4-991-003-A01
2-7-4Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-5 Aft Cargo Compartment Doors
**ON A/C A320-200
Aft Cargo Compartment Door
1. This section gives Aft cargo compartment door clearances.
2-7-5Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
22.69 m
(74 ft 5.3 in)
1.82 m(5 ft 11.65 in)
(FROM NOSE)
FWD
FWD
A
A
2.03 m(6 ft 7.92 in)
1.23 m(4 ft 0.42 in)
3.945 m
(12 ft 11.3 in)
1.43 m(4 ft 8.29 in)
2−3
SEECHAPTER
A A
N_AC_020705_1_0030101_01_00
Doors ClearancesAft Cargo Compartment DoorFIGURE-2-7-5-991-003-A01
2-7-5Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-6 Bulk Cargo Compartment Doors
**ON A/C A320-200
Bulk Cargo Compartment Door
1. This section gives the bulk cargo compartment door clearances.
2-7-6Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0.95 m(3 ft 1.39 in)
0.89 m(2 ft 11 in)
FWD
2.19 m(7 ft 2.22 in)
6.10 m(20 ft)
0.77 m(2 ft 6.31 in)
2−3
SEECHAPTER
A
A
A A
N_AC_020706_1_0010101_01_01
Doors ClearancesBulk Cargo Compartment Door
FIGURE-2-7-6-991-001-A01
2-7-6Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-7 Main Landing Gear Doors
**ON A/C A320-200
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances.
2-7-7Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
A
NOTE: VALUE OF CG: 25% RC.
16.358 m(53 ft 8 in)
1.826 m(5 ft 11.88 in)
GROUND LINE
0.207 m
(8.14 in)
0.485 m
(1 ft 7.09 in)
AIRCRAFT
1.23 m(4 ft 0.42 in)
0.14 m(5.51 in)
1.761 m(5 ft 9.32 in)
84°
1.942 m(6 ft 4.45 in)
A
N_AC_020707_1_0030101_01_02
Doors ClearancesMain Landing Gear Doors
FIGURE-2-7-7-991-003-A01
2-7-7Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
GROUND LINE1.268 m
(4 ft 1.92 in)
0.16 m(6.29 in)
1.761 m(5 ft 9.32 in)
0.485 m
(1 ft 7.09 in)
1.942 m(6 ft 4.45 in)
82.5°
NOTE: VALUE OF CG: 25% RC.
AIRCRAFT
A
16.227 m(53 ft 2.85 in)
2.23 m(7 ft 3.79 in)
A
N_AC_020707_1_0040101_01_02
Doors ClearancesMain Landing Gear Doors (Bogie)
FIGURE-2-7-7-991-004-A01
2-7-7Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-8 Radome
**ON A/C A320-200
Radome
1. This section gives the radome clearances.
2-7-8Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0.63 m(2 ft 0.79 in)
STA 3500FR1
65°
(5 ft 0.62 in)1.54 m
N_AC_020708_1_0030101_01_00
Doors ClearancesRadome
FIGURE-2-7-8-991-003-A01
2-7-8Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-9 APU and Nose Landing Gear Doors
**ON A/C A320-200
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances.
2-7-9Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FR80
FR84
3.23
m(1
0 ft
7.16
in)
3.86
m(1
2 ft
7.96
in)
NOTE: VALUE OF CG: 25% RC.
1.5
m(4
ft 1
1 in
)
1.4
m(4
ft 7
.11
in)
N_AC_020709_1_0030101_01_00
Doors ClearancesAPU and Nose Landing Gear Doors
FIGURE-2-7-9-991-003-A01
2-7-9Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0 Escape Slides
**ON A/C A320-200
Escape Slides
1. GeneralThis section gives location of cabin escape facilities and related clearances.
2. LocationEscape facilities are provided at the following locations:- one slide-raft at each passenger/crew door (total four)- one slide for emergency exit doors (total two). Dual lane offwing escape slides are installed above
the wings in the left and right wing-to-fuselage fairings for off-the-wing evacuation.
2-8-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FWD CABIN ESCAPE SLIDE
OFF WING ESCAPE SLIDE
N_AC_020800_1_0050101_01_00
AFT CABINESCAPE SLIDE
Escape SlidesLocation
FIGURE-2-8-0-991-005-A01
2-8-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_020800_1_0060101_01_00
EMERGENCY DESCENT DEVICETHROUGH WINDOW OPENING
GRID EQUALS 1 m (3.28 ft) IN REALITY
Escape SlidesDimensions
FIGURE-2-8-0-991-006-A01
2-8-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0 Landing Gear
**ON A/C A320-200
Landing Gear
1. General
The landing gear is of the conventional retractable tricycle type comprising:- Two main gears with twin wheel or four wheels bogie assembly,- A twin wheel nose gear.
The main landing gear twin wheel landing gears are located under the wing and retract sidewaystowards the fuselage centerline.The nose landing gear retracts forward into a fuselage compartment located between STA 5394/FR 9and STA 8077/FR 20.
The landing gear and landing gear doors operation is controlled electrically and hydraulicallyoperated.In abnormal operation, the landing gear can be extended by gravity.
For landing gear footprint and tire size, refer to 7-2-0.
2. Main Landing Gear
A. Twin wheel
Each of the two main landing gear assemblies consists of a conventional two wheel direct typewith an integral shock absorber supported in the fore and aft direction by a fixed drag strut andlaterally by a folding strut mechanically locked when in the DOWN position.
B. Four wheels - Bogie
Each of the two main landing gear assemblies consists of a direct action shock absorber onwhich is installed a bogie beam and four wheels.The shock absorber is supported in the fore and aft direction by a fixed drag strut and laterallyby a folding strut mechanically locked when in the DOWN position.
3. Nose Landing Gear
The nose landing gear comprises a leg with a built-in shock absorber strut, carrying twin wheel withadequate shimmy damping and a folding strut mechanically locked when in the DOWN position.
4. Nose Wheel Steering
Steering is controlled by two hand wheels in the cockpit. For steering angle controlled by the handwheels, refer to AMM 32-51-00.For steering angle limitation, refer to AMM 09-10-00.
2-9-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
A steering disconnection box installed on the nose landing gear to allow steering deactivation fortowing purpose.
5. Landing Gear Servicing Points
A. General
Filling of the landing gear shock absorbers is through MS28889 standard valves.
Charging of the landing gear shock absorbers is accomplished with nitrogen through MS28889standard valves.
B. Charging Pressure
For charging of the landing gear shock absorbers, refer to AMM 12-14-32.
6. Braking
A. General
The four main wheels are equipped with carbon multidisc brakes.
The braking system is electrically controlled and hydraulically operated.
The braking system has four braking modes plus autobrake and anti-skid systems:- Normal braking with anti-skid capability- Alternative braking with anti-skid capability- Alternative braking without anti-skid capability- Parking brake with full pressure application capability only.
B. In-Flight Wheel Braking
The main gear wheels are braked automatically before the wheels enter the wheel bay.
The nose gear wheels are stopped by the wheels contacting a rubbing strip (the brake band)when the gear is in the retracted position.
2-9-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TORQUELINK
DOWNLOCKACTUATOR
MAIN FITTING
SHOCK ABSORBER
SIDE STAY
ACTUATING CYLINDER
LOCK STAY
A
E
D
MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION.NOTE: N_AC_020900_1_0100101_01_00
MAIN DOOR(HYDRAULICALLY OPERATED)
FIXEDRAMPS
UPLOCKROLLER
ADJUSTABLERAMP
STEPS
FIXEDFAIRING
HINGEDFAIRING
HINGED FAIRING(MECHANICALLY OPERATED)
PROXIMITY SENSORS
DOOR ACTUATING CYLINDER
A
B
C
Landing GearMain Landing Gear - Twin Wheel (Sheet 1 of 2)
FIGURE-2-9-0-991-010-A01
2-9-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
DOORACTUATINGCYLINDER
FLAG
LOCKSTAYACTUATINGCYLINDER
GROUND LOCK SLEEVE
FLAG
BC
LOCKINGPIN
LOCKINGPIN
N_AC_020900_1_0100102_01_00
BOTTOM FILLING ANDCHARGING CONNECTIONMS28889
EDEXAMPLE
TOP FILLING AND CHARGING CONNECTION MS28889
Landing GearMain Landing Gear - Twin Wheel (Sheet 2 of 2)
FIGURE-2-9-0-991-010-A01
2-9-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_020900_1_0110101_01_00
Y=COMPRESSED
EXTENDED
58.4
0 %
AM
C
3 795 mm
3 453 mm(135.94 in) 80°30
RETRACTIONANGLE
(36.50 in)927.10 mm
2 868.70 mm(112.94 in)
2 265 mm(89.17 in)
X= 20 252.50 mm(797.34 in)
469.90 mm(18.50 in)
(149.41 in)
Landing GearMain Landing Gear Dimensions - Twin Wheel
FIGURE-2-9-0-991-011-A01
2-9-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
DOWNLOCKACTUATOR
ACTUATING CYLINDER
LOCK STAY
LEG UNIT
SHOCK ABSORBER
PITCH TRIMMER
BRAKE BAR
TORQUELINK
STRUT ASSEMBLY
HINGEDFAIRING
FIXEDFAIRING
AJUSTABLERAMP
UPLOCKROLLER
DOORRAMPS
STEPS
MAIN DOOR
A
D
DOOR ACTUATINGCYLINDER B
MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION.NOTE:
A
N_AC_020900_1_0120101_01_00
C
Landing GearMain Landing Gear - Four Wheels - Bogie (Sheet 1 of 2)
FIGURE-2-9-0-991-012-A01
2-9-0Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
DOORACTUATINGCYLINDER
FLAG
TOP FILLING AND CHARGING CONNECTION MS28889
LOCKSTAYACTUATINGCYLINDER
GROUND LOCK SLEEVE
FLAG
BC
LOCKINGPIN
LOCKINGPIN
DN_AC_020900_1_0120102_01_00
Landing GearMain Landing Gear - Four Wheels - Bogie (Sheet 2 of 2)
FIGURE-2-9-0-991-012-A01
2-9-0Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1 005 mm(39.57 in)
780 mm(30.71 in)
80°30RETRACTION
Y = 3 795 mm(149.41 in)
ANGLE
X = 20 266 mm(797.87 in)
419.
10 m
m(1
6.50
in)
COMPRESSED
EXTENDED
2 506 mm(98.66 in)
2 978.70 mm(117.27 in)
58.4
0 %
AM
C
N_AC_020900_1_0130101_01_00
Landing GearMain Landing Gear Dimensions - Four Wheels - Bogie
FIGURE-2-9-0-991-013-A01
2-9-0Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_020900_1_0140101_01_00
ACTUATINGCYLINDER
NOSE WHEELSTEERINGSERVO CONTROL
STEERINGACTUATINGCYLINDER
TORQUELINK
DOWNLOCKPROXIMITY
DETECTORS
SHOCKABSORBER
TOWINGFITTING
LEG DOOR
AFT DOORS
ASSEMBLYFITTING
FWD DOORS
CONTROL ROD
DOORACTUATINGCYLINDER
CRANK
DOOR UPLOCKASSEMBLY GEAR UPLOCK
ASSEMBLY
BELL
FR20
FR9
DRAG STRUTASSEMBLY
A
A
ROTATING ROD
BC
E
D
Landing GearNose Landing Gear (Sheet 1 of 2)
FIGURE-2-9-0-991-014-A01
2-9-0Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TOWING LEVER
(NOSE WHEEL STREERINGNORMAL POSITION
(TOWING POSITION)SAFETY PIN
(NOSE WHEEL STEERING DEACTIVATED)TOWING POSITION
E
DOOR HINGE
NLG DOOR
NLG DOORSAFETY PIN
FLAG
LH SYMMETRICALRH SHOWN
C
D
OPERATIONAL)
FLAG
DOWNLOCKSAFETY PIN
LOCKSTAY
B
N_AC_020900_1_0140102_01_00
CONNECTION MS28889FILLING AND CHARGING
Landing GearNose Landing Gear (Sheet 2 of 2)
FIGURE-2-9-0-991-014-A01
2-9-0Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_020900_1_0150101_01_00
92°
9°
X =
500 mm(19.69 in)
7 561 mm(297.68 in)
430 mm(16.93 in)
1 957.03 mm(77.05 in)
2 338 mm(92.05 in)
EXTENDED
COMPRESSED
Landing GearNose Landing Gear Dimensions
FIGURE-2-9-0-991-015-A01
2-9-0Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
Landing Gear Maintenance Pits
1. Description
The minimum maintenance pit envelopes for the main gear shock absorber removal are shown inFigures 1 and 2.
All dimensions shown are minimum dimensions with zero clearances.
The dimensions for the pits have been determined as follows:- The length and width of the pits allow the gear to rotate as the weight is taken off the landing
gear- The depth of the pits allows the shock absorber to be removed when all the weight is taken off
the landing gear.Dimensions for elevators and associated mechanisms must be added to those in Figures 1 and 2.
2-9-0Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
= =
==
7.61
m(2
4.97
ft)
5.28
m
1 m
(3.2
8 ft)
1.5
m(4
.92
ft)
(17.
32 ft
)
1.92
m(6
.30
ft)
20.2
5 m
(66.
44 ft
)
20.1
0 m
(65.
94 ft
)
7.59
m(2
4.90
ft)
2.95
m(9
.68
ft)
3.76
m(1
2.34
ft)
3.79
m(1
2.43
ft)
6.49
m(2
1.29
ft)
2.5
m(8
.20
ft)
MA
IN J
AC
KIN
G P
OIN
TM
AIN
JA
CK
ING
PO
INT
MA
IN J
AC
KIN
G P
OIN
T
FROM X0
FW
D J
AC
KIN
G P
OIN
T
N_AC_020900_1_0240101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-024-A01
2-9-0Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:1 2
0.52
1.1
73.
84
mft
AB
mft
AB
ST
AT
IC G
RO
UN
D L
INE
1
2
1
2
7.6
1 m
(24.
97 ft
)
1.7
1
RE
PR
ES
EN
TS
TO
P O
F M
EC
HA
NIC
AL
OR
HY
DR
AU
LIC
ELE
VA
TO
R, W
ITH
AIR
CR
AF
T W
EIG
HT
SU
PP
OR
TE
DA
ND
LA
ND
ING
GE
AR
SH
OC
K A
BS
OR
BE
RS
EX
TE
ND
ED
.
RE
PR
ES
EN
TS
TO
P O
F M
EC
HA
NIC
AL
OR
HY
DR
AU
LIC
ELE
VA
TO
R, S
HO
WN
WIT
H Z
ER
O C
LEA
RA
NC
ELO
WE
RE
D F
OR
SH
OC
K A
BS
OR
BE
R R
EM
OV
AL.
1.60
m(5
.25
ft)0.
40 m
(1.3
1 ft)
20
.25
m(6
6.44
ft)
DIM
QU
OT
ED
ISW
ITH
WH
EE
LS R
EM
OV
ED
AN
D 1
53 m
m (
6.02
in)
CLE
AR
AN
CE
AT
JAC
KIN
G D
OM
E
FROM X0
N_AC_020900_1_0250101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-025-A01
2-9-0Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0 Exterior Lighting
**ON A/C A320-200
Exterior Lighting
1. General
This section gives the location of the aircraft exterior lighting.
EXTERIOR LIGHTINGITEM DESCRIPTION
1 RIGHT NAVIGATION LIGHT (GREEN)
2 TAIL NAVIGATION LIGHT (WHITE)
3 LEFT NAVIGATION LIGHT (RED)
4 RETRACTABLE LANDING LIGHT5 RUNWAY TURN OFF LIGHT6 TAXI LIGHT7 TAKE-OFF LIGHT8 LOGO LIGHT
9 UPPER ANTI-COLLISION LIGHT/BEACON (RED)
10 LOWER ANTI-COLLISION LIGHT/BEACON (RED)
11 WING STROBE LIGHT (HIGH INTENSITY, WHITE)
12 TAIL STROBE LIGHT (HIGH INTENSITY, WHITE)
13 WING/ENGINE SCAN LIGHT
14 WHEEL WELL LIGHT (DOME)
15 CARGO COMPARTMENT FLOOD LIGHT
2-10-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
6 75 4
10
12
9
13
8
2
8
N_AC_021000_1_0090101_01_00
11
1
3
111
3
RH
LH
RH
LH
Exterior LightingFIGURE-2-10-0-991-009-A01
2-10-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1
2
3
55
7
N_AC_021000_1_0100101_01_00
Exterior LightingFIGURE-2-10-0-991-010-A01
2-10-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
12
11
1313
4
11
N_AC_021000_1_0110101_01_00
109
6
Exterior LightingFIGURE-2-10-0-991-011-A01
2-10-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
14
8 8
15 15
N_AC_021000_1_0190101_01_00
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
Exterior LightingFIGURE-2-10-0-991-019-A01
2-10-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0 Antennas and Probes Location
**ON A/C A320-200
Antennas and Probes Location
1. This section gives the location of antennas and probes.
2-11-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RADIO ALTIMETER(2)
RADIO ALTIMETER(1)
VHF(2)
DME(2)
PITOT PROBE(1)
PITOT PROBE(3)
DME(1)
TAT PROBE
VHF(1)
TAT PROBE
PITOT PROBE(2)
GPS(2)
GPS(1)
ATC(1)
ADF(1)
VHF(3)
ELT
ATC(2)
WEATHER RADAR
EMERGENCY STATIC PROBE
TCAS TOP
AOA SENSOR(1)
MARKER
TCAS BOTTOM
STATIC PROBE(1)
STATIC PROBE(2)
LOC
GLIDE
HF
VOREMERGENCY STATIC PROBE
AOA SENSOR(2)
STATIC PROBE(2)
STATIC PROBE(1)
ATC(3)
AOA SENSOR(3) STBY
ATC(4)
N_AC_021100_1_0030101_01_00NOTE: DEPENDING ON AIRCRAFT CONFIGURATION
Antennas and ProbesLocation
FIGURE-2-11-0-991-003-A01
2-11-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0 Power Plant
**ON A/C A320-200
Auxiliary Power Unit
1. General
The APU is installed at the rear part of the fuselage in the tail cone. An air intake system with aflap-type door is installed in front of the APU compartment. The exhaust gases pass overboard at theend of the fuselage cone.
2. Controls and Indication
The primary APU controls and indications are installed on the overhead panel, on the center pedestaland on the center instrument panel. Additionally, an external APU panel is installed on the noselanding gear to initiate an APU emergency shutdown.
2-12-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
Z310
AIR INTAKE FIXEDON ACCESS DOOR
CUT OUT SEALED WITHLABYRINTH GASKET
FRONTFIREWALL
FIREWALL
FIREWALL RH
LOUVER LH
REARFIREWALL
CUT OUT SEALED WITHLABYRINTH GASKET
B
A
UPPER
A
/ FR80
/FR84STA38945
STA37295
LH ACCESS DOORNOTE: NOT SHOWN FOR CLARITY315AL
RH ACCESS DOOR316AR
N_AC_021200_1_0050101_01_00
Auxiliary Power UnitAccess Doors
FIGURE-2-12-0-991-005-A01
2-12-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
OIL
CO
OLE
R O
UT
LET
AIR
INT
AK
E D
UC
T
AP
U−
FU
EL−
LIN
E
AIR
INT
AK
E H
OU
SIN
G
DIV
ER
TE
R
FR
ON
T F
IRE
WA
LL
BLE
ED
AIR
LIN
E
FIR
E E
XT
ING
UIS
HIN
GB
OT
TLE
GE
NE
RA
TO
R
AP
U S
US
PE
NS
ION
(7 R
OD
S)
AP
U
FIR
E O
VE
RH
EA
T D
ET
EC
TO
R
AP
U S
US
PE
NS
ION
(7 R
OD
S)
EX
HA
US
TM
UF
FLE
R
B
N_AC_021200_1_0060101_01_00
/ FR
87
/ FR
84
/ FR
80
/ FR
78
/ FR
77
ST
A40
113
ST
A38
945
ST
A37
295
ST
A36
657
ST
A36
545
Auxiliary Power UnitGeneral Layout
FIGURE-2-12-0-991-006-A01
2-12-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
Engine and Nacelle
1. Engine and Nacelle - CFM Engine
A. EngineThe engine is a dual-rotor, variable stator, high bypass ratio turbo fan power plant for subsonicservices. The principal modules of the engine are:- low pressure compressor (fan stator and fan rotor)- high pressure compressor- turbine frame- combustion chamber- high pressure turbine- low pressure turbine- accessory drives (gear box).The 9 stage high pressure compressor is driven by 1 stage high pressure turbine, and theintegrated front fan and booster is driven by 4 stage low pressure turbine. An annular combustorconverts fuel and compressor discharge air into energy to provide engine thrust part throughprimary exhaust and to drive the turbines. The accessory drive system extracts energy from thehigh pressure rotor to drive the engine accessories and the engine mounted aircraft accessories.Reverse thrust for braking the aircraft after landing is supplied by an integrated system whichacts on the fan discharge airflow.
B. NacelleThe cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine ishoused in a nacelle suspended from a pylon attached to the wing lower surface. The nacelleconsists of the demountable powerplant, the fan cowls and the thrust reverser cowls.The nacelle installation is designed to provide cooling and ventilation air for engine accessoriesmounted along the fan and core casing. The nacelle provides:- protection for the engine and the accessories- airflow around the engine during its operation- lighting protection- HIRF and EMI attenuation.
2. Engine and Nacelle - IAE Engine
A. EngineThe engine is a two spool, axial flow, high bypass ratio turbofan powerplant for subsonic sevice.The main modules of the engine are:- low pressure compressor (fan and booster) assembly- LP compressor/intermediate case- No. 4 bearing and combustion section- high pressure compressor- HP turbine section- LP turbine section- accessory drives (gear box).
2-12-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The four stage Low Pressure Compressor (LPC) is driven by a five stage Low Pressure Turbine(LPT) and the ten stage High Pressure Compressor (HPC) by a two stage High PressureTurbine (HPT). The HPT also drives a gearbox which, in turn drives the engines and aircraftmounted accessories. The two shafts are supported by five main bearings.The V2500 incorporates a Full Authority Digital Engine Control (FADEC) which governs allengine functions, including power management. Reverse thrust for braking the aircraft afterlanding is supplied by an integrated system which acts on the fan discharge airflow.
B. NacelleThe cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine ishoused in a nacelle suspended from a pylon attached below the wing.The nacelle installation is designed to provide cooling and ventilation air for engine accessoriesmounted along the fan and core casing. The nacelle provides:- protection for the engine and the accessories- airflow around the engine during its operation- lighting protection- HIRF and EMI attenuation.
2-12-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FAN AND BOOSTER COMPRESSOR
TURBINEHP
TURBINELP
DRIVEACCESSORY
AGB TGB
1 820 mm(71.65 in)
1 130 mm(44.49 in)
989 mm(38.94 in)
1 978 mm(77.87 in)
2 145 mm(84.45 in) FWD
2 943 mm(115.87 in)
TURBINEFRAME
2 600 mm(102.36 in)1 125 mm
(44.28 in)
FWD HOISTINGPOINT
FWDHANDLING
POINT
AFT HANDLINGAND HANDLING
POINTDIA 986 mm
(38.82 in)
B
A
BN_AC_021200_1_0270101_01_00
A
COMBUSTOR
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-027-A01
2-12-0Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
BLOCKER DOOREXTENDED
1.9 m(6.2 ft)
C C
1.2 m(3.9 ft)
1.8 m(5.9 ft)
D D
2.07 m(6.8 ft)
B B
2.1 m(6.9 ft)
A A
FAN COWL
CENTERBODY
FANREVERSER
6°
PRIMARYNOZZLE
11 m(36.1 ft)
0.93 m
(3.1 ft)
1.3 m(4.3 ft)
1.2 m(3.9 ft)
1.2 m(3.9 ft)
DISTANCE FROMTHE NOSE
0.33 m(1.1 ft)
2.3 m(7.5 ft)
ENGINE AIRINLET COWL
A
A
B
B
C
C
D
D
0.57 m(1.9 ft)
1.6 m(5.2 ft)
N_AC_021200_1_0280101_01_00
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-028-A01
2-12-0Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021200_1_0290101_01_00
0.56 m(1.8 ft)
NOTE: APPROXIMATE DIMENSIONS
3.73 m(12.3 ft)
4.25 m(14 ft)
40°55°
0.81 m(2.67 ft)
1.2 m(3.96 ft)
1.51 m(4.98 ft)
1.85 m(6.1 ft)
Power Plant HandlingFan Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-029-A01
2-12-0Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021200_1_0300101_01_00
3.7 m(12.1 ft)
3.3 m(10.8 ft)
35°45°
1 m(3.3 ft)
(3 ft)0.9 m
CAUTIONDO NOT ACTUATE SLATS:
− WITH THRUST REVERSER COWLS 45° OPEN POSITION− WITH BLOCKER DOORS OPEN AND THRUST REVERSER COWLS AT 35° AND 45° OPEN POSITION
APPROXIMATE DIMENSIONSNOTE:
GROUND
0.56 m(1.8 ft)
0.7 m(2.3 ft)
1 m(3.3 ft)
Power Plant HandlingThrust Reverser Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-030-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FAN AND BOOSTER COMPRESSOR
COMBUSTOR
HPTURBINE
LPTURBINE
TURBINEFRAME
A
3 101 mm(122.1 in)
1 715 mm(67.5 in)
1 067 mm(42.0 in)
DRIVEACCESSORY
FWD
A
N_AC_021200_1_0310101_01_00
Power Plant HandlingMajor Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-031-A01
2-12-0Page 10
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021200_1_0320101_01_00
0.5°6°
5.26 m(17.27 ft)
1.50 m(4.95 ft)
5.25 m(17.23 ft)
2.01 6.58 0.99 3.25 1.10 3.63 1.41 4.62
W U V PPS
m ft m ft m ft m ft
ATCOMPONENT
INLETATTACH FLG
TORQUE BOX"V" BLADE
COMB. CHAMBERENTRY FLG
COMB. CHAMBEREXIT FLG
TECH FLGTURB. EXIT CASE
AFT ENDCNA
2.01 6.58 1.00 3.29 1.11 3.64 2.59 8.50
1.98 6.50 0.97 3.19 1.07 3.52 3.26 10.70
1.93 6.32 0.93 3.06 1.03 3.39 3.63 11.90
1.64 5.38 0.78 2.57 0.86 2.83 4.60 15.10
1.24 4.07 0.60 1.96 0.64 2.11 −−−− −−−−
W
U
V
F
F
E
E
D
D
C
C
B
B
A
A
DISTANCE FROMTHE NOSE
11.12 m(36.5 ft)
A−A
B−B
C−C
D−D
E−E
F−F
Power Plant HandlingMajor Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-032-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021200_1_0330101_01_00
2 m
(6.6 ft)
CLOSEDWL100
(5.2 ft)1.2 m(3.9 ft)
GROUND
WL100
3.9 m
(12.8 ft)
FWD VIEW
FAN COWLOPEN 50°
0.67 m(2.2 ft)
APPROXIMATE DIMENSIONSNOTE:
1.6 m
Power Plant HandlingFan Cowls - IAE V2500 Series Engine
FIGURE-2-12-0-991-033-A01
2-12-0Page 12
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021200_1_0340101_01_00
1.1 m(3.6 ft)
1 m(3.3 ft)
THRUST REVERSEROPEN 45°
0.67 m(2.2 ft)
2 m
(6.6 ft)
AFT VIEW
WL100CLOSED
3.6 m
(11.8 ft)
0.9 m(3 ft)
WL100
APPROXIMATE DIMENSIONSNOTE:
Power Plant HandlingThrust Reverser Halves - IAE V2500 Series Engine
FIGURE-2-12-0-991-034-A01
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Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0 Leveling, Symmetry and Alignment
**ON A/C A320-200
Leveling, Symmetry and Alignment
1. Quick LevelingThere are three alternative procedures to level the aircraft:- Quick leveling procedure with Air Data/Inertial Reference Unit (ADIRU).- Quick leveling procedure with a spirit level in the passenger compartment.- Quick leveling procedure with a spirit level in the FWD cargo compartment.
2. Precise LevelingFor precise leveling, it is necessary to install sighting rods in the receptacles located under thefuselage (points 11 and 12 for longitudinal leveling) and under the wings (points 2LH and 2RH forlateral leveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until thereference marks on the sighting rods are aligned in the sighting plane (aircraft level).
3. Symmetry and Alignment CheckPossible deformation of the aircraft is measured by photogrammetry.
2-13-0Page 1
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2LH
RIB10
2RH
RIB10
FR34FR31
FR50 FR53
12
11
N_AC_021300_1_0040101_01_00
Location of the Leveling PointsFIGURE-2-13-0-991-004-A01
2-13-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0 Jacking
**ON A/C A320-200
Jacking for Maintenance
1. Jacking for Maintenance
A. General
The A320 aircraft can be jacked:- at no more than the maximum permitted aircraft weight for jacking (59 000 kg (130 072
lb)) and,- within the limits of the permissible wind speed when the aircraft is jacked outside a closed
environment.
B. Primary Jacking Points
The aircraft is provided with three jacking points:- one located under the forward fuselage (STA5194/FR8),- two located under the wings: one under each wing, located at the intersection of
STA4862/RIB9 and the rear of spar-datum.
Three jacking adapters are used as intermediary parts between the airplane and jacks:- one male spherical jacking adapter of 19 mm (0.75 in) radius, forming part of the airplane
structure, FR8,- a wing jack pad, attached to each wing at RIB 9 by 2 bolts, provides the location for
jacking adaptor.Wing jack pads are ground equipment.
C. Auxiliary Jacking Points - Safety Stay
When the aircraft is on jacks, it is recommended that a safety stay be placed under the fuselage,between FR73 and FR74 to prevent tail tipping caused by accidental displacement of the centerof gravity.
The safety stay is not used to lift the aircraft.
A male spherical ball pad with a 19 mm (0.75 in) radius forming part of the airplane structure isprovided for using the safety stay.
2. Jack design
In fully retracted position (jack stroke at minimum) the height is such that the jack may be placedbeneath the airplane under the most adverse conditions, namely, tires deflated and shock absorbersdepressurized.
2-14-0Page 1
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
In addition, a clearance of 50 mm (1.97 in) approximately must be provided between the airplanejacking point and the jack upper end. The lifting jack stroke enables the aircraft to be jacked up sothat the fuselage longitudinal datum line (aircraft center line) parallel to the ground, with a 100 mm(3.94 in) clearance between the main landing gear wheels and the ground.In particular, this enables the landing gear extension/retraction tests to be performed.
Jacking Point Location Z Maximum Permitted Load
Forward Fuselage Jacking Point-1.987 m(-6.52 ft)
6 800 daN(15 287 lbf)
Wing Jacking Point-0.828 m(-2.72 ft)
28 500 daN(64 071 lbf)
Safety Stay-0.748 m(-2.45 ft)
2 000 daN(4 496 lbf)
The maximum permitted aircraft weight for the jacking procedure is 59 000 kg (130 073 lb).Centerline at 4.6 mm (0.18 in) parallel to the ground.
3. Shoring Cradles
When it is necessary to support the aircraft in order to relieve the loads on the structureaccomplishment of modifications or major work, shoring cradles shall be placed under each wing andfuselage as necessary.
NOTE : Aircraft must not be lifted or supported by the wings or fuselage alone without adequatesupport of the other.
A. Under the Fuselage
Frames which are capable of supporting loads are noted below as well as the maximumpermissible loads for each frame.
Under the Fuselage
FR 15 6 700 daN (15 062 lbf)
FR 33 3 400 daN (7 644 lbf)
FR 42 1 000 daN (2 248 lbf)
FR 62/FR 63 3 000 daN (6 744 lbf)
FR 73/FR 74 Safety Stay Pad 2 000 daN (4 496 lbf)
B. Under the Wings
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Shoring cradles are used when it is necessary to stress-jack the aircraft to carry out maintenanceand repair work. These are used to oppose the deflections of the wings and reduce the stressesto an acceptable level at the area of maintenance and repair.
The shoring cradles, each with two adjustable pads, 152.4 mm (6.00 in) square, are positionedat three locations under each wing. These locations are detailed in Table 3.
The adjustable pads are faced with thin rubber and contact the wing profile at the datumintersections of the ribs and the front and rear spars (F/S and R/S).
Table 3 shows the maximum load limit allowed at each jack pad when the wings are supportedby the cradles. These load limits apply to all A320 aircraft and variants.
The maximum permitted load, as specified in Table 3, is for a wing with its engines removed.When the wing(s) are held with the shoring cradles, and with the engines installed, the level ofshear stress caused (at the front spar) is not permitted. The weight of the engine can also causea torsion load that will lift the rear spar from its cradle.
Thus it is recommended that you remove the applicable engine(s) before you use the shoringcradles. However, for minor repairs the engines may be installed if their full weight is held.
It is important that the loads at each rib position are not exceeded because damage to theaircraft may occur.
Maximum Allowable Load at each Jack Pad
Maximum Stress Relief Jacking Forces (LIMIT)
Rib 4 Rib 13 Rib 22Configuration
F/Spar R/Spar F/Spar R/Spar F/Spar R/Spar
Engine &MLGRemoved
790 daN(1 776 lbf)
1 330 daN(2 990 lbf)
670 daN(1 506 lbf)
550 daN(1 236 lbf)
320 daN(719 lbf)
380 daN(854 lbf)
EngineRemoved
530 daN(1 191 lbf)
2 510 daN(5 643 lbf)
610 daN(1 371 lbf)
610 daN(1 371 lbf)
310 daN(697 lbf)
380 daN(854 lbf)
4. Airplane Jacking for Removal/Installation of Landing Gear Shock Absorbers
For removal/installation of the nose gear shock absorber with the gear fully extended and the wheelsremoved, the fuselage longitudinal datum line must be not less than 5 300 mm (208.66 in) above theground.
2-14-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
For removal/installation of the main landing gear shock absorber, after removing the bogie beam, thefuselage longitudinal datum line must be not less than 5 210 mm (205.12 in) above the ground.
For reference, for landing gear swinging tests, the fuselage longitudinal datum line must be not lessthan 4 600 mm (181.10 in) above the ground.
2-14-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2.74 m(8.99 ft)
FWD JACKINGPOINT
WING JACKING
6.5 m(21.33 ft)
SAFETYPOINT
WING JACKING
17.56 m(57.61 ft)
32.57 m(106.86 ft)
CL
POINT
POINT
N_AC_021400_1_0300101_01_00
Jacking for MaintenanceJacking Point Location
FIGURE-2-14-0-991-030-A01
2-14-0Page 5
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
A
N_AC_021400_1_0310101_01_00
POINT A DETAIL
Z−1 979.8Z−1 987
FR8
A
SPHERICAL RADIUS19 mm (0.75 in)
B
B
Jacking for MaintenanceForward Jacking Point
FIGURE-2-14-0-991-031-A01
2-14-0Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
A
A
N_AC_021400_1_0320101_01_00
LOWER SURFACE
A
WING JACK PAD
POINT BB’ DETAIL
Z−895
Z−828.35
RE
AR
SP
AR
DA
TU
M
INTERSECTION WITH REARSPAR DATUM
RIB9
SPHERICAL RADIUS32 mm (1.26 in)
EXAMPLE
B
B
Jacking for MaintenanceWing Jacking Points
FIGURE-2-14-0-991-032-A01
2-14-0Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
A
Z−748.44
SPHERICAL RADIUS 19 mm (0.75 in)(19 D535−71 595)
X =
35
106
A
Z−729.441
N_AC_021400_1_0330101_01_00
(4.97 in)
126.15 mm
Jacking for MaintenanceSafety Stay
FIGURE-2-14-0-991-033-A01
2-14-0Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
THE CENTER LINE (CL) IS A FICTITIOUS LINE AROUND WHICH THE AIRCRAFT IS BUILT.SAFETY STAY IS NOT USED FOR JACKING.SEE SECTION 1−10, FOR GROUND CLEARANCES A/C ON JACKS.
NOTE:
L
M
L M
1 675 mm(65.94 in)
2 801 mm(110.28 in)
2 858 mm(112.52 in)
2 599 mm(102.32 in)
3 751 mm(147.68 in)
3 834 mm(150.94 in)
1 897 mm(74.69 in)
3 178 mm(125.12 in)
3 391 mm(133.50 in)
1 545 mm(60.83 in)
2 761 mm(108.70 in)
2 940 mm(115.75 in)
N
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED AND
AIRCRAFT ON WHEELS, NLG SHOCK ABSORBER DEFLATED
AIRCRAFT ON JACKS, CENTER LINE (CL) PARALLEL TO GROUNDSHOCK ABSORBERS EXTENDED MAIN WHEEL CLEARANCE(STANDARD TIRES) (49 x 17) 120 mm (4.72 in) FOR EXTENDED
AIRCRAFT ON WHEELS, (STANDARD TIRES) AT MAX.PERMITTED WEIGHT FOR JACKING
FLAT TIRES
AND RETRACTED LANDING GEARS
AND FLAT TIRES
N
N_AC_021400_1_0340101_01_00
Jacking for MaintenanceJacking Design
FIGURE-2-14-0-991-034-A01
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Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0
3
6
9
12
6.93
25 30 35 40 45 50 55 60 65 70 75
55 66 77 88 99 110 121 132 143 154 165
1000 kg
A/C WEIGHT
MAX PERMISSIBLE LOAD
AS AN EXAMPLE ASSUME THAT THE AIRCRAFT HAS A GROSS WEIGHTOF 66 000 kg AND THE CENTER OF GRAVITY (CG) IS AT 25 %. THUS THEFORCE AT THE FORWARD FUSELAGE JACKING POINT IS 5 300 kg.
NOTE:
LOAD AT FORWARDFUSELAGE JACKING POINT
1000 kg
CG 15 %
CG 25 %
CG 35 %
CG 45 %
1000 lb
N_AC_021400_1_0350101_01_00
Loads at the Aircraft Jacking PointsForward Fuselage Jacking Point - Twin Wheel/Bogie
FIGURE-2-14-0-991-035-A01
2-14-0Page 10
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021400_1_0360101_01_00
25 30 35 40 45 50 55 60 65 70 75
55 66 77 88 99 110 121 132 143 154 165
1000 kg
1000 lb
A/C WEIGHT
10
15
20
25
30
35
29.06
EXAMPLE:GROSS WT: 60 000 kgCG 25 %FORCE AT EACH WINGJACKING POINT 27 350 kg
MAX PERMISSIBLE LOAD
CG 45 %
CG 35 %
CG 25 %
CG 15 %
LOAD AT WING JACKING POINT AT1000 kg
STA4067 FR8/
Loads at the Aircraft Jacking PointsWing Jacking Point Rib 8 - Twin Wheel/Bogie
FIGURE-2-14-0-991-036-A01
2-14-0Page 11
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021400_1_0370101_01_00
(SAFETY STAY)
FR63
FR73 FR74
FR42
FR33
FR15
/
RIB4 RIB4
RIB22
RIB13
RIB22
RIB13
NOTE: THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
FR64
Jacking for MaintenanceLocation of Shoring CradlesFIGURE-2-14-0-991-037-A01
2-14-0Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
Jacking for Wheel Change
1. General
Landing gear jacking will be required especially for replacing wheels and brake unit components.
The maximum permitted aircraft weight for jacking is 59 000 kg (130 073 lb).
2. Main Gear Jacking (Twin Wheel)
The main gears are normally jacked up by placing a jack directly under the ball pad.
The ball spherical radius is 19 mm (0.75 in).
It is also possible to jack the main gear using a cantilever jack.
3. Main Gear Jacking (4 Wheels Bogie)
The fore and aft pair of MLG wheels can be jacked by placing a jack directly under the ball padslocated at each end of the bogie beam.
The ball spherical radius is 19 mm (0.75 in).
The leading dimensions and environmental distances of these jacking points are shown on Figures 4,5 and 6.
The reactions at each of the jacking points are shown on the graph (Ref. Figure 7).
4. Nose Gear Jacking
For nose gear jacking a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shockabsorber sliding tube. Jacking can be accomplished either by placing a jack directly under the ballpad, or using an adapter fitting provided with an identical ball pad.
2-14-0Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021400_1_0450101_01_00
NOTE:
45 x 16 R20
552 mm(21.73 in)
38 mm(1.5 in)
DIA. BALL
25 mm (1 in)
218 mm(8.58 in)
180 mm(7.09 in)
ON THE RIM
200 mm(7.87 in)FULLY
RETRACTED
49 x 19 R20
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES.TWIN WHEEL TRACK IS 927 mm (36.5 in).
THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)CLEARANCE BETWEEN THE TIRE AND GROUND.
600 mm(23.62 in)FULLY
EXTENDED
FLAT TIRES
INFLATED TIRES
Landing Gear Jacking for Wheel ChangeMLG Jacking Point Location - Twin Wheels
FIGURE-2-14-0-991-045-A01
2-14-0Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
MLG TIRE 49 x 19 R20
TWIN WHEEL TRACK
DOUBLE FLAT MLG TIRES
FORK
CONTOUR OF TIRES ON GROUND
CANTILEVERARM
1 620 mm(63.78 in)
MIN
218 mm (8.58 in)(180 mm (7.09 in)
ON RIM)
552 mm(21.73 in)
FWD
APPROX
N_AC_021400_1_0460101_01_00
643 mm(25.32 in)
927 mm(36.5 in)
MIN25 mm(1 in)
25 mm(1 in)
409 mm(16.1 in)
25 mm(1 in)
Landing Gear Jacking for Wheel ChangeMLG Jacking with Cantilever Jack - Twin Wheels
FIGURE-2-14-0-991-046-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
300
35 40 45 50 55 60 65 70 75 80
5
10
15
20
25
35
40
30
CG 40 %
CG 30 %CG 25 %
CG 20 %CG 17 %
180170160150140130120110100908070
A/C WEIGHT1 000 kg
1 000 lb
LOAD AT MLGJACKING POINT
1 000 kg
N_AC_021400_1_0470101_01_00
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking Points - Twin Wheels
FIGURE-2-14-0-991-047-A01
2-14-0Page 16
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021400_1_0480101_01_00
JAC
KIN
G P
OIN
T 1
80 m
m (
7.09
in)
SIT
TIN
G O
N R
IMS
133
mm
(5.
24 in
)
TWO FRONT TIRES DEFLATED
JAC
KIN
G P
OIN
T 2
29 m
m
ONE FRONT TIRE DEFLATED
JAC
KIN
G P
OIN
T 2
70 m
m
NORMAL ATTITUDE
FWD
(10.
63 in
)(9
.02
in)
JAC
KIN
G P
OIN
T 2
70 m
m(1
0.63
in)
FWD
FWD
Landing Gear Jacking for Wheel ChangeMLG Jacking Point Location Bogie
FIGURE-2-14-0-991-048-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021400_1_0490101_01_00
JAC
KIN
G P
OIN
T 1
80 m
m (
7.09
in)
ON
RIM
S 1
33 m
m (
5.24
in) ALL FOUR TIRES DEFLATED
JAC
KIN
G P
OIN
T 1
80 m
m (
7.09
in)
ON
RIM
S 1
33 m
m (
5.24
in)
JAC
KIN
G P
OIN
T 1
80 m
m (
7.09
in)
ON
RIM
S 1
33 m
m (
5.24
in)
TWO REAR TIRES DEFLATED
JAC
KIN
G P
OIN
T 2
29 m
m
ONE REAR TIRE DEFLATED
FWD
FWD
FWD (9.0
2 in
)
Landing Gear Jacking for Wheel ChangeMLG Jacking Point Location Bogie
FIGURE-2-14-0-991-049-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_021400_1_0500101_01_00
780 mm
46 m
mFLAT TIRE DIMENSIONS
JAC
KIN
G P
OIN
T 3
80 m
m
25 m
m C
LEA
R
MAX DIAMETER915 mm (36.02 in)
REAR WHEELS JACKED UP
25 m
m C
LEA
R
MAX DIAMETER915 mm (36.02 in)
FRONT WHEELS JACKED UP
JAC
KIN
G P
OIN
T 3
80 m
m
(14.
96 in
)
(0.9
8 in
)
(14.
96 in
)
(30.71 in) (0.9
8 in
)
(1.8
1 in
)
(5.51 in)140 mm
(12.99 in)330 mm
(48.43 in)1 230 mm
Landing Gear Jacking for Wheel ChangeMLG Jacking Point Location Bogie
FIGURE-2-14-0-991-050-A01
2-14-0Page 19
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
300
35 40 45 50 55 60 65 70 75 80
180170160150140130120110100908070
5
10
15
20
A/C WEIGHT1 000 kg
1 000 lb
LOAD AT MLGJACKING POINT
1 000 kg
LOADS GIVEN ARE THOSE AT EACH BOGIE BEAMJACKING POINT (FRONT AND REAR)
NOTE:
CG 40 %CG 30 %
CG 25 %CG 20 % CG 17 %
N_AC_021400_1_0510101_01_00
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking Points - Bogie Version
FIGURE-2-14-0-991-051-A01
2-14-0Page 20
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
45 50 55 60 65 70 75 80
KEY:−
18
20
22
24
26
28
30
32
34
36
37.5% CG
33.0% CG
28.0% CG
17.0% CG
LOAD AT MLGJACKING POINT
1 000 kg
N_AC_021400_1_0520101_01_00
x1 000 lb
x1 000 kg
180170160150140130120110100
AIRCRAFT WEIGHT
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking Points - 77 000 kg
FIGURE-2-14-0-991-052-A01
2-14-0Page 21
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
APPROX326 mm
(12.83 in)38 mm(1.5 in)
DIA. BALLSAE AS 33559
25 mm(1 in)
128 mm(5.06 in)
40 mm(1.57 in)
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES.THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)CLEARANCE BETWEEN THE TIRE AND GROUND.
NOTE:
FWD
500 mm (19.69 in)
INFLATED TIRESFLAT TIRES
198 mm(7.8 in)
264 mm MIN (10.39 in)289 mm MAX (11.38 in)
N_AC_021400_1_0530101_01_00
A
A
Landing Gear Jacking for Wheel ChangeNLG Jacking - Point LocationFIGURE-2-14-0-991-053-A01
2-14-0Page 22
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 70 80
2
3
4
5
6
7
8
9
10
11
12
54
LOAD AT NLGJACKING POINT
1 000 kg
CG 45%
CG 40%
CG 35%
CG 30%
CG 20%
CG 15%
CG 25%
N_AC_021400_1_0540101_01_00
AIRCRAFT WEIGHT
180170160150140130120 x 1 000 lb190 200
x 1 000 kg
Landing Gear Jacking for Wheel ChangeLoads at NLG Jacking PointsFIGURE-2-14-0-991-054-A01
2-14-0Page 23
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
45 50 55 60 65 70 75 80
KEY:−
3
4
5
6
7
8
9
10
11
17.0% CG
28.0% CG
33.0% CG
37.5% CG
LOAD AT NLGJACKING POINT
1 000 kg
N_AC_021400_1_0550101_01_00
AIRCRAFT WEIGHT
180170160150140130120110100 x 1 000 lb
x 1 000 kg
Landing Gear Jacking for Wheel ChangeLoads at NLG Jacking Points - 77 000 kg
FIGURE-2-14-0-991-055-A01
2-14-0Page 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0 General Information
**ON A/C A320-200
General Information
1. This section gives standard day temperatures.
Section 3-2 indicates payload range information at specific altitudes recommended for long rangecruise with a given fuel reserve condition.
Section 3-3 represents FAR take-off runway length requirements at ISA and ISA +15˚C (+59˚F) forCFM56-5A, CFM56-5B and IAE V2500 series engine conditions for FAA certification.
Section 3-4 represents FAR landing runway length requirements for FAA certification.
Section 3-5 indicates final approach speeds.
Standard day temperatures for the altitudes shown are tabulated below:
Standard day temperatures for the altitude
Altitude Standard Day Temperature
FEET METERS ˚F ˚C0 0 59.0 15.02000 610 51.9 11.14000 1219 44.7 7.16000 1829 37.6 3.18000 2438 30.5 -0.8
3-1-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-0 Payload / Range
**ON A/C A320-200
Payload / Range
1. Payload / Range
3-2-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1 ISA Conditions
**ON A/C A320-200
ISA Conditions
1. This section gives the payload / range at ISA conditions.
3-2-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
20 10 0
(100
0 lb
)(1
000
kg)
PA
YLO
AD
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.
NO
TE
:
50 40 30 20 10 00
1000
2000
3000
4000
7000
6000
4000
5000
3000
2000
1000
0R
AN
GE
(KM
)
RA
NG
E(N
M)
77t
73.5
t75.5
t
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
150
PA
SS
EN
GE
RS
N_AC_030201_1_0060101_01_00
Payload / RangeCFM56-5A series engine
FIGURE-3-2-1-991-006-A01
3-2-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
20 10 0
(100
0 lb
)(1
000
kg)
PA
YLO
AD
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.
NO
TE
:
50 40 30 20 10 00
1000
2000
3000
4000
7000
6000
4000
5000
3000
2000
1000
0R
AN
GE
(KM
)
RA
NG
E(N
M)
73.5
t
77t
75.5
t
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
150
PA
SS
EN
GE
RS
N_AC_030201_1_0070101_01_00
Payload / RangeCFM56-5B series engine
FIGURE-3-2-1-991-007-A01
3-2-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
20 10 0
(100
0 lb
)(1
000
kg)
PA
YLO
AD
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.
NO
TE
:
50 40 30 20 10 00
1000
2000
3000
4000
7000
6000
4000
5000
3000
2000
1000
0R
AN
GE
(KM
)
RA
NG
E(N
M)
77t
73.5
t
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
150
PA
SS
EN
GE
RS
75.5
t
N_AC_030201_1_0080101_01_00
Payload / RangeIAE V2500-A1 series engineFIGURE-3-2-1-991-008-A01
3-2-1Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
20 10 0
(100
0 lb
)(1
000
kg)
PA
YLO
AD
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.
NO
TE
:
50 40 30 20 10 00
1000
2000
3000
4000
7000
6000
4000
5000
3000
2000
1000
0R
AN
GE
(KM
)
RA
NG
E(N
M)
77t
73.5
t
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
150
PA
SS
EN
GE
RS
75.5
t
N_AC_030201_1_0090101_01_00
Payload / RangeIAE V2500-A5 series engineFIGURE-3-2-1-991-009-A01
3-2-1Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-0 FAR / JAR Takeoff Weight Limitation
**ON A/C A320-200
FAR / JAR Take-off Weight Limitation
1. FAR / JAR Take-off Weight Limitation
3-3-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1 ISA Conditions
**ON A/C A320-200
ISA Conditions
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RUNWAY LENGTH
1 000 ft
1 000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
16141210864
54321
8
20
46
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(1
000
ft)
1 000 kg
TA
KE
−O
FF
WE
IGH
T
1 000 lb
N_AC_030301_1_0050101_01_01
FAR / JAR Take-off Weight LimitationISA Conditions -- CFM56 series engine
FIGURE-3-3-1-991-005-A01
3-3-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RUNWAY LENGTH
1 000 ft
1 000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
16141210864
54321
46
8
02
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(1
000
ft)
1 000 kg
TA
KE
−O
FF
WE
IGH
T
1 000 lb
N_AC_030301_1_0060101_01_01
FAR / JAR Take-off Weight LimitationISA Conditions -- IAE V2500 series engine
FIGURE-3-3-1-991-006-A01
3-3-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2 ISA +15˚C (+59˚F) Conditions
**ON A/C A320-200
ISA +15˚C (+59˚F) Conditions
1. This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions.
3-3-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
16141210864
54321
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
02468
N_AC_030302_1_0050101_01_01
FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56 series engine
FIGURE-3-3-2-991-005-A01
3-3-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1000 ft
1000 m
8
6420
RUNWAY LENGTH
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
110
100
90
80
70
60
50
40
16141210864
54321
110
120
130
140
150
160
170
180
190
200
210
220
230
N_AC_030302_1_0060101_01_00
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- IAE V2500 series engine
FIGURE-3-3-2-991-006-A01
3-3-2Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-0 FAR / JAR Landing Field Length
**ON A/C A320-200
FAR / JAR Landing Field Length
1. FAR / JAR Landing Field Length
3-4-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1 ISA Conditions
**ON A/C A320-200
ISA Conditions
1. This section gives the landing field length.
3-4-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2.5
2.0
1.5 1
8 7 6 5 4 3
6080
100
120
140
160
180
9080
7060
5040
3020LE
NG
TH
(100
0 m
)
F.A
.R. L
AN
DIN
GT
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
NO
TE
:
GR
OS
S W
EIG
HT
(100
0 lb
)
GR
OS
S W
EIG
HT
(100
0 kg
)
(100
0 ft)
FA
R L
AN
DIN
G F
IELD
LE
NG
TH
= A
CT
UA
L D
IST
AN
CE
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(100
0 ft)
24
68
10
LEV
EL
N_AC_030401_1_0050101_01_00
0.6
SE
A
FAR / JAR Landing Field LengthCFM56 series engine
FIGURE-3-4-1-991-005-A01
3-4-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2.5
2.0
1.5 1
8 7 6 5 4 3
6080
100
120
140
160
180
9080
7060
5040
3020LE
NG
TH
(100
0 m
)
F.A
.R. L
AN
DIN
GT
HE
SE
CU
RV
ES
AR
E G
IVE
N F
OR
INF
OR
MA
TIO
N O
NLY
TH
E A
PP
RO
VE
D V
ALU
ES
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
NO
TE
:
GR
OS
S W
EIG
HT
(100
0 lb
)
GR
OS
S W
EIG
HT
(100
0 kg
)
(100
0 ft)
FA
R L
AN
DIN
G F
IELD
LE
NG
TH
= A
CT
UA
L D
IST
AN
CE
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(100
0 ft)
24
68
100.
6
N_AC_030401_1_0060101_01_00
LEV
EL
SE
A
FAR / JAR Landing Field LengthIAE V2500 series engine
FIGURE-3-4-1-991-006-A01
3-4-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0 Final Approach Speed
**ON A/C A320-200
Final Approach Speed
1. This section gives the final approach speed.
3-5-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
C.A
.S (
Kts
)
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.
NO
TE
:
GR
OS
S W
EIG
HT
(100
0 lb
)
GR
OS
S W
EIG
HT
(100
0 kg
)
170
160
150
140
130
120
110
100 60
8010
012
014
016
018
020
0
2030
4050
6070
8090
100
LAN
DIN
G G
EA
R E
XT
EN
DE
DS
LAT
S 2
7 D
EG
.F
LAP
S 3
5 D
EG
.S
EA
LE
VE
L
N_AC_030500_1_0050101_01_00
Final Approach SpeedCFM56 series engine
FIGURE-3-5-0-991-005-A01
3-5-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
I.A.S
(K
ts)
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
S A
RE
ST
AT
ED
IN T
HE
"O
PE
RA
TIN
GM
AN
UA
LS"
SP
EC
IFIC
TO
TH
E A
IRLI
NE
OP
ER
AT
ING
TH
E A
IRC
RA
FT
.
NO
TE
:
GR
OS
S W
EIG
HT
(100
0 lb
)
GR
OS
S W
EIG
HT
(100
0 kg
)
170
160
150
140
130
120
110
100 60
8010
012
014
016
018
020
0
2030
4050
6070
8090
100
LAN
DIN
G G
EA
R E
XT
EN
DE
DS
LAT
S 2
7 D
EG
.F
LAP
S 4
0 D
EG
.S
EA
LE
VE
L
N_AC_030500_1_0060101_01_00
Final Approach SpeedIAE V2500 series engine
FIGURE-3-5-0-991-006-A01
3-5-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A320-200
General Information
1. This section provides airplane turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.
In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the using airlines prior to layout planning.
4-1-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0 Turning Radii
**ON A/C A320-200
Turning Radii
1. This section gives the turning radii.
4-2-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
R1
R2R3
R5
R4
R6
50°
60°
70°
N_AC_040200_1_0050101_01_01
NOTE:
TURN TYPE:
1. ASYMMETRIC THRUST DIFFERENTIAL BRAKING
FOR STEERING DIMENSION TABLE SEE SHEET 2.
(PIVOTTING ON ONE MAIN GEAR).
2. SYMMETRIC THRUST NO BRAKING.
12.64 m(41.47 ft)
7.59 m(24.9 ft)
Turning Radii, No Slip AngleTurning Radii -- Dual Landing Gear
FIGURE-4-2-0-991-005-A01
4-2-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_040200_1_0100101_01_00
706560555040353029
.3
34.2
39.0
48.6
53.3
57.9
62.4
66.8
19.4
15.5
12.5
8.0
6.3
4.8
3.5
2.4
64 51 41 26 21 16 12 8
27.0
23.1
20.1
15.6
13.9
12.4
11.1
9.9
89 76 66 51 46 41 36 33
26.2
22.8
20.4
17.1
16.0
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14.4
13.9
86 75 67 56 52 50 47 46
39.8
35.9
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28.5
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25.4
24.1
22.9
131
118
108
94 88 83 79 75
40.7
36.8
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29.4
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133
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94 84 77 69 66 64 62 61
34.4
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103
95 84 81 78 75 73
MA
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IGH
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mft
ft
ft
m
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mft
mft
R6
TH
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mft
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174
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7518
.360
21.8
72
24.4
19.5
32.3
40.2
106
132
81107
30.9
38.2
45.1
52.9
46.0
53.8
151
176
33.0
39.8
108
131
39.0
46.0
128
151
22 2 2 2 2 2 2 2 2 2 2
75 (
MA
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7065605550
71.9
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4.7
6.2
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13.4
21.6
22.5
7418
.260
21.6
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53.6
48.8
9.6
10.9
12.3
13.8
15.5
13.8
14.3
15.0
15.9
17.0
22.6
23.9
25.2
26.7
28.4
23.5
24.7
26.0
27.6
29.3
7781859096
18.4
18.8
19.3
20.0
20.9
6162636668
22.1
22.8
23.6
24.5
25.6
73757780841 1 1 1 1 1
284
444547495256
717478838893
3236404551
711152026
4543
.810
.133
17.6
5818
.561
30.5
100
31.4
103
22.1
7227
.189
AB
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0°, A
IRLI
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S M
AY
US
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OR
TY
PE
2 T
UR
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DE
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ON
TH
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TU
RN
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SE
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TU
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LY.
TY
PE
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UR
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IT IS
PO
SS
IBLE
TO
GE
T L
OW
ER
VA
LUE
S T
HA
N T
HO
SE
FR
OM
TY
PE
1 B
Y A
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LYIN
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IFF
ER
EN
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L B
RA
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UR
ING
NO
TE
:
TH
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HO
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UR
N.
AS
YM
ME
TR
IC T
HR
US
T D
UR
ING
TH
E W
HO
LE T
UR
N; A
ND
DIF
FE
RE
NT
IAL
BR
AK
ING
TO
INIT
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E
SY
MM
ET
RIC
TH
RU
ST
DU
RIN
G T
HE
WH
OLE
TU
RN
; AN
D N
O D
IFF
ER
EN
TIA
L B
RA
KIN
G A
T A
LL.
Turning Radii, No Slip AngleTurning Radii -- Dual Landing Gear
FIGURE-4-2-0-991-010-A01
4-2-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
R5
R3
R4
R1
R6
R2
50°
60°
70°
N_AC_040200_1_0060101_01_02
NOTE: FOR STEERING DIMENSION TABLE SEE SHEET 2.
12.64 m(41.47 ft)
7.59 m(24.9 ft)
Turning Radii, No Slip AngleTurning Radii -- Bogie Landing Gear
FIGURE-4-2-0-991-006-A01
4-2-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
mft
R3
R4
R5
R6
mft
mft
mft
mft
mft
R2
R1
ST
EE
RIN
GA
NG
LE(d
eg)
116
13.7
110
173
22.3
973
22.4
035
.28
8325
.29
30.8
6
106
10.7
294
6419
.40
6620
.02
32.3
276
23.2
528
.56
988.
388
5616
.98
6018
.24
29.9
271
21.7
626
.81
926.
2783
4914
.95
5516
.86
27.9
068
20.6
525
.42
864.
5180
4313
.19
5215
.79
26.1
765
19.8
024
.29
812.
9677
3811
.64
4914
.95
24.6
463
19.1
623
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781.
5574
3410
.23
4714
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23.2
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18.6
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720.
2672
298.
9445
13.8
121
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6018
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128
17.5
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111
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9228
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6
45 35 27 21 15 10 5 1706560555045403530
N_AC_040200_1_0110101_01_00
Turning Radii, No Slip AngleTurning Radii -- Bogie Landing Gear
FIGURE-4-2-0-991-011-A01
4-2-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A320-200
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
EFFECTIVESTEERING Y A
R3NLG
R4 WING R5NOSE
R6THS
726072457515
21.918.322.013.822.84.6m
ft
WING TIP FENCE
DUAL LANDING GEAR
BOGIE LANDING GEAR
70.0°75 (MAX)
ANGLE
STEERINGANGLE(DEG)
N_AC_040300_1_0030101_01_01
R6
R3
R5
R412.6 m
NOTE:MINIMUM TURNING RADIUS.SLOW CONTINUOUS TURNING.APPROXIMATELY IDLE THRUST
THEORETICAL CENTER OF TURN FOR
(41 ft)
STEERINGANGLE 75°
Y
ON ALL ENGINES.NO DIFFERENTIAL BRAKING.NOSE GEAR RADII TRACK MEASUREDFROM OUTSIDE FACE OF TIRE.
NOTE:BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1
TYPEOF
TURN
1
2
STEERINGANGLE(DEG)
75 (MAX)
75 (MAX)
EFFECTIVESTEERING
ANGLE
71.9°
70.2°
m
m
ft
ft
Y
4.1
4.5
14
15
A
22.3
22.8
73
75
R3NLG
13.4
13.6
44
44
R4 WINGWING TIP
FENCE
21.6
22.0
71
72
SHARKLET
22.5
22.9
74
75
R5NOSE
18.2
18.3
60
60
R6THS
21.6
21.8
71
72
PAVEMENTWIDTH FOR180° TURN
MINIMUM
A
OUTSIDE FACE OF TIRE
EFFECTIVETURN
Minimum Turning RadiiFIGURE-4-3-0-991-003-A01
4-3-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A320-200
Visibility from Cockpit in Static Position
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30°
20°
10.14 m(33 ft 3.24 in)
5.07 m(16 ft 7.56 in)
VISUAL ANGLES IN VERTICALPLANE THROUGH PILOTEYE POSITION.
NOT TO BE USED FORLANDING APPROACH VISIBILITY
DIMENSIONS ARE APPROXIMATE
2.41 m(7 ft 10.92 in)4.56 m
(14 ft 11.52 in)
111°
133°
CAPTAIN FIELD OF VIEW
133°
111°
MAX AFT VISION WITH HEAD TURNEDAROUND SPINAL COLUMN.WING TIP CAN BE SEEN WHEN HEAD IS MOVEDTO THE SIDE.
VISUAL ANGLES IN HORIZONTALPLANE THROUGH PILOTEYE POSITION.
FIRST OFFICERFIELD OF VIEW
0.53 m(1 ft 8.88 in)
46°
32°
33°
25°
32°
25°
VISUAL ANGLES IN PLANEPERPENDICULAR TOLONGITUDINAL AXIS.
46°
33°
WITH HEAD MOVED125 mm (5 in) OUTBOARD
NOTE:PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
ZONE THAT CANNOT BE SEEN
N_AC_040400_1_0010101_01_03
Visibility from Cockpit in Static PositionFIGURE-4-4-0-991-001-A01
4-4-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FIR
ST
OF
FIC
ER
FIX
ED
WIN
DO
WF
IRS
T O
FF
ICE
RS
LID
ING
WIN
DO
WF
IRS
T O
FF
ICE
RW
IND
SH
IELD
CA
PT
AIN
WIN
DS
HIE
LDC
AP
TA
IN S
LID
ING
WIN
DO
WC
AP
TA
INF
IXE
D W
IND
OW
PIL
OT
EY
E P
OS
ITIO
N(C
AP
TA
IN P
OS
ITIO
N)
AS
580
B
A32
0
CA
PT
AIN
FIE
LD O
F V
IEW
SH
OW
N.
FIR
ST
OF
FIC
ER
FIE
LD O
F V
IEW
SY
MM
ET
RIC
AL.
EX
AM
PLE
: WH
EN
CA
PT
AIN
TU
RN
S H
IS H
EA
D B
Y 8
0° L
EF
T, V
ISIB
ILIT
YW
ILL
BE
35°
UP
AN
D 2
5° D
OW
N T
HR
OU
GH
TH
E S
LID
ING
WIN
DO
W F
RA
ME
.
35°
30°
20°
10°
0° 10°
20°
25°
110°
100°
90°
80°
70°
50°
40°
30°
20°
10°
0°10
°20
°40
°50
°60
°80
°90
°10
0°13
0°12
0°60
°30
°70
°11
0°
N_AC_040400_1_0050101_01_00
Binocular Visibility Through Windows from Captain Eye PositionFIGURE-4-4-0-991-005-A01
4-4-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A320-200
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A320-200
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FAA LEAD−IN FILLET
L = 45 m (150 ft)
TAXIWAYCENTERLINE
RUNWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
APPROX 4.3 m(14 ft)
NOTE: FAA GROUP III FACILITIES.
30 m
N_AC_040501_1_0040101_01_01
NLG PATH
MLG PATH
15 m(50 ft)
(100 ft)
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-004-A01
4-5-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TAXIWAYCENTERLINE
RUNWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
FAA LEAD−IN FILLET
L = 45 m (150 ft)
APPROX 3.2 m(10 ft)
30 m
NOTE: FAA GROUP III FACILITIES.
N_AC_040501_1_0120101_01_00
NLG PATH
MLG PATH
15 m(50 ft)
(100 ft)
135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-1-991-012-A01
4-5-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A320-200
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
APPROX 5.8 m(19 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
RUNWAY CENTERLINE
FAA LEAD−IN FILLETL = 45 m (150 ft)
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.N_AC_040502_1_0040101_01_01
NLG PATH
MLG PATH
30 m(100 ft)
15 m(50 ft)
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-004-A01
4-5-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
APPROX 9.2 m(30 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
RUNWAY CENTERLINE
FAA LEAD−IN FILLETL = 45 m (150 ft)
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATH
30 m(100 ft)
15 m(50 ft)
N_AC_040502_1_0090101_01_00
90˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-2-991-009-A01
4-5-2Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A320-200
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 m(100 ft)
NOTE: TYPE 1 VALUES.
RUNWAY CENTERLINE
R3 = 13.4 m(44 ft)
R5 = 18.2 m(60 ft)
R4
3.15 m(10 ft)
5.75 m(19 ft)
N_AC_040503_1_0060101_01_00
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
WINGTIP FENCES:R4 = 21.6 m (71 ft)SHARKLETS:R4 = 22.5 m (74 ft)
180˚ Turn on a RunwayEdge of Runway Method (Sheet 1 of 2)
FIGURE-4-5-3-991-006-A01
4-5-3Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 m(100 ft)
NOTE: TYPE 1 VALUES.
RUNWAY CENTERLINE
4.33 m(14 ft)
3.13 m(10 ft)
25°
N_AC_040503_1_0060102_01_00
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
WINGTIP FENCES:R4 = 21.6 m (71 ft)SHARKLETS:R4 = 22.5 m (74 ft)
R3 = 13.4 m(44 ft)
R5 = 18.2 m(60 ft)
R4
180˚ Turn on a RunwayCenter of Runway Method (Sheet 2 of 2)
FIGURE-4-5-3-991-006-A01
4-5-3Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4 135˚ Turn - Taxiway to Taxiway
**ON A/C A320-200
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway.
4-5-4Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FAA LEAD−IN FILLET
APPROX 4.9 m(16 ft)
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
FILLET R = 16.5 m
TURN R = 30 m
15 m(50 ft)
15 m(50 ft)
N_AC_040504_1_0060101_01_00
(100 ft)
(55 ft)
L = 45 m (150 ft)
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-4-991-006-A01
4-5-4Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
FILLET R = 16.5 m
TURN R = 30 m
FAA LEAD−IN FILLET
APPROX 3 m
N_AC_040504_1_0060102_01_00
15 m(50 ft)
15 m(50 ft)
L = 45 m (150 ft)(55 ft)
(100 ft)
(10 ft)
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-4-991-006-A01
4-5-4Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5 90˚ Turn - Taxiway to Taxiway
**ON A/C A320-200
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-5Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_040505_1_0020101_01_01
TAXIWAY CENTERLINE
NLG PATH
MLG PATHTAXIWAY CENTERLINE
APPROX 5.2 m(17 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft)
NOTE: FAA GROUP III FACILITIES.
15 m(50 ft)
15 m(50 ft)
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-5-991-002-A01
4-5-5Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TAXIWAY CENTERLINE
NOTE:
NLG PATH
MLG PATH
FAA GROUP III FACILITIES.
TAXIWAY CENTERLINE
APPROX 9 m(29 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft)
N_AC_040505_1_0020102_01_00
15 m(50 ft)
15 m(50 ft)
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-5-991-002-A01
4-5-5Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A320-200
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RUNWAY CENTERLINETAXIWAY
CENTERLINE
HOLDING POINT
12.2 m
NOTE: COORDINATE WITH USING AIRLINE FOR SPECIFIC PLANNED OPERATING PROCEDURES.
N_AC_040600_1_0030101_01_01
190 m
23 m(75 ft)
45 m(150 ft)
61 m(200 ft)61 m
(200 ft)
6.1 m(20 ft)
6.1 m(20 ft)
190 m(625 ft)
(40 ft)
90 m(300 ft)
Runway Holding Bay (Apron)FIGURE-4-6-0-991-003-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
**ON A/C A320-200
Terminal Servicing
1. GeneralThis chapter provides typical ramp layouts, corresponding minimum turnaround time estimations,locations of ground service points and service requirements.The information given in this chapter reflects ideal conditions. Actual ramp layouts and servicerequirements may vary according to local regulations, airline procedures and the airplane condition.- Section 5.1 shows typical ramp layouts for passenger aircraft at the gate or on an open apron.- Section 5.2 shows the minimum turnaround schedules for full servicing arrangements.- Section 5.3 shows the minimum turnaround schedule for reduced servicing arrangements.- Section 5.4 gives the locations of ground service connections, the standard of connections used
and typical capacities and requirements.- Section 5.5 provides the engine starting pneumatic requirements for different engine types and
different ambient temperatures.- Section 5.6 provides the air conditioning requirements for heating and cooling (pull-down and
pull-up) using ground conditioned air for different ambient temperatures.- Section 5.7 provides the air conditioning requirements for heating and cooling to maintain a
constant cabin air temperature using low pressure conditioned air.- Section 5.8 shows the ground towing requirements taking into account different ground surface
and aircraft conditions.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-0 Servicing Arrangements
**ON A/C A320-200
Airplane Servicing Arrangements
1. GeneralThis chapter provides typical ramp layouts, showing the various GSE items in position during typicalturnaround scenarios for the passenger aircraft.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.
The associated turnaround chart for full servicing is given in section 5.2.The associated turnaround chart for minimum servicing arrangement is given in section 5.3.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A320-200
Symbols Used on Servicing Diagrams
1. This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC AIR CONDITIONING UNITAS AIR STARTING UNITBULK BULK TRAINCAT CATERING TRUCKCB CONVEYOR BELTCLEAN CLEANING TRUCKFUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNITLD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLEPBB PASSENGER BOARDING BRIDGEPS PASSENGER STAIRSTOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2 Typical Ramp Layout - Open Apron
**ON A/C A320-200
Typical Ramp Layout - Open Apron
1. This section gives the typical servicing arrangement for pax version (Open Apron).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m from theaircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks inposition on landing gears).
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_050102_1_0030101_01_03
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6
CAT
CAT
LV
FUEL
ASTOW
WV
GPU
CB
CB
BULK
BULK
PS
PS
AC
Typical Ramp LayoutOpen Apron - Bulk LoadingFIGURE-5-1-2-991-003-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_050102_1_0090101_01_00
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6
CAT
ULD
CAT
LV
ULD
FUEL
ASTOW
WV
BULK
GPU
CB
PS
PS
LD CL
LD CL
AC
Typical Ramp LayoutOpen Apron - ULD LoadingFIGURE-5-1-2-991-009-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3 Typical Ramp Layout - Gate
**ON A/C A320-200
Typical Ramp Layout - Gate
1. This section gives the typical servicing arrangement for pax version (Passenger Bridge).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m from theaircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks inposition on landing gears).
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
LD CL
LD CL
N_AC_050103_1_0020101_01_03
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6
CAT
ULD
CAT
LV
ULDPBB
FUEL
ASTOW
WV
BULK
GPU
CB
AC
Typical Ramp LayoutGate
FIGURE-5-1-3-991-002-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0 Terminal Operations - Full Servicing
**ON A/C A320-200
Terminal Operations - Full Servicing Turn Round Time
1. This section provides typical turn round time chart showing the typical times for ramp activitiesduring aircraft turn round.
Actual times may vary due to each operator’s specific practice and operating conditions.
For each turn round time chart, the associated typical ramp layout is given in Section 5-1.
2. Assumptions for full turn round chart
A. PASSENGER HANDLING150 pax, all Y/CAll passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 2 min
Deboarding:- 150 pax at door L1- Deboarding rate = 22 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 150 pax at door L1- Boarding rate = 18 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +2 min- No Passenger with Reduced Mobility
B. CARGO2 cargo loaders + 1 belt loaderEquipment positioning/removal + opening/closing door = +1 min
Cargo exchange:- FWD cargo compartment: 3 LD3- AFT cargo compartment: 4 LD3- Bulk compartment: 500 kg (1102 lb)
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Bulk off-loading/loading times:- Bulk off-loading rate = 120 kg/min (265 lb/min)- Bulk loading rate = 100 kg/min (220 lb/min)
C. REFUELLING2 hoses, one side7134 l (1885 US gal) at 50 psi (3 bar)Dispenser positioning/removal = 4 min
D. CLEANINGPerformed in available time
E. CATERING1 catering truck for servicing galleys sequentially at doors R1 & R2Equipment positioning/removal + door opening/closing = 2 minTime to drive from one door to the other = 1 minFull Size Trolley Equivalent (FSTE) to unload and load:- 4 FSTE at door R1- 7 FSTE at door R2Time for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING SERVICINGStart of operations:- Bridges: t0 = 0- Other equipment: t = t0 + 1 minPotable water servicing: 100% uplift, 200 l (53 US gal), max filling pressure = 3.45 bar (50 psi)Toilet servicing: draining + rinsing = 5 min, max rinse & precharge pressure = 3.45 bar (50psi)
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0 5 15 20 25 30 35 40
CATERING AT DOOR R1
CATERING AT DOOR R2
CLEANING
CARGO FWD CC
BULK
REFUELLING
TOILET SERVICING
HEADCOUNTING
CARGO AFT CC
TRT: 43 min
10 45
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
DEBOARDING/BOARDING AT DOOR L1
POTABLE WATERSERVICING
N_AC_050200_1_0060101_01_01
min
AVAILABLE TIME
Turn Round StationsFull Servicing (43 Min.)
FIGURE-5-2-0-991-006-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0 Terminal Operation - Transit
**ON A/C A320-200
Terminal Operation - Minimum Servicing Turn Round Time
1. This section provides typical turn round time chart showing the typical times for ramp activitiesduring aircraft turn round.
Actual times may vary due to each operator’s specific practice and operating conditions.
For each turn round time chart, the associated typical ramp layout is given in Section 5-1.
2. Assumptions for minimum turn round chart
A. PASSENGER HANDLING180 pax, all Y/C2 Stairways used at doors L1 & L2Equipment positioning/removal + opening/closing door = 2 min
Deboarding:- 90 pax at door L1- 90 pax at door L2- Deboarding rate = 20 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 90 pax at door L1- 90 pax at door L2- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +2 min- No Passenger with Reduced Mobility
B. CARGO2 cargo loadersEquipment positioning/removal + opening/closing door = +1 min
Cargo exchange:- FWD cargo compartment: 3 LD3- AFT cargo compartment: 4 LD3- Bulk cargo compartment: 500 kg (1102 lb)
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Bulk off-loading/loading times:- Off-loading rate = 120 kg/min (265 lb/min)- Loading rate = 100 kg/min (220 lb/min)
C. REFUELLING2 hoses, one side7134 l (1885 US gal) at 50 psi (3 bar)Dispenser positioning/removal = 4 min
D. CLEANINGPerformed in available time
E. CATERINGNo catering
F. GROUND HANDLING SERVICINGStart of operations:- Bridges: t0 = 0- Other equipment: t = t0 + 1 minNo potable water servicingNo toilet servicing
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TRT: 23 min
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
0 5 15 20 25 3010
AVAILABLE TIME
AVAILABLE TIME
min
N_AC_050300_1_0030101_01_01
HEADCOUNTING
CATERING
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CARGO AFT CC
DEBOARDING/BOARDING AT DOOR L1
DEBOARDING/BOARDING AT DOOR L2
Turn Round StationsMinimum Servicing (23 Min.)FIGURE-5-3-0-991-003-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-0 Ground Service Connections
**ON A/C A320-200
Ground Service Connections
1. Ground Service Connections.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1 Ground Service Connections Layout
**ON A/C A320-200
Ground Service Connections Layout
1. This section gives the ground service connections layout.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1 2 3 11 12 2 4 14−6 7−
141
CONNECTOR (LP) PANELS
EXTERNAL POWER RECEPTACLETOILET SERVICE DOORGROUNDING POINT NLGPOTABLE WATER SERVICE DOORGROUND SERVICE CONDITIONED AIR
IDG OIL FILLINGENGINE OIL FILLING CONNECTOR APU OIL FILLING
GRAVITY REFUEL
HYDRAULIC SYSTEM GROUND SERVICESGROUNDING POINT MLGREFUEL/DEFUEL CONNECTORSREFUEL/DEFUEL PANELGROUND AIR START CONNECTOR (HP)1 −
2 −3 −4 −5 −
8 −9 −
10 −11 −12 −
6 −7 −
13 −14 −
13
10
10
13
67
6
7
42 5 8 12
29
N_AC_050401_1_0050101_01_01
Ground Service ConnectionsGround Service Connections Layout
FIGURE-5-4-1-991-005-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2 Grounding Points
**ON A/C A320-200
Grounding Points
1. Grounding Points.
DISTANCE: Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUNDOn Nose Landing Gearleg:
5.07 m(16.63 ft) on centerline
0.94 m(3.08 ft)
On left Main LandingGear leg:
20.25 m(66.44 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
On right Main LandingGear leg:
20.25 m(66.44 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).
B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for:- refuel/defuel operations,- maintenance operations,- bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
(2)(1)
GROUND CABLE(OPTIONAL)
LANDINGGEAR
NOSE LANDING GEAR
MAIN LANDING GEAR
(1)
A
A
A
(1)
N_AC_050402_1_0050101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-005-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE: R SIDE SYMMETRICAL
A
FWD
A
FOR SPECIFICATIONS REFERTO FLIGHT MANUAL
B
B
RIB20
RIB19
N_AC_050402_1_0060101_01_00
A
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-006-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3 Hydraulic System
**ON A/C A320-200
Hydraulic System
1. Access.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green System:Access door 197CB
19.17(62.89)
1.27(4.17)
1.76(5.77)
Yellow System:Access door 198CB
19.17(62.89)
1.27(4.17)
1.76(5.77)
Blue System:Access door 197EB
20.22(66.34)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.
2. Reservoir Pressurization.On the air pressurization manifold:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Access door 195BB15.65(51.35)
0.25(0.82)
1.74(5.71)
NOTE : Distances are approximate.- One 1/4 in. AEROQUIP AE 96994E self-sealing connection common to the 3 reservoirs.
3. Accumulator Charging.Four (MS28889-1) connections (one for each accumulator) for:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Yellow Systemaccumulator:Access door 196BB
16.1(52.82)
0.25(0.82)
1.99(6.53)
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green Systemaccumulator:Left MLG door
16.77(55.02)
0.25(0.82)
3.2(10.5)
Blue Systemaccumulator:Access door 195BB
18.2(59.71)
0.25(0.82)
1.99(6.53)
Yellow System brakingaccumulator:Access door 196BB
16.1(52.82)
0.76(2.49)
1.74(5.71)
NOTE : Distances are approximate.
4. Reservoir Filling.On the Green system ground service panel:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Access door 197CB19.17(62.89)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximateOne 1/4 in. AEROQUIP AE96993E self-sealing connection for pressurized supply.One handpump filling connection for unpressurized (suction) supply.
5. Reservoir Drain.On 3/8 in. self-sealing connection on reservoir for:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Yellow System:Access door 196BB -198CB
16.1(52.82)
1.43(4.69)
1.90(6.23)
Green System:Left MLG door
16.77(55.02)
1.27(4.17)
2.61(8.56)
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Blue SystemAccess door 197EB
20.22(66.34)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.On 3/8 in. self-sealing connection for the Blue system on:- Blue system ground service panel.
6. Ground Test.On each ground service panel:- One self-sealing connector AE80532N (suction).- One self-sealing connector AE80531K (delivery).
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RESERVOIR FILL SYSTEMHAND PUMP FILL CONNECTION
GROUND TESTPRESSURE
CONNECTION
GROUND TESTSUCTION
CONNECTIONRESERVOIR FILLCONNECTION
AE96993GM
GROUND SUPPLY
AE80531K AE80532N
1698GM
1008GM 1007GM 1006GM
197CB
A
AN_AC_050403_1_0040101_01_00
Hydraulic SystemGreen System Ground Service Panel
FIGURE-5-4-3-991-004-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
GROUND CONNECTIONSUCTION
GROUNDCONNECTION
DELIVERY
AE80531K
AE80532N
2006GM
2008GM
A
Z197
A
N_AC_050403_1_0050101_01_00
Hydraulic SystemBlue System Ground Service Panel
FIGURE-5-4-3-991-005-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
GROUND TESTPRESSURE CONNECTION
GROUND TESTSUCTION CONNECTION
AE80531K AE80532N
A
A
3008GM 3006GM
198CB
N_AC_050403_1_0060101_01_00
Hydraulic SystemYellow System Ground Service Panel
FIGURE-5-4-3-991-006-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4 Electrical System
**ON A/C A320-200
Electrical System
1. Electrical System.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
A/C External Power:Access door 121AL
2.55(8.37) on centerline
2.00(6.56)
NOTE : Distances are approximate.
2. Technical SpecificationsThis chapter gives data related to the location of the ground service connections.
A. External Power Receptacle:- One Style3 ISO 461 receptacle - 90 KVA.
B. Power Supply:- Three-phase, 400 Hz, 115/200V
C. Electrical Connectors for Servicing:- AC outlets: HUBBELL 5258- DC outlets: HUBBELL 7472
D. Electrical Loads in Ground ConfigurationIn ground configuration, in addition to the power necessary for maintenance, all the circuits,except those which are connected to the engines, are supplied as in flight.In these conditions, the maximum power on ground is approximately 75 KVA; this value doesnot take into account the supply of the galleys, which according to the aircraft interior layout,may reach 30 KVA.
E. Electrical Power necessary for Maintenance at Line Stop and Workshops- Hydraulic electric-pumps: 34 KVA- Air Conditioning/Ventilation: 20.8 KVA- Fuel pumps: 12 KVA- Lighting commercial: 6.7 KVA- Lighting technical: 3 KVA- Ice and rain protection: 3 KVA- Cargo loading: 3 KVA- AFS, Flight controls, ADS, Recorders: 3.3 KVA- Communications: 1.3 KVA
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- Radio navigation: 1.2 KVA.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
108VU
A
N_AC_050404_1_0010101_01_01
A
121AL
Ground Service ConnectionsExternal Power ReceptaclesFIGURE-5-4-4-991-001-A01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5 Oxygen System
**ON A/C A320-200
Oxygen System
1. Oxygen System.
DISTANCE: Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDOne service connection(external charging in theavionics compartment)MS22066 Std.
3.45 m(11.32 ft)
1.15 m(3.77 ft)
2.60 m(8.53 ft)
3/8” UNF × 24 TPI
Nominal pressure: 1850 psi (127.55 bar)
Max fill pressure: 2035 psi (140.31 bar)
NOTE : Internal charging connection provided.
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6 Fuel System
**ON A/C A320-200
Fuel System
1. Refuel/Defuel Control Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Refuel/DefuelIntegrated Panel:Access door 192MB
16.4(53.81)
1.8(5.91)
1.8(5.91)
2. Refuel/Defuel Connectors.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Refuel/Defuel coupling,LeftAccess Door 522HB(Optional)
17.59(57.71)
9.83(32.25)
3.65(11.98)
Refuel/Defuel coupling,RightAccess Door 622HB
17.59(57.71)
9.83(32.25)
3.65(11.98)
Gravity Refuel Coupling19.1(62.66)
12.4(40.68)
12.4(40.68)
3.7(12.14)
A. Refuel/Defuel couplings:- Right wing: one standard ISO 45, 2.5 in.- Left wing: one optional standard ISO 45, 2.5 in.
B. Refuel pressure:- Maximum pressure: 3.45 bar (50 psi).
C. Refuel Flow:- 1400 l/minute (369.84 US gal/minute).
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3. Overpressure Protector and NACA Flame Arrestor.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Overpressure Protector 20.36(66.80)
14.9(48.88)
14.9(48.88)
4.32(14.17)
NACA Flame Arrestor 19.8(64.96)
13.7(44.95)
13.7(44.95)
4.02(13.19)
NOTE : Distances are approximate.
5-4-6Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
REFUEL/DEFUELCONTROL PANEL
NOTE: STANDARD CONFIGURATION OF REFUEL/DEFUEL PANEL.
A
FUELkg x 1000
QTY
RIGHTCTRLEFT
LEFT CTR RIGHT
LVLHI
OPEN
NORM
SHUT
OPEN
NORM
SHUT
REFUEL VALVESOPEN
NORM
SHUT
BATT POWERTESTHI LVL ON
OPEN LTS NORM
MODE SELECTREFUEL
OFF
DEFUEL / XFR
kg x 1000
PRESELECTED
DEC INC
ACTUALREFUEL
CKPT END
A
N_AC_050406_1_0010101_01_00
Ground Service ConnectionsRefuel/Defuel Panel
FIGURE-5-4-6-991-001-A01
5-4-6Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RIB15
RIB14
A
41QM
40QM
LEADINGEDGE
WING FRONTSPAR
A
N_AC_050406_1_0020101_01_00
Ground Service ConnectionsRefuel/Defuel Couplings
FIGURE-5-4-6-991-002-A01
5-4-6Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
RIB19
RIB20
A
ADAPTER(REF ONLY)
GROUND CONNECTION(REF ONLY)
44QM
(45QM)
AFWD
N_AC_050406_1_0030101_01_00
Ground Service ConnectionsGravity Refuel Couplings
FIGURE-5-4-6-991-003-A01
5-4-6Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
A
A ALH SHOWN
RH SYMMETRICAL
FWD
NACA VENT INTAKE
NACA FLAME ARRESTOR
OVERPRESSURE PROTECTOR
N_AC_050406_1_0040101_01_00
B
C
RIB25RIB24
RIB23
RIB22
550CB (650CB)
550AB (650AB)
C
B
Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor
FIGURE-5-4-6-991-004-A01
5-4-6Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7 Pneumatic System
**ON A/C A320-200
Pneumatic System
1. High Pressure Air Connectors.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINEAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
HP ConnectorAccess door 191DB
12.98(42.59)
0.84(2.76)
1.76(5.77)
NOTE : Distances are approximate.
A. Connector:- One standard 3 in. ISO TC20 connection (MS33740) for engine starting and cabin air
preconditioning (HP) installed on the left side of the belly fairing
2. Low Pressure Air Connectors.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINEAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
LP ConnectorAccess door 191CB
12.45(40.85)
1.11(3.64)
1.73(5.68)
NOTE : Distances are approximate.
A. Connector:- One standard 8 in. connection (SAE AS4262 type B) for cabin air preconditioning (LP)
installed on the left side of the belly fairing
5-4-7Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8 Potable Water System
**ON A/C A320-200
Potable Water System
1. Potable Water Ground Service Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Potable WaterGround ServicePanel:Access door 171AL:
31.3(102.69)
0.3(0.98)
2.6(8.53)
NOTE : Distances are approximate
2. Potable Water Ground Drain Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Potable WaterGround ServicePanel:Access door 133AL(Optional)
11.8(38.71)
0.15(0.49)
1.75(5.74)
Potable WaterGround ServicePanel:Access door 192NB
12.5(41.01)
0.51(1.67)
1.75(5.74)
NOTE : Distances are approximate
3. Technical Specifications
A. Connectors:
(1) On the potable ground service panel (Access Door 171AL)- Fill/Drain Nipple 3/4 in (ISO 17775).- One ground pressurization connector.
5-4-8Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(2) On drain panel (Access Door 133AL and/or 192NB)- Drain Nipple 3/4 in (ISO 17775)
B. Usable capacity:- Standard configuration - one tank:200 l (52.83 US gal)
C. Filling pressure:- 3.45 bar (50 psi).
D. Typical flow rate:- 50 l/min (13.21 US gal/min).
5-4-8Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
DRAIN CONNECTION
DRAIN CONNECTIONDISCHARGE ANDOVERFLOW PORT
FILL ANDDRAIN PORT
GROUND CONNECTION
PRESSURIZATION
Z133
Z171
Z138
A
B
B
C
A
C
N_AC_050408_1_0020101_01_00
Ground Service ConnectionsPotable Water Ground Drain Panel
FIGURE-5-4-8-991-002-A01
5-4-8Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9 Oil System
**ON A/C A320-200
Oil System
1. Engine Oil Replenishment for CFM56 Series Engine (See FIGURE 5---9-99--001-A):One gravity filling cap and one pressure filling connection per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Engine Oil GravityFilling Cap:Access door: 437BL(LH),447BL (RH)
13.12(43.04)
6.63(21.75)
4.82(15.81)
1.46(4.79)
Engine Oil PressureFilling Port:
13(42.65)
6.49(21.29)
4.74(15.55)
1.42(4.66)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 19.6 l (5.18 US gal)- Usable: 9.46 l (2.50 US gal)
B. Maximum delivery pressure required: 25 psi (1.72 bar)Maximum delivery flow required: 180 l/h (47.55 US gal/h)
2. IDG Oil Replenishment for CFM56 Series Engine (See FIGURE 5---9-99--002-A):One pressure filling connection per engine: OMP 2506-18 plus one connection overflow: OMP2505-18.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
IDG Oil PressureFilling Connection:Access door 438DR(LH),448DR (RH)
12.2(40.03)
6.9(22.64)
5.52(18.11)
0.68(2.23)
NOTE : Distances are approximate
5-4-9Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
A. Tank capacity: 5 l (1.32 US gal)
B. Delivery pressure required: 5 to 40 psi (0.34 to 2.76 bar) at the IDG inlet.
3. Starter Oil Replenishment for CFM56 Series Engine (See FIGURE 5---9-99--003-A:One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Starter Oil FillingConnection:
12.7(41.67)
5.3(17.39)
6.2(20.34)
0.76(2.49)
NOTE : Distances are approximate
A. Tank capacity: 0.8 l (0.21 US gal)
4. Engine Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5---9-99--004-B):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Engine Oil GravityFilling Cap:Access door 437BL(LH),447BL (RH)
12.24(40.16)
6.56(21.52)
4.92(16.14)
1.22(4)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 28 l (7.4 US gal)- Usable: 23.50 l (6.21 US gal)
1. IDG Oil Replenishment for IAE V2500 Series Engine:One pressure filling connection per engine: OMP 2506-2 plus one overflow connection: OMP 2505-2.
5-4-9Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
IDG Oil PressureFilling Connection:
12.8(41.99)
5.42(17.78)
6.04(19.82)
0.8(2.62)
NOTE : Distances are approximate
A. Tank capacity: 4.1 l (1.08 US gal)
5. Starter Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5---9-99--006-B):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Starter Oil FillingConnection:
15.4(50.52)
5.3(17.39)
6.14(20.14)
0.75(2.46)
NOTE : Distances are approximate
A. Tank capacity: 0.35 l (0.09 US gal)
6. APU Oil System (See FIGURE 5---9-99--007-A):APU oil gravity filling cap.
AFT OF NOSEm (ft)
FROM AIRPLANECENTERLINE(LEFT HAND)
m (ft)
MEAN HEIGHT FROMGROUND
m (ft)
GTCP 36-30035.49(116.44)
0.3(0.98)
4.83(15.85)
APS 320035.49(116.44)
0.3(0.98)
4.78(15.68)
131-935.39(116.11)
0.35(1.15)
4.32(14.17)
NOTE : Distances are approximate
A. Tank capacity (usable):- APU type GTCP 36-300: 6.20 l (1.64 US gal)- APU type APS 3200: 5.40 l (1.43 US gal)
5-4-9Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- APU type 131-9: 6.25 l (1.65 US gal)
5-4-9Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ACCESS PANEL: 437BL (LEFT)447BL (RIGHT) OIL IN
VENT
OIL LEVELTRANSMITTER(OPTIONAL)
OIL CAP
SIGHT WINDOW
ANTI−SIPHONDEVICE
AIR PRESSURESWITCH NIPPLE
SELF−SEALING MAGNETICDRAIN PLUG
PRESSURE NIPPLE
OIL OUT
OIL/FUEL HEATEXCHANGER
SERVO FUELHEATER
A
A
B
FWD
B
N_AC_050409_1_0010101_01_00
Ground Service ConnectionsEngine Oil Tank -- CFM56 Series Engine
FIGURE-5-4-9-991-001-A01
5-4-9Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
C
A
B
SIGHT GLASS
NOTE: ATHE YELLOW BAND, OIL SERVICINGIS REQUIRED.
BTHE GREEN AND YELLOW BANDS,OIL SERVICING IS NOT REQUIRED.
CTHE GREEN BAND, OIL SERVICINGIS REQUIRED.
1 − PRESSURE FILL VALVE2 − CASE DRAIN PLUG3 − DUST CAP4 − DUST CAP5 − OVERFLOW DRAIN VALVE6 − OIL LEVEL INDICATOR
(SIGHT GLASS)
1
2
34
5
6
A B
A
B
OVERFULL
ADDOIL
ADDOIL
CFM−56
IF THE OIL LEVEL IS ABOVE
IF THE OIL LEVEL IS WITHIN
IF THE OIL LEVEL IS BELOW
N_AC_050409_1_0020101_01_01
Ground Service ConnectionsIDG Oil Tank -- CFM56 Series Engine
FIGURE-5-4-9-991-002-A01
5-4-9Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
DRAIN PORTAND MAGNETICPLUG
OVERFLOWPLUG
STARTER
OIL FILLERPLUG
A
A
N_AC_050409_1_0030101_01_02
Ground Service ConnectionsStarter Oil Tank -- CFM56 Series Engine
FIGURE-5-4-9-991-003-A01
5-4-9Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
’FULL’ LEVEL NOTCH27.3 LT29.0 US QTS6.0 IMP GAL(WITHIN 60 MIN FROM SHUTDOWN)
NOTCH ’3’20 LT22 US QTS4.5 IMP GAL
NOTCH ’1’26 LT27 US QTS5.7 IMP GALNOTCH ’2’
23 LT24 US QTS5.1 IMP GAL
FCOC
PRISMALITELEVEL INDICATOR
OIL TANK
GRAVITYFILLER CAP
ACCESS PANEL: 437BL (LEFT)447BL (RIGHT)
B
A
A
B
FWD
N_AC_050409_1_0040201_01_00
Ground Service ConnectionsEngine Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-9-991-004-B01
5-4-9Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
THE OIL LEVEL MUST NOT BE INTHE YELLOW BAND BUT IT CANBE IMMEDIATELY ABOVE THELOWER LIMIT OF THE YELLOWBAND BECAUSE OF THE AIRCRAFTRAMP ANGLE
DO THE IDG SERVICINGTO GET THE CORRECT IDGOIL LEVEL.
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
INCORRECTLY FILLED IDG
THE OIL LEVEL MUST NOT BEIN THE RED BAND
PERFORM IDG OIL SERVICINGTO GET THE CORRECT IDG OIL LEVEL.DO NOT USE THE OVERFLOW DRAIN HOSETO GET THE CORRECT IDG OIL LEVEL.
AT ALL TIMES(HOT OR COLD OIL/IDG)
OIL LEVEL CAN BEIN THE GREEN BAND OR THEYELLOW BAND
AFTER ENGINESHUTDOWN
CORRECTLY FILLED IDG
OIL LEVELINDICATOR
DUST CAPPRESSUREFILL HOSE
OIL LEVEL MUST BE AT OR NEARTHE LINE BETWEEN THE YELLOW BANDAND THE GREEN BAND
(HOT OIL/IDG)
PRESSUREFILL VALVE
DUST CAP
OVER FLOWDRAIN VALVE
OVER FLOWDRAIN HOSE
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
IDG
B
BB
A
B
A
B
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
N_AC_050409_1_0050201_01_00
Ground Service ConnectionsIDG Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-9-991-005-B01
5-4-9Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
OIL OVERFLOWPOINT
SIGHT GLASS
EXTERNAL GEARBOX
OIL FILLING POINT
ADAPTER
B
A
B
THE STARTER IS FULL WHEN THE OIL LEVELSHOWS NOT LESS THAN 3/4 FULL
ON THE SIGHT GLASS
*
PNEUMATIC STARTERA
*
N_AC_050409_1_0060201_01_00
Ground Service ConnectionsStarter Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-9-991-006-B01
5-4-9Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FR80
Z316Z315
FR84
GRAVITYOIL FILLER
PRESSUREFILL PORT
OVERFLOWDRAIN VALVE
A
A
OIL LEVELSIGHT GLASS
N_AC_050409_1_0070101_01_00
Ground Service ConnectionsAPU Oil Tank
FIGURE-5-4-9-991-007-A01
5-4-9Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10 Vacuum Toilet System
**ON A/C A320-200
Vacuum Toilet System
1. Vacuum Toilet System.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) R SIDEm (ft)
L SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Waste WaterGround ServicePanel:Access door 172AR
31.3(102.69)
0.8(2.62)
2.8(9.18)
NOTE : Distances are approximate
2. Technical Specifications
A. Connectors:- Draining: 4 in (ISO 17775).- Flushing and filling: 1 in (ISO 17775).
B. Usable waste tank capacity:- Standard configuration - on tank: 177 l (30.91 US gal).
C. Waste tank - Rinsing:- Operating pressure: 3.45 bar (50 psi).
D. Waste tank - Precharge:- 10 l (2.64 US gal).
5-4-10Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FILL AND RINSECONNECTION
TOILET DRAINCONNECTION
FR66 FR65
A
Z172
A
N_AC_050410_1_0010101_01_00
Ground Service ConnectionsWaste Water Ground Service Panel
FIGURE-5-4-10-991-001-A01
5-4-10Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A320-200
Engine Starting Pneumatic Requirements
1. Engine Starting Pneumatic Requirements.To determinate the airflow required at ground connection, refer to the example given in FIGURE 5---0-99--003-A.
For engine starting pneumatic requirements for:- Low ambient temperatures, refer to 5-5-1,- Medium ambient temperatures, refer to 5-5-2,- High ambient temperatures, refer to 5-5-3.
5-5-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
220°C200°C
150°C
100°C
50°C
0°C
230
3
4
40
50
60
5
6
70
80
90
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
MIN. PRESSUREAT GROUND CONNECTION: 33 PSIG
RECOMMENDED PRESSURE:38 PSIG AT GROUNDCONNECTION
SEA LEVEL
Z = 8000 ft
40s
50s70s
35s
Z = 8000 ft
SEA LEVEL
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
ESTIMATED STARTINGTIMES UP TO IDLE
0.80 1.00 2.001.801.601.401.20 kg/s
48 60 8472 kg/min12010896
SEA LEVEL
MAXIM
UM T
EMPERATURE L
IMIT
AIR FLOW REQUIRED AT GROUND CONNECTION
N_AC_050500_1_0030101_01_00
EXAMPLE TO DETERMINATE THE AIRFLOW REQUIRED AT THE FUSELAGE CONNECTION:−FOR AN AIR START UNIT DELIVERING 60 PSIA (4.14 BARS) AIR PRESSURE AT THE
FUSELAGE CONNECTOR
1. DRAW AN HORIZONTAL LINE FROM THE SUPPLIED AIR PRESSURE (60 PSIA (4.14 BARS)).2. FROM THE INTERSECTION WITH THE AIR SUPPLY TEMPERATURE AT FUSELAGE
CONNECTION (220°C (428°F)), DRAW A VERTICAL LINE.3. THE INTERSECTION WITH THE HORIZONTAL AXIS GIVES THE REQUIRED AIRFLOW AT GROUND
CONNECTION (78 kg/min (1.3 kg/s)).
−AT A SUPPLIED AIR TEMPERATURE OF 220°C (428°F) AT THE FUSELAGE CONNECTOR
Engine Starting Pneumatic RequirementsFIGURE-5-5-0-991-003-A01
5-5-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-1 Low Ambient Temperatures
**ON A/C A320-200
Low Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature of -40˚C(-40˚F).
5-5-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
220°C200°C
150°C
100°C
50°C
MAXIM
UM T
EMPERATURE L
IMIT
MAXIMUM DUCT PRESSURE: 60 PSIG
PSIA ABSOLUTE BARS
35S
Z = 8000 ft
SEA LEVEL38 PSIG AT GROUNDRECOMMENDED PRESSURE:
30
40
50
60
70
80
90
2
3
4
5
6
48 60 72 84 96 108 120
0°C
Z = 8000 ft
SEA LEVEL
Z = 8000 ft
SEA LEVEL
CONNECTION
MIN. PRESSUREAT GROUND CONNECTION: 33 PSIG
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
AIR FLOW REQUIRED AT GROUND CONNECTION
40s
50s
70s
ESTIMATED STARTINGTIMES UP TO IDLE
N_AC_050501_1_0050101_01_01
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- CFM56 series engine
FIGURE-5-5-1-991-005-A01
5-5-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
90
80
70
60
50
40
30 2
3
4
5
6
40 50 60 70 80 90 100 110 120
AIR SUPPLY PRESSUREAT GROUND CONNECTION
220°C
200°C
150°C
100°C
50°C
MAXIMUM T
EMPERATURE LIMIT
MAXIMUM DUCT PRESSURE
AIR FLOW REQUIRED AT GROUND CONNECTION
PSIA ABSOLUTE BARS
75s
70s
65s
60s
0°C
kg/mn
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
ESTIMATED STARTINGTIMES UP TO IDLE
N_AC_050501_1_0060101_01_00
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- IAE V2500 series engine
FIGURE-5-5-1-991-006-A01
5-5-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-2 Medium Ambient Temperatures
**ON A/C A320-200
Medium Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature of +15˚C(+59˚F).
5-5-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
kg/mn
220°C
200°C
150°C
100°C
50°C
35s
90
80
70
60
50
40
30
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
2
3
4
5
6
48 60 72 84 96 108 120
AT GROUND CONNECTION: 22 PSIGMIN. PRESSURE
Z = 8000 ft
SEA LEVEL
0°C
33 PSIG AT GROUND CONNECTIONRECOMMENDED PRESSURE:
Z = 8000 ft
SEA LEVELM
AXIMUM
TEM
PERATURE LIM
IT
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
AIR FLOW REQUIRED AT GROUND CONNECTION
TIMES UP TO IDLEESTIMATED STARTING
40s
50s
60s
70s
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
N_AC_050502_1_0050101_01_01
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- CFM56 series engine
FIGURE-5-5-2-991-005-A01
5-5-2Page 2
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
120 kg/mn
PSIA ABSOLUTE BARS
220°C200°C
150°C
100°C
50°C
0°C
60s
MAXIMUM T
EMPERATURE LIMIT
MAXIMUM DUCT PRESSURE
TIMES UP TO IDLEESTIMATED STARTING
90
6
80
705
604
50
40
3
30 2
55s
50s
45s
40 50 60 70 80 90 100 110
AIR FLOW REQUIRED AT GROUND CONNECTION
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
N_AC_050502_1_0060101_01_00
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- IAE V2500 series engine
FIGURE-5-5-2-991-006-A01
5-5-2Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-3 High Ambient Temperatures
**ON A/C A320-200
High Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature upper:- +50˚C (+122˚F) -- IAE V2500- +55˚C (+131˚F) -- CFM56
5-5-3Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30
40
50
60
70
80
906
5
4
3
2
48 60 72 84 96 108 120
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
220°C200°C
150°C
100°C
50°C
MAXIM
UM T
EMPERATURE L
IMIT
PSIA ABSOLUTE BARS
AT GROUND CONNECTION: 22 PSIGMIN. PRESSURE
33 PSIG AT GROUND CONNECTION
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
AIR FLOW REQUIRED AT GROUND CONNECTION
40s
50s
70s
Z = 8000 ft
SEA LEVEL
35s
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
Z = 8000 ft
TIMES UP TO IDLEESTIMATED STARTING
SEA LEVEL
Z = 8000 ft
N_AC_050503_1_0050101_01_00
RECOMMENDED PRESSURE:
60s
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +55˚C (+131˚F) -- CFM56 series engine
FIGURE-5-5-3-991-005-A01
5-5-3Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
120 kg/mn
PSIA ABSOLUTE BARS
220°C200°C
150°C
100°C
50°C
0°C
60s
MAXIMUM T
EMPERATURE LIMIT
MAXIMUM DUCT PRESSURE
TIMES UP TO IDLEESTIMATED STARTING
90
6
80
705
604
50
40
3
30 2
55s
50s
45s
40 50 60 70 80 90 100 110
AIR FLOW REQUIRED AT GROUND CONNECTION
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
N_AC_050503_1_0060101_01_00
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +50˚C (+122˚F) -- IAE V2500 series engine
FIGURE-5-5-3-991-006-A01
5-5-3Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A320-200
Ground Pneumatic Power Requirements
1. Ground Pneumatic Power Requirements
NOTE : The air flow rates and temperature requirements given in sections 5.6 and 5.7 are given ataircraft connection.
5-6-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-1 Heating
**ON A/C A320-200
Heating
1. This section provides the ground pneumatic power requirements heating.
5-6-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
1.29
8
1.21
1
1.12
5
1.03
8
0.95
2
0.86
5
0.77
9
0.69
2
0.51
9
0.60
6
0.43
3
1.5
1.2
1.0
0.5
3040
50
TIM
E T
O H
EA
T C
AB
IN T
O 2
1°C
(69
.8°
F)
ON
GR
OU
ND
TIM
E (
min
)
MA
X. A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
1.30
1.73
2.16
2.60
3.0
2.5
2.0
1.5
(lb/s
)
NO
RM
AL
AIR
FLO
W (
1 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T −
23°
C (
−9.
4°F
)T
EM
PE
RA
TU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N 7
0°C
(15
8°F
)E
MP
TY
CA
BIN
ELE
CT
RIC
AL
LOA
D =
310
0 W
RE
CIR
CU
LAT
ION
: ON
NO
OT
HE
R H
EA
T L
OA
D
CABIN AIRFLOW
N_AC_050601_1_0030101_01_01
Ground Pneumatic Power RequirementsHeating
FIGURE-5-6-1-991-003-A01
5-6-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-2 Cooling
**ON A/C A320-200
Cooling
1. This section provides the ground pneumatic power requirements cooling.
5-6-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
1.29
8
1.21
1
1.12
5
1.03
8
0.95
2
0.86
5
0.77
9
0.69
2
0.51
9
0.60
6
0.43
3
1.5
1.2
1.0
0.5
3040
50T
IME
(m
in)
1.30
1.73
2.16
2.60
3.0
2.5
2.0
1.5
(lb/s
)
NO
RM
AL
AIR
FLO
W (
1 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
CABIN AIRFLOW
MA
X. A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T −
23°
C (
−9.
4°F
)T
EM
PE
RA
TU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N 7
0°C
(15
8°F
)E
MP
TY
CA
BIN
ELE
CT
RIC
AL
LOA
D =
310
0 W
RE
CIR
CU
LAT
ION
: ON
NO
OT
HE
R H
EA
T L
OA
D
TIM
E T
O H
EA
T C
AB
IN T
O 2
1°C
(69
.8°
F)
ON
GR
OU
ND
N_AC_050602_1_0030101_01_01
Ground Pneumatic Power RequirementsCooling
FIGURE-5-6-2-991-003-A01
5-6-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A320-200
Preconditioned Airflow Requirements
1. This section gives the preconditioned airflow requirements for cabin air conditioning.
A. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 1TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.433 0.955 -42.7 -44.90.6 1.32 0.519 1.144 -31.1 -24.00.7 1.54 0.606 1.336 -22.7 -8.90.8 1.76 0.692 1.526 -16.5 2.30.9 1.98 0.779 1.717 -11.6 11.11.0 2.20 0.865 1.907 -7.7 18.11.1 2.43 0.952 2.099 -4.5 23.91.2 2.65 1.038 2.288 -1.9 28.61.3 2.87 1.125 2.480 0.4 32.71.4 3.09 1.211 2.670 2.3 36.11.5 3.31 1.298 2.862 4.0 39.2
NOTE : Data for stabilized conditions see 5-7-0.
B. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 2TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.433 0.955 27.8 82.00.6 1.32 0.519 1.144 26.6 79.90.7 1.54 0.606 1.336 25.7 78.30.8 1.76 0.692 1.526 25.1 77.20.9 1.98 0.779 1.717 24.6 76.31.0 2.20 0.865 1.907 24.2 75.61.1 2.43 0.952 2.099 23.8 74.81.2 2.65 1.038 2.288 23.5 74.31.3 2.87 1.125 2.480 23.3 73.91.4 3.09 1.211 2.670 23.1 73.6
5-7-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
FRESH AIRFLOW CURVE 2TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
1.5 3.31 1.298 2.862 22.9 73.2
NOTE : Data for stabilized conditions see 5-7-0.
C. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 3TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.433 0.955 32.2 90.00.6 1.32 0.519 1.144 30.2 86.40.7 1.54 0.606 1.336 28.8 83.80.8 1.76 0.692 1.526 27.8 82.00.9 1.98 0.779 1.717 26.9 80.41.0 2.20 0.865 1.907 26.3 79.31.1 2.43 0.952 2.099 25.7 78.31.2 2.65 1.038 2.288 25.3 77.51.3 2.87 1.125 2.480 24.9 76.81.4 3.09 1.211 2.670 24.6 76.31.5 3.31 1.298 2.862 24.3 75.7
NOTE : Data for stabilized conditions see 5-7-0.
D. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 4TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.433 0.955 38.9 102.00.6 1.32 0.519 1.144 35.8 96.40.7 1.54 0.606 1.336 33.6 92.50.8 1.76 0.692 1.526 31.9 89.40.9 1.98 0.779 1.717 30.6 87.11.0 2.20 0.865 1.907 29.6 85.31.1 2.43 0.952 2.099 28.7 83.71.2 2.65 1.038 2.288 28.0 82.41.3 2.87 1.125 2.480 27.4 81.31.4 3.09 1.211 2.670 26.9 80.4
5-7-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
FRESH AIRFLOW CURVE 4TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
1.5 3.31 1.298 2.862 26.4 79.5
NOTE : Data for stabilized conditions see 5-7-0.
5-7-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TOTAL AIRFLOW(kg/
s)TOTAL AIRFLOW
CABIN AIRFLOW
1.29
8
1.21
1
1.12
5
1.03
8
0.95
2
0.86
5
0.77
9
0.69
2
0.51
9
0.60
61.
30
1.73
2.16
2.60
3.0
2.5
2.0
1.5
(lb/s
)
0.5
1.0
1.2
1.5
0.43
3
OA
T =
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E
−40
−30
−20
−10
010
2030
40
−40
−10
010
5010
0
OA
T =
−23
°C
(−
9.4°
F)
OA
T =
−30
°C
(−
22°
F)
OA
T =
−40
°C
(−
40°
F)
(°C
)IN
LET
FLO
WT
EM
PE
RA
TU
RE
(°F
)
NO
TE
:LP
GR
OU
ND
CO
NN
EC
TIO
N M
AX
IMU
M P
RE
SS
UR
E 4
0 m
b
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
CABIN AIRFLOW
CU
RV
E 1
: CA
BIN
AT
27°
C (
80.6
°F
)16
4 P
AS
SE
NG
ER
S, 4
CA
BIN
AT
TE
ND
AN
TS
, 3 C
RE
W M
EM
BE
RS
BR
IGH
T D
AY
SO
LAR
LO
AD
: 385
0 W
ELE
CT
RIC
AL
LOA
D =
670
0 W
RE
CIR
CU
LAT
ION
: ON
OA
T (
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E)
= 3
8°C
(10
0.4°
F)
CU
RV
E 2
, 3, 4
CA
BIN
AT
21°
C (
69.8
°F
)
NO
OT
HE
R H
EA
T L
OA
D
ELE
CT
RIC
AL
LOA
D =
450
0 W
RE
CIR
CU
LAT
ION
: ON
NO
PA
SS
EN
GE
R O
R C
AB
INA
TT
EN
DA
NT
S
(1 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)N
OR
MA
L A
IRF
LOW
N_AC_050700_1_0030101_01_01
Preconditioned Airflow RequirementsFIGURE-5-7-0-991-003-A01
5-7-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A320-200
Ground Towing Requirements
1. GeneralThis section provides information on aircraft towing.This aircraft is designed with means for conventional or towbarless towing.Information/procedures can be found for both in chapter 9 of the Aircraft Maintenance Manual.Status on towbarless towing equipment qualification can be found in SIL 09-002.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a tow bar attached to the nose gear leg (refer to AMM chap 9 for conditions andlimitations).One tow bar fitting is installed at the front of the leg.The main landing gears have attachment points for towing or debogging (for details, refer to chapter07 of the Aircraft Recovery Manual).
A. The first part of this section shows the chart to determine the draw bar pull and tow tractormass requirements as function of the following physical characteristics:- Aircraft weight.- Number of engines at idle.- Slope.The chart is based on the engine type with the highest idle thrust level.
B. The second part of this section supplies guidelines for the tow bar.
NOTE : Information on aircraft towing procedures and corresponding aircraft limitations aregiven in chapter 9 on the Aircraft Maintenance Manual.
The aircraft tow bar shall respect the following norms:- SAE AS1614 C, ”Main Line Aircraft Tow Bar Attach Fitting Interface”.- SAE ARP1915 D, ”Aircraft Tow Bar”.- ISO 8267-1, ”Aircraft - Tow bar attachment fitting - Interface requirements - Part 1: Main
line aircraft”.- ISO 9667, ”Aircraft ground support equipment - Tow bars”.- IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Tow
bar”.A conventional type tow bar is required which should be equipped with a damping system toprotect the nose gear against jerks and with towing shear pins:- A traction shear pin calibrated at 9425 daN (21188 lbf).- A torsion pin calibrated at 826 m.daN (7311 lbf.in).The towing head is designed according to SAE AS1614 C (Aircraft Weight Category I).
5-8-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A320 AT 70 t, AT 1.5% SLOPE,1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (70 t)− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%)− FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL NO OF ENGINES AT IDLE = 2− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER OF ENGINES (1)− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5.8 t)− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS
THE RECOMMENDED MINIMUM TRACTOR WEIGHT (10.1 t)
DRAWBAR PULL [ t ] A/C WEIGHT [ t ]
10
0 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0
5
0
TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]
75
455055606570
HA
RD
SN
OW
m =
0.2
ICE m = 0.05
10.15
1 ENGINE ON5.8
1.5% SLOPE70 tons
DR
Y C
ON
CR
ET
E m
= 0
.8
AT IDLE
WE
T C
ON
CR
ET
E m
= 0
.57
BREAKAWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 525 daN
N_AC_050800_1_0010301_01_03
Ground Towing RequirementsFIGURE-5-8-0-991-001-C01
5-8-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0 De-Icing and External Cleaning
**ON A/C A320-200
De-Icing and External Cleaning
1. De-Icing and External Cleaning on GroundThe mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heightsup to approximately 13 m (42.65 ft).
2. De-Icing
Wing Top Surface(Both Sides)
Wingtip Devices(Both Inside andOutside Surfaces)
(Both Sides)
HTP Top Surface(Both Sides)
VTP(Both Sides)AIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A320 99.7 1073.16 1.8 19.38 27 290.63 43 462.85A320 Sharklet 99.7 1073.16 9.6 103.33 27 290.63 43 462.85
Fuselage Top Surface(Top Third - 120˚ Arc)
Nacelle and Pylon(Top Third - 120˚ Arc)
(All Engines)Total De-Iced Area
AIRCRAFT TYPE
m2 ft2 m2 ft2 m2 ft2
A320 137.9 1484.34 23.6 254.03 333 3584A320 Sharklet 137.9 1484.34 23.6 254.03 341 3670
NOTE : Dimensions are approximate
3. External Cleaning
Wing TopSurface
(Both Sides)
Wing LowerSurface
(Including FlapTrack Fairing)(Both Sides)
Wingtip Devices(Both Inside and
OutsideSurfaces)
(Both Sides)
HTP TopSurface
(Both Sides)
HTP LowerSurface
(Both Sides)AIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2 m2 ft2
A320 99.7 1073.16 103.4 1112.99 1.8 19.38 27 290.63 27 290.63A320 Sharklet 99.7 1073.16 103.4 1112.99 9.6 103.33 27 290.63 27 290.63
VTP(Both Sides)
Fuselage andBelly Fairing
Nacelle and Pylon(All Engines) Total Cleaned Area
AIRCRAFT TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A320 43 462.85 421.2 4533.76 73.2 787.92 796 8568
5-9-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
VTP(Both Sides)
Fuselage andBelly Fairing
Nacelle and Pylon(All Engines) Total Cleaned Area
AIRCRAFT TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A320 Sharklet 43 462.85 421.2 4533.76 73.2 787.92 804 8654
NOTE : Dimensions are approximate
5-9-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A320-200
Engine Exhaust Velocities and Temperatures
1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway, Maximum Takeoff conditions.
6-1-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A320-200
Engine Exhaust Velocities Contours - Ground Idle Power
1. This section gives engine exhaust velocities contours at ground idle power.
6-1-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ELE
VA
TIO
N
FE
ET
PLA
NA
IRP
LAN
E
V (
m/s
)
GR
OU
ND
PLA
NE
ME
TE
RS
4530
2520
1510
4530
2520
1510
40 30 20 10 0036912
mft
40 30 20 10 0036912
mft
N_AC_060101_1_0050101_01_00
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
Engine Exhaust VelocitiesGround Idle Power -- CFM56 series engine
FIGURE-6-1-1-991-005-A01
6-1-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
VE
LOC
ITY
= ft
/s (
m/s
)
FE
ET
050
100
150
200
7590
PLA
N
100
(30)
50 (15)
30 (9)
100
(30)
50 (15)
30 (9)
ftm
15 10 5 0
60 40 20 0
ftm
60
15 10 5 0
40 20 0
N_AC_060101_1_0060101_01_00
Engine Exhaust VelocitiesGround Idle Power -- IAE V2500 series engine
FIGURE-6-1-1-991-006-A01
6-1-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A320-200
Engine Exhaust Temperatures Contours - Ground Idle Power
1. This section gives engine exhaust temperatures contours at ground idle power.
6-1-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ELE
VA
TIO
N
FE
ET
PLA
NA
IRP
LAN
E
T (
°K
)
GR
OU
ND
PLA
NE
ME
TE
RS
400
350
300
325
40 30 20 10 0036912
mft
40 30 20 10 0036912
mft
40035
030
032
5
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
N_AC_060102_1_0050101_01_00
Engine Exhaust TemperaturesGround Idle Power -- CFM56 series engine
FIGURE-6-1-2-991-005-A01
6-1-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
TE
MP
ER
AT
UR
E =
°K
FE
ET
050
100
150
200
7590
PLA
N
32531
8 308
300
325
318
308
300
ftm
15 10 5 0
60 40 20 0
ftm
60
15 10 5 0
40 20 0
N_AC_060102_1_0060101_01_00
Engine Exhaust TemperaturesGround Idle Power -- IAE V2500 series engine
FIGURE-6-1-2-991-006-A01
6-1-2Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A320-200
Engine Exhaust Velocities Contours - Breakaway Power
1. This section gives engine exhaust velocities contours at breakaway power.
6-1-3Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
(38%
N1)
NO
TE
:−
add
+ 1
% N
1 pe
r +
15°
C (
27°
F)
AB
OV
E IS
A T
EM
PE
RA
TU
RE
CO
ND
ITIO
NS
− a
dd +
1%
N1
per
2000
ft
3000
lbs
OF
TH
RU
ST
V (
m/s
)
4020
15
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
PLA
NA
IRP
LAN
E
GR
OU
ND
PLA
NE
ME
TE
RS
4020
15
40 30 20 10 0036912
mft
40 30 20 10 0036912
mft
N_AC_060103_1_0030101_01_00
Engine Exhaust VelocitiesBreakaway Power -- CFM56 series engine
FIGURE-6-1-3-991-003-A01
6-1-3Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
VE
LOC
ITY
= ft
/s (
m/s
)
FE
ET
050
100
150
200
7590
PLA
N
100
(30)
50 (15)
30 (9)
100
(30)
50 (15)
30 (9)1.
05
1.04
1.03
050
0010
000
FN
= 3
000
lbf
ISA
/ O
MN
"V25
27A
5MD
V"
BA
SIS
RU
NW
AY
ALT
(ft)
FP
R
A32
0
ftm
15 10 5 0
60 40 20 0
ftm
60
15 10 5 0
40 20 0
N_AC_060103_1_0040101_01_00
Engine Exhaust VelocitiesBreakaway Power -- IAE V2500 series engine
FIGURE-6-1-3-991-004-A01
6-1-3Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A320-200
Engine Exhaust Temperatures Contours - Breakaway Power
1. This section gives engine exhaust temperatures contours at breakaway power.
6-1-4Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
PLA
NA
IRP
LAN
E
GR
OU
ND
PLA
NE
ME
TE
RS
400
350
300
325
400
350
300
325
3000
lbs
OF
TH
RU
ST
T (
°K
)
40 30 20 10 0036912
mft
40 30 20 10 0036912
mft
N_AC_060104_1_0030101_01_00
Engine Exhaust TemperaturesBreakaway Power -- CFM56 series engine
FIGURE-6-1-4-991-003-A01
6-1-4Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
TE
MP
ER
AT
UR
E =
°K
FE
ET
050
100
150
200
7590
PLA
N
325
318
308
300
325
318
308
300
ftm
60
15 10 5 0
40 20 0
ftm
60
15 10 5 0
40 20 0
N_AC_060104_1_0040101_01_00
Engine Exhaust TemperaturesBreakaway Power -- IAE V2500 series engine
FIGURE-6-1-4-991-004-A01
6-1-4Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A320-200
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power.
6-1-5Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
420
390
360
330
300
270
240
210
180
150
120
9060
3000
100
200
300
400
500
700
600
800
900
1000
1100
1200
1300
1400
ME
TE
RS
FE
ET
ftm
ftV
= 4
0 m
/sV
= 2
0 m
/sV
= 1
2 m
/s
V =
40
m/s
V =
20
m/s
V =
12
m/s
PLA
NA
IRP
LAN
E
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
TA
KE
OF
F P
OW
ER
INC
LUD
ES
(W
OR
ST
CA
SE
)G
RO
UN
D P
LAN
EH
EA
DW
IND
(20
KT
S.)
m
450
1500
42 36 30 24 18 12 6 0
140
120
100 80 60 40 200
42 36 30 24 18 12 6 0
140
120
100 80 60 40 200
N_AC_060105_1_0050101_01_00
Engine Exhaust VelocitiesTakeoff Power -- CFM56 series engine
FIGURE-6-1-5-991-005-A01
6-1-5Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
VE
LOC
ITY
= ft
/s (
m/s
)
FE
ET
050
100
150
200
7590
PLA
N
200
(60)
150
(45)
100
(30)
50 (15)
30 (9)
200
(60)
150
(45)
100
(30)
50 (15)
30 (9)
ftm
60
15 10 5 0
40 20 0
ftm
60
15 10 5 0
40 20 0
N_AC_060105_1_0060101_01_01
Engine Exhaust VelocitiesTakeoff Power -- IAE V2500 series engine
FIGURE-6-1-5-991-006-A01
6-1-5Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A320-200
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power.
6-1-6Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 40 20 0
ftm
18 12 6 0E
LEV
AT
ION
GR
OU
ND
PLA
NE
2040
6080
100
120
140
160
TA
KE
OF
F P
OW
ER
INC
LUD
ES
(W
OR
ST
CA
SE
):G
RO
UN
D P
LAN
EH
EA
DW
IND
(20
KT
S.)
FE
ET
ME
TE
RS
0
PLA
N
T =
425
°K
T =
370
°K
T =
315
°K
T =
425
°K
T =
370
°K
T =
315
°K
AIR
PLA
NE
1020
3040
500
60 40 20 0
ftm
18 12 6 0
N_AC_060106_1_0050101_01_00
Engine Exhaust TemperaturesTakeoff Power -- CFM56 series engine
FIGURE-6-1-6-991-005-A01
6-1-6Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
FE
ET
050
100
150
200
7590
PLA
N
400
350
325
318
400
350
325
318
300
300
ftm
15 10 5 0
60 40 20 0
ftm
15 10 5 0
60 40 20 0
N_AC_060106_1_0060101_01_00
Engine Exhaust TemperaturesTakeoff Power -- IAE V2500 series engine
FIGURE-6-1-6-991-006-A01
6-1-6Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-0 Airport and Community Noise
**ON A/C A320-200
Airport and Community Noise
1. Airport and Community Noise Data
This section gives data concerning engine maintenance run-up noise to permit evaluation of possibleattenuation requirements.
6-2-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-1 Noise Data
**ON A/C A320-200
Noise Data
1. Noise Data for CFM56-5A series engine
A. Description of test conditions:
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 3˚C (37˚F)- Relative humidity: 66%- Atmospheric pressure: 1016 hPa- Wind speed: Negligible- No rain
2. Noise Data for CFM56-5B series engine
A. Description of test conditions:
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 22˚C (72˚F)- Relative humidity: 42%- Atmospheric pressure: 1003 hPa- Wind speed: Negligible- No rain
3. Noise Data for IAE V2500 series engine
A. Description of test conditions:
6-2-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 12˚C (54˚F)- Relative humidity: 62.5%- Atmospheric pressure: 1000 hPa- Wind speed: Negligible- No rain
6-2-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOISE REFERENCEPOINT
112110108106104102100989694929088868482
150°
140°
130°
120°
110°
100°
90°
80°
70°
60°
50°
40°
30°
20°10°
0°350°
340°
330°
320°
310°
300°
290°
280°
270°
260°
250°
240°
230°
220°
210°
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
20.8% 90%
8078
N_AC_060201_1_0070101_01_00
Airport and Community NoiseCFM56-5A series engine
FIGURE-6-2-1-991-007-A01
6-2-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOISE REFERENCEPOINT
112110108106104102100989694929088868482
150°
140°
130°
120°
110°
100°
90°
80°
70°
60°
50°
40°
30°20°
10°0°
350°340°
330°
320°
310°
300°
290°
280°
270°
260°
250°
240°
230°
220°
210°
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
18.9% 87%
7880
N_AC_060201_1_0080101_01_00
Airport and Community NoiseCFM56-5B series engine
FIGURE-6-2-1-991-008-A01
6-2-1Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOISE REFERENCEPOINT
1121101081061041021009896949290888684
150°
140°
130°
120°
110°
100°
90°
80°
70°
60°
50°
40°
30°20°
10°0°
350°340°
330°
320°
310°
300°
290°
280°
270°
260°
250°
240°
230°
220°
210°
GROUND IDLE
N2
CURVE
MAX THRUST POSSIBLEON BRAKES
57.7% 92.5%
E.P.R 1.007 1.397
255°
225°
285°
315°
345°15°
45°
105°
135°
75°
78
8280
N_AC_060201_1_0090101_01_00
Airport and Community NoiseIAE V2500 series engine
FIGURE-6-2-1-991-009-A01
6-2-1Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A320-200
Danger Areas of Engines
1. Danger Areas of the Engines.
6-3-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1 Ground Idle Power
**ON A/C A320-200
Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions.
6-3-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30°TO 55 m (180 ft) INCLUDES CROSS WIND EFFECT
EXHAUST WAKE DANGER AREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGER AREA 65 MPH (105 km/h)OR LESS
NO
EN
TR
Y 1
7 m
(55
ft) A
FT
OF
NO
ZZ
LE
(20 ft)
6.1 m
45°
1.5 m(5 ft)
(7.2 ft)R = 2.2 m
INTAKE SUCTION DANGER AREA
ENTRY CORRIDOR
N_AC_060301_1_0050101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE-6-3-1-991-005-A01
6-3-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0.75 m(2.5 ft)
R = 5.15 m(17 ft)
TO 59 m (195 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)30°
INTAKE SUCTION DANGER AREAMINIMUM POWER
ENTRY CORRIDOR
EXHAUST DANGER AREA
N_AC_060301_1_0060101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE-6-3-1-991-006-A01
6-3-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2 Takeoff Power
**ON A/C A320-200
Takeoff Power
1. This section gives danger areas of the engines at max takeoff conditions.
6-3-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
40°
30°
1.8 m(6 ft)
TO
275
m (
900
ft) A
FT
OF
FA
N N
OZ
ZLE
TO 150 m (500 ft) AFTOF FAN NOZZLE
R = 5.9 m(19.5 ft)
INLET SUCTION DANGER AREA
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
N_AC_060302_1_0050101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE-6-3-2-991-005-A01
6-3-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1.5 m(5.5 ft)
R = 5.15 m(17 ft)
TO 348 m (1150 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST DANGER AREA
30°
N_AC_060302_1_0060101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE-6-3-2-991-006-A01
6-3-2Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A320-200
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1 APU
**ON A/C A320-200
APU - APIC & GARRETT
1. This section gives APU exhaust velocities and temperatures.
6-4-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0 PLAN 5 10 15 2520
0 16.404 32.808 49.212 65.616 82.02
0
0
FEET
0
5
ELEVATION
10
0
16.404
32.808
80°C176°F
100°C212°F
120°C248°F
150°C302°F
200°C392°F
300°C572°F
METERS
HEIGHT
m ft
FEET
METERS
45 m/s147 ft/s
30 m/s98 ft/s
20 m/s65 ft/s
10 m/s32 ft/s
5 m/s16 ft/s
5 10 15 20
16.404 32.808 49.212 65.616
N_AC_060401_1_0030101_01_00
Exhaust Velocities and TemperaturesAPU -- APIC & GARRETTFIGURE-6-4-1-991-003-A01
6-4-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A320-200
General Information
1. General Information
This brief description of the pavement charts that follow will help in their use for airport planning.
To aid in the interpolation between the discrete values shown, each airplane configuration is shownwith a minimum range of five loads on the main landing gear.
All curves on the charts represent data at a constant specified tire pressure with:- The airplane loaded to the maximum ramp weight.- The Center of Gravity (CG) at its maximum permissible aft position.
Pavement requirements for commercial airplanes are derived from the static analysis of loads imposedon the main landing gear struts.
The A/C codes are used for configuration management of chapter 07 only. There is no relationbetween these A/C codes and the ICAO A/C codes used for determining the airplane wing span andouter main gear wheel span as described in ICAO-Annex 14 Volume 1, Aerodrome Design andOperation Chapter 1.4, Table 1-1.
Section 7-2-0 presents basic data on the landing gear footprint configuration, maximum ramp weightsand tire sizes and pressures.
Section 7-3-0 shows maximum vertical and horizontal pavement loads for certain critical conditions atthe tire-ground interfaces.
Section 7-4-1 contain charts to find these loads throughout the stability limits of the airplane at reston the pavement.
These main landing gear loads are used as the point of entry to the pavement design charts whichfollow, interpolating load values where necessary.
Section 7-5-1 uses procedures in Instruction Report No S-77-1 ”Procedures for Development of CBRDesign Curves”, dated June 1977 and as modified according to the methods described in ICAOAerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCNMethod), and utilizing the alpha factors approved by ICAO in October 2007.
7-1-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The report was prepared by the U.S. Army Corps Engineers Waterways Experiment Station, Soils andPavement Laboratory, Vicksburg, Mississippi.
The line showing 10 000 coverages is used to calculate Aircraft Classification Number (ACN).
The procedure that follows is used to develop flexible pavement design curves such as shown inSection 7-5-1.- With the scale for pavement thickness at the bottom and the scale for CBR at the top, an
arbitrary line is drawn representing 10 000 coverages.- Incremental values of the weight on the main landing gear are then plotted.- Annual departure lines are drawn based on the load lines of the weight on the main landing gear
that is shown on the graph.
Section 7-7-1 gives the rigid pavement design curves that have been prepared with the use of theWestergaard Equation. This is in general accordance with the procedures outlined in the PortlandCement Association publications, ”Design of Concrete Airport Pavement”, 1973 and ”ComputerProgram for Airport Pavement Design”, (Program PDILB), 1967 both by Robert G. Packard.
The procedure that follows is used to develop rigid pavement design curves such as shown in Section7-7-1.- With the scale for pavement thickness to the left and the scale for allowable working stress to the
right, an arbitrary load line is drawn. This represents the main landing gear maximum weight tobe shown.
- All values of the subgrade modulus (k values) are then plotted.- Additional load lines for the incremental values of weight on the main landing gear are drawn on
the basis of the curve for k = 300 already shown on the graph.
All Load Classification Number (LCN) curves shown in Section 7-6-1 and Section 7-8-2 have beendeveloped from a computer program based on data provided in International Civil AviationOrganisation (ICAO) document 7920-AN/865/2, Aerodrome Manual, Part 2, ”Aerodrome PhysicalCharacteristics”, Second Edition, 1965.
The flexible pavement charts in Section 7-6-1 show LCN against equivalent single wheel load, andequivalent single wheel load against pavement thickness.
The rigid pavement charts in Section 7-8-2 show LCN against equivalent single wheel load andequivalent single wheel load against radius of relative stiffness.
Section 7-9-0 gives ACN data prepared according to the ACN/PCN system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 Fourth Edition July 2004, incorporating Amendments 1 to 6.
7-1-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The ACN/PCN system gives a standardized international airplane/pavement rating system replacingthe various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world.
The ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.
An aircraft having an ACN equal to or less than the PCN can operate without restriction on thepavement.
Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.The derived single wheel is defined as the load on a single tire inflated to 1.25 Mpa (181 psi) thatwould have the same pavement requirements as the aircraft.
Computationally the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1 forflexible pavements to calculate ACN values.The Airport Authority must decide on the method of pavement analysis and the results of theirevaluation shown as follows:
PCNPAVEMENT
TYPESUBGRADECATEGORY
TIRE PRESSURE CATEGORY EVALUATION METHOD
R -- Rigid A -- High W -- No Limit T -- Technical
F -- Flexible B -- Medium X -- To 1.5 Mpa (217 psi) U -- Using Aircraft
C -- Low Y -- To 1.0 Mpa (145 psi)
D -- Ultra Low Z -- To 0.5 Mpa (73 psi)
Section 7-9-1 shows the aircraft ACN values for flexible pavements.
The four subgrade categories are:- A. High Strength CBR 15- B. Medium Strength CBR 10- C. Low Strength CBR 6- D. Ultra Low Strength CBR 3
Section 7-9-2 shows the aircraft ACN for rigid pavements.
The four subgrade categories are:- A. High Strength Subgrade k = 150 MN/m3 (550 pci)- B. Medium Strength Subgrade k = 80 MN/m3 (300 pci)- C. Low Strength Subgrade k = 40 MN/m3 (150 pci)- D. Ultra Low Strength Subgrade k = 20 MN/m3 (75 pci)
7-1-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
MODEL WVAIRCRAFT
CODE
A320−2XX
06 E
A320−2XX
05 F
A320−2XX
01 G
A320−2XX
02 H
A320−2XX
13 04 I
A320−2XX
08 00 14 J
A320−2XX
16 K
A320−2XX
03 09 L
A320−2XX
11 M
A320−2XX
10 07 N
A320−2XX
12 O
A320−2XX
15 P
A320−2XXBogie L/G
00 TT
NOTE: FOR WEIGHT VARIANT DEFINITION, REFER TO CHAPTER 02−01−01.
NOTE: THE A/C CODES ARE USED FOR CONFIGURATION MANAGEMENT OFCHAPTER 07 ONLY.THERE IS NO RELATION BETWEEN THESE A/C CODES AND THE ICAO A/C CODES USED FOR DETERMINING THE AIRPLANE WING SPAN ANDOUTER MAIN GEAR WHEEL SPAN AS DESCRIBED IN ICAO−ANNEX 14 VOLUME 1, AERODROME DESIGN AND OPERATION CHAPTER 1.4, TABLE 1−1.
N_AC_070100_1_0030101_01_01
A320−2XXA320−2XX
17 Q18 R
Aircraft CodesFIGURE-7-1-0-991-003-A01
7-1-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A320-200
Landing Gear Footprint
1. This section gives Landing Gear Footprint.
NOTE : For AC Code definition, refer to chapter 07-01-00.
7-2-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
9.2 bar (133 psi)10.2 bar (148 psi)
49 x 19 − 2049 x 17 − 2046 x 17 R20
(46 x 16 − 20)
12.3 bar (178 psi)
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
A/C CODE
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
(30 x 8.8 − 15)
30 x 8.8 R15
11 bar (160 psi)
E
SEE SECTION 7−4−1
N_AC_070200_1_0100101_01_01
Landing Gear FootprintFIGURE-7-2-0-991-010-A01
7-2-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
30 x 8.8 R15
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
11.4 bar (165 psi)
46 x 17 R20 49 x 19 − 2049 x 17 − 20
10.9 bar (158 psi)9.6 bar (139 psi)10.6 bar (154 psi)12.8 bar (186 psi)
A/C CODE F
SEE SECTION 7−4−1
1 270 x 455 R22
(49 x 18 − 22)
N_AC_070200_1_0270101_01_00
Landing Gear FootprintFIGURE-7-2-0-991-027-A01
7-2-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
(30 x 8.8 − 15)
30 x 8.8 R15
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
11.4 bar (165 psi)
(46 x 16 − 20)
46 x 17 R2049 x 17 − 20 49 x 19 − 20
(49 x 18 − 22)
1 270 x 455 R22
9.6 bar (139 psi)10.6 bar (154 psi)10.9 bar (158 psi)12.8 bar (186 psi)
A/C CODE G
SEE SECTION 7−4−1
N_AC_070200_1_0110101_01_01
Landing Gear FootprintFIGURE-7-2-0-991-011-A01
7-2-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
(30 x 8.8 − 15)
30 x 8.8 R15
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
11.4 bar (165 psi)
(46 x 16 − 20)
46 x 17 R2049 x 17 − 20 49 x 19 − 20
(49 x 18 − 22)
1 270 x 455 R22
9.6 bar (139 psi)10.6 bar (154 psi)10.9 bar (158 psi)12.8 bar (186 psi)
A/C CODE H
SEE SECTION 7−4−1
N_AC_070200_1_0120101_01_01
Landing Gear FootprintFIGURE-7-2-0-991-012-A01
7-2-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_070200_1_0130101_01_02
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
(30 x 8.8 − 15)
30 x 8.8 R15NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
12.3 bar (178 psi)
(46 x 16 − 20)
46 x 17 R2049 x 17 − 20 49 x 19 − 20
(49 x 18 − 22)
1 270 x 455 R22
10.3 bar (149 psi)11.4 bar (165 psi)11.8 bar (171 psi)13.8 bar (200 psi)
A/C CODE I − R
SEE SECTION 7−4−1PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
Landing Gear FootprintFIGURE-7-2-0-991-013-A01
7-2-0Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
(30 x 8.8 − 15)
30 x 8.8 R15
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
12.3 bar (178 psi)
(46 x 16 − 20)
46 x 17 R2049 x 17 − 20 49 x 19 − 20
(49 x 18 − 22)
1 270 x 455 R22
10.3 bar (149 psi)11.4 bar (165 psi)11.8 bar (171 psi)13.8 bar (200 psi)
A/C CODE J − K
SEE SECTION 7−4−1
N_AC_070200_1_0140101_01_01
Landing Gear FootprintFIGURE-7-2-0-991-014-A01
7-2-0Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
(30 x 8.8 − 15)
30 x 8.8 R15
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
12.3 bar (178 psi)
(46 x 16 − 20)
46 x 17 R2049 x 17 − 20 49 x 19 − 20
(49 x 18 − 22)
1 270 x 455 R22
10.3 bar (149 psi)11.4 bar (165 psi)11.8 bar (171 psi)13.8 bar (200 psi)
A/C CODE L − M
SEE SECTION 7−4−1
N_AC_070200_1_0150101_01_01
Landing Gear FootprintFIGURE-7-2-0-991-015-A01
7-2-0Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
(30 x 8.8 − 15)
30 x 8.8 R15
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
12.3 bar (178 psi)
(46 x 16 − 20)
46 x 17 R2049 x 17 − 20 49 x 19 − 20
(49 x 18 − 22)
1 270 x 455 R22
10.7 bar (155 psi)12 bar (174 psi)12.3 bar (178 psi)14.4 bar (209 psi)
A/C CODE N − O
SEE SECTION 7−4−1
N_AC_070200_1_0160101_01_01
Landing Gear FootprintFIGURE-7-2-0-991-016-A01
7-2-0Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_070200_1_0170101_01_02
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
(30 x 8.8 − 15)
30 x 8.8 R15
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
12.3 bar (178 psi)
(46 x 16 − 20)
46 x 17 R20
(49 x 18 − 22)
1 270 x 455 R22
12.3 bar (178 psi)14.4 bar (209 psi)
A/C CODE P − Q
SEE SECTION 7−4−1
Landing Gear FootprintFIGURE-7-2-0-991-017-A01
7-2-0Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
(30 x 8.8 − 15)
30 x 8.8 R15
12.3 bar (178 psi)
12.2 bar (177 psi)
(36 x 11 − 16)
915 x 300 R16
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
927 mm(36.5 in)
500 mm(19.7 in)
12 640 mm(41 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
1005 mm(39.5 in)
A/C CODE TT
SEE SECTION 7−4−1
N_AC_070200_1_0180101_01_01
Landing Gear FootprintFIGURE-7-2-0-991-018-A01
7-2-0Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A320-200
Maximum Pavement Loads
1. This section gives Maximum Pavement Loads.
NOTE : For A/C code definition, refer to chapter 7-1-0.
7-3-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1
A/C
CO
DE
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
(1)
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
GE66
400
68 4
00
VM
G (
PE
R S
TR
UT
)V
NG
146
375
150
800
20 3
75
20 9
75
9 24
0
9 51
0
32 2
75
33 2
2515
070
14 6
4069
550
71 6
50
31 5
40
32 5
00
22 7
50
23 4
25
10 3
20
10 6
30
55 6
25
57 3
00
25 2
30
26 0
00
22
(2)
V(N
G)
V(M
G)
H
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
GH
(1)
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
FW
D C
G =
17
% M
AC
(2)
AF
T C
G =
43
% M
AC
N_AC_070300_1_0100101_01_01
A/C
CO
DE
E −
G
E −
G
Maximum Pavement LoadsFIGURE-7-3-0-991-010-A01
7-3-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
F67
400
VM
G (
PE
R S
TR
UT
)V
NG
148
600
20 6
759
370
32 7
5014
850
70 6
0032
020
23 1
0010
470
56 4
7525
620
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
H
(1)
MR
W =
67
400
kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
FW
D C
G =
17
% M
AC
AT
A/C
WE
IGH
T =
67
400
kg
A/C
CO
DE
F
(2)
MR
W =
67
400
kgA
FT
CG
= 4
3 %
MA
C A
T A
/C W
EIG
HT
= 6
7 40
0 kg
F
N_AC_070300_1_0320101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-032-A01
7-3-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
(1)
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
I − RH
70 4
00
71 9
00
VM
G (
PE
R S
TR
UT
)V
NG
155
200
158
500
21 5
75
22 0
25
9 79
0
9 99
0
34 1
50
34 8
5015
810
15 4
9073
200
(2)
74 8
75 (
3)
33 2
00 (
2)
33 9
60 (
3)
24 1
25
24 6
25
10 9
40
11 1
70
58 5
50
59 9
00
26 5
60
27 1
70
22
V(N
G)
V(M
G)
H
A/C
CO
DE
V(N
G)
V(M
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
GH
(1) NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T.
FW
D C
G =
17
% M
AC
(2)
AF
T C
G =
41
% M
AC
AF
T C
G =
41.
42 %
MA
C(3
)
A/C
CO
DE
H −
I −
RH
I − R
N_AC_070300_1_0110101_01_02
Maximum Pavement LoadsFIGURE-7-3-0-991-011-A01
7-3-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
(1)
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
L −
M
J −
K73
900
75 9
00
VM
G (
PE
R S
TR
UT
)V
NG
162
925
167
325
22 0
50
22 0
50
10 0
00
10 0
00
34 9
00
34 9
0015
830
15 8
3076
550
(2)
78 2
50 (
3)
34 7
20 (
2)
35 4
90 (
3)
25 3
25
26 0
00
11 4
80
11 8
00
61 2
50
62 6
00
27 7
80
28 3
90
V(N
G)
V(M
G)
H
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1) N
OT
E:
ALL
LO
AD
S C
ALC
ULA
TE
D U
SIN
G A
IRP
LAN
E M
AX
IMU
M R
AM
P W
EIG
HT
FW
D C
G =
17
% M
AC
AT
A/C
WE
IGH
T =
72
000
kg(2
)A
FT
CG
= 4
0 %
MA
CA
FT
CG
= 3
8.7
% M
AC
N_AC_070300_1_0120101_01_01
(3)
A/C
CO
DE
J −
K −
L −
MJ
− K
L −
M
Maximum Pavement LoadsFIGURE-7-3-0-991-012-A01
7-3-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
(1)
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
P −
Q
N −
O77
400
78 4
00
VM
G (
PE
R S
TR
UT
)V
NG
170
650
172
850
22 0
50
22 0
50
10 0
00
10 0
00
34 9
00
34 9
0015
830
15 8
3079
450
(2)
80 2
50 (
3)
36 0
30 (
2)
36 4
00 (
3)
26 5
25
26 8
50
12 0
30
12 1
80
63 5
50
64 2
00
28 8
30
29 1
20
V(N
G)
V(M
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
22
V(N
G)
V(M
G)
H
A/C
CO
DE
H
(1)
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T.
FW
D C
G =
17
% M
AC
AT
A/C
WE
IGH
T =
72
000
kg
(2)
AF
T C
G =
37.
5 %
MA
CA
FT
CG
= 3
6.8
% M
AC
(3)
A/C
CO
DE
N −
O −
P −
Q
N −
OP
− Q
N_AC_070300_1_0130101_01_02
Maximum Pavement LoadsFIGURE-7-3-0-991-013-A01
7-3-0Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
TT
73 9
00
VM
G (
PE
R S
TR
UT
)V
NG
162
925
22 1
5010
050
35 0
0015
870
76 5
0034
700
25 3
2511
480
61 2
0027
760
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
H
(1)
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
FW
D C
G =
17
% M
AC
AT
A/C
WE
IGH
T =
72
000
kg
(2)
AF
T C
G =
40
% M
AC
N_AC_070300_1_0140101_01_01
A/C
CO
DE
TT
TT
Maximum Pavement LoadsFIGURE-7-3-0-991-014-A01
7-3-0Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A320-200
Landing Gear Loading on Pavement
1. General
In the example shown in Section 7-4-1 Landing Gear Loading on Pavement, A/C Code E-F-G, theGross Aircraft Weight is 49 000 kg (108 025 lb) and the percentage of weight on the Main LandingGear is 94.95 %.
For these conditions the total weight on the MLG Group is 46 520 kg (102 575 lb).
7-4-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-1 Landing Gear Loading on Pavement
**ON A/C A320-200
Landing Gear Loading on Pavement
1. This section gives Landing Gear Loading on Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-4-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
TAKE OFF & LANDING
TAKE OFF LANDING
MTOW = 66 000 kg
MTOW = 67 000 kg
MTOW = 68 000 kg
MLW = 64 500 kg
MZFW = 60 500 kg
35
40
45
50
55
60
65
70W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
35
40
45
50
55
60
65
70
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
(x
1 00
0 kg
)
CG FOR ACNCALCULATION
A/C CODE E − F − G
N_AC_070401_1_0110101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-011-A01
7-4-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
35
40
45
50
55
60
65
70
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
35
40
45
50
55
60
65
70W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
MZFW = 60 500 kg
MLW = 64 500 kg
MTOW = 70 000 kg
TAKE OFF & LANDING
TAKE OFF LANDING
CG FOR ACNCALCULATION
A/C CODE H
N_AC_070401_1_0120101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-012-A01
7-4-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
35
40
45
50
55
60
65
75W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
35
40
45
50
55
60
70
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
TAKE OFF & LANDING
TAKE OFF LANDING
MZFW = 61 000 kg
MLW = 64 500 kg
MTOW = 71 500 kg
65
70
CG FOR ACNCALCULATION
A/C CODE I
N_AC_070401_1_0130101_01_02
MZFW = 60 500 kg
Landing Gear Loading on PavementFIGURE-7-4-1-991-013-A01
7-4-1Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
MZFW = 61 000 kg
MZFW = 61 500 kg
MLW = 64 500 kg
MTOW = 73 500 kg
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
TAKE OFF & LANDING
TAKE OFF LANDING
35
40
45
50
55
60
65
75W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
70
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
35
40
45
50
55
60
70
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
65
MZFW = 60 500 kg
CG FOR ACNCALCULATION
A/C CODE J − TT
N_AC_070401_1_0140101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-014-A01
7-4-1Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
35
40
45
50
55
60
70
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
65
35
40
45
50
55
60
65
75W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
70
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
TAKE OFF
MZFW = 62 500 kg
MTOW = 73 500 kg
MLW = 66 000 kg
TAKE OFF & LANDING
LANDING
CG FOR ACNCALCULATION
A/C CODE K
N_AC_070401_1_0150101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-015-A01
7-4-1Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
35
40
45
50
55
60
65
75W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
70
35
40
45
50
55
60
70
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)65
TAKE OFF & LANDING
TAKE OFFLANDING
MTOW = 75 500 kg
CG FOR ACNCALCULATIONS
MLW = 64 500 kg
MLW = 60 500 kg
MZFW = 61 000 kg
A/C CODE L
N_AC_070401_1_0160101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-016-A01
7-4-1Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
35
40
45
50
55
60
70
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)65
35
40
45
50
55
60
65
75W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
70
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
TAKE OFF & LANDING
TAKE OFF LANDING
MZFW = 62 500 kg
MLW = 66 000 kg
MTOW = 75 500 kg
CG FOR ACNCALCULATION
A/C CODE M
N_AC_070401_1_0170101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-017-A01
7-4-1Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
35
40
45
50
55
60
65
70
75
80W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
35
40
45
50
55
60
65
70
75
80
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
TAKE OFF & LANDING
TAKE OFF LANDING
CG FOR ACNCALCULATIONS
MLW = 64 500 kg
MTOW = 77 000 kg
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
A/C CODE N
MZFW = 61 000 kg
MZFW = 60 500 kg
N_AC_070401_1_0180101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-018-A01
7-4-1Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
35
40
45
50
55
60
65
70
75
80
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
35
40
45
50
55
60
65
70
75
80W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
TAKE OFF & LANDING
TAKE OFFLANDING
MZFW = 62 500 kg
MLW = 66 000 kg
MTOW = 77 000 kg
CG FOR ACNCALCULATION
A/C CODE O
N_AC_070401_1_0190101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-019-A01
7-4-1Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
35
40
45
50
55
60
65
70
75
80W
EIG
HT
ON
MA
IN L
AN
DIN
G G
EA
R −
(x
1 00
0 kg
)
35
40
45
50
55
60
65
70
75
80
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
5 10 15 20 25 30 35 40 45 50 55
PERCENTAGE MAC
MTOW = 78 000 kg
CG FOR ACNCALCULATION
MLW = 64 500 kg
MZFW = 61 000 kg
TAKE OFF & LANDING
TAKE OFFLANDING
A/C CODE P
N_AC_070401_1_0200101_01_02
Landing Gear Loading on PavementFIGURE-7-4-1-991-020-A01
7-4-1Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
82 84 86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
80
35
40
45
50
55
60
65
70
75
805 10 15 20 25 30 35 40 45 50 55
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
PERCENTAGE MAC
MTOW = 78 000 kg
A/C CODE Q
MLW = 66 000 kg
MZFW = 62 500 kg
CG FOR ACNCALCULATIONS
TAKE OFFLANDING
TAKE OFFAND LANDING
N_AC_070401_1_0850101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-085-A01
7-4-1Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
82 84 86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
35
40
45
50
55
60
65
70
755 10 15 20 25 30 35 40 45 50 55
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
PERCENTAGE MAC
MTOW = 71 500 kg
A/C CODE R
MLW = 66 000 kg
MZFW = 62 500 kg
CG FOR ACNCALCULATIONS
TAKE OFFLANDING
TAKE OFFAND LANDING
N_AC_070401_1_0860101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-086-A01
7-4-1Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A320-200
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
1. General
In order to determine a particular Flexible Pavement Thickness, the Subgrade Strength (CBR), theAnnual Departure Level and the weight on one Main Landing Gear must be known.
In the example shown in Section 7-5-1 Flexible Pavement Requirements, A/C Code E (Main GearTire Size 46 x 17 R20 (46 x 16 - 20), inflated at 12.3 bar (178 psi)):- a CBR value of 10- an Annual Departure Level of 15 000- the Load on one MLG of 20 000 kg (44 100 lb).
For these conditions, the Flexible Pavement Thickness is 41.5 cm (16.3 in).
The line showing 10 000 Coverages is used to calculate the Aircraft Classification Number (ACN).
7-5-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A320-200
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
1. This section gives Flexible Pavement Requirements.
NOTE : For A/C Code definition, refer to chapter 07-01-00.
7-5-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 12.3 bar (178 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE E ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
N_AC_070501_1_0720101_01_00
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR31 540 kg (69 550 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Flexible Pavement RequirementsFIGURE-7-5-1-991-072-A01
7-5-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRES
TIRE PRESSURE CONSTANT AT 10.2 bar (148 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
A/C CODE E ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0730101_01_00
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR31 540 kg (69 550 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-073-A01
7-5-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRES
TIRE PRESSURE CONSTANT AT 9.2 bar (133 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
A/C CODE E ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_0740101_01_00
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
31 540 kg (69 550 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
FOR ACN CALCULATIONS10 000 COVERAGES USED
Flexible Pavement RequirementsFIGURE-7-5-1-991-074-A01
7-5-1Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
32 020 kg (70 600 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE F ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
N_AC_070501_1_0750101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-075-A01
7-5-1Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE F ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
32 020 kg (70 600 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRES
TIRE PRESSURE CONSTANT AT 10.6 bar (154 psi)N_AC_070501_1_0760101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-076-A01
7-5-1Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE F ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
32 020 kg (70 600 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 10.9 bar (158 psi)N_AC_070501_1_0770101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-077-A01
7-5-1Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
32 020 kg (70 600 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRES
TIRE PRESSURE CONSTANT AT 9.6 bar (139 psi)N_AC_070501_1_0780101_01_00
A/C CODE F
Flexible Pavement RequirementsFIGURE-7-5-1-991-078-A01
7-5-1Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
32 500 kg (71 650 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)N_AC_070501_1_0790101_01_00
A/C CODE G
Flexible Pavement RequirementsFIGURE-7-5-1-991-079-A01
7-5-1Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
32 500 kg (71 650 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRES
TIRE PRESSURE CONSTANT AT 10.6 bar (154 psi)
A/C CODE G
N_AC_070501_1_0800101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-080-A01
7-5-1Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
32 500 kg (71 650 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 10.9 bar (158 psi)
A/C CODE G
N_AC_070501_1_0810101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-081-A01
7-5-1Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
32 500 kg (71 650 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRES
TIRE PRESSURE CONSTANT AT 9.6 bar (139 psi)
A/C CODE G
N_AC_070501_1_0820101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-082-A01
7-5-1Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
33 200 kg (73 200 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
WEIGHT ON ONE MAIN LANDING GEAR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
A/C CODE H
N_AC_070501_1_0830101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-083-A01
7-5-1Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRES
TIRE PRESSURE CONSTANT AT 10.6 bar (154 psi)
A/C CODE H
N_AC_070501_1_0840101_01_00
33 200 kg (73 200 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
WEIGHT ON ONE MAIN LANDING GEAR
Flexible Pavement RequirementsFIGURE-7-5-1-991-084-A01
7-5-1Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R 22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 10.9 bar (158 psi)
A/C CODE H
N_AC_070501_1_0850101_01_00
33 200 kg (73 200 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
WEIGHT ON ONE MAIN LANDING GEAR
Flexible Pavement RequirementsFIGURE-7-5-1-991-085-A01
7-5-1Page 15
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRES
TIRE PRESSURE CONSTANT AT 9.6 bar (139 psi)
A/C CODE H
N_AC_070501_1_0860101_01_00
33 200 kg (73 200 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
WEIGHT ON ONE MAIN LANDING GEAR
Flexible Pavement RequirementsFIGURE-7-5-1-991-086-A01
7-5-1Page 16
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9A/C CODE I − R
N_AC_070501_1_0870101_01_01
WEIGHT ON ONE MAIN LANDING GEAR33 960 kg (74 875 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
3 0006 00015 000
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
1 200
Flexible Pavement RequirementsFIGURE-7-5-1-991-087-A01
7-5-1Page 17
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRES
TIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
N_AC_070501_1_0880101_01_01
A/C CODE I − R
WEIGHT ON ONE MAIN LANDING GEAR33 960 kg (74 875 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
1 2003 0006 00015 000
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
Flexible Pavement RequirementsFIGURE-7-5-1-991-088-A01
7-5-1Page 18
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 11.8 bar (171 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
1 2003 0006 00015 000
N_AC_070501_1_0890101_01_01
A/C CODE I − R
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
WEIGHT ON ONE MAIN LANDING GEAR33 960 kg (74 875 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-089-A01
7-5-1Page 19
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRES
TIRE PRESSURE CONSTANT AT 10.3 bar (149 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
N_AC_070501_1_0900101_01_01
A/C CODE I − R
3 0006 00015 000
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
1 200
WEIGHT ON ONE MAIN LANDING GEAR33 960 kg (74 875 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-090-A01
7-5-1Page 20
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE J−K
WEIGHT ON ONE MAIN LANDING GEAR33 960 kg (74 875 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
N_AC_070501_1_0910101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-091-A01
7-5-1Page 21
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRES
TIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE J−K
WEIGHT ON ONE MAIN LANDING GEAR34 720 kg (76 550 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
N_AC_070501_1_0920101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-092-A01
7-5-1Page 22
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 11.8 bar (171 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE J−K
WEIGHT ON ONE MAIN LANDING GEAR34 720 kg (76 550 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
N_AC_070501_1_0930101_01_00
Flexible Pavement RequirementsFlexible Pavement Requirements
FIGURE-7-5-1-991-093-A01
7-5-1Page 23
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRES
TIRE PRESSURE CONSTANT AT 10.3 bar (149 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE J−K
WEIGHT ON ONE MAIN LANDING GEAR34 720 kg (76 550 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
N_AC_070501_1_0940101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-094-A01
7-5-1Page 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE L−M
WEIGHT ON ONE MAIN LANDING GEAR35 490 kg (78 250 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
N_AC_070501_1_0950101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-095-A01
7-5-1Page 25
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRES
TIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE L−M
WEIGHT ON ONE MAIN LANDING GEAR35 490 kg (78 250 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
N_AC_070501_1_0960101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-096-A01
7-5-1Page 26
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 11.8 bar (171 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE L−M
WEIGHT ON ONE MAIN LANDING GEAR35 490 kg (78 250 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
N_AC_070501_1_0970101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-097-A01
7-5-1Page 27
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 10.3 bar (149 psi)
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR35 490 kg (78 250 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
ALPHA FACTOR = 0.9A/C CODE L−M
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0980101_01_00
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
Flexible Pavement RequirementsFIGURE-7-5-1-991-098-A01
7-5-1Page 28
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 14.4 bar (209 psi)
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR36 030 kg (79 450 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
ALPHA FACTOR = 0.9A/C CODE N−O
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0990101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-099-A01
7-5-1Page 29
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 12 bar (174 psi)
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
WEIGHT ON ONE MAIN LANDING GEAR36 030 kg (79 450 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
ALPHA FACTOR = 0.9A/C CODE N−O
N_AC_070501_1_1000101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-100-A01
7-5-1Page 30
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.3 bar (178 psi)
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
WEIGHT ON ONE MAIN LANDING GEAR36 030 kg (79 450 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
ALPHA FACTOR = 0.9A/C CODE N−O
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_1010101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-101-A01
7-5-1Page 31
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 10.7 bar (155 psi)
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
WEIGHT ON ONE MAIN LANDING GEAR36 030 kg (79 450 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
ALPHA FACTOR = 0.9A/C CODE N−O
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_1020101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-102-A01
7-5-1Page 32
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 TIRES
TIRE PRESSURE CONSTANT AT 14.4 bar (209 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR36 400 kg (80 250 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
N_AC_070501_1_1030101_01_01
A/C CODE P − Q
Flexible Pavement RequirementsFIGURE-7-5-1-991-103-A01
7-5-1Page 33
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
8060403020151063
SUBGRADE STRENGTH − CBR
8060403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 12.3 bar (178 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9A/C CODE P − Q
3 0006 00015 000
WEIGHT ON ONE MAIN LANDING GEAR36 400 kg (80 250 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
1 200
N_AC_070501_1_1050101_01_01
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
Flexible Pavement RequirementsFIGURE-7-5-1-991-105-A01
7-5-1Page 34
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
10 15 20 30 40 60 80 100 120 150 180(cm)
FLEXIBLE PAVEMENT THICKNESS
915 x 300 R16 (36 x 11−16) TIRESTIRE PRESSURE CONSTANT AT 12.2 bar (177 psi)
(in)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
ALPHA FACTOR = 0.8
USED FOR ACN10 000 COVERAGES
CALCULATIONS
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
N_AC_070501_1_1070101_01_01
WEIGHT ON ONE MAIN LANDING GEAR34 700 kg (76 500 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)
A/C CODE TT
Flexible Pavement RequirementsFIGURE-7-5-1-991-107-A01
7-5-1Page 35
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A320-200
Flexible Pavement Requirements - LCN Conversion
1. General
In order to determine the airplane weight that can be accommodated on a particular FlexiblePavement, both the LCN of the pavement and the thickness (h) must be known.
In the example shown in Section 7-6-1 Flexible Pavement Requirements - LCN Conversion, A/C CodeE (Main Gear Tire Size 46 x 17 R20 (46 x 16 - 20), inflated at 12.3 bar (178 psi)) for:The thickness (h) is shown at 20 inches with an LCN of 53.
For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).
7-6-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-1 Flexible Pavement Requirements - LCN Conversion
**ON A/C A320-200
Flexible Pavement Requirements - LCN Conversion
1. This section gives Flexible Pavement Requirements - LCN Conversion.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-6-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)46
x 1
7 R
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
31 5
40 k
g
(69
550
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
2 03
21
524
1 01
676
225
450
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
E
N_AC_070601_1_0750101_01_00
70
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-075-A01
7-6-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
31 5
40 k
g
(69
550
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
2 03
21
524
1 01
676
225
450
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
E
N_AC_070601_1_0760101_01_00
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.2
bar
(148
psi
)49
x 1
7−20
TIR
ES
70
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-076-A01
7-6-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
31 5
40 k
g
(69
550
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
2 03
21
524
1 01
676
225
450
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
E
N_AC_070601_1_0770101_01_00
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.2 b
ar (
133
psi)
49 x
19−
20 T
IRE
S
70
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-077-A01
7-6-1Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
2 03
21
524
1 01
676
225
450
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
F
46 x
17
R20
TIR
ES
N_AC_070601_1_0780101_01_00
70
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-078-A01
7-6-1Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:E
QU
IVA
LEN
T S
ING
LE W
HE
EL
LOA
DS
AR
E D
ER
IVE
D B
Y M
ET
HO
DS
SH
OW
N IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3 S
econ
d E
ditio
n 19
65
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.6
bar
(154
psi
)49
x 1
7−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
F
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
70
N_AC_070601_1_0790101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-079-A01
7-6-1Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.9
bar
(158
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
F
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
70
N_AC_070601_1_0800101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-080-A01
7-6-1Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.6 b
ar (
139
psi)
49 x
19−
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
F
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
70
N_AC_070601_1_0810101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-081-A01
7-6-1Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)46
x 1
7 R
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
G
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
70
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:E
QU
IVA
LEN
T S
ING
LE W
HE
EL
LOA
DS
AR
E D
ER
IVE
D B
Y M
ET
HO
DS
SH
OW
N IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3 S
econ
d E
ditio
n 19
65
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.6
bar
(154
psi
)49
x 1
7−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
G
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
70
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.9
bar
(158
psi
)1
270
x 45
5 R
22 (
19 x
18−
22)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
G
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
70
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.6 b
ar (
139
psi)
49 x
19−
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
G
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
70
N_AC_070601_1_0850101_01_00
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)46
x 1
7 R
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
70
N_AC_070601_1_0860101_01_00
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7-6-1Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.6
bar
(154
psi
)49
x 1
7−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
70
N_AC_070601_1_0870101_01_00
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7-6-1Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.9
bar
(158
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
70
N_AC_070601_1_0880101_01_00
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Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.6 b
ar (
139
psi)
49 x
19−
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
2 03
21
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
70
N_AC_070601_1_0890101_01_00
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
X 1
7 R
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
33 9
60 k
g
(74
875
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
70
N_AC_070601_1_0900101_01_01
A/C
CO
DE
I −
R
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-090-A01
7-6-1Page 17
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)49
X 1
7−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
70
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
33 9
60 k
g
(74
875
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
A/C
CO
DE
I −
R
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**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)1
270
X 4
55 R
22 (
49 x
18−
22)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
33 9
60 k
g
(74
875
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
70
N_AC_070601_1_0920101_01_01
A/C
CO
DE
I −
R
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
33 9
60 k
g
(74
875
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
70
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.3
bar
(149
psi
)49
X 1
9−20
TIR
ES
A/C
CO
DE
I −
R
N_AC_070601_1_0930101_01_01
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
X 1
7 R
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
34 7
20 k
g
(76
550
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
A/C
CO
DE
J−
K
70
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)49
X 1
7−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
34 7
20 k
g
(76
550
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
A/C
CO
DE
J−
K
70
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)1
270
X 4
55 R
22 (
49 x
18−
22)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
34 7
20 k
g
(76
550
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
A/C
CO
DE
J−
K
70
N_AC_070601_1_0960101_01_00
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.3
bar
(149
psi
)49
X 1
9−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
34 7
20 k
g
(76
550
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
A/C
CO
DE
J−
K
70
N_AC_070601_1_0970101_01_00
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7-6-1Page 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
X 1
7 R
20 T
IRE
S
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
35 4
90 k
g
(78
250
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
A/C
CO
DE
L−
M
70
N_AC_070601_1_0980101_01_00
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@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)49
X 1
7−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)2
032
1 52
41
016
762
508
254
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
35 4
90 k
g
(78
250
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
A/C
CO
DE
L−
M
70
N_AC_070601_1_0990101_01_00
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7-6-1Page 26
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
L−
M
2 03
21
524
1 01
6
70
WE
IGH
T O
N O
NE
MA
IN
35 4
90 k
g
(78
250
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1000101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-100-A01
7-6-1Page 27
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.3
bar
(149
psi
)49
x 1
9−20
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
L−
M
2 03
21
524
1 01
6
70
WE
IGH
T O
N O
NE
MA
IN
35 4
90 k
g
(78
250
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1010101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-101-A01
7-6-1Page 28
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.4
bar
(209
psi
)46
x 1
7 R
20 T
IRE
S
40 30 25 20 15 10 5 010
012
070
5040
3020
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607090
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
80
35
60
80M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
A/C
CO
DE
N−
O
WE
IGH
T O
N O
NE
MA
IN
36 0
30 k
g
(79
450
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1020101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-102-A01
7-6-1Page 29
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2 ba
r (1
74 p
si)
49 x
17−
20 T
IRE
S
40 30 25 20 15 10 5 010
012
070
5040
3020
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607090
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
80
35
60
80M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
A/C
CO
DE
N−
O
WE
IGH
T O
N O
NE
MA
IN
36 0
30 k
g
(79
450
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1030101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-103-A01
7-6-1Page 30
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)1
270
x 45
5 R
22
40 30 25 20 15 10 5 010
012
070
5040
3020
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607090
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
80
35
60
80M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
A/C
CO
DE
N−
O
WE
IGH
T O
N O
NE
MA
IN
36 0
30 k
g
(79
450
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1040101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-104-A01
7-6-1Page 31
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.7
bar
(155
psi
)49
x 1
9−20
TIR
ES
40 30 25 20 15 10 5 010
012
070
5040
3020
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607090
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
80
35
60
80M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
A/C
CO
DE
N−
O
WE
IGH
T O
N O
NE
MA
IN
36 0
30 k
g
(79
450
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1050101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-105-A01
7-6-1Page 32
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.4
bar
(209
psi
)46
x 1
7 R
20 T
IRE
S
40 30 25 20 15 10 5 010
012
070
5040
3020
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607090
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
80
35
60
80M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
TW
EIG
HT
ON
ON
E M
AIN
36 4
00 k
g
(80
250
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1060101_01_01
A/C
CO
DE
P −
Q
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-106-A01
7-6-1Page 33
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)1
270
x 45
5 R
22
40 30 25 20 15 10 5 010
012
070
5040
3020
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607090
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
80
35
60
80M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
TW
EIG
HT
ON
ON
E M
AIN
36 4
00 k
g
(80
250
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
N_AC_070601_1_1080101_01_01
A/C
CO
DE
P −
Q
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-108-A01
7-6-1Page 34
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.2
bar
(177
psi
)91
5 x
300
R16
(36
x 1
1−16
)
10 5 080
120
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
70
15202530354045505560M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
A/C
CO
DE
TT
WE
IGH
T O
N O
NE
MA
IN
34 7
00 k
g
(76
500
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
100
N_AC_070601_1_1100101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-110-A01
7-6-1Page 35
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A320-200
Rigid Pavement Requirements - Portland Cement Association Design Method
1. GeneralIn order to determine a Rigid Pavement Thickness, the Subgrade Modulus (k), the allowable workingstress and the weight on one Main Landing Gear must be known.
In the example shown in Section 7-7-1 Rigid Pavement Requirements (PCA), A/C Code E (MainGear Tire Size 46 x 17 R20 (46 x 16 - 20), inflated at 12.3 bar (178 psi)) for:- a ”k” value of 80 MN/m3 (300 lb/in3)- an allowable working stress of 32 kg/cm2 (450 lb/in2)- a load on one MLG of 25 000 kg (55 125 lb).
For these conditions, the Rigid Pavement Thickness is 23 cm (9.1 in).
7-7-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A320-200
Rigid Pavement Requirements - Portland Cement Association Design Method
1. This section gives Rigid Pavement Requirements.
NOTE : For A/C Code definition, refer to chapter 07-01-00.
7-7-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
31 540 kg (69 550 lb)
A/C CODE E
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 12.3 bar (178 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
N_AC_070701_1_0720101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-072-A01
7-7-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
31 540 kg (69 550 lb)
A/C CODE E
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 10.2 bar (148 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
N_AC_070701_1_0730101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-073-A01
7-7-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 9.2 bar (133 psi)
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
31 540 kg (69 550 lb)
A/C CODE E
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_0740101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-074-A01
7-7-1Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 10.6 bar (154 psi)
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
32 010 kg (70 550 lb)
A/C CODE F
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_0750101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-075-A01
7-7-1Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)32 010 kg (70 550 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 10.9 bar (158 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
N_AC_070701_1_0760101_01_00
A/C CODE F
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-076-A01
7-7-1Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)32 010 kg (70 550 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 9.6 bar (139 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
A/C CODE F
N_AC_070701_1_0770101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-077-A01
7-7-1Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)32 010 kg (70 550 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
A/C CODE F
N_AC_070701_1_0780101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-078-A01
7-7-1Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)32 500 kg (71 650 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
A/C CODE G
N_AC_070701_1_0790101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-079-A01
7-7-1Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)32 500 kg (71 650 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 10.6 bar (154 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
A/C CODE G
N_AC_070701_1_0800101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-080-A01
7-7-1Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)32 500 kg (71 650 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
A/C CODE G
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 10.9 bar (158 psi)
N_AC_070701_1_0810101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-081-A01
7-7-1Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)32 500 kg (71 650 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
A/C CODE G
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 9.6 bar (139 psi)
N_AC_070701_1_0820101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-082-A01
7-7-1Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 200 kg (73 200 lb)
A/C CODE H
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
N_AC_070701_1_0830101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-083-A01
7-7-1Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 200 kg (73 200 lb)
A/C CODE H
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 10.6 bar (154 psi)
N_AC_070701_1_0840101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-084-A01
7-7-1Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 200 kg (73 200 lb)
A/C CODE H
N_AC_070701_1_0850101_01_00
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 10.9 bar (158 psi)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-085-A01
7-7-1Page 15
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 200 kg (73 200 lb)
A/C CODE H
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 9.6 bar (139 psi)
N_AC_070701_1_0860101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-086-A01
7-7-1Page 16
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 960 kg (74 875 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
100
55
61
N_AC_070701_1_0870101_01_01
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE I − R
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-087-A01
7-7-1Page 17
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 960 kg (74 875 lb)
N_AC_070701_1_0880101_01_01
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE I − R
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-088-A01
7-7-1Page 18
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 11.8 bar (171 psi)
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 960 kg (74 875 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE I − R
N_AC_070701_1_0890101_01_01
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-089-A01
7-7-1Page 19
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)33 960 kg (74 875 lb)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 10.3 bar (149 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
A/C CODE I − R
N_AC_070701_1_0900101_01_01
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-090-A01
7-7-1Page 20
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
100
55
61
N_AC_070701_1_0910101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)34 720 kg (76 550 lb)
A/C CODE J−K
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-091-A01
7-7-1Page 21
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)34 720 kg (76 550 lb)
A/C CODE J−K
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_0920101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-092-A01
7-7-1Page 22
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 11.8 bar (171 psi)
100
55
61
N_AC_070701_1_0930101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)34 720 kg (76 550 lb)
A/C CODE J−K
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-093-A01
7-7-1Page 23
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)34 720 kg (76 550 lb)
A/C CODE J−K
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 10.3 bar (149 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
N_AC_070701_1_0940101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-094-A01
7-7-1Page 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)35 490 kg (78 250 lb)
A/C CODE L−M
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
100
55
61
N_AC_070701_1_0950101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-095-A01
7-7-1Page 25
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
100
55
61
N_AC_070701_1_0960101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)35 490 kg (78 250 lb)
A/C CODE L−M
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-096-A01
7-7-1Page 26
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 11.8 bar (171 psi)
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)35 490 kg (78 250 lb)
A/C CODE L−M
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_0980101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-098-A01
7-7-1Page 27
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)35 490 kg (78 250 lb)
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 10.3 bar (149 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_0990101_01_00
A/C CODE L−M
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-099-A01
7-7-1Page 28
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)36 030 kg (79 450 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 14.4 bar (209 psi)
N_AC_070701_1_1000101_01_00
A/C CODE N−O
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-100-A01
7-7-1Page 29
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)36 030 kg (79 450 lb)
A/C CODE N−O
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_1010101_01_00
49 x 17−20 TIRESTIRE PRESSURE CONSTANT AT 12 bar (174 psi)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-101-A01
7-7-1Page 30
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)36 030 kg (79 450 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.3 bar (178 psi)
N_AC_070701_1_1020101_01_00
A/C CODE N−O
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-102-A01
7-7-1Page 31
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)36 030 kg (79 450 lb)
49 x 19−20 TIRESTIRE PRESSURE CONSTANT AT 10.7 bar (155 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_1030101_01_00
A/C CODE N−O
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-103-A01
7-7-1Page 32
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)36 400 kg (80 250 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
46 x 17 R20 TIRESTIRE PRESSURE CONSTANT AT 14.4 bar (209 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE P − Q
N_AC_070701_1_1040101_01_01
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-104-A01
7-7-1Page 33
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
33
31
29
27
25
23
21
19
17200
300
400
500
600
700
800
900
49
43
37
31
25
19
13
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
100
55
61
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)36 400 kg (80 250 lb)
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.3 bar (178 psi)
A/C CODE P − Q
N_AC_070701_1_1060101_01_01
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-106-A01
7-7-1Page 34
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
7
8
9
10
11
12
13
1436
34
32
30
28
26
24
22
20
200
300
400
500
600
700
800
900
56
50
44
38
32
26
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
915 x 300 R16 (36 x 11−16)TIRE PRESSURE CONSTANT AT 12.2 bar (177 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
62
68
N_AC_070701_1_1080101_01_00
15 1 000
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
30 000 kg (66 150 lb)34 700 kg (76 500 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE TT
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-108-A01
7-7-1Page 35
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-1 Radius of Relative Stiffness
**ON A/C A320-200
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
d6.06.57.07.5
k=75 k=100 k=150 k=200 k=250 k=300 k=350 k=400 k=550
8.08.59.09.5
10.010.511.011.512.012.513.013.514.014.515.015.516.016.517.017.518.019.020.021.022.023.024.025.0
31.4833.4335.3437.2239.0640.8842.6744.4346.1847.9049.6051.2852.9454.5956.2257.8359.4361.0262.5964.1565.6967.2368.7570.2671.7674.7377.6680.5583.4186.2489.0491.81
29.3031.1132.8934.6336.3538.0439.7141.3542.9744.5746.1647.7249.2750.8052.3253.8255.3156.7858.2559.7061.1362.5663.9865.3866.7869.5472.2774.9677.6380.2682.8685.44
26.4728.1129.7231.2932.8534.3735.8837.3638.8340.2841.7143.1244.5245.9047.2748.6349.9851.3152.6353.9455.2456.5357.8159.0860.3462.8465.3067.7470.1472.5274.8777.20
24.6326.1627.6529.1230.5731.9933.3934.7736.1437.4838.8140.1341.4342.7243.9945.2646.5147.7548.9850.2051.4152.6153.8054.9856.1558.4860.7763.0465.2867.4969.6871.84
23.3024.7426.1527.5428.9130.2531.5832.8934.1735.4536.7137.9539.1840.4041.6142.8043.9845.1646.3247.4748.6249.7550.8852.0053.1155.3157.4759.6261.7363.8365.9067.95
22.2623.6424.9926.3227.6228.9130.1731.4232.6533.8735.0736.2637.4438.6039.7540.8942.0243.1544.2645.3646.4547.5448.6149.6850.7452.8454.9156.9658.9860.9862.9664.92
21.4222.7424.0425.3226.5827.8129.0330.2331.4232.5933.7534.8936.0237.1438.2539.3540.4441.5142.5843.6444.7045.7446.7747.8048.8250.8452.8454.8156.7558.6860.5862.46
20.7222.0023.2524.4925.7026.9028.0829.2430.3931.5232.6433.7434.8435.9236.9938.0639.1140.1541.1942.2143.2344.2445.2446.2347.2249.1751.1053.0154.8956.7558.5960.41
19.1320.3121.4722.6123.7424.8425.9327.0028.0629.1130.1432.1632.1733.1734.1635.1436.1237.0838.0338.9839.9240.8541.7842.7043.6145.4147.1948.9550.6952.4154.1155.79
L = Ed
= 24.1652dk
RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES
43 3
4
12 (1 − ) k2
N_AC_070801_1_0030101_01_01
E = YOUNG’S MODULUS = 4 x 10 psi
k = SUBGRADE MODULUS, lb/in
d = RIGID PAVEMENT THICKNESS, (in)
= POISSON’S RATIO = 0.15
WHERE6
3
Radius of Relative Stiffness(Reference: Portland Cement Association)
FIGURE-7-8-1-991-003-A01
7-8-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-2 Rigid Pavement Requirements - LCN Conversion
**ON A/C A320-200
Rigid Pavement Requirements - LCN Conversion
1. GeneralIn order to determine the airplane weight that can be accommodated on a particular Rigid Pavement,both the LCN of the pavement and the Radius of Relative Stiffness (L) must be known.
In the example shown in this section Rigid Pavement Requirements - LCN Conversion, A/C Code E(Main Gear Tire Size 46 x 17 R20 (46 x 16 - 20), inflated at 12.3 bar (178 psi)) for:- The Radius of Relative Stiffness is shown at 762 mm (30 in) with an LCN of 57.
For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-8-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_070802_1_0750101_01_01
508
762
1 01
61
270
1 52
42
540
2 03
2
6080
5040
3020
10051015202530
2030
4050
100
9080
7060
010203040506070
70
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)F
LEX
IBLE
PA
VE
ME
NT
TH
ICK
NE
SS
(m
m)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
540
kg
(6
9 55
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
A/C
CO
DE
E
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-075-A01
7-8-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.2
bar
(148
psi
)49
x 1
7−20
TIR
ES
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
20030
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
1015202530
A/C
CO
DE
E
100
WE
IGH
T O
N O
NE
MA
IN
31 5
40 k
g
(69
550
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
762
2 54
01
270
1 01
61
524
2 03
2
N_AC_070802_1_0760101_01_00
508
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-076-A01
7-8-2Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.2 b
ar (
133
psi)
49 x
19−
20 T
IRE
S
5 070
5040
3020
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
20030
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
1015202530
A/C
CO
DE
E
100
WE
IGH
T O
N O
NE
MA
IN
31 5
40 k
g
(69
550
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
762
2 54
01
270
1 01
61
524
2 03
250
8
N_AC_070802_1_0770101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-077-A01
7-8-2Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)46
x 1
7 R
20 T
IRE
S
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
20030
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
1015202530
A/C
CO
DE
F
100
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
762
2 54
01
270
1 01
61
524
2 03
250
8
N_AC_070802_1_0780101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-078-A01
7-8-2Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.6
bar
(154
psi
)49
x 1
7−20
TIR
ES
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
200
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
30762
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202530
A/C
CO
DE
F
100
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
1 52
42
032
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0790101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-079-A01
7-8-2Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.9
bar
(158
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202530
A/C
CO
DE
F
100
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
1 52
42
032
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0800101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-080-A01
7-8-2Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.6 b
ar (
139
psi)
49 x
19−
20 T
IRE
S
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202530
A/C
CO
DE
F
100
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
1 52
42
032
WE
IGH
T O
N O
NE
MA
IN
32 0
20 k
g
(70
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0810101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-081-A01
7-8-2Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)46
x 1
7 R
20 T
IRE
S
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202530
A/C
CO
DE
G
100
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
1 52
42
032
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0820101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-082-A01
7-8-2Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.6
bar
(154
psi
)49
x 1
7−20
TIR
ES
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202530
A/C
CO
DE
G
100
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
1 52
42
032
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0830101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-083-A01
7-8-2Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.9
bar
(158
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202530
A/C
CO
DE
G
100
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
1 52
42
032
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0840101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-084-A01
7-8-2Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.6 b
ar (
139
psi)
49 x
19−
20 T
IRE
S
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506070
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202530
A/C
CO
DE
G
100
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
1 52
42
032
N_AC_070802_1_0850101_01_00
WE
IGH
T O
N O
NE
MA
IN
32 5
00 k
g
(71
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-085-A01
7-8-2Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)46
x 1
7 R
20 T
IRE
S
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506080
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202535
100
1 52
42
032
7030
A/C
CO
DE
H
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
LAN
DIN
G G
EA
R
15 0
00 k
g
(33
075
lb)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
N_AC_070802_1_0860101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-086-A01
7-8-2Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.6
bar
(154
psi
)49
x 1
7−20
TIR
ES
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506080
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202535
100
1 52
42
032
7030
A/C
CO
DE
H
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
N_AC_070802_1_0870101_01_00
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-087-A01
7-8-2Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.9
bar
(158
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506080
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202535
100
1 52
42
032
7030
A/C
CO
DE
H
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
N_AC_070802_1_0880101_01_00
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-088-A01
7-8-2Page 15
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
NO
TE
:EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.6 b
ar (
139
psi)
49 x
19−
20 T
IRE
S
5 080
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
10203040506080
9080
7060
5040
2003076
250
8
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 54
01
270
1 01
6
1015202535
100
1 52
42
032
7030
A/C
CO
DE
H
WE
IGH
T O
N O
NE
MA
IN
33 2
00 k
g
(73
200
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
N_AC_070802_1_0890101_01_00
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-089-A01
7-8-2Page 16
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
I −
R
6090
5040
3020
1005101520253035
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R33
960
kg
(7
4 87
5 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0900101_01_01
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-090-A01
7-8-2Page 17
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6090
5040
3020
1005101520253035
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R33
960
kg
(7
4 87
5 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
I −
R
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_0910101_01_01
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-091-A01
7-8-2Page 18
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
1270
x 4
55 R
22 (
49 x
18−
22)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R33
960
kg
(7
4 87
5 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
I −
R
N_AC_070802_1_0920101_01_01
2030
4050
100
9080
600102030405060708050
876
21
016
1 27
01
524
2 54
02
032
6090
5040
3020
1005101520253035
70
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-092-A01
7-8-2Page 19
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6080
5040
3020
10
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
3 ba
r (1
49 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R33
960
kg
(7
4 87
5 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0930101_01_01
A/C
CO
DE
I −
R
05101520253035
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-093-A01
7-8-2Page 20
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
J−
K
6090
5040
3020
1005101520253035
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
720
kg
(7
6 55
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0940101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-094-A01
7-8-2Page 21
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6090
5040
3020
1005101520253035
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
720
kg
(7
6 55
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
J−
K
N_AC_070802_1_0950101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-095-A01
7-8-2Page 22
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6090
5040
3020
1005101520253035
1270
x 4
55 R
22 (
49 x
18−
22)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
720
kg
(7
6 55
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
J−
K
N_AC_070802_1_0960101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-096-A01
7-8-2Page 23
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6080
5040
3020
1005101520253035
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
3 ba
r (1
49 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
720
kg
(7
6 55
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
J−
K
N_AC_070802_1_0970101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-097-A01
7-8-2Page 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
L−
M
N_AC_070802_1_0980101_01_00
6090
5040
3020
1005101520253035
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R35
490
kg
(7
8 25
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-098-A01
7-8-2Page 25
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6090
5040
3020
1005101520253035
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R35
490
kg
(7
8 25
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
L−
M
N_AC_070802_1_0990101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-099-A01
7-8-2Page 26
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6090
5040
3020
1005101520253035
1270
x 4
55 R
22 (
49 x
18−
22)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R35
490
kg
(7
8 25
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
L−
M
N_AC_070802_1_1000101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-100-A01
7-8-2Page 27
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
6080
5040
3020
1005101520253035
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
3 ba
r (1
49 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R35
490
kg
(7
8 25
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
A/C
CO
DE
L−
M
N_AC_070802_1_1010101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-101-A01
7-8-2Page 28
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
N−
O
6090
5040
3020
1005101520253035
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.4
bar
(209
psi
)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R36
030
kg
(7
9 45
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_1020101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-102-A01
7-8-2Page 29
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
N−
O
6090
5040
3020
1005101520253035
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12
bar
(174
psi
)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R36
030
kg
(7
9 45
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_1030101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-103-A01
7-8-2Page 30
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
N−
O
6090
5040
3020
1005101520253035
1 27
0 x
455
R22
(49
x 1
8−22
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
3 ba
r (1
78 p
si)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R36
030
kg
(7
9 45
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_1040101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-104-A01
7-8-2Page 31
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
01020304050607080
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
N−
O
6090
5040
3020
1005101520253035
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
7 ba
r (1
55 p
si)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R36
030
kg
(7
9 45
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_1050101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-105-A01
7-8-2Page 32
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
508
762
1 01
61
270
1 52
42
540
2 03
2
6090
5040
3020
1005101520253035
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R36
400
kg
(8
0 25
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.4
bar
(209
psi
)
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
P −
Q
N_AC_070802_1_1060101_01_01
2030
4050
100
9080
7060
01020304050607080
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-106-A01
7-8-2Page 33
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
508
762
1 01
61
270
1 52
42
540
2 03
2
6090
5040
3020
1005101520253035
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R36
400
kg
(8
0 25
0 lb
)30
000
kg
(6
6 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
2030
4050
100
9080
7060
01020304050607080
1 27
0 x
455
R22
(49
x 1
8−22
)T
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
3 ba
r (1
78 p
si)
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
P −
Q
N_AC_070802_1_1080101_01_01
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-108-A01
7-8-2Page 34
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
2030
4050
100
9080
7060
0102030405060
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
508
762
1 01
61
270
1 52
42
540
2 03
2
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
TT
6010
050
4030
2010
0510152025
915
x 30
0 R
16 (
36 x
11−
16)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.2
bar
(177
psi
)
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GW
EIG
HT
ON
ON
E M
AIN
LA
ND
ING
GE
AR
34 7
00 k
g
(76
500
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
N_AC_070802_1_1100101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-110-A01
7-8-2Page 35
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-3 Radius of Relative Stiffness (Other values of E and L)
**ON A/C A320-200
Radius of Relative Stiffness (Other values of ”E” and ”L”)
1. General
The table of Section 7-8-1, Radius of Relative Stiffness, presents ”L” values based on Young’sModulus (E) of 4 000 000 psi and Poisson’s Ratio (µ) of 0.15.
To find ”L” values based on other values of ”E” and ”µ”, see Section 7-8-4.
For example, to find an ”L” value based on an ”E” of 3 000 000 psi, the ”E” factor of 0.931 ismultiplied by the ”L” value found in the table of Section 7-8-1.
The effect of variations of ”µ” on the ”L” value is treated in a similar manner.
7-8-3Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-4 Radius of Relative Stiffness
**ON A/C A320-200
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-4Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0.80
0.85
0.90
0.95
1.00
1.05
1.10
0 1 2 3 4 5
0.995
1.000
1.005
1.010
1.015
0.00 0.05 0.10 0.15 0.20 0.25
E F
AC
TO
R
BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF TABLE 7−8−1NOTE:
EFFECT OF ON L VALUES
E, Young’s Modulus (10 , PSI)
EFFECT OF E ON L VALUES
, Poisson’s Ratio
FA
CT
OR
N_AC_070804_1_0030101_01_01
Radius of Relative Stiffness(Effect E and µ on ”L” values)
FIGURE-7-8-4-991-003-A01
7-8-4Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0 ACN/PCN Reporting System
**ON A/C A320-200
ACN/PCN Reporting System
1. General
To determine the ACN of an aircraft on flexible or rigid pavement, both the aircraft gross weight andthe subgrade strength must be known.
In the example shown in Section 7-9-1 Aircraft Classification Number -- Flexible Pavement, A/C CodeE (Main Gear Tire Size 46 x 17 R20 (46 x 16 - 20), inflated at 12.3 bar (178 psi)), for an aircraftgross weight of 55 000 kg (121 250 lb) and medium subgrade strength (code B), the ACN for theflexible pavement is 28.
In the example shown in Section 7-9-2 Aircraft Classification Number -- Rigid Pavement, A/C Code E(Main Gear Tire Size 46 x 17 R20 (46 x 16 - 20), inflated at 12.3 bar (178 psi)), for an aircraft grossweight of 55 000 kg (121 250 lb) and medium subgrade strength (code B), the ACN for the rigidpavement is 32.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref.: ICAO Aerodrome Design Manual Part 3, Chapter 1, Second Edition 1983).
7-9-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-1 Aircraft Classification Number - Flexible Pavement
**ON A/C A320-200
Aircraft Classification Number - Flexible Pavement
1. This section gives the Aircraft Classification Number - Flexible Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-9-1Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
E
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0870101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-087-A01
7-9-1Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
2 ba
r (1
48 p
si)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
E
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0880101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-088-A01
7-9-1Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
9.2
bar
(13
3 ps
i)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
E
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0890101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-089-A01
7-9-1Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
N_AC_070901_1_0900101_01_00
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
F
ALP
HA
FA
CT
OR
= 0
.9
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-090-A01
7-9-1Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
6 ba
r (1
54 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0910101_01_00
A/C
CO
DE
F
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-091-A01
7-9-1Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
ON
PA
VE
ME
NT
− A
/C C
OD
E F
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
9 ba
r (1
58 p
si)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
F
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0920101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-092-A01
7-9-1Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
9.6
bar
(13
9 ps
i)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
F
ALP
HA
FA
CT
OR
= 0
.9
ON
PA
VE
ME
NT
− A
/C C
OD
E F
N_AC_070901_1_0930101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-093-A01
7-9-1Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
G
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0940101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-094-A01
7-9-1Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
6 ba
r (1
54 p
si)
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
G
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0950101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-095-A01
7-9-1Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
G
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
9 ba
r (1
58 p
si)
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0960101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-096-A01
7-9-1Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
45 35 30 25 20 15 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
G
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 9
.6 b
ar (
139
psi)
ALP
HA
FA
CT
OR
= 0
.9
49 x
19−
20 T
IRE
S
N_AC_070901_1_0970101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-097-A01
7-9-1Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
A/C
CO
DE
H
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)
45 35 25 15
N_AC_070901_1_0980101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-098-A01
7-9-1Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
6 ba
r (1
54 p
si)
A/C
CO
DE
H
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
45 35 25 15
N_AC_070901_1_0990101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-099-A01
7-9-1Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
A/C
CO
DE
H
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
9 ba
r (1
58 p
si)
45 35 25 15
N_AC_070901_1_1000101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-100-A01
7-9-1Page 15
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
9.6
bar
(13
9 ps
i)
A/C
CO
DE
H
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
D −
CB
R
3 (U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
45 35 25 15
N_AC_070901_1_1010101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-101-A01
7-9-1Page 16
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
ALP
HA
FA
CT
OR
= 0
.9
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E I
− R
A/C
CO
DE
I −
R
N_AC_070901_1_1020101_01_01
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-102-A01
7-9-1Page 17
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
ALP
HA
FA
CT
OR
= 0
.9
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
7−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
I −
R
A/C
CO
DE
I −
R
N_AC_070901_1_1030101_01_01
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-103-A01
7-9-1Page 18
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
ALP
HA
FA
CT
OR
= 0
.9
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
I −
R
A/C
CO
DE
I −
R
N_AC_070901_1_1040101_01_01
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-104-A01
7-9-1Page 19
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
ALP
HA
FA
CT
OR
= 0
.9
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
9−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.3
bar
(149
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
I −
R
A/C
CO
DE
I −
R
N_AC_070901_1_1050101_01_01
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-105-A01
7-9-1Page 20
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
A/C
CO
DE
J−
K
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.95560
N_AC_070901_1_1060101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
J−
K
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-106-A01
7-9-1Page 21
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.95560
A/C
CO
DE
J−
K
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E J
−K
N_AC_070901_1_1070101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-107-A01
7-9-1Page 22
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.95560
A/C
CO
DE
J−
K
N_AC_070901_1_1080101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
8 ba
r (1
71 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E J
−K
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-108-A01
7-9-1Page 23
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.95560
A/C
CO
DE
J−
K
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
3 ba
r (1
49 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E J
−K
N_AC_070901_1_1090101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-109-A01
7-9-1Page 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
5560
A/C
CO
DE
L−
M
80
170
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_1100101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E L
−M
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-110-A01
7-9-1Page 25
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
75
9010
011
012
013
014
015
016
0
(x 1
000
lb)
5560
A/C
CO
DE
L−
M
80
170
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_1110101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
7−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
L−
M
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-111-A01
7-9-1Page 26
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
7065
6055
5045
4035
101520253035404550
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
75
9010
011
012
013
014
015
068
0
(x 1
000
lb)
5560
A/C
CO
DE
L−
M
80
720
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_1120101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
L−
M
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-112-A01
7-9-1Page 27
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
9−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.3
bar
(149
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
L−
M
60 40 35 30 20 15 10
3540
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
2555 50 45
4550
5560
6570
7580
C −
CB
R 6
(LO
W)
B −
CB
R 1
0 (M
ED
IUM
)A
− C
BR
15
(HIG
H)
D −
CB
R 3
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
L−
M
170
160
150
140
130
120
110
100
9080
N_AC_070901_1_1130101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-113-A01
7-9-1Page 28
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 40 35 30 20 15 10
3540
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
2555 50 45
4550
5560
6570
7580
A/C
CO
DE
N−
O
170
160
150
140
130
120
110
100
9080
N_AC_070901_1_1140101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
4 ba
r (2
09 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E N
−O
C −
CB
R 6
(LO
W)
B −
CB
R 1
0 (M
ED
IUM
)A
− C
BR
15
(HIG
H)
D −
CB
R 3
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-114-A01
7-9-1Page 29
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 40 35 30 20 15 10
3540
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
2555 50 45
4550
5560
6570
7580
A/C
CO
DE
N−
O
170
160
150
140
130
120
110
100
9080
N_AC_070901_1_1150101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
7−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2 ba
r (1
74 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E N
−O
C −
CB
R 6
(LO
W)
B −
CB
R 1
0 (M
ED
IUM
)A
− C
BR
15
(HIG
H)
D −
CB
R 3
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-115-A01
7-9-1Page 30
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 40 35 30 20 15 10
3540
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
2555 50 45
4550
5560
6570
7580
A/C
CO
DE
N−
O
170
160
150
140
130
120
110
100
9080
N_AC_070901_1_1160101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
N−
O
C −
CB
R 6
(LO
W)
B −
CB
R 1
0 (M
ED
IUM
)A
− C
BR
15
(HIG
H)
D −
CB
R 3
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-116-A01
7-9-1Page 31
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 40 35 30 20 15 10
3540
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
2555 50 45
4550
5560
6570
7580
A/C
CO
DE
N−
O
170
160
150
140
130
120
110
100
9080
N_AC_070901_1_1170101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
9−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.7
bar
(155
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
N−
O
C −
CB
R 6
(LO
W)
B −
CB
R 1
0 (M
ED
IUM
)A
− C
BR
15
(HIG
H)
D −
CB
R 3
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.9
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-117-A01
7-9-1Page 32
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 40 35 30 20 15 10
3540
2555 50 45
4550
5560
6570
7580
170
160
150
140
130
120
110
100
9080
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.8
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
4 ba
r (2
09 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E P
− Q
(x 1
000
lb)
ALP
HA
FA
CT
OR
= 0
.9
B −
CB
R 1
0 (M
ED
IUM
)A
− C
BR
15
(HIG
H)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)C
− C
BR
6
(LO
W)
A/C
CO
DE
P −
Q
N_AC_070901_1_1180101_01_01
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-118-A01
7-9-1Page 33
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
60 40 35 30 20 15 10
3540
2555 50 45
4550
5560
6570
7580
170
160
150
140
130
120
110
100
9080
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.8
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
P −
Q
(x 1
000
lb)
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
N_AC_070901_1_1200101_01_01
A/C
CO
DE
P −
Q
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-120-A01
7-9-1Page 34
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0
3540
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
40
4550
5560
6570
7580
170
160
150
140
130
120
110
100
9080
A/C
CO
DE
TT
35 30 25 20 15 10 5
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
915
x 30
0 R
16 (
36 x
11−
16)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.2
bar
(177
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
TT
C −
CB
R 6
(LO
W)
B −
CB
R 1
0 (M
ED
IUM
)A
− C
BR
15
(HIG
H)
D −
CB
R 3
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ALP
HA
FA
CT
OR
= 0
.8
N_AC_070901_1_1220101_01_01
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-122-A01
7-9-1Page 35
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-2 Aircraft Classification Number - Rigid Pavement
**ON A/C A320-200
Aircraft Classification Number - Rigid Pavement
1. This section gives the Aircraft Classification Number - Rigid Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-9-2Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.3
bar
(178
psi
)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
N_AC_070902_1_1280101_01_00
A/C
CO
DE
E
ON
PA
VE
ME
NT
− A
/C C
OD
E E
15253545
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-128-A01
7-9-2Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
2 ba
r (1
48 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
N_AC_070902_1_1290101_01_00
A/C
CO
DE
E
ON
PA
VE
ME
NT
− A
/C C
OD
E E
15253545S
UB
GR
AD
E S
TR
EN
GT
HD
− K
=
20 M
N/m
³ (
ULT
RA
LO
W)
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-129-A01
7-9-2Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
9.2
bar
(13
3 ps
i)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
N_AC_070902_1_1300101_01_00
A/C
CO
DE
E
ON
PA
VE
ME
NT
− A
/C C
OD
E E
15253545
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-130-A01
7-9-2Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
N_AC_070902_1_1310101_01_00
A/C
CO
DE
F
ON
PA
VE
ME
NT
− A
/C C
OD
E F
15253545
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-131-A01
7-9-2Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
6 ba
r (1
54 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1320101_01_00
A/C
CO
DE
F
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-132-A01
7-9-2Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
9 ba
r (1
58 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
A −
K =
150
MN
/m³
(H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
45 35 25 15
N_AC_070902_1_1330101_01_00
A/C
CO
DE
F
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-133-A01
7-9-2Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
9.6
bar
(13
9 ps
i)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1340101_01_00
A/C
CO
DE
F
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-134-A01
7-9-2Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1350101_01_00
A/C
CO
DE
G
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-135-A01
7-9-2Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
6 ba
r (1
54 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1360101_01_00
A/C
CO
DE
G
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-136-A01
7-9-2Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
9 ba
r (1
58 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1370101_01_00
A/C
CO
DE
G
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-137-A01
7-9-2Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
9.6
bar
(13
9 ps
i)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1380101_01_00
A/C
CO
DE
G
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-138-A01
7-9-2Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 20 1035
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1390101_01_00
A/C
CO
DE
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-139-A01
7-9-2Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 20 1035
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
6 ba
r (1
54 p
si)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
N_AC_070902_1_1400101_01_00
A/C
CO
DE
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-140-A01
7-9-2Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 20 1035
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
9 ba
r (1
58 p
si)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
SU
BG
RA
DE
ST
RE
NG
TH
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)45 35 25 15
A/C
CO
DE
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
N_AC_070902_1_1410101_01_00
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-141-A01
7-9-2Page 15
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 20 1035
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
9.6
bar
(13
9 ps
i)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
45 35 25 15
A/C
CO
DE
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
N_AC_070902_1_1420101_01_00
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-142-A01
7-9-2Page 16
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
A/C
CO
DE
I −
R
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H45 35 25 15
N_AC_070902_1_1430101_01_01
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E I
− R
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-143-A01
7-9-2Page 17
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
7−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H45 35 25 15
ON
PA
VE
ME
NT
− A
/C C
OD
E I
− R
A/C
CO
DE
I −
R
N_AC_070902_1_1440101_01_01
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-144-A01
7-9-2Page 18
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H45 35 25 15
A/C
CO
DE
I −
R
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
I −
R
N_AC_070902_1_1450101_01_01
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-145-A01
7-9-2Page 19
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
7075
160
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H45 35 25 15
A/C
CO
DE
I −
R
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1.42
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
9−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.3
bar
(149
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
I −
R
N_AC_070902_1_1460101_01_01
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-146-A01
7-9-2Page 20
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
(x 1
000
kg)
(x 1
000
lb)
4050
8090
100
110
120
130
140
150
4045
5055
6065
7075
160
60
A/C
CO
DE
J−
K
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
45 35 25 1555
N_AC_070902_1_1470101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
−K
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-147-A01
7-9-2Page 21
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
405080
9010
011
012
013
014
015
0
4045
5055
6065
70
A/C
CO
DE
J−
K
75
160
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H45 35 25 15
ON
PA
VE
ME
NT
− A
/C C
OD
E J
−K
N_AC_070902_1_1480101_01_00
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-148-A01
7-9-2Page 22
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
8 ba
r (1
71 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
4050
8090
100
110
120
130
140
150
4045
5055
6065
7075
160
60
A/C
CO
DE
J−
K
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
45 35 25 1555
N_AC_070902_1_1490101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
−K
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-149-A01
7-9-2Page 23
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
3 ba
r (1
49 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
4050
8090
100
110
120
130
140
150
4045
5055
6065
70
A/C
CO
DE
J−
K
75
160
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
60 45 35 25 1555
N_AC_070902_1_1500101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
−K
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-150-A01
7-9-2Page 24
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
4050
8090
100
110
120
130
140
150
4045
5055
6065
7075
160
6017
0
80
A/C
CO
DE
L−
M
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
45 35 25 1555
N_AC_070902_1_1510101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
−M
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-151-A01
7-9-2Page 25
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G49
x 1
7−20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
4050
8090
100
110
120
130
140
150
4045
5055
6065
7075
160
6017
0
80
A/C
CO
DE
L−
M
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
45 35 25 1555
N_AC_070902_1_1520101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
−M
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-152-A01
7-9-2Page 26
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.8
bar
(171
psi
)
30 20 1035
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
4050
8090
100
110
120
130
140
150
4045
5055
6065
7075
160
6017
0
80
A/C
CO
DE
L−
M
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
45 35 25 1555
N_AC_070902_1_1530101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
−M
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-153-A01
7-9-2Page 27
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.7
% M
AC
.
152025303540455055
3540
4550
5560
6570
7580
AIR
CR
AF
T G
RO
SS
WE
IGH
T
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
3 ba
r (1
49 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
L−
M
80
10
9010
011
012
013
014
015
016
017
060
N_AC_070902_1_1540101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
−M
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-154-A01
7-9-2Page 28
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.
152025303540455055
3540
4550
5560
6570
7580
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.4
bar
(209
psi
)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
N−
O
106080
9010
011
012
013
014
015
016
017
0
N_AC_070902_1_1550101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E N
−O
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-155-A01
7-9-2Page 29
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.
152025303540455055
3540
4550
5560
6570
7580
AIR
CR
AF
T G
RO
SS
WE
IGH
T
49 x
17−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12
bar
(174
psi
) (x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
N−
O
80
10
9010
011
012
013
014
015
016
017
060
N_AC_070902_1_1560101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E N
−O
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-156-A01
7-9-2Page 30
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.
152025303540455055
3540
4550
5560
6570
7580
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
3 ba
r (1
78 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
N−
O
80
10
9010
011
012
013
014
015
016
017
060
N_AC_070902_1_1570101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E N
−O
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-157-A01
7-9-2Page 31
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.
152025303540455055
3540
4550
5560
6570
7580
AIR
CR
AF
T G
RO
SS
WE
IGH
T
49 x
19−
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
7 ba
r (1
55 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
N−
O
80
10
9010
011
012
013
014
015
016
017
060
N_AC_070902_1_1580101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E N
−O
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-158-A01
7-9-2Page 32
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
152025303540455055
4045
5055
6065
7075
8010
9010
011
012
013
014
015
016
017
060
80
35
AIRCRAFT CLASSIFICATION NUMBER (ACN)
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
P −
Q
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.8
% M
AC
.S
EE
SE
CT
ION
7−
4−1
FIG
UR
E 1
246
x 1
7 R
20 T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
4 ba
r (2
09 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E P
− Q
N_AC_070902_1_1590101_01_01
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-159-A01
7-9-2Page 33
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
152025303540455055
4045
5055
6065
7075
8010
9010
011
012
013
014
015
016
017
060
80
35
AIRCRAFT CLASSIFICATION NUMBER (ACN)
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
P −
Q
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36.
8 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
3 ba
r (1
78 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E P
− Q
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
N_AC_070902_1_1610101_01_01
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-161-A01
7-9-2Page 34
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 4
0 %
MA
C.
15202530
3540
4550
5560
6570
7580
AIR
CR
AF
T G
RO
SS
WE
IGH
T
915
x 30
0 R
16 (
36 x
11−
16)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.2
bar
(177
psi
)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
80
10
9010
011
012
013
014
015
016
017
0
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
TT
5 0
N_AC_070902_1_1630101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E T
T
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-163-A01
7-9-2Page 35
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
**ON A/C A320-200
Scaled Drawings
1. This section provides the scaled drawings.
NOTE : When printing this drawing, make sure to adjust for proper scaling.
8-0-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
0 10 20 30 40 50FEET
0 5 10 15METERS
010
2030
4050
FE
ET
05
1015
ME
TE
RS
N_AC_080000_1_0030101_01_00
WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.NOTE:
Scaled DrawingFIGURE-8-0-0-991-003-A01
8-0-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A320-200
Aircraft Rescue and Fire Fighting
1. Aircraft Rescue and Fire Fighting ChartsThis sections gives data related to aircraft rescue and fire fighting.The figures contained in this section are the figures that are in the Aircraft Rescue and Fire FightingCharts poster available for download on AIRBUSWorld and the Airbus website.
10-0-0Page 1
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0010301_01_00
Front PageFIGURE-10-0-0-991-001-C01
10-0-0Page 2
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0020301_01_00
Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-002-C01
10-0-0Page 3
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0030101_01_00
Wheel Safety Area(Sheet 1 of 2)
FIGURE-10-0-0-991-003-A01
10-0-0Page 4
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0030102_01_00
Wheel Safety AreaRecommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-003-A01
10-0-0Page 5
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0040301_01_00
Composite MaterialsFIGURE-10-0-0-991-004-C01
10-0-0Page 6
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
A AB
B
N_AC_100000_1_0050101_01_00
LG Ground Lock Safety DevicesFIGURE-10-0-0-991-005-A01
10-0-0Page 7
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
C L
N_AC_100000_1_0060301_01_00
Evacuation/Escape Slide/RaftFIGURE-10-0-0-991-006-C01
10-0-0Page 8
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0070101_01_00
Pax/Crew DoorsFIGURE-10-0-0-991-007-A01
10-0-0Page 9
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0080301_01_00
Emergency Exit HatchFIGURE-10-0-0-991-008-C01
10-0-0Page 10
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
134A
R15
4AR
/
198C
B
N_AC_100000_1_0090101_01_00
FWD and AFT Lower Deck Cargo DoorsFIGURE-10-0-0-991-009-A01
10-0-0Page 11
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
FL
T IN
T
LIG
HT
TE
ST
CK
PT
CA
LL
RE
SE
T
AP
U S
HU
T O
FF
AP
U F
IRE
AD
IRU
&C
KP
T C
AL
LA
VN
CS
VE
NT
AV
AIL
NO
T IN
US
E
EL
T
108V
U
EX
T P
WR
ENG
MAS
TER
2M
ASTE
R 1
ON
OF
F
ON
OF
FM
OD
E
IGN
ENG 1
FIR
E
FA
ULT
FIR
E
FA
ULT
21
CR
AN
KS
TA
RT
ENG 2
NO
RM
A
D
RA
IN R
PL
NT
SL
OW
FA
ST
OF
FW
IPE
R
MA
IN S
TA
RT
12
EN
G
OV
RD
FA
UL
TA U T O
BLO
WE
R
OV
RD
FA
UL
TA U T O
EX
TR
AC
TV
EN
TIL
AT
ION
OF
F
CA
B F
AN
S
ON
ON
TE
ST
AF
T
DIS
CH
22V
U
HO
T
AF
T
CA
RG
O S
MO
KE
CO
LD
OF
F
FA
UL
T
HO
T A
IR
OF
F
FA
UL
T
AF
T IS
OL V
ALV
E
CA
RG
O
DIS
CH
SM
OK
E
FW
D
DIS
CH
DIS
CH
SM
OK
E
APU
SH
PU
SH
PU
SH
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
AG
EN
T 1
AG
EN
T 2
AG
EN
T 1
AG
EN
T 2
TE
ST
TE
ST
TE
ST
AG
EN
T
F I R E
F I R E
AP
UFI
RE
FIR
EEN
G2
FIR
EEN
G1
B
C E
ED
B C
FA
ULT
FA
ULT
OF
F
OF
F
OF
F
FA
ULT
OF
F
FA
ULT
OF
F
FA
ULT
OF
F
FA
ULT
OF
F
FA
ULT
ALT
N
FA
ULT
ON
AV
AIL
E L E CID
G 2
GE
N 2
DC
BU
S 2
AC
ES
S F
EE
D
EX
T P
WR
AP
U G
EN
GE
N 1
BA
T 2
BA
T2
1B
AT
1
AC
BU
S 1
DC
BU
S 1
CO
MM
ER
CIA
L
GA
LY &
CA
B
IDG
1
E L E C
BU
S T
IEA U T O
VV
35V
U
OF
F
A U T O
AC
BU
S 2
AC E
SS B
US
ON
FA
ULT
ON
FA
ULT
ON
FA
ULT
ON
FA
ULT
ON
AN
TI IC
EPR
OBE
/WIN
DO
WH
EAT
EN
G 1
EN
G 2
WIN
GM
AN
V/S
CTL
MO
DE
SE
LLD
G E
LEV
AU
TOD
ITC
HIN
GC
ABIN
PR
ESS
UP
ON
A U T O
A U T O
25V
U
ON
FA
ULT
ON
AV
AIL
INT
LT
SIG
NS
APU
STB
Y C
OM
PA
SS
AN
N L
TD
OM
ETE
ST
BR
T
DIM
OFFDIM
BR
T
OFF
SE
AT
BE
LTS
NO
SM
OK
ING
EM
ER
EX
IT L
T
A U T OO
FFO
FF
ON
ON
ON
AR
M
OFF
BRT
OFFOV
HD
INTE
G L
T
MA
STE
R S
W
STA
RT
WIN
GN
AV
& L
OG
OS
TRO
BE
BE
AC
ON
OFF
OFF
OFF
ON
ON
ON
OFF
EXT
LT
A U T O
RW
Y T
UR
N O
FFO
NO
N
OFF
OFF
OFF
RETR
ACT
LAN
DL
RN
OS
ET.
O
TAX
I
ON
OF
F
N_AC_100000_1_0120101_01_00
Control PanelsFIGURE-10-0-0-991-012-A01
10-0-0Page 12
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
316A
R
A
315A
L
A
N_AC_100000_1_0130101_01_00
APU Access DoorFIGURE-10-0-0-991-013-A01
10-0-0Page 13
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0140301_01_00
Aircraft Ground ClearancesFIGURE-10-0-0-991-014-C01
10-0-0Page 14
Jun 01/12
@A320AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_100000_1_0150101_01_00
Structural Break-in PointsFIGURE-10-0-0-991-015-A01
10-0-0Page 15
Jun 01/12