@AIRBUSA340-200/-300
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: Jul 30/92 Rev: Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 26 - Aug 01/19
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 6
Section 6-3
Subject 6-3-0
Danger Areas of Engines R NOTE AMENDED
HIGHLIGHTSPage 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 26 - Aug 01/19
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 1
Subject 1-1-0
Introduction Jan 01/17
Subject 1-2-1
Glossary Jan 01/17
CHAPTER 2
Subject 2-1-1
General Aircraft Characteristics Data Jan 01/14
Subject 2-2-0
General Aircraft Dimensions Jan 01/17
FIGURE General Aircraft Dimensions Jan 01/14
FIGURE General Aircraft Dimensions Jan 01/14
Subject 2-3-0
Ground Clearances Jan 01/17
FIGURE Ground Clearances Oct 01/15
FIGURE Ground Clearances Oct 01/15
FIGURE Ground Clearances - Ailerons -- Up Oct 01/15
FIGURE Ground Clearances - Ailerons -- Down Oct 01/15
FIGURE Ground Clearances - Spoilers -- Extended Oct 01/15
FIGURE Ground Clearances - Leading Edge Slats -- Extended Oct 01/15
FIGURE Ground Clearances - Trailing Edge Flaps -- Extended Oct 01/15
FIGURE Ground Clearances - Flap Tracks -- Extended Oct 01/15
FIGURE Ground Clearances - Flap Tracks -- Retracted Oct 01/15
FIGURE Ground Clearances - Flap Tracks -- 1 + F Oct 01/15
Subject 2-4-1
Interior Arrangements - Plan View Jan 01/17
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FIGURE Interior Arrangements - Plan View - Typical Configuration Jan 01/17
FIGURE Interior Arrangements - Plan View - Typical Configuration Jan 01/17
FIGURE Interior Arrangements - Plan View - Typical Configuration Jan 01/17
Subject 2-5-0
Interior Arrangements - Cross Section Jan 01/14
FIGURE Interior Arrangements - Cross Section - TypicalConfiguration
Jan 01/14
Subject 2-6-1
Lower Deck Cargo Compartments Oct 01/15
FIGURE Lower Deck Cargo Compartments - Location and Dimensions Jan 01/14
FIGURE Lower Deck Cargo Compartments - Loading Combinations Oct 01/15
FIGURE Lower Deck Cargo Compartments - Loading Combinations Oct 01/15
Subject 2-7-0
Door Clearances Oct 01/15
FIGURE Door Clearances - Door Identification Jul 01/18
FIGURE Door Clearances - Door Identification Jul 01/18
FIGURE Door Clearances - Forward Passenger/Crew Doors Oct 01/15
FIGURE Door Clearances - Mid Passenger/Crew Doors Oct 01/15
FIGURE Door Clearances - Emergency Exits Oct 01/15
FIGURE Door Clearances - Aft Passenger/Crew Doors Oct 01/15
FIGURE Door Clearances - Forward Cargo Compartment Door Oct 01/15
FIGURE Door Clearances - Aft Cargo Compartment Door Oct 01/15
FIGURE Door Clearances - Bulk Cargo Compartment Door Oct 01/15
FIGURE Door Clearances - Radome Oct 01/15
FIGURE Door Clearances - Main and Center Landing Gear Doors Oct 01/15
FIGURE Door Clearances - APU and Nose Landing Gear Doors Oct 01/15
FIGURE Door Clearances - APU and Nose Landing Gear Doors Oct 01/15
Subject 2-8-0
Escape Slides Oct 01/15
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FIGURE Escape Slides - Location Oct 01/15
FIGURE Escape Slides - Location Oct 01/15
Subject 2-9-0
Landing Gear Maintenance Pits Jan 01/14
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes Jan 01/14
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes Jan 01/14
Landing Gear Jan 01/17
FIGURE Main Landing Gear - General Jan 01/14
FIGURE Centerline Landing Gear - General Jan 01/14
FIGURE Nose Landing Gear - General Jan 01/14
FIGURE Tow Truck Power Jan 01/17
Subject 2-10-0
Exterior Lighting Jan 01/17
FIGURE Exterior Lighting Jan 01/14
FIGURE Exterior Lighting Jan 01/14
Subject 2-11-0
Antennas and Probes Location Jan 01/14
FIGURE Antennas and Probes - Location Jan 01/14
FIGURE Antennas and Probes - Location Jan 01/14
Subject 2-12-0
Engine and Nacelle Jan 01/14
FIGURE Engine and Nacelle - Engine Dimensions - CFM 56-5C Jan 01/14
FIGURE Engine and Nacelle - Nacelle Dimensions - CFM 56-5C Jan 01/14
FIGURE Engine and Nacelle - Fan Cowls - CFM 56-5C Jan 01/14
FIGURE Engine and Nacelle - Thrust Reverser Cowls - CFM 56-5C Jan 01/14
Subject 2-12-1
Auxiliary Power Unit Jan 01/14
FIGURE Auxiliary Power Unit - Access Doors Jan 01/14
Subject 2-13-0
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Leveling, Symmetry and Alignment Jan 01/14
FIGURE Location of Leveling Points Jan 01/14
FIGURE Location of Leveling Points Jan 01/14
Subject 2-14-0
Jacking for Maintenance Jan 01/17
FIGURE Jacking for Maintenance - Jacking Points Location Jan 01/14
FIGURE Jacking for Maintenance - Jacking Points Location Jan 01/14
FIGURE Jacking for Maintenance - Forward Jacking Point Jan 01/14
FIGURE Jacking for Maintenance - Wing Jacking Points Jan 01/14
FIGURE Jacking for Maintenance - Auxiliary Jacking Point - SafetyStay
Jan 01/14
FIGURE Jacking for Maintenance - Jacking Dimensions Jan 01/14
FIGURE Jacking for Maintenance - Jacking Dimensions Jan 01/14
FIGURE Jacking for Maintenance - Load at the Aircraft JackingPoints
Jan 01/14
FIGURE Jacking for Maintenance - Load at the Aircraft JackingPoints
Jan 01/14
Subject 2-14-1
Jacking of the Landing Gear Oct 01/15
FIGURE Jacking of the Landing Gear - MLG Jacking Point Heights Jul 01/18
FIGURE Jacking of the Landing Gear - Jacking of the NLG Oct 01/15
FIGURE Jacking of the Landing Gear - Jacking of the CLG Oct 01/15
FIGURE Jacking of the Landing Gear - MLG Jacking Point Loads Oct 01/15
FIGURE Jacking of the Landing Gear - MLG Jacking Point Loads Oct 01/15
FIGURE Jacking of the Landing Gear - NLG Jacking Point Loads Oct 01/15
FIGURE Jacking of the Landing Gear - NLG Jacking Point Loads Oct 01/15
FIGURE Jacking of the Landing Gear - CLG Jacking Point Loads Oct 01/15
FIGURE Jacking of the Landing Gear - CLG Jacking Point Loads Oct 01/15
Subject 2-14-2
Support of Aircraft Jan 01/14
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FIGURE Support of Aircraft - Location of Shoring Cradles Jan 01/14
FIGURE Support of Aircraft - Location of Shoring Cradles Jan 01/14
CHAPTER 3
Subject 3-1-0
General Information Oct 01/15
Subject 3-2-1
Payload / Range - ISA Conditions Oct 01/15
FIGURE Payload / Range - ISA Conditions - CFM56-5C2 engine Oct 01/15
FIGURE Payload / Range - ISA Conditions - CFM56-5C2 engine Oct 01/15
FIGURE Payload / Range - ISA Conditions - CFM56-5C3 engine Oct 01/15
FIGURE Payload / Range - ISA Conditions - CFM56-5C3 engine Oct 01/15
FIGURE Payload / Range - ISA Conditions - CFM56-5C4 engine Oct 01/15
FIGURE Payload / Range - ISA Conditions - CFM56-5C4 engine Oct 01/15
FIGURE Payload / Range - ISA Conditions - CFM56-5C4 engine Oct 01/15
Subject 3-3-1
Take-Off Weight Limitation - ISA Conditions Oct 01/15
FIGURE Take-Off Weight Limitation - ISA Conditions -- CFM56-5C2engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA Conditions -- CFM56-5C2engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA Conditions -- CFM56-5C3engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA Conditions -- CFM56-5C3engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA Conditions -- CFM56-5C4engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA Conditions -- CFM56-5C4engine
Oct 01/15
Subject 3-3-2
Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions Oct 01/15
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FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- CFM56-5C2 engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- CFM56-5C2 engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- CFM56-5C3 engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- CFM56-5C3 engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- CFM56-5C4 engine
Oct 01/15
FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- CFM56-5C4 engine
Oct 01/15
Subject 3-4-1
Landing Field Length - ISA Conditions Oct 01/15
FIGURE Landing Field Length - ISA Conditions -- CFM56-5C2 engine Oct 01/15
FIGURE Landing Field Length - ISA Conditions -- CFM56-5C2 engine Oct 01/15
FIGURE Landing Field Length - ISA Conditions -- CFM56-5C3 engine Oct 01/15
FIGURE Landing Field Length - ISA Conditions -- CFM56-5C3 engine Oct 01/15
FIGURE Landing Field Length - ISA Conditions -- CFM56-5C4 engine Oct 01/15
FIGURE Landing Field Length - ISA Conditions -- CFM56-5C4 engine Oct 01/15
Subject 3-5-0
Final Approach Speed Jan 01/14
CHAPTER 4
Subject 4-1-0
General Information Oct 01/15
Subject 4-2-0
Turning Radii Jan 01/17
FIGURE Turning Radii - (Sheet 1) Jan 01/14
FIGURE Turning Radii - (Sheet 2) Jan 01/14
FIGURE Turning Radii - (Sheet 2) Jan 01/14
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Subject 4-3-0
Minimum Turning Radii Jan 01/17
FIGURE Minimum Turning Radii Jan 01/14
FIGURE Minimum Turning Radii Jan 01/14
Subject 4-4-0
Visibility from Cockpit in Static Position Jul 01/19
FIGURE Visibility from Cockpit in Static Position Jul 01/19
FIGURE Binocular Visibility Through Windows from Captain EyePosition
Jan 01/14
Subject 4-5-0
Runway and Taxiway Turn Paths Jan 01/14
Subject 4-5-1
135˚ Turn - Runway to Taxiway Jan 01/14
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
Jan 01/14
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
Jan 01/14
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
Subject 4-5-2
90˚ Turn - Runway to Taxiway Jan 01/14
FIGURE 90˚ Turn - Runway to Taxiway - Judgement OversteeringMethod
Jan 01/14
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
FIGURE 90˚ Turn - Runway to Taxiway - Judgement OversteeringMethod
Jan 01/14
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
Subject 4-5-3
180˚ Turn on a Runway Jan 01/17
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FIGURE 180˚ Turn on a Runway Jan 01/14
FIGURE 180˚ Turn on a Runway Jan 01/14
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway Jan 01/14
FIGURE 135˚ Turn - Taxiway to Taxiway - JudgementalOversteering Method
Jan 01/14
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
FIGURE 135˚ Turn - Taxiway to Taxiway - JudgementalOversteering Method
Jan 01/14
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway Jan 01/14
FIGURE 90˚ Turn - Taxiway to Taxiway - Judgement OversteeringMethod
Jan 01/14
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
FIGURE 90˚ Turn - Taxiway to Taxiway - Judgement OversteeringMethod
Jan 01/14
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
Jan 01/14
Subject 4-6-0
Runway Holding Bay (Apron) Oct 01/15
FIGURE Runway Holding Bay (Apron) Oct 01/15
Subject 4-7-0
Minimum Line-Up Distance Corrections Jan 01/14
FIGURE Minimum Line-Up Distance Corrections - 90˚ Turn onRunway Entry
Jan 01/14
FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn onRunway Turn Pad
Jan 01/14
FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn onRunway Width
Jan 01/14
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Subject 4-8-0
Aircraft Mooring Oct 01/15
FIGURE Aircraft Mooring Oct 01/15
CHAPTER 5
Subject 5-1-0
Aircraft Servicing Arrangements Jan 01/14
Subject 5-1-1
Symbols Used on Servicing Diagrams Jan 01/14
Subject 5-1-2
Typical Ramp Layout - Open Apron Jan 01/17
FIGURE Typical Ramp Layout - Open Apron Jan 01/14
FIGURE Typical Ramp Layout - Open Apron Jan 01/14
Subject 5-1-3
Typical Ramp Layout - Gate Jan 01/17
FIGURE Typical Ramp Layout - Gate Jan 01/14
FIGURE Typical Ramp Layout - Gate Jan 01/14
Subject 5-2-0
Terminal Operations - Full Servicing Turn Round Time Oct 01/15
FIGURE Full Servicing Turn Round Time Chart Oct 01/15
Terminal Operations - Full Servicing Turn Round Time Oct 01/15
FIGURE Full Servicing Turn Round Time Chart Oct 01/15
Subject 5-3-0
Terminal Operations - Minimum Servicing Turn-Round Time Jan 01/14
FIGURE Minimum Servicing Turn-Round Time Jan 01/14
Terminal Operations - Minimum Servicing Turn-Round Time Jan 01/14
FIGURE Minimum Servicing Turn-Round Time Jan 01/14
Subject 5-4-1
Ground Service Connections Layout Oct 01/15
FIGURE Ground Service Connections Layout Oct 01/15
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Subject 5-4-2
Grounding (Earthing) Points Oct 01/15
FIGURE Ground Service Connections - Grounding (Earthing) Points Oct 01/15
FIGURE Ground Service Connections - Grounding (Earthing) Points Oct 01/15
Subject 5-4-3
Hydraulic Servicing Oct 01/15
FIGURE Ground Service Connections - Green System Ground ServicePanel
Jan 01/14
FIGURE Ground Service Connections - Blue System Ground ServicePanel
Jan 01/14
FIGURE Ground Service Connections - Yellow System Ground ServicePanel
Jan 01/14
FIGURE Ground Service Connections - RAT Oct 01/15
Subject 5-4-4
Electrical Servicing Jan 01/17
FIGURE Ground Service Connections - Electrical Service Panel Oct 01/15
Subject 5-4-5
Oxygen Servicing Jan 01/17
FIGURE Ground Service Connections - Oxygen Servicing Oct 01/15
Subject 5-4-6
Fuel System Jul 01/18
FIGURE Ground Service Connections - Refuel/Defuel Control Panel Oct 01/15
FIGURE Ground Service Connections - Refuel/Defuel Coupling Oct 01/15
FIGURE Ground Service Connections - Overpressure Protector andNACA Flame Arrestor - Wing
Oct 01/15
FIGURE Ground Service Connections - Overpressure Protector andNACA Flame Arrestor - Trim Tank
Oct 01/15
Subject 5-4-7
Pneumatic Servicing Jan 01/17
FIGURE Ground Service Connections - LP and HP GroundConnectors
Jan 01/14
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Subject 5-4-8
Oil Servicing Oct 01/15
FIGURE Ground Service Connections - Engine Oil Tank - CFM56-5C2Series Engine
Oct 01/15
FIGURE Ground Service Connections - IDG Oil Tank - CFM56-5C2Series Engine
Oct 01/15
FIGURE Ground Service Connections - Starter Oil Tank - CFM56-5C2Series Engine
Oct 01/15
APU Oil Servicing Oct 01/15
FIGURE Ground Service Connections - APU Oil Servicing Oct 01/15
Subject 5-4-9
Potable Water Servicing Oct 01/15
FIGURE Ground Service Connections - Potable-Water Ground ServicePanels
Oct 01/15
FIGURE Ground Service Connections - Potable-Water Tanks Location Oct 01/15
Potable Water Servicing Oct 01/15
FIGURE Ground Service Connections - Potable-Water Ground ServicePanels
Oct 01/15
FIGURE Ground Service Connections - Potable-Water Tanks Location Oct 01/15
Subject 5-4-10
Waste Water Servicing Oct 01/15
FIGURE Ground Service Connections - Waste Water Ground ServicePanel
Jan 01/14
FIGURE Ground Service Connections - Waste Tanks Location Oct 01/15
Subject 5-4-11
Cargo Control Panels Oct 01/15
FIGURE Forward Cargo Control Panels Oct 01/15
FIGURE Aft Cargo Control Panels Oct 01/15
Subject 5-5-0
Engine Starting Pneumatic Requirements Jan 01/14
FIGURE Example for Use of the Charts Jan 01/14
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FIGURE Engine Starting Pneumatic Requirements - CFM56-5C2Series
Jan 01/14
Subject 5-6-0
Ground Pneumatic Power Requirements Oct 01/15
FIGURE Ground Pneumatic Power Requirements - Heating Jan 01/14
FIGURE Ground Pneumatic Power Requirements - Cooling Jan 01/14
Subject 5-7-0
Preconditioned Airflow Requirements Oct 01/15
FIGURE Preconditioned Airflow Requirements Jan 01/14
Subject 5-8-0
Ground Towing Requirements Jul 01/18
FIGURE Ground Towing Requirements Jan 01/14
Subject 5-9-0
De-Icing and External Cleaning Jan 01/17
CHAPTER 6
Subject 6-1-0
Engine Exhaust Velocities and Temperatures Jul 01/18
Subject 6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power Jan 01/14
FIGURE Engine Exhaust Velocities - Ground Idle Power - CFM56-5Cseries engine
Jan 01/14
Subject 6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power Jan 01/14
FIGURE Engine Exhaust Temperatures - Ground Idle Power -CFM56-5C series engine
Jan 01/14
Subject 6-1-3
Engine Exhaust Velocities Contours - Breakaway Power Jan 01/14
FIGURE Engine Exhaust Velocities - Breakaway Power - CFM56-5Cseries engine
Jan 01/14
Subject 6-1-4
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Engine Exhaust Temperatures Contours - Breakaway Power Jan 01/14
FIGURE Engine Exhaust Temperatures - Breakaway Power -CFM56-5C series engine
Jan 01/14
Subject 6-1-5
Engine Exhaust Velocities Contours - Takeoff Power Jan 01/14
FIGURE Engine Exhaust Velocities - Takeoff Power - CFM56-5Cseries engine
Jan 01/14
Subject 6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power Jan 01/14
FIGURE Engine Exhaust Temperatures - Takeoff Power - CFM56-5Cseries engine
Jan 01/14
Subject 6-3-0
Danger Areas of Engines R Aug 01/19
Subject 6-3-1
Ground Idle Power Oct 01/15
FIGURE Danger Areas of Engines - CFM56-5C series engine Jan 01/14
Subject 6-3-2
Breakaway Power Oct 01/15
FIGURE Danger Areas of Engines - CFM56-5C series engine Jan 01/14
Subject 6-3-3
Takeoff Power Oct 01/15
FIGURE Danger Areas of Engines - CFM56-5C series engine Jan 01/14
Subject 6-4-0
APU Exhaust Velocities and Temperatures Jan 01/14
Subject 6-4-1
APU - GARRETT Jan 01/14
FIGURE Exhaust Velocities and Temperatures - GARRETT GTCP331-350
Jan 01/14
CHAPTER 7
Subject 7-1-0
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General Information Oct 01/15
Subject 7-2-0
Landing Gear Footprint Oct 01/15
FIGURE Landing Gear Footprint Jan 01/14
FIGURE Landing Gear Footprint Jan 01/14
Subject 7-3-0
Maximum Pavement Loads Oct 01/15
FIGURE Maximum Pavement Loads Jan 01/14
FIGURE Maximum Pavement Loads Jan 01/14
Subject 7-4-0
Landing Gear Loading on Pavement Oct 01/15
FIGURE Landing Gear Loading on Pavement - WV000, MRW 254400 kg, CG 37.7%
Jan 01/14
FIGURE Landing Gear Loading on Pavement - WV021, MRW 275900 kg, CG 37%
Jan 01/14
FIGURE Landing Gear Loading on Pavement - WV000, MRW 254400 kg, CG 38.18%
Jan 01/14
FIGURE Landing Gear Loading on Pavement - WV028, MRW 277400 kg, CG 35%
Jan 01/14
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method
Jan 01/17
FIGURE Flexible Pavement Requirements - WV000, MRW 254 400kg, CG 37.7%
Jan 01/17
FIGURE Flexible Pavement Requirements - WV000, MRW 254 400kg, CG 38.18%
Jan 01/17
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion Oct 01/15
Subject 7-7-0
Rigid Pavement Requirements - Portland Cement Association DesignMethod
Oct 01/15
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FIGURE Rigid Pavement Requirements - WV000, MRW 254 400 kg,CG 37.7%
Jan 01/17
FIGURE Rigid Pavement Requirements - WV000, MRW 254 400 kg,CG 38.18%
Jan 01/17
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion Oct 01/15
Subject 7-9-0
Aircraft Classification Number - Flexible and Rigid Pavements Jan 01/17
FIGURE Aircraft Classification Number - ACN Table Jan 01/14
FIGURE Aircraft Classification Number - Flexible Pavement - WV000,MRW 254 400 kg, CG 37.7%
Jan 01/17
FIGURE Aircraft Classification Number - Flexible Pavement - WV021,MRW 275 900 kg, CG 37%
Jan 01/17
FIGURE Aircraft Classification Number - ACN Table Jan 01/14
FIGURE Aircraft Classification Number - Flexible Pavement - WV000,MRW 254 400 kg, CG 38.18%
Jan 01/17
FIGURE Aircraft Classification Number - Flexible Pavement - WV028,MRW 277 400 kg, CG 35%
Jan 01/17
CHAPTER 8
Subject 8-0-0
Scaled Drawings Jan 01/14
FIGURE Scaled Drawing Jan 01/17
FIGURE Scaled Drawing Jan 01/17
CHAPTER 10
Subject 10-0-0
Aircraft Rescue and Fire Fighting Oct 01/15
FIGURE Front Page Jan 01/17
FIGURE Highly Flammable and Hazardous Materials and Components Oct 01/15
FIGURE Batteries Location and Access Oct 01/15
FIGURE Crew Rest Compartments Location Jan 01/14
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FIGURE Wheel/Brake Overheat - Wheel Safety Area Jan 01/14
FIGURE Composite Materials Location Jan 01/17
FIGURE Ground Lock Safety Devices Jan 01/14
FIGURE Emergency Evacuation Devices Oct 01/15
FIGURE Pax/Crew Doors and Emergency Exits Jan 01/14
FIGURE FWD and AFT Lower Deck Cargo Doors Jan 01/14
FIGURE Control Panels Jan 01/14
FIGURE APU Compartment Access Jan 01/14
FIGURE Ground Clearances Oct 01/15
FIGURE Structural Break-in Points Jan 01/14
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TABLE OF CONTENTS
1 SCOPE
1-1-0 Purpose
1-2-1 Glossary
2 AIRCRAFT DESCRIPTION
2-1-1 General Aircraft Characteristics Data
2-2-0 General Aircraft Dimensions
2-3-0 Ground Clearances
2-4-1 Interior Arrangements - Plan View
2-5-0 Interior Arrangements - Cross Section
2-6-1 Lower Deck Cargo Compartments
2-7-0 Door Clearances
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 Engine and Nacelle
2-12-1 Auxiliary Power Unit
2-13-0 Levelling, symmetry and Alignment
2-14-0 Jacking for Maintenance
2-14-1 Jacking of the Landing Gear
2-14-2 Support of Aircraft
3 AIRCRAFT PERFORMANCE
3-1-0 General Information
3-2-1 Payload / Range - ISA Conditions
3-3-1 Take-Off Weight Limitation - ISA Conditions
3-3-2 Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
3-4-1 Landing Field Length - 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
T.O.C.Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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)
4-7-0 Minimum Line-Up Distance Corrections
4-8-0 Aircraft Mooring
5 TERMINAL SERVICING
5-1-0 Aircraft 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 Operations - Transit
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 Oil System
5-4-9 Potable Water System
5-4-10 Waste Water System
5-4-11 Cargo Control Panels
5-5-0 Engine Starting Pneumatic Requirements
5-6-0 Ground Pneumatic Power Requirements
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
T.O.C.Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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
6-3-0 Danger Areas of Engines
6-3-1 Ground Idle Power
6-3-2 Breakaway Power
6-3-3 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
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-6-0 Flexible Pavement Requirements - LCN Conversion
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-0 Rigid Pavement Requirements - LCN Conversion
7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements
8 SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
10 AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
T.O.C.Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0 Purpose
**ON A/C A340-200 A340-300
Introduction
1. GeneralThe A340-200/-300 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCEPLANNING (AC) manual is issued for the A340-200 and A340-300 basic versions to providenecessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO) for airportand maintenance facilities planning.
This document is not customized and must not be used for training purposes.
The A340 is part of an integrated family sharing the same modern technology as the A330 andmaintaining the commonality that is integrated into the Airbus Fly-by-Wire family. It has undergonea program of continuous improvement and still delivers the value that airline customers expect, as theA340 has over 50 customers and operators with more than 350 A340s flying to over 150 airportsevery week.
The different models of the A340 family can carry from 250 to 440 passengers and are operating onsome of the world’s longest routes.
A stand-out benefit of the four-engine A340 is that it does not require any ETOPS certification. Thisallows quick start-up of long-haul operations. It also has good ’hot and high’ capability at airportsthat would be off-limits to other aircraft.
The A340 has one of the quietest and most comfortable cabins in the sky, with state-of-the-art LED(Light Emitting Diode) lighting, mood styles of lighting and AVOD IFE systems.
The A340 combines good capability, economics and passenger product in one package.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services1, Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1-2-1 Glossary
**ON A/C A340-200 A340-300
Glossary
1. List of Abbreviations
A/C Aircraft
ACN Aircraft Classification NumberAMM Aircraft Maintenance ManualAPU Auxiliary Power Unit
B/C Business Class
C/L Center Line
CBR California Bearing Ratio
CC Cargo Compartment
CG Center of Gravity
CKPT Cockpit
CLG Centerline Landing Gear
E Young’s Modulus
ELEC Electric, Electrical, Electricity
ESWL Equivalent Single Wheel Load
F/C First Class
FAA Federal Aviation AdministrationFDL Fuselage Datum Line
FR FrameFSTE Full Size Trolley Equivalent
FWD ForwardGPU Ground Power UnitGSE Ground Support Equipment
HYD Hydraulic
ICAO International Civil Aviation Organisation
IDG Integrated Drive Generator
ISA International Standard Atmosphere
L Radius of relative stiffnessLCN Load Classification NumberLD Load DeviceLD Lower DeckL/G Landing Gear
LH Left HandLPS Last Pax Seating
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
MAC Mean Aerodynamic Chord
MAX MaximumMD Main DeckMIN MinimumMLG Main Landing Gear
NLG Nose Landing Gear
OAT Outside Air Temperature
PAX Passenger
PB/D Passenger Boarding/Deboarding
PBB Passenger Boarding Bridge
PCA Portland Cement AssociationPCN Pavement Classification NumberPRM Passenger with Reduced Mobility
RH Right Hand
ULD Unit Load DeviceUS United StatesWV Weight Variant
Y/C Economy Class
2. Design Weight Terminology- Maximum Design Ramp Weight (MRW):
Maximum weight for ground maneuver (including weight of taxi and run-up fuel) as limited byaircraft strength and airworthiness requirements. It is also called Maximum Design Taxi Weight(MTW).
- Maximum Design Landing Weight (MLW):Maximum weight for landing as limited by aircraft strength and airworthiness requirements.
- Maximum Design Take-Off Weight (MTOW):Maximum weight for take-off as limited by aircraft strength and airworthiness requirements. (Thisis the maximum weight at start of the take-off run).
- Maximum Design Zero Fuel Weight (MZFW):Maximum permissible weight of the aircraft without usable fuel.
- Maximum Seating Capacity:Maximum number of passengers specifically certified or anticipated for certification.
- Usable Volume:Usable volume available for cargo, pressurized fuselage, passenger compartment and cockpit.
- Water Volume:Maximum volume of cargo compartment.
- Usable Fuel:Fuel available for aircraft propulsion.
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-1 General Aircraft Characteristics Data
**ON A/C A340-200 A340-300
General Aircraft Characteristics Data
**ON A/C A340-300
1. The following table provides characteristics of A340-300 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004
Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)
254 400 kg(560 856 lb)
257 900 kg(568 572 lb)
260 900 kg(575 186 lb)
257 900 kg(568 572 lb)
260 900 kg(575 186 lb)
Maximum Take-Off Weight(MTOW)
253 500 kg(558 872 lb)
257 000 kg(566 588 lb)
260 000 kg(573 202 lb)
257 000 kg(566 588 lb)
260 000 kg(573 202 lb)
Maximum Landing Weight(MLW)
186 000 kg(410 060 lb)
186 000 kg(410 060 lb)
186 000 kg(410 060 lb)
188 000 kg(414 469 lb)
188 000 kg(414 469 lb)
Maximum Zero Fuel Weight(MZFW)
174 000 kg(383 604 lb)
174 000 kg(383 604 lb)
174 000 kg(383 604 lb)
178 000 kg(392 423 lb)
178 000 kg(392 423 lb)
Aircraft CharacteristicsWV020 WV021 WV023 WV024 WV025
Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)
271 900 kg(599 437 lb)
275 900 kg(608 255 lb)
262 900 kg(579 595 lb)
275 900 kg(608 255 lb)
260 900 kg(575 186 lb)
Maximum Take-Off Weight(MTOW)
271 000 kg(597 453 lb)
275 000 kg(606 271 lb)
262 000 kg(577 611 lb)
275 000 kg(606 271 lb)
260 000 kg(573 202 lb)
Maximum Landing Weight(MLW)
190 000 kg(418 878 lb)
190 000 kg(418 878 lb)
190 000 kg(418 878 lb)
192 000 kg(423 287 lb)
190 000 kg(418 878 lb)
Maximum Zero Fuel Weight(MZFW)
178 000 kg(392 423 lb)
178 000 kg(392 423 lb)
178 000 kg(392 423 lb)
180 000 kg(396 832 lb)
178 000 kg(392 423 lb)
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Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsWV026 WV027 WV028 WV029
Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)
275 900 kg(608 255 lb)
271 900 kg(599 437 lb)
277 400 kg(611 562 lb)
260 900 kg(575 186 lb)
Maximum Take-Off Weight(MTOW)
275 000 kg(606 271 lb)
271 000 kg(597 453 lb)
276 500 kg(609 578 lb)
260 000 kg(573 202 lb)
Maximum Landing Weight(MLW)
192 000 kg(423 287 lb)
192 000 kg(423 287 lb)
190 000 kg(418 878 lb)
188 000 kg(414 469 lb)
Maximum Zero Fuel Weight(MZFW)
181 000 kg(399 037 lb)
178 000 kg(392 423 lb)
178 000 kg(392 423 lb)
178 000 kg(392 423 lb)
Aircraft CharacteristicsWV050 WV051 WV052 WV053 WV054
Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)
275 900 kg(608 255 lb)
275 900 kg(608 255 lb)
277 400 kg(611 562 lb)
277 400 kg(611 562 lb)
275 900 kg(608 255 lb)
Maximum Take-Off Weight(MTOW)
275 000 kg(606 271 lb)
275 000 kg(606 271 lb)
276 500 kg(609 578 lb)
276 500 kg(609 578 lb)
275 000 kg(606 271 lb)
Maximum Landing Weight(MLW)
192 000 kg(423 287 lb)
192 000 kg(423 287 lb)
192 000 kg(423 287 lb)
192 000 kg(423 287 lb)
192 000 kg(423 287 lb)
Maximum Zero Fuel Weight(MZFW)
180 000 kg(396 832 lb)
181 000 kg(399 037 lb)
181 000 kg(399 037 lb)
183 000 kg(403 446 lb)
183 000 kg(403 446 lb)
2. The following table provides characteristics of A340-300 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard Seating Capacity 335
140 640 l(37 153 US gal)Usable Fuel Capacity
(density = 0.785 kg/l) 110 402 kg(243 395 lb)
Pressurized Fuselage Volume(A/C non equipped)
1 056 m3
(37 292 ft3)
Passenger CompartmentVolume
372 m3
(13 137 ft3)
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics
Cockpit Volume12 m3
(424 ft3)
Usable Volume, FWD CC(Based on LD3)
78 m3
(2 754 ft3)
Usable Volume, AFT CC(Based on LD3)
60.7 m3
(2 142 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC107 m3
(3 789 ft3)
Water Volume, AFT CC85.7 m3
(3 026 ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
**ON A/C A340-200
3. The following table provides characteristics of A340-200 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002 WV021
Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)
254 400 kg(560 856 lb)
257 900 kg(568 572 lb)
260 900 kg(575 186 lb)
275 900 kg(608 255 lb)
Maximum Take-Off Weight(MTOW)
253 500 kg(558 872 lb)
257 000 kg(566 588 lb)
260 000 kg(573 202 lb)
275 000 kg(606 271 lb)
Maximum Landing Weight(MLW)
181 000 kg(399 037 lb)
181 000 kg(399 037 lb)
181 000 kg(399 037 lb)
185 000 kg(407 855 lb)
Maximum Zero Fuel Weight(MZFW)
169 000 kg(372 581 lb)
169 000 kg(372 581 lb)
169 000 kg(372 581 lb)
173 000 kg(381 400 lb)
4. The following table provides characteristics of A340-200 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard Seating Capacity 303
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft Characteristics140 640 l
(37 153 US gal)Usable Fuel Capacity(density = 0.785 kg/l) 110 402 kg
(243 395 lb)
Pressurized Fuselage Volume(A/C non equipped)
946 m3
(33 408 ft3)
Passenger CompartmentVolume
345 m3
(12 184 ft3)
Cockpit Volume12 m3
(424 ft3)
Usable Volume, FWD CC(Based on LD3)
60.7 m3
(2 142 ft3)
Usable Volume, AFT CC(Based on LD3)
52 m3
(1 836 ft3)
Usable Volume, Bulk CC19.7 m3
(695 ft3)
Water Volume, FWD CC84.6 m3
(2 988 ft3)
Water Volume, AFT CC71.1 m3
(2 511 ft3)
Water Volume, Bulk CC22.7 m3
(802 ft3)
2-1-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0 General Aircraft Dimensions
**ON A/C A340-200 A340-300
General Aircraft Dimensions
1. This section provides general aircraft dimensions.
2-2-0Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
(126.44 ft)38.54 m
(3.18 ft)0.97 m
(35.04 ft)10.68 m
(41.37 ft)12.61 m
(61.48 ft)18.74 m
(2.33 ft)0.71 m
(197.83 ft)60.3 m
(63.65 ft)19.4 m
(26.71 ft)8.14 m
(25.52 ft)7.78 m
(171.98 ft)52.42 m
(206.17 ft)62.84 m
(208.86 ft)63.66 m
(21.88 ft)6.67 m
(105.15 ft)32.05 m − MLG
(108.4 ft)33.04 m − CLG
(18.5 ft)5.64 m
(27.23 ft)8.3 m
(10.17 ft)3.1 m
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. F_AC_020200_1_0070101_01_02
General Aircraft Dimensions(Sheet 1 of 2)
FIGURE-2-2-0-991-007-A01
2-2-0Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
(73.46 ft)22.39 m
(95.01 ft)28.96 m
(138.52 ft)42.22 m
(128.28 ft)39.1 m
(202.33 ft)61.67 m
(208.96 ft)63.69 m
(34.45 ft)10.5 m
(8.2 ft)2.5 m
(6.63 ft)2.02 m
(21.1 ft)6.43 m
(35.7 ft)10.88 m
7.46 m
(46.
62 ft
)14
.21
m
(57.
91 ft
)17
.65
m
(24.48 ft)
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
F_AC_020200_1_0070102_01_00
General Aircraft Dimensions(Sheet 2 of 2)
FIGURE-2-2-0-991-007-A01
2-2-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
(3.18 ft)0.97 m
(35.04 ft)10.68 m
(41.37 ft)12.61 m
(61.48 ft)18.74 m
(128.61 ft)39.2 m
(2.33 ft)0.71 m
(197.83 ft)60.3 m
(63.65 ft)19.4 m
(26.7 ft)8.14 m
(25.59 ft)7.8 m
(157.97 ft)48.15 m
(192.16 ft)58.57 m
(194.85 ft)59.39 m
(21.88 ft)6.67 m
(98.13 ft)29.91 m − MLG
(101.41 ft)30.91 m − CLG
(27.23 ft)8.3 m
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
(10.17 ft)3.1 m
(18.5 ft)5.64 m
F_AC_020200_1_0080101_01_02
General Aircraft Dimensions(Sheet 1 of 2)
FIGURE-2-2-0-991-008-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.
(66.44 ft)20.25 m
(88.02 ft)26.83 m
(132.22 ft)40.3 m
(121.29 ft)36.97 m
(188.32 ft)57.4 m
(194.95 ft)59.42 m
(34.45 ft)10.5 m
(8.43 ft)2.57 m
(6.63 ft)2.02 m
(21.1 ft)6.43 m
(35.7 ft)10.88 m
7.46 m(24.48 ft)
(57.
91 ft
)17
.65
m
(46.
62 ft
)14
.21
m
F_AC_020200_1_0080102_01_00
General Aircraft Dimensions(Sheet 2 of 2)
FIGURE-2-2-0-991-008-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0 Ground Clearances
**ON A/C A340-200 A340-300
Ground Clearances
1. This section provides the height of various points of the aircraft, above the ground, for differentaircraft configurations.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,- An aircraft at Maximum Ramp Weight with a FWD CG and an AFT CG,- Aircraft on jacks, FDL at 6.50 m (21.33 ft).
NOTE : Passenger and cargo door ground clearances are measured from the center of the door silland from floor level.
2-3-0Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
CP D1 D2N1 N2
D3 W2 W1 D4 AP
VTF5
C3 C2 F3BF
F2F4
C1 F1HT
ENGINE/NACELLE
FUSELAGE
D1D2D3D4C1C2C3F1F2F3F4F5BFCPW1W2HTAPVTN1N2
4.454.725.145.492.583.273.431.842.062.457.548.301.825.237.556.008.047.1916.881.252.35
14.5915.5016.8618.018.4610.7311.256.036.758.0324.7327.235.97
17.1524.7619.6826.3723.5855.364.107.70
4.604.795.105.362.713.183.321.982.132.397.668.181.835.417.485.947.836.98
16.671.282.35
15.0915.7116.7317.588.8810.4310.896.496.987.83
25.1226.836.0017.7424.5419.4825.6822.8954.684.207.70
4.594.845.315.702.733.443.582.132.272.377.768.422.02
7.916.358.147.3016.991.422.59
15.0515.8717.4218.698.9511.2811.746.987.447.7725.4527.626.62
25.9420.8326.7023.9455.724.658.49
6.326.326.326.534.144.244.393.683.683.689.329.323.267.108.967.559.238.1017.622.793.98
20.7320.7320.7321.4213.5813.9114.4012.0712.0712.0730.5830.5810.7023.3029.4024.7730.2826.5757.819.15
13.06
WINGS
TAILPLANE
DOORS
A/C CONFIGURATIONMRW
FWD CG AFT CGm ft m ft
MID CGm ft m ft
125 000 kg(275 578 lb) A/C JACKED
FDL = 6.50 m (21.33 ft)
NOTE:PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROMTHE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
F_AC_020300_1_0050101_01_03
Ground ClearancesFIGURE-2-3-0-991-005-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
ENGINE/NACELLE
FUSELAGE
D1D2D3D4C1C2C3F1F2F3F4F5BFCPW1W2HTAPVTN1N2
4.444.715.135.492.583.413.411.832.082.467.548.291.865.217.576.018.057.2016.901.222.34
14.5615.4516.8318.018.4611.1811.186.006.828.0624.7327.196.10
17.0924.8319.7126.4123.6155.434.007.67
4.564.775.105.382.683.183.331.952.132.417.648.191.855.367.505.967.887.02
16.721.262.34
14.9515.6516.7317.648.7910.4310.926.406.987.90
25.0626.866.0717.5824.6019.5525.8423.0254.854.137.67
4.584.865.325.702.733.453.582.142.262.667.788.432.02
7.956.378.187.3317.031.412.60
15.0215.9417.4518.698.9511.3111.747.027.418.7225.5227.656.62
26.0820.8926.8324.0455.864.628.53
6.326.326.326.534.144.244.393.683.683.689.329.323.267.108.967.559.238.1017.622.793.98
20.7320.7320.7321.4213.5813.9114.4012.0712.0712.0730.5830.5810.7023.3029.4024.7730.2826.5757.819.15
13.06
WINGS
TAILPLANE
DOORS
A/C CONFIGURATIONMRW
FWD CG AFT CGm ft m ft
MID CGm ft m ft
124 000 kg(273 373 lb) A/C JACKED
FDL = 6.50 m (21.33 ft)
NOTE:PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASURED FROMTHE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
CP D1 D2N1 N2
D3 W2 W1 D4 AP
VT C3 C2 F3BF
F2F4
C1 F1HTF5
F_AC_020300_1_0050201_01_01
Ground ClearancesFIGURE-2-3-0-991-005-B01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
20.616.28 5.99 19.65 5.95 19.52
21.206.46 6.15 20.18 6.10 20.02
21.976.70 6.36 20.86 6.30 20.68
m ft m ft m ft
A
B
AILERONS UP
MRWAFT CG
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CGDESCRIPTION
AILERON 1/2
AILERON 1 INBD
CAILERON 2 OUTBD
ABC
F_AC_020300_1_0080101_01_03
Ground ClearancesAilerons -- Up
FIGURE-2-3-0-991-008-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
17.615.37 5.08 16.65 5.04 16.52
18.725.71 5.40 17.70 5.35 17.55
20.166.15 5.80 19.04 5.75 18.86
m ft m ft m ft
A
B
AILERONS DOWN
MRWAFT CG
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CGDESCRIPTION
AILERON 1/2
AILERON 1 INBD
CAILERON 2 OUTBD
AC B
F_AC_020300_1_0100101_01_03
Ground ClearancesAilerons -- Down
FIGURE-2-3-0-991-010-A01
2-3-0Page 5
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
19.956.08 5.85 19.19 5.82 19.11
20.456.23 5.98 19.64 5.96 19.55
20.896.37 6.10 20.02 6.07 19.92
21.346.50 6.22 20.42 6.19 20.32
15.604.75 4.56 14.97 4.55 14.91
17.385.30 5.09 16.69 5.07 16.63
18.705.70 5.49 18.01 5.47 17.95
19.365.90 5.68 18.64 5.66 18.58
m ft m ft m ft
B
C
SPOILERS EXTENDED
D
E
F
G
A
MRWAFT CG
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
SPOILER 1 OUTBD
SPOILER 2 INBD
SPOILER 2/3
SPOILER 3/4
SPOILER 4/5
SPOILER 6 OUTBD
SPOILER 1 INBD
DESCRIPTION
H
SPOILER 5/6
ABCDEFGH
F_AC_020300_1_0110101_01_03
Ground ClearancesSpoilers -- Extended
FIGURE-2-3-0-991-011-A01
2-3-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
m ft m ft m ft
A
B
C
MRWAFT CG
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CGDESCRIPTION
SLAT 1 INBD
SLAT 1 OUTBD
SLAT 2 INBD
11.32
13.98
14.01
3.45
4.26
4.27
3.26
4.05
4.08
10.70
13.29
13.39
3.28
4.06
4.09
10.76
13.32
13.42
LEADING EDGE SLATS EXTENDED
DSLAT 2/3 15.194.63 4.43 14.53 4.43 14.53
ESLAT 3/4 16.244.95 4.73 15.52 4.72 15.49
FSLAT 4 OUTBD 17.195.24 5.00 16.40 4.98 16.34
GSLAT 5 INBD 17.395.30 5.06 16.60 5.03 16.50
HSLAT 5/6 18.275.57 5.30 17.39 5.27 17.29
JSLAT 6/7 19.135.83 5.53 18.14 5.49 18.01
KSLAT 7 OUTBD 19.886.06 5.73 18.80 5.68 18.64
D E F G H J KCA B
F_AC_020300_1_0210101_01_01
Ground ClearancesLeading Edge Slats -- Extended
FIGURE-2-3-0-991-021-A01
2-3-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
m ft m ft m ft
MRWAFT CG
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CGDESCRIPTION
AFLAP 1 INBD 8.862.70 2.50 8.22 2.48 8.14
BFLAP 1 OUTBD 13.083.99 3.77 12.38 3.75 12.30
CFLAP 2 INBD 13.053.98 3.76 12.34 3.74 12.26
DFLAP 2 OUTBD 16.765.11 4.82 15.81 4.78 15.67
FLAPS EXTENDED
AD BC
F_AC_020300_1_0220101_01_01
Ground ClearancesTrailing Edge Flaps -- Extended
FIGURE-2-3-0-991-022-A01
2-3-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
m ft m ft m ft
MRWAFT CG
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CGDESCRIPTION
FLAP TRACKS EXTENDED
AFLAP TRACK 2 9.582.92 2.73 8.95 2.70 8.86
BFLAP TRACK 3 11.293.44 3.25 10.66 3.22 10.55
CFLAP TRACK 4 12.013.66 3.47 11.38 3.43 11.26
DFLAP TRACK 5 13.073.98 3.79 12.44 3.75 12.30
AD BC
F_AC_020300_1_0230101_01_01
Ground ClearancesFlap Tracks -- Extended
FIGURE-2-3-0-991-023-A01
2-3-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
AIRCRAFTTYPE
A340−300
A340−200
m ft m ft m ft
A
B
C
MRWAFT CG
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CGDESCRIPTION
FLAP TRACK 2
FLAP TRACK 3
FLAP TRACK 4
12.63
14.14
15.05
3.85
4.31
4.59
3.66
4.12
4.37
12.01
13.51
14.33
3.64
4.10
4.33
11.94
13.45
14.20
FLAP TRACKS RETRACTED
DFLAP TRACK 5 16.074.90 4.66 15.28 4.61 15.12
12.663.86 3.66 12.01 3.64 11.94
14.204.33 4.11 13.48 4.10 13.45
15.094.60 4.37 14.33 4.34 14.23
16.174.93 4.66 15.28 4.62 15.15
FLAP TRACK 2
FLAP TRACK 3
FLAP TRACK 4
FLAP TRACK 5
A
B
C
D
ABCD
F_AC_020300_1_0300101_01_00
Ground ClearancesFlap Tracks -- Retracted
FIGURE-2-3-0-991-030-A01
2-3-0Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
m ft m ft m ft
A
B
C
MRWFWD CG
A/C IN MAINTENANCECONFIGURATION
MID CGDESCRIPTION
FLAP TRACK 2
FLAP TRACK 3
FLAP TRACK 4
FLAP TRACK 5
FLAP TRACK 2
FLAP TRACK 3
FLAP TRACK 4
FLAP TRACK 5
11.42
12.93
13.84
3.48
3.94
4.22
3.29
3.75
4.00
10.79
12.30
13.12
FLAP TRACKS 1+F
MRWAFT CG
D 14.864.53 4.29 14.07
AIRCRAFTTYPE
A340−300
A
B
C
11.48
13.06
13.29
3.50
3.98
4.05
3.30
3.76
3.82
10.83
12.34
12.53
3.27
3.73
3.97
10.73
12.24
13.02
D 14.834.52 4.25 13.94 4.25 13.94
A340−200
3.27
3.73
3.96
10.73
12.24
12.99
4.24 13.91
AD BC
F_AC_020300_1_0330101_01_00
Ground ClearancesFlap Tracks -- 1 + F
FIGURE-2-3-0-991-033-A01
2-3-0Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1 Interior Arrangements - Plan View
**ON A/C A340-200 A340-300
Interior Arrangements - Plan View
1. This section provides the typical interior configuration.
2-4-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
305 ECONOMY CLASS SEATS
ATTENDANT SEATS 9
GALLEYS 6
LAVATORIES 8
STOWAGES 3
PASSENGER SEATS (335 TOTAL)
30 FIRST CLASS SEATS
ATTENDANT SEATSTOWAGEGALLEYSTOWAGE
GALLEYSTOWAGE
AFT PASSENGER/AFT PASSENGER/CREW DOOR 4 RH CREW DOOR 4 LH
LAVATORYLAVATORY
ATTENDANT SEAT ATTENDANT SEAT
ATTENDANT SEATATTENDANT SEAT
LAVATORYLAVATORY
GALLEY
GALLEY
ATTENDANT SEAT
GALLEY
LAVATORYGALLEY
LAVATORY
ATTENDANT SEAT
ECONOMYCLASS SEATS
ECONOMYCLASS SEATS
ECONOMYCLASS SEATS
FIRST CLASS SEATS
EMERGENCY EXITDOOR 3 RH
EMERGENCY EXITDOOR 3 LH
FWD PASSENGER/CREW DOOR 1 RH
FWD PASSENGER/CREW DOOR 1 LH
MID PASSENGER/CREW DOOR 2 LHMID PASSENGER/
CREW DOOR 2 RH
F_AC_020401_1_0030101_01_01
Interior Arrangements - Plan ViewTypical Configuration
FIGURE-2-4-1-991-003-A01
2-4-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
PASSENGER SEATS (303 TOTAL)
30 FIRST CLASS SEATS
273 ECONOMY CLASS SEATS
ATTENDANT SEATS 9
GALLEYS 5
LAVATORIES 7
STOWAGES 3
FWD PASSENGER/CREW DOOR 1 RH
GALLEY
LAVATORY
LAVATORY
FWD PASSENGER/CREW DOOR 1 LHATTENDANT SEAT
ATTENDANT SEAT
FIRST CLASS SEATS
ECONOMYCLASS SEATS
GALLEY
MID PASSENGER/CREW DOOR 2 RH
LAVATORY
ECONOMYCLASS SEATS
MID PASSENGER/CREW DOOR 2 LHATTENDANT SEATLAVATORY
ATTENDANT SEAT
GALLEY
ATTENDANT SEAT
EMERGENCY EXITDOOR 3 LH
EMERGENCY EXITDOOR 3 RH
ATTENDANT SEAT
ECONOMYCLASS SEATS
LAVATORY
AFT PASSENGER/CREW DOOR 4 LH
AFT PASSENGER/CREW DOOR 4 RH
ATTENDANT SEAT
GALLEYSTOWAGE
ATTENDANT SEAT
GALLEYSTOWAGE
STOWAGE
F_AC_020401_1_0040101_01_01
Interior Arrangements - Plan ViewTypical Configuration
FIGURE-2-4-1-991-004-A01
2-4-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
48 BUSINESS CLASS SEATS
170 ECONOMY CLASS SEATS
ATTENDANT SEATS 14
CREW REST COMPARTMENTS 2
GALLEYS 10
PASSENGER SEATS (228 TOTAL)
10 FIRST CLASS SEATS
LAVATORIES 8
STOWAGES 4
FWD PASSENGER/CREW DOOR 1 LH
FWD PASSENGER/CREW DOOR 1 RH
LAVATORYGALLEY
ATTENDANT SEAT
STOWAGE
ATTENDANT SEAT
GALLEYLAVATORY
FIRST CLASS SEATS
BUSINESSCLASS SEATS
MID PASSENGER/CREW DOOR 2 RH
GALLEY
STOWAGE
ATTENDANT SEAT
GALLEY
MID PASSENGER/CREW DOOR 2 LH
LAVATORY
ATTENDANT SEAT
BUSINESSCLASS SEATS
LAVATORYATTENDANT SEAT
ECONOMYCLASS SEATS
EMERGENCY EXITDOOR 3 RHLAVATORY
ATTENDANT SEAT
LAVATORY
EMERGENCY EXITDOOR 3 LH
ECONOMYCLASS SEATS
AFT PASSENGER/CREW DOOR 4 LH
ATTENDANT SEAT
AFT PASSENGER/CREW DOOR 4 RH
ATTENDANT SEATSTOWAGE
GALLEY
ATTENDANT SEATSTOWAGE
GALLEY
ATTENDANT SEAT
ATTENDANT SEAT
CREW RESTCOMPARTMENT
CREW RESTCOMPARTMENT
GALLEY
F_AC_020401_1_0050101_01_01
Interior Arrangements - Plan ViewTypical Configuration
FIGURE-2-4-1-991-005-A01
2-4-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0 Interior Arrangements - Cross Section
**ON A/C A340-200 A340-300
Interior Arrangements - Cross Section
1. This section gives the typical configuration of A340-200/-300 models.
2-5-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
C D C
F N M
H
K K
222 in5.640 m
208 in5.290 m
FIRST CLASS, 6 ABREAST BUSINESS CLASS, 7 ABREAST
TOURIST CLASS, 8 ABREAST CHARTER CLASS, 9 ABREAST
A − 54.0 in (1371.6 mm)B − 21.0 in (533 mm)C − 39.6 in (1006 mm)D − 17.7 in (450 mm)E − 72.0 in (1829 mm)F − 19.0 in (483 mm)
G − 48.0 in (1219 mm)H − 19.8 in (503 mm)K − 41.5 in (1054.1 mm)M − 57.1 in (1450 mm)N − 16.5 in (419 mm)
C
ABA
D
F G
C D
DCH
C C
E
M
91.7 in2.330 mA
F_AC_020500_1_0020101_01_00
Interior Arrangements - Cross SectionTypical Configuration
FIGURE-2-5-0-991-002-A01
2-5-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-1 Lower Deck Cargo Compartments
**ON A/C A340-200 A340-300
Lower Deck Cargo Compartments
1. This section provides the following data about lower deck cargo compartments:- Location and dimensions- Loading combinations.
2-6-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
0.95 m(3.12 ft)
2.75 m(9.02 ft)
2.78 m(9.12 ft)
15.02 m(49.28 ft)
A340−300
12.88 m(42.26 ft)
A340−200
12.32 m(40.42 ft)
10.19 m(33.43 ft)
4.04 m(13.25 ft)
4.04 m(13.25 ft)
LOWER DECKFWD CARGO
COMPARTMENT
LOWER DECKAFT CARGO
COMPARTMENT
LOWER DECKBULK CARGO
COMPARTMENT
FR39.1 FR53.2 FR65 FR73FR20
NOTE:APPROXIMATE DIMENSIONS DEPENDING ON AIRCRAFT CONFIGURATION.
F_AC_020601_1_0050101_01_02
Lower Deck Cargo CompartmentsLocation and Dimensions
FIGURE-2-6-1-991-005-A01
2-6-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
14 LD3 60.4 in X 61.5 in
5 PALLETS 96 in X 125 in
5 PALLETS 88 in X 125 in
12 LD3 60.4 in X 61.5 in
4 PALLETS 96 in X 125 in
4 PALLETS 88 in X 125 in
F_AC_020601_1_0060101_01_04
Lower Deck Cargo CompartmentsLoading Combinations
FIGURE-2-6-1-991-006-A01
2-6-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
18 LD3 60.4 in X 61.5 in
6 PALLETS 96 in X 125 in
6 PALLETS 88 in X 125 in
14 LD3 60.4 in X 61.5 in
4 PALLETS 96 in X 125 in
5 PALLETS 88 in X 125 in
F_AC_020601_1_0060201_01_02
Lower Deck Cargo CompartmentsLoading Combinations
FIGURE-2-6-1-991-006-B01
2-6-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0 Door Clearances
**ON A/C A340-200 A340-300
Door Clearances
1. This section provides door location, identification and clearances.
2-7-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
DOOR 1L
DOOR 2L
DOOR 3L
DOOR 4L
BULK CARGOCOMPARTMENT
DOOR AFT CARGO
COMPARTMENTDOOR
DOOR 4R
DOOR 3R DOOR 1R
DOOR 2R
FWD CARGOCOMPARTMENT
DOOR
F_AC_020700_1_0080101_01_01
Door ClearancesDoor Identification (Sheet 1 of 2)
FIGURE-2-7-0-991-008-A01
2-7-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
46.69 m(153.18 ft)
33.83 m(110.99 ft)
17.74 m(58.2 ft)
5.85 m(19.19 ft)
43.07 m(141.31 ft)
9.53 m(31.27 ft)
40.09 m(131.53 ft)
F_AC_020700_1_0080102_01_00
Door ClearancesDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-008-A01
2-7-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
DOOR 1L DOOR 2L DOOR 3LDOOR 4L
BULK CARGOCOMPARTMENT
DOOR AFT CARGO
COMPARTMENTDOOR
DOOR 4RDOOR 3R DOOR 1RDOOR 2R
FWD CARGOCOMPARTMENT
DOOR
F_AC_020700_1_0080201_01_01
Door ClearancesDoor Identification (Sheet 1 of 2)
FIGURE-2-7-0-991-008-B01
2-7-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
50.96 m(167.19 ft)
35.96 m(117.98 ft)
17.74 m(58.2 ft)
5.85 m(19.19 ft)
47.35 m(155.35 ft)
9.53 m(31.27 ft)
44.36 m(145.54 ft)
F_AC_020700_1_0080202_01_00
Door ClearancesDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-008-B01
2-7-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
3.30 m(10.83 ft)
CLEARANCELIMIT
CRITICAL
SEECHAPTER
2−3
1.93 m(6.33 ft)
3.00 m(9.84 ft)
5.85 m(19.19 ft)
1.07 m(3.51 ft)0.64 m
(2.10 ft)
2.43 m(7.97 ft)
0.05 m(0.16 ft)
0.75 m(2.46 ft)
F_AC_020700_1_0300101_01_00
Door ClearancesForward Passenger/Crew Doors
FIGURE-2-7-0-991-030-A01
2-7-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
0.05 m(0.16 ft)
SEECHAPTER
2−3
1.93 m(6.33 ft)
0.64 m(2.10 ft)
FWD
A A
17.74 m(58.20 ft)
(FROM NOSE)
3.41 m(11.19 ft)
0.75 m(2.46 ft)
1.07 m(3.51 ft)
2.43 m(7.97 ft)
(TOP OF FLOOR)
A
A
F_AC_020700_1_0310101_01_00
Door ClearancesMid Passenger/Crew DoorsFIGURE-2-7-0-991-031-A01
2-7-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
A
A
A A
A340−200: 33.83 m (110.99 ft)A340−300: 35.96 m (117.98 ft)
SEE
2−3CHAPTER
3.41 m(11.19 ft)
(TOP OF FLOOR)
0.59 m(1.94 ft)
1.93 m(6.33 ft)
0.04 m(0.13 ft)
(FROM NOSE)
CL
0.77 m(2.53 ft)
2.36 m(7.74 ft)
1.07 m(3.51 ft)
F_AC_020700_1_0320101_01_00
Door ClearancesEmergency Exits
FIGURE-2-7-0-991-032-A01
2-7-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
CL
A A
0.05 m(0.16 ft)
A340−200: 46.69 m (153.18 ft)A340−300: 50.96 m (167.19 ft)
3.00 m(9.84 ft)
0.64 m(2.10 ft)
1.99 m(6.53 ft)
1.07 m(3.51 ft)
0.75 m(2.46 ft)
CRITICALCLEARANCE
LIMIT
2.43 m(7.97 ft)
(FROM NOSE)
SEE
2−3CHAPTER
A
A
F_AC_020700_1_0330101_01_00
Door ClearancesAft Passenger/Crew DoorsFIGURE-2-7-0-991-033-A01
2-7-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
CL
A A
2.70 m(8.86 ft)
9.53 m(31.27 ft)
FWD
(FROM NOSE)
5.27 m(17.29 ft)
A
A
SEECHAPTER
2−3
2.04 m(6.69 ft)
1.70 m(5.58 ft)
F_AC_020700_1_0340101_01_00
Door ClearancesForward Cargo Compartment Door
FIGURE-2-7-0-991-034-A01
2-7-0Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
A A
A340−200: 40.09 m (131.53 ft)A340−300: 44.36 m (145.54 ft)
(FROM NOSE)
CL
5.19 m(17.03 ft)
2.03 m(6.66 ft) 1.68 m
(5.51 ft)
FWD
2.78 m(9.12 ft)
A
A
SEECHAPTER
2−3
F_AC_020700_1_0350101_01_00
Door ClearancesAft Cargo Compartment DoorFIGURE-2-7-0-991-035-A01
2-7-0Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
SEECHAPTER
2−3
(FROM NOSE)
FWD
A
A
A340−200: 43.08 m (141.34 ft)A340−300: 47.34 m (155.31 ft)
1.11 m(3.64 ft)
0.95 m(3.12 ft)
1.41 m(4.63 ft)
1.07 m(3.51 ft)
A A
F_AC_020700_1_0360101_01_00
Door ClearancesBulk Cargo Compartment Door
FIGURE-2-7-0-991-036-A01
2-7-0Page 12
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
1.32 m(4.33 ft)
1.25 m(4.10 ft)
67°
1.65 m(5.41 ft)
FR1
F_AC_020700_1_0370101_01_00
Door ClearancesRadome
FIGURE-2-7-0-991-037-A01
2-7-0Page 13
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
Z−2.00 m (6.56 ft)
LH SHOWNRH SYMMETRICAL
A/C
A
C L
GROUND LINE
0.06 m(0.20 ft)
2.70 m(8.86 ft)
0.23 m(0.75 ft)
1.56 m(5.12 ft)
0.85 m(2.79 ft)
A340−200: 27.31 m (89.60 ft)A340−300: 29.45 m (96.62 ft)
01
NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01
1.10 m(3.61 ft)
GROUND LINE
0.95 m(3.12 ft)
A
2.34 m(7.68 ft)
0.97 m(3.18 ft)
3.03 m(9.94 ft)
3.96 m(12.99 ft)
81°
F_AC_020700_1_0380101_01_00
Door ClearancesMain and Center Landing Gear Doors
FIGURE-2-7-0-991-038-A01
2-7-0Page 14
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
FR101FR95
FWD
MAX. 6.85 m (22.47 ft)MIN. 6.11 m (20.05 ft)
MAX. 6.51 m (21.36 ft)MIN. 5.77 m (18.93 ft)
MAX. 1.57 m (5.15 ft)MIN. 1.39 m (4.56 ft)
MAX. 2.00 m (6.56 ft)MIN. 1.82 m (5.97 ft)
01
01
0101
NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01 F_AC_020700_1_0390101_01_00
Door ClearancesAPU and Nose Landing Gear Doors
FIGURE-2-7-0-991-039-A01
2-7-0Page 15
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FR101FR95
FWD
01
0101
01
MAX. 6.88 m (22.57 ft)MIN. 6.14 m (20.14 ft)
MAX. 6.53 m (21.42 ft)MIN. 5.79 m (19.00 ft)
MAX. 1.58 m (5.18 ft)MIN. 1.40 m (4.59 ft)
MAX. 2.01 m (6.59 ft)MIN. 1.83 m (6.00 ft)
NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01 F_AC_020700_1_0400101_01_00
Door ClearancesAPU and Nose Landing Gear Doors
FIGURE-2-7-0-991-040-A01
2-7-0Page 16
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0 Escape Slides
**ON A/C A340-200 A340-300
Escape Slides
1. GeneralThis section provides the location of the cabin escape facilities and their related clearances.
2. LocationEscape facilities are provided at the following locations:
A. Door Escape Facility- One dual lane escape slide-raft at each passenger/crew door (total six)- One single lane escape slide at each emergency exit door (total two).The slides are installed in a container in the lower part of the door.
2-8-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
COCKPITESCAPE ROPE
FWD CABIN DUAL−LANEESCAPE SLIDE/RAFT
MID CABIN DUAL−LANEESCAPE SLIDE/RAFT
AFT CABIN DUAL−LANEESCAPE SLIDE/RAFT
NOTE:− LH SHOWN, RH SYMMETRICAL.− *THE SINGLE−LANE ESCAPE SLIDE SHOWN IS FOR A TYPE "1" DOOR.
A DUAL−LANE ESCAPE SLIDE/RAFT IS AVAILABLE FOR AIRCRAFT FITTED WITH A TYPE "A" DOOR.
EMERGENCY EXITSINGLE−LANE
ESCAPE SLIDE*
F_AC_020800_1_0030101_01_01
Escape SlidesLocation (Sheet 1 of 2)
FIGURE-2-8-0-991-003-A01
2-8-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
GR
ID E
QU
ALS
1 m
(3.
28 ft
) IN
RE
ALI
TY
0 −3
−6 −9
−12
−15 −21
−18
−24
−27
−30 −33
EM
ER
GE
NC
Y D
ES
CE
NT
TH
RO
UG
H T
HE
WIN
DO
W O
PE
NIN
G W
ITH
TH
E E
SC
AP
E R
OP
E
EM
ER
GE
NC
Y E
VA
CU
AT
ION
NO
TE
:−
LH
SH
OW
N, R
H S
YM
ME
TR
ICA
L.−
DIM
EN
SIO
NS
AR
E A
PP
RO
XIM
AT
E.
F_AC_020800_1_0030102_01_01
Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-003-A01
2-8-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
COCKPITESCAPE ROPE
EMERGENCY EXITSINGLE−LANE
ESCAPE SLIDE*
NOTE:− LH SHOWN, RH SYMMETRICAL.− *THE SINGLE−LANE ESCAPE SLIDE SHOWN IS FOR A TYPE "1" DOOR.
A DUAL−LANE ESCAPE SLIDE/RAFT IS AVAILABLE FOR AIRCRAFT FITTED WITH A TYPE "A" DOOR.
FWD CABIN DUAL−LANEESCAPE SLIDE/RAFT
MID CABIN DUAL−LANEESCAPE SLIDE/RAFT
AFT CABIN DUAL−LANEESCAPE SLIDE/RAFT
F_AC_020800_1_0030201_01_01
Escape SlidesLocation (Sheet 1 of 2)
FIGURE-2-8-0-991-003-B01
2-8-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
GR
ID E
QU
ALS
1 m
(3.
28 ft
) IN
RE
ALI
TY
0 −3
−6 −9
−12
−15 −21
−18
−24
−27
−30 −33
EM
ER
GE
NC
Y D
ES
CE
NT
TH
RO
UG
H T
HE
WIN
DO
W O
PE
NIN
G W
ITH
TH
E E
SC
AP
E R
OP
E
EM
ER
GE
NC
Y E
VA
CU
AT
ION
NO
TE
:−
LH
SH
OW
N, R
H S
YM
ME
TR
ICA
L.−
DIM
EN
SIO
NS
AR
E A
PP
RO
XIM
AT
E.
F_AC_020800_1_0030202_01_01
Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-003-B01
2-8-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0 Landing Gear
**ON A/C A340-200 A340-300
Landing Gear Maintenance Pits
1. General
The minimum maintenance pit envelopes for the main landing gear shock absorber removal are shownin Figures 1 and 2.
All dimensions shown are minimum dimensions with zero clearances.
The dimensions for the pits have been determined for these design factors:- 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 allow 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.
A. Elevators
These can be either mechanical or hydraulic. Elevators are used to:- permit easy movement of persons and equipment around the main landing gears- to lift and remove landing gear assemblies out of the pits.
B. Jacking
The aircraft must be in position over the pits to put the gear on the elevators. Jacks must beinstalled and engaged with all the jacking points (Ref. Section 2-14 for Jacking).Jacks must support the total aircraft weight, i.e. when the landing gears do not touch theelevators on retraction/extension tests.When tripod support jacks are used, the tripod-base circle radius must be limited because thelocations required for positioning the jacks are close to the sides of the pits.
2-9-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FR
ON
T O
F N
OS
E R
AD
OM
E
FO
RW
AR
D J
AC
KIN
G P
OIN
T
WIN
G J
AC
KIN
G P
OIN
T
AIR
CR
AF
T C
EN
TE
R L
INE
WIN
G J
AC
KIN
G P
OIN
T31
.55
m(1
03.5
1 ft)
3.58
m(1
1.75
ft)
8.51
m(2
7.92
ft)
3.89
m(1
2.76
ft)
6.31
m(2
0.7
ft)
5.34
m(1
7.52
ft)
34.3
1 m
(112
.57
ft)25.3
8 m
(83.
27 ft
)
3.65
m(1
1.98
ft)
NO
TE
:E
NV
ELO
PE
S S
HO
WN
WIT
H Z
ER
O C
LEA
RA
NC
E T
O O
UT
SID
E E
DG
E O
F T
IRE
S.
F_AC_020900_1_0030101_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 1 of 2)
FIGURE-2-9-0-991-003-A01
2-9-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
DIM
EN
SIO
NS
mm
ftft
MA
IN L
AN
DIN
G G
EA
R
6.53
m(2
1.42
ft)
FU
SE
LAG
E H
OR
IZO
NT
AL
DA
TU
M
(103
.02
ft)31
.4 m
33.1
3 m
(108
.69
ft)
FR
ON
T O
F N
OS
E R
AD
OM
EAB
C6.
67 m
(21.
88 ft
)
D
1.53
5.02
0.2
0.66
0.81
2.66
mft
BC
D
mft
A
1.56
5.12
3. ’C
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E D
EF
LAT
ED
AN
DC
OM
PR
ES
SE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
4. ’D
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E E
XT
EN
DE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
1. ’A
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
NLG
WH
EE
LA
BO
VE
ST
AT
IC G
RO
UN
D L
INE
WIT
H A
IRC
RA
FT
LEV
ELL
ED
AN
D J
AC
KE
D.
A P
IT IS
NO
T R
EQ
UIR
ED
FO
R T
HE
NLG
.
2. ’B
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
LO
WE
ST
MLG
MA
IN W
HE
EL
AB
OV
E S
TA
TIC
GR
OU
ND
LIN
EW
ITH
AIR
CR
AF
T J
AC
KE
D IN
TO
PO
SIT
ION
AB
OV
E H
YD
RA
ULI
C O
R M
EC
HA
NIC
AL
ELE
VA
TO
R,
FO
R R
ET
RA
CT
ION
/EX
TE
NS
ION
TE
ST
S.
NO
TE
:
F_AC_020900_1_0030102_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 2 of 2)
FIGURE-2-9-0-991-003-A01
2-9-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
3.58
m(1
1.75
ft)
8.51
m(2
7.92
ft)
3.89
m(1
2.76
ft)
6.31
m(2
0.7
ft)
5.34
m(1
7.52
ft)
32.1
8 m
(105
.58
ft)
29.4
1 m
(96.
49 ft
)
23.2
4 m
(76.
25 ft
)
3.65
m(1
1.98
ft)
FR
ON
T O
F N
OS
E R
AD
OM
E
FO
RW
AR
D J
AC
KIN
G P
OIN
T
WIN
G J
AC
KIN
G P
OIN
T
AIR
CR
AF
T C
EN
TE
R L
INE
WIN
G J
AC
KIN
G P
OIN
T
NO
TE
:E
NV
ELO
PE
S S
HO
WN
WIT
H Z
ER
O C
LEA
RA
NC
E T
O O
UT
SID
E E
DG
E O
F T
IRE
S.
F_AC_020900_1_0030201_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 1 of 2)
FIGURE-2-9-0-991-003-B01
2-9-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
DIM
EN
SIO
NS
mm
ftft
MA
IN L
AN
DIN
G G
EA
R
6.53
m(2
1.42
ft)
FU
SE
LAG
E H
OR
IZO
NT
AL
DA
TU
M
FR
ON
T O
F N
OS
E R
AD
OM
EAB
C6.
67 m
(21.
88 ft
)
D
1.53
5.02
0.2
0.66
0.81
2.66
mft
BC
D
mft
A
1.56
5.12
(95.
83 ft
)29
.21
m
30.4
m
(99.
74 ft
)
3. ’C
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E D
EF
LAT
ED
AN
DC
OM
PR
ES
SE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
4. ’D
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
HY
DR
AU
LIC
OR
ME
CH
AN
ICA
L E
LEV
AT
OR
WIT
H T
HE
MLG
SH
OC
K A
BS
OR
BE
R IN
TH
E E
XT
EN
DE
D C
ON
DIT
ION
FO
R S
HO
CK
AB
SO
RB
ER
RE
MO
VA
L.
1. ’A
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
NLG
WH
EE
LA
BO
VE
ST
AT
IC G
RO
UN
D L
INE
WIT
H A
IRC
RA
FT
LEV
ELL
ED
AN
D J
AC
KE
D.
A P
IT IS
NO
T R
EQ
UIR
ED
FO
R T
HE
NLG
.
2. ’B
’ RE
PR
ES
EN
TS
PO
SIT
ION
OF
LO
WE
ST
MLG
MA
IN W
HE
EL
AB
OV
E S
TA
TIC
GR
OU
ND
LIN
EW
ITH
AIR
CR
AF
T J
AC
KE
D IN
TO
PO
SIT
ION
AB
OV
E H
YD
RA
ULI
C O
R M
EC
HA
NIC
AL
ELE
VA
TO
R,
FO
R R
ET
RA
CT
ION
/EX
TE
NS
ION
TE
ST
S.
NO
TE
:
F_AC_020900_1_0030202_01_00
Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 2 of 2)
FIGURE-2-9-0-991-003-B01
2-9-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
Landing Gear
1. General
The aircraft has:- Two Main Landing Gears (MLG) with four wheel bogie assembly and related doors,- A Centerline Landing Gear (CLG) with twin wheel assembly and related doors,- A Nose Landing Gear (NLG) retracts forward into a fuselage compartment below the cockpit.
The main landing gears are located under each wing and retract sideways towards the fuselagecenterline.The centerline landing gear is located on the belly and retract forward into a bay in the fuselage.The nose landing gear retracts forward into a fuselage compartment below the cockpit.The retraction and extension of the landing gears and landing gear doors are operated hydraulicallyand mechanically. The control, sequence and indication are electrical.In abnormal operation, the landing gears can be extended by gravity.
For the dimensions of the landing gear footprint and tire size, refer to 07-02-00.
2. Main Landing Gear and Doors
Each MLG has a leg assembly and a four-wheel bogie beam. The MLG leg includes a shorteningmechanism, a bogie pitch trimmer and an oleo-pneumatic shock absorber. In-flight, with the MLGextended, the bogie is held in a trailing condition (rear wheels low) by an articulation linkage and apitch trimmer. The folding sidestay is locked mechanically by a lockstay (which is operated by thedownlock actuator) when the MLG is fully extended.
Each MLG bay has the following doors:- A hydraulically-operated main door,- A mechanically-operated hinged door,- A fairing door on the MLG leg.
All the doors close when the MLG retracts. When the MLG is extended the main door closes and thehinged door stays open. A manually operated mechanism (for maintenance personnel) lets the maindoors be opened for access to the MLG bay when the aircraft is on the ground.
3. Centerline Landing Gear and Doors
The CLG includes a twin-wheel axle assembly and a leg assembly that includes an oleo-pneumaticshock absorber. The CLG is supported longitudinally by a two-piece folding dragstay. The dragstay islocked mechanically by the lock links when the CLG is fully extended.
Each CLG bay has the following doors:
2-9-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Two hydraulically-operated FWD doors,- Two mechanically-operated AFT doors,- A fixed fairing door on the CLG leg.
All the doors close when the CLG retracts. When the CLG is extended the FWD doors close and theAFT doors stay open. A door opening mechanism lets the FWD doors be opened on the ground foraccess to the CLG bay.
4. Nose Landing Gear and Doors
The NLG includes a twin-wheel axle assembly and an oleo-pneumatic shock absorber. The NLG issupported longitudinally by a two-piece dragstay. The dragstay is locked mechanically by the locklinks when the NLG is fully extended.
Each NLG bay has the following doors:- Two hydraulically-operated FWD doors,- Two mechanically-operated AFT doors,- A fixed fairing door on the NLG leg.
All the doors close when the NLG retracts. When the NLG is extended the FWD doors close and theAFT doors stay open. A door opening mechanism lets the FWD doors be opened on the ground foraccess to the NLG bay.
5. Nose Wheel Steering (NWS)
Nose wheel steering system is a computer controlled electro-hydraulic system. The system uses thegreen main hydraulic power system to operate the hydraulic components.The steering is controlled by two hand wheel transmitters in the cockpit, which supply the primarysteering inputs to the BSCU (Brake and Steering Control Unit).A steering disconnection box is installed on the NLG to disconnect the steering for towing.
For the operation and control of nose wheel steering, refer to AMM 32-51-00.For the steering angle limits, refer to AMM 09-10-00.
6. Tow Truck Power
Electric power to the navigation lights can be provided through the tow truck power connector on the5GC or 8GH service panel, see FIGURE 2-9-0-991-016-A and for connector definition, see 05-04-04.
7. Landing Gear Servicing Points
A. GeneralFluid filling and gas charging of the MLG, CLG and NLG shock absorbers are accomplishedthrough MS28889 standard valves.
B. Charging PressuresFor charging of the landing gear shock absorbers, refer to AMM 12-14-32.
2-9-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
8. Landing Gear Control
The landing gear and door operation is controlled electrically by one of the two Landing Gear Controland Interface Units (LGCIU). Control changes from one LGCIU to the other after each extensioncycle.In normal operation, the landing gears and doors are operated by the green hydraulic system.In abnormal operation, the landing gears can be extended by the operation of electro-mechanical free-fall system. The related electrical switches in the cockpit disengages the doors and the landing gearuplocks. The landing gears then extend by free-fall and the downlock links of each landing gear (L/G)are locked in position by springs.
9. Braking
A. GeneralCarbon multi-disc brakes are installed on each wheel of the MLG. Each brake assembly has twowear indicators installed.
The braking system has four braking modes with autobrake and anti-skid systems:- Normal braking with anti-skid,- Alternate braking with anti-skid,- Alternate braking without anti-skid,- Parking brake with full brake pressure.
B. In-Flight Wheel BrakingBraking occurs automatically during the retraction of the landing gears. This stops the rotationof the MLG wheels before the landing gears go into their related bays.The wheels of the NLG are braked by spring loaded pads.
10. Tire Pressure Indicating System (TPIS)
The TPIS automatically monitors the tire pressures and shows these values on Test Equipment(BITE) and also supplies other data and warnings on the WHEEL page of the System Display (SD).
11. Built In Test Equipment (BITE)
The BITE has hardware and software for these functions:- to automatically do a self test at power-up,- to continuously monitor the related systems for failures,- to continuously monitor the interface with other specified systems in the aircraft,- to keep a record of each failure and defect and send this data to other systems in the aircraft,- to automatically do a functional test of some related systems before a landing,- to do specified system tests during ground maintenance.
The BITE for the following systems is described in these chapters:- The Brakes and Steering AMM 32-46-00,- The TPIS AMM 32-49-00,
2-9-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- The Landing GearAMM 32-69-00.
2-9-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
MAIN DOOR
HINGED DOOR
FIXED FAIRING DOOR
A
B
C
D
F
E
DOWNLOCKACTUATOR
SHORTENINGMECHANISM
SIDE STAYASSEMBLY MLG LEG
ASSEMBLY
TORQUE LINKS
BOGIE PITCHTRIMMER
BOGIE BEAMASSEMBLY
SHOCK ABSORBER
ARTICULATING LINKS
RADIAL OR BIASPLY TIRES
A
(HYDRAULICALLYOPERATED)
FWD AXLE
AFT AXLE
BRAKE RODASSEMBLY
F_AC_020900_1_0090101_01_00
Main Landing GearGeneral (Sheet 1 of 3)
FIGURE-2-9-0-991-009-A01
2-9-0Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
C
WARNING FLAG
GROUND LOCK PIN
LOCK STAY
BLH SHOWN
RH SYMMETRICAL
QUICK RELEASE PIN
SAFETYCOLLAR
WARNING FLAG
WARNING FLAG
QUICK RELEASE PIN
DOOR ACTUATOR
F_AC_020900_1_0090102_01_00
Main Landing GearSafety Devices (Sheet 2 of 3)FIGURE-2-9-0-991-009-A01
2-9-0Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
SEAL CHANGEOVERVALVE
BLEED/INFLATIONVALVE
D
E
F
FWD
FILL VALVE
GROUND POINT
F_AC_020900_1_0090103_01_00
Main Landing GearServicing (Sheet 3 of 3)
FIGURE-2-9-0-991-009-A01
2-9-0Page 12
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
E
F
RETRACTIONACTUATOR
SIDE MEMBER
MAIN FITTING
BARREL
UPLOCK PIN
WEIGHT AND BALANCE SENSORATTACHMENT POINTS
SHOCKABSORBER
AXLE
TORQUE LINKS
SERVICING PLATE
HINGED DOOR DRIVE MECHANISM
ATTACHEMENT POINT
A
AFT DOOROPERATING ROD
AFT DOOR
FIXED FAIRING
FWD DOOR
A
D
(MECHANICALLYOPERATED)
(HYDRAULICALLYOPERATED)
C
B
B
RADIAL OR BIASPLY TIRES
F_AC_020900_1_0100101_01_00
Centerline Landing GearGeneral (Sheet 1 of 3)
FIGURE-2-9-0-991-010-A01
2-9-0Page 13
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
BRH SHOWN
LH SYMMETRICAL
GROUNDLOCK PIN
DRAG STAY
DOWNLOCK SPRINGS
C
ASSEMBLY
SAFETYCOLLAR
QUICK RELEASE PIN
WARNING FLAG
WARNING FLAG
QUICK RELEASE PIN
WARNINGFLAG
DOOR ACTUATOR
F_AC_020900_1_0100102_01_00
Centerline Landing GearSafety Devices (Sheet 2 of 3)FIGURE-2-9-0-991-010-A01
2-9-0Page 14
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
D
G
OIL FILLERVALVE
INFLATION VALVE(FIRST STAGE)
E
INFLATION VALVE(SECOND STAGE)
F
FWD
SEAL CHANGEOVERVALVE
G
FWD
F_AC_020900_1_0100103_01_00
Centerline Landing GearServicing (Sheet 3 of 3)
FIGURE-2-9-0-991-010-A01
2-9-0Page 15
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
RETRACTION ACTUATOR
DOWNLOCKACTUATOR
MAIN FITTING
DOWNLOCK SPRINGS
TORQUE LINKS
RADIAL OR BIASPLY TIRES
TOWING BRACKET
SHOCK ABSORBER
AXLE
NWS ACTUATORS
LOWER DRAGSTAY(FOLDING STRUT)
UPPER DRAGSTAY(FOLDING STRUT)
EH
D
AFT DOOR(MECHANICALLY OPERATED)
FWD DOORS
A
(HYDRAULICALLY
AFT DOOR(MECHANICALLY OPERATED)
FIXED FAIRING
A
C
F
G
OPERATED)
B
B
F_AC_020900_1_0110101_01_00
Nose Landing GearGeneral (Sheet 1 of 4)
FIGURE-2-9-0-991-011-A01
2-9-0Page 16
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
B
DRAG STAYATTACHMENT
GROUNDLOCK PIN
LOCK SPRINGATTACHMENT
LOWERLOCK−LINK
UPPERLOCK−LINK
DOWN LOCKACTUATOR
ATTACHMENT
WARNING FLAG
C
RH SHOWNLH SYMMETRICAL
SAFETYCOLLAR
QUICK RELEASE PIN
WARNING FLAG
WARNING FLAG
QUICK RELEASE PIN
DOOR ACTUATOR
F_AC_020900_1_0110102_01_00
Nose Landing GearSafety Devices (Sheet 2 of 4)FIGURE-2-9-0-991-011-A01
2-9-0Page 17
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
SEAL CHANGEOVERVALVE
CHARGE VALVE
BLEED VALVE
E
D
INFLATION VALVE(FIRST STAGE)
FWD
F_AC_020900_1_0110103_01_00
Nose Landing GearServicing (Sheet 3 of 4)
FIGURE-2-9-0-991-011-A01
2-9-0Page 18
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
INFLATION VALVE(SECOND STAGE)
LANDING GEAR
GROUND POINT
FWD
F
TOWING LEVER
SAFETY PIN(TOWING POSITION)
WARNING FLAG
NORMAL POSITION(NOSE WHEEL STEERING
OPERATIONAL)
TOWING POSITION(NOSE WHEEL STEERING
DEACTIVATED)
G
H
F_AC_020900_1_0110104_01_00
Nose Landing GearServicing and Steering Disconnection Box (Sheet 4 of 4)
FIGURE-2-9-0-991-011-A01
2-9-0Page 19
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
5GC
5GCB
TOW−TRUCK POWER CABLE 03
TOW−TRUCK POWER CABLE 02
8GH 01
B
8GH
SAFETY PIN
ELECTRIC BOX(NLG OVERSTEER WARNING)
ELECTRICALDEACTIVATION BOX
WARNING FLAG
IF ELECTRICAL BOX03
CONNECT THE TOW−TRUCK POWER CABLE TO CONNECTOR02IF INSTALLED01
IS INSTALLED ON THE AIRCRAFT.
TO CONNECTOR
NOTE:
8GH IS NOT INSTALLED, CONNECT THE TOW−TRUCK POWER CABLE
8GH
5GC.
8GHB
8GHB IF ELECTRICAL BOX
5GCB ON ELECTRICAL DEACTIVATION BOX
AB
CONNECTOR
CONNECTOR
FOR PIN ALLOCATIONSEE 05−04−04
FOR PIN ALLOCATION
ASEE 05−04−04
F_AC_020900_1_0160101_01_00
Tow Truck PowerFIGURE-2-9-0-991-016-A01
2-9-0Page 20
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0 Exterior Lighting
**ON A/C A340-200 A340-300
Exterior Lighting
1. GeneralThis section provides the location of the aircraft exterior lighting.
EXTERIOR LIGHTINGITEM DESCRIPTION
1 RIGHT NAVIGATION LIGHT (GREEN)
2 LEFT NAVIGATION LIGHT (RED)
3 TAIL NAVIGATION LIGHT (WHITE)
4 UPPER ANTI-COLLISION LIGHT/BEACON(RED)
5 LOWER ANTI-COLLISION LIGHT/BEACON(RED)
6 LOGO LIGHTS7 ENGINE SCAN LIGHTS8 WING SCAN LIGHTS9 WING STROBE LIGHT (HIGH INTENSITY,
WHITE)
10 TAIL STROBE LIGHT (HIGH INTENSITY,WHITE)
11 LANDING LIGHTS12 RUNWAY TURN-OFF LIGHTS13 TAXI LIGHTS14 TAKE-OFF LIGHTS15 CARGO COMPARTMENT FLOOD LIGHTS16 LANDING GEAR BAY/WELL LIGHTS (DOME)
2-10-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
1 RH
2 LH
87 9
5
10
3
64
F_AC_021000_1_0040101_01_00
Exterior Lighting(Sheet 1 of 5)
FIGURE-2-10-0-991-004-A01
2-10-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
13 12 11
14
NOTE:LIGHTS 13 AND 14 ARE THE SAME, BUT THEY OPERATE WITH DIFFERENT POWER SETTINGS.
F_AC_021000_1_0040102_01_00
Exterior Lighting(Sheet 2 of 5)
FIGURE-2-10-0-991-004-A01
2-10-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
7
21
3
7
12 12
13
14
F_AC_021000_1_0040103_01_00
Exterior Lighting(Sheet 3 of 5)
FIGURE-2-10-0-991-004-A01
2-10-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
99
4 5
8
10
8
1111
F_AC_021000_1_0040104_01_00
Exterior Lighting(Sheet 4 of 5)
FIGURE-2-10-0-991-004-A01
2-10-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
6
6
15 16 15 16
F_AC_021000_1_0040105_01_00
Exterior Lighting(Sheet 5 of 5)
FIGURE-2-10-0-991-004-A01
2-10-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
1 RH
LH
4
78
6
2
9
3
10
5
F_AC_021000_1_0050101_01_00
Exterior Lighting(Sheet 1 of 5)
FIGURE-2-10-0-991-005-A01
2-10-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
12
14
1113
NOTE:LIGHTS 13 AND 14 ARE THE SAME, BUT THEY OPERATE WITH DIFFERENT POWER SETTINGS.
F_AC_021000_1_0050102_01_00
Exterior Lighting(Sheet 2 of 5)
FIGURE-2-10-0-991-005-A01
2-10-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
21
7
12
13
14
12
7
3
F_AC_021000_1_0050103_01_00
Exterior Lighting(Sheet 3 of 5)
FIGURE-2-10-0-991-005-A01
2-10-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
99
10
8
54
8
1111
F_AC_021000_1_0050104_01_00
Exterior Lighting(Sheet 4 of 5)
FIGURE-2-10-0-991-005-A01
2-10-0Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
6
6
15 16 15 16
F_AC_021000_1_0050105_01_00
Exterior Lighting(Sheet 5 of 5)
FIGURE-2-10-0-991-005-A01
2-10-0Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0 Antennas and Probes Location
**ON A/C A340-200 A340-300
Antennas and Probes Location
1. This section gives the location of antennas and probes.
2-11-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
LOC
GP
S(1
)
GP
S(2
)
TC
AS
TO
P
VH
F(1
)
GP
S(2
)V
HF
(3)
ELT
MA
RK
ER
GP
S(1
)
ST
AT
IC P
RO
BE
(1)
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
ST
AT
IC P
RO
BE
(2)
RA
DIO
ALT
IME
TE
R(2
)
RA
DIO
ALT
IME
TE
R(1
)
AT
C(4
)
WE
AT
HE
R R
AD
AR
VH
F(4
)
HF
TC
AS
BO
TT
OM
DM
E(2
)
PIT
OT
PR
OB
E(3
)
GLI
DE
AO
A S
EN
SO
R(1
)
TA
T P
RO
BE
ICE
DE
TE
CT
OR
PR
OB
E
PIT
OT
PR
OB
E(1
)
DM
E(1
)
AT
C(1
)
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0040101_01_00
Antennas and ProbesLocation (Sheet 1 of 2)
FIGURE-2-11-0-991-004-A01
2-11-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
AD
F(2
)
AD
F(1
)
VO
R
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
AT
C(3
)
PIT
OT
PR
OB
E(2
)
ICE
DE
TE
CT
OR
PR
OB
E
TA
T P
RO
BE
SA
TC
OM
VH
F(2
)S
TA
TIC
PR
OB
E(1
)
ST
AT
IC P
RO
BE
(2)
AT
C(2
)AO
A S
EN
SO
R(2
)
AO
A S
EN
SO
R(3
) S
TB
Y
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0040102_01_00
Antennas and ProbesLocation (Sheet 2 of 2)
FIGURE-2-11-0-991-004-A01
2-11-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
GP
S(1
)
GP
S(2
)
TC
AS
TO
P
VH
F(1
)
AT
C(4
)
GP
S(2
)V
HF
(3)
ELT
GP
S(1
)
WE
AT
HE
R R
AD
AR
HF
ST
AT
IC P
RO
BE
(1)
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
ST
AT
IC P
RO
BE
(2)
TC
AS
BO
TT
OM
AO
A S
EN
SO
R(1
)
ICE
DE
TE
CT
OR
PR
OB
E
PIT
OT
PR
OB
E(1
)
LOC
MA
RK
ER
DM
E(2
)
DM
E(1
)
AT
C(1
)VH
F(4
)
PIT
OT
PR
OB
E(3
)
GLI
DE
TA
T P
RO
BE
RA
DIO
ALT
IME
TE
R(2
)
RA
DIO
ALT
IME
TE
R(1
)
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0050101_01_00
Antennas and ProbesLocation (Sheet 1 of 2)
FIGURE-2-11-0-991-005-A01
2-11-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
AD
F(2
)
AD
F(1
)
VO
R
AO
A S
EN
SO
R(3
) S
TB
Y
AO
A S
EN
SO
R(2
)
AT
C(2
)S
TA
TIC
PR
OB
E(2
)
EM
ER
GE
NC
Y S
TA
TIC
PR
OB
E(3
)
ST
AT
IC P
RO
BE
(1)
VH
F(2
)
AT
C(3
)T
AT
PR
OB
E
PIT
OT
PR
OB
E(2
)
ICE
DE
TE
CT
OR
PR
OB
E
SA
TC
OM
NO
TE
:D
EP
EN
DIN
G O
N A
IRC
RA
FT
CO
NF
IGU
RA
TIO
N
F_AC_021100_1_0050102_01_00
Antennas and ProbesLocation (Sheet 2 of 2)
FIGURE-2-11-0-991-005-A01
2-11-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0 Engine and Nacelle
**ON A/C A340-200 A340-300
Engine and Nacelle
1. Engine and Nacelle - CFM 56-5C Engine
A. EngineThe engine is an axial flow, dual spool, high bypass ratio, turbofan engine.The principal modules of the engine are:- The fan and booster- The high pressure compressor- The combustion chamber- The High Pressure Turbine (HPT)- The Low Pressure Turbine (LPT)- The accessory drive gearbox.
The fan and booster assembly consists of a single-stage fan rotor and a four-stage axial booster,cantilever-mounted at the rear of the fan disk. The compressor is a nine-stage axial flowassembly. Air, taken in through the fan and booster sections, passes through successive stagesof rotor blades and stator vanes, being compressed as it passes from stage to stage. Afterpassing through the 9 high pressure compressor stages, the air is fully compressed. The InletGuide Vanes (IGV) and the first 3 stages of the compressor are variable. The combustionchamber is a short, annular structure. The combustion of fuel takes place in the combustorinstalled in the combustion casing. The HPT module consists of a single-stage nozzle and rotor.The HPT is an air-cooled single-stage high-energy turbine. Rotor blades are individuallyreplaceable without the need for rotor disassembly or re-balancing. The LPT consists of 5 stagesof blades and vanes. The LPT drives the fan rotor through the inner concentric shaft and isaerodynamically coupled to the high pressure system. The engine and aircraft accessories aremounted on the accessory gearbox which is located on the lower portion of the fan casing and isdriven by a shaft from the transfer gearbox. Power for the engine and the aircraft accessories isextracted from the high pressure compressor rotor shaft through an inlet gearbox through theradial drive shaft to the transfer gearbox.
B. NacelleThe nacelle provides protection for the engine and the engine accessories, and aerodynamicairflow around the engine during operation. Each engine is housed in a nacelle suspended from apylon attached below the wing. The nacelle consists of the following major components:
(1) Air Intake Cowl AssemblyThe engine air intake cowl structure is an interchangeable aerodynamically-faired assembly.It is installed on the forward face of the engine fan case.
2-12-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
(2) Fan Cowl AssemblyThe fan cowls are interchangeable units. They enclose the engine fan case between the airintake cowl and the thrust reverser. Three hinges at the pylon support each fan cowl. Thefan cowls are latched at the bottom with three adjustable tension hook latches.
(3) Fan Thrust ReverserThe thrust reverser comprises two cowls. Each cowl is hinged at the top to the pylon andlatched to the other cowl along the bottom centerline; the forward end is secured onto theaft outer flange of the fan case and the aft end onto the forward outer barrel of theexhaust nozzle. The fan thrust reverser assembly forms the passage for fan airstream flowbetween the fan case aft frame and the exhaust nozzle/mixer inlet. When in reverse thrustmode, four pivoting doors turn the engine fan air flow forward and provide a braking effectto reduce the aircraft stopping distance. The thrust reverser is designed for groundoperation only. A hydraulically-actuated cowl-opening system allows each thrust reversercowl to be opened independently.
(4) Exhaust NozzleThe exhaust nozzle attaches to the thrust reverser when the reverser cowls are closed.When they are open the exhaust nozzle is maintained on the mixer by two support pinslocated on the upper forward part of the mixer and by a strut. The nozzle can be removedalone or together with the engine.
2-12-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
HP COMPRESSORFAN AND BOOSTER
1.01 m(3.31 ft)
2.62 m(8.6 ft)
2.99 m(9.81 ft)
COMBUSTIONSECTION
1.07 m(3.51 ft)
HP TURBINE
LP TURBINE
TURBINEREAR FRAME
ACCESSORY DRIVESECTION
A
1.98 m(6.5 ft)
1.05 m(3.44 ft)
2.09 m(6.86 ft)
1.28 m(4.2 ft)
2.25 m(7.38 ft)
A
B
B
NOTE:APPROXIMATE DIMENSIONS
FWD
F_AC_021200_1_0160101_01_00
Engine and NacelleEngine Dimensions - CFM 56-5C
FIGURE-2-12-0-991-016-A01
2-12-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
(4.63 ft)1.41 m
E E
(6.66 ft)2.03 m
(6.43 ft)1.96 m
D D
(7.22 ft)2.2 m BLOCKER
DOOREXTENDED
3.17 m(10.4 ft)
C C
(7.32 ft)2.23 m
(7.91 ft)2.41 m
NOTE:APPROXIMATE DIMENSIONS
A A B B
NAC STA
(27.99 ft)8.53 m
NAC STA
(22.28 ft)6.79 m
NAC STA
(19.13 ft)5.83 m
NAC STA
(12.43 ft)3.79 m
NAC STA
(9.35 ft)2.85 m
NAC STA
(17.03 ft)5.19 m
(18.67 ft)5.69 m
FANCOWL
EXHAUSTNOZZLETHRUST
REVERSERDISTANCE FROM
THE NOSE
A
A
B
B
C
C
E
E
D
D
AIR INTAKECOWL
DISTANCE FROMTHE NOSE A340−300 A340−200
(73.46 ft)22.39 m
(66.44 ft)20.25 m
(95.01 ft)28.96 m
(88.02 ft)26.83 m
INBOARDENGINE
OUTBOARDENGINE
(7.97 ft)2.43 m
F_AC_021200_1_0170101_01_00
Engine and NacelleNacelle Dimensions - CFM 56-5C
FIGURE-2-12-0-991-017-A01
2-12-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
4.43 m(14.53 ft)
2.01 m(6.59 ft)
1.99 m(6.53 ft)
55°
0.8 m(2.62 ft)
0.76 m2.49 ft
CONDITIONS: MTOW, MID C.G., STATIC, CFM ENGINES.
INBOARDENGINE
OUTBOARDENGINE
(REFER TOCHAPTER 2−3)
A
NOTE:APPROXIMATE DIMENSIONS
1.24 m (4.07 ft)
2.53 m (8.3 ft)
A
F_AC_021200_1_0180101_01_00
Engine and NacelleFan Cowls - CFM 56-5C
FIGURE-2-12-0-991-018-A01
2-12-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
ABSORBERS AND TIRES ARE AT NOMINAL PRESSURE.HEIGHT DATA GIVEN IS CORRECT WHEN LANDING GEAR SHOCK STRUT
1.69 m(5.54 ft)
NOTE:APPROXIMATE DIMENSIONS
DISTANCE FROMTHE GROUND
INBOARDENGINE
OUTBOARDENGINE
1.21 m(3.97 ft)
2.99 m(9.81 ft)
2.52 m(8.27 ft)
A B
4.05 m(13.29 ft)
* *
45°
A
*
GROUND LINE
*
* * FWD: 1.72 m (5.64 ft)AFT: 1.61 m (5.28 ft)
FWD: 1.2 m (3.94 ft)AFT: 1.33 m (4.36 ft)
B
F_AC_021200_1_0190101_01_00
Engine and NacelleThrust Reverser Cowls - CFM 56-5C
FIGURE-2-12-0-991-019-A01
2-12-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-1 Auxiliary Power Unit
**ON A/C A340-200 A340-300
Auxiliary Power Unit
1. GeneralThe Auxiliary Power Unit (APU) and its related mechanical components are installed at the rear partof the fuselage in the tailcone section. The APU compartment is a fireproof area (identified as theFire Zone).The APU is a pneumatic and shaft-power gas-turbine engine and is used for the ground and in-flightpower supply of the aircraft.
The APU supplies:- mechanical shaft-power to operate a generator- bleed-air to the Main Engine Start (MES) and the Environmental Control System (ECS).
A part of the automatic system, with the pneumatic and the electromechanical controls, operates thestart and the acceleration functions of the APU.An air intake system with a flap-type door is installed in front of the APU compartment. The exhaustgases pass overboard at the end of the fuselage cone.
2. PowerplantThe APU is the Garrett Gas-Turbine Compressor Power-unit (GTCP) 331-350C with a single shaftengine.
The engine is the primary component of the APU, which is of the modular design. The modules ofthe engine are:- The power section- The load compressor- The accessory drive gearbox with LRU(s).
The power section has a two-stage centrifugal compressor, a reverse-flow annular combustionchamber and a three-stage axial turbine. The power section directly operates the one-stagecentrifugal load-compressor which supplies the bleed-air to the pneumatic system. The inlet guidevanes as part of the load compressor, control the airflow.The power section also operates the gearbox which is attached to the load compressor. The followingLRU’s are mounted on the gearbox :- the APU generator,- the starter motor,- the oil pump,- the Fuel Control Unit (FCU),- the cooling air fan.The APU has a gearbox-driven oil-cooled AC generator.
2-12-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The cooling air and ventilation system of the APU supplies the air for cooling of the APU and theequipment on the APU. It also supplies the air for ventilation of the APU compartment.
3. Control circuitThe Electronic Control Box (ECB), which controls the Fuel Control Unit (FCU) and the Inlet GuideVanes (IGV), keeps the APU at a constant speed. The control circuit is used to start the APU, toshut it down, to control it and to prevent internal failure.
4. Controls and IndicationThe primary APU controls and indications are installed in the overhead panel, on the center pedestalpanel and on the forward center panel. External APU panels are also installed on the nose landinggear and on the refuel/defuel panel, to initiate an APU emergency shut-down.
2-12-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
FR106A
FR103
FR101
FR95
FR94
FR92
FR91 317AL
315AL
313AL
Z310
A B
A
316AR
F_AC_021201_1_0020101_01_00
Auxiliary Power UnitAccess Doors (Sheet 1 of 2)FIGURE-2-12-1-991-002-A01
2-12-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
FIRE EXTINGUISHERBOTTLE
AIR INTAKE DUCT
APU
FIRE WALL
BLEED AIR LINE
OIL COOLER OUTLET
EXHAUST MUFFLER
FIXED DIVERTER
GUTTER
FR90
FR92
FR95
FR106A
FIRE WALL
FR101
B
AIR INTAKE
FORWARD
REAR
F_AC_021201_1_0020102_01_00
Auxiliary Power UnitGeneral Layout (Sheet 2 of 2)FIGURE-2-12-1-991-002-A01
2-12-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0 Levelling, symmetry and Alignment
**ON A/C A340-200 A340-300
Leveling, Symmetry and Alignment
1. Quick LevelingThere are three alternative procedures to level the aircraft:- Quick leveling procedure with Air Data/Inertial Reference System (ADIRS)- Quick leveling procedure with a spirit level in the passenger compartment- Quick leveling procedure with a spirit level in the FWD cargo compartment.
2. Precision LevelingFor precise leveling, it is necessary to install sighting rods in the receptacles located under thefuselage (points 12 and 13 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
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
FR57 FR58RIB12
RIB12
FR38 FR39
13
2 RH
2 LH
12
F_AC_021300_1_0040101_01_00
Location of Leveling PointsFIGURE-2-13-0-991-004-A01
2-13-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FR38 FR39
RIB12
FR58FR57.4RIB12
132 LH
2 RH
12
F_AC_021300_1_0050101_01_00
Location of Leveling PointsFIGURE-2-13-0-991-005-A01
2-13-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0 Jacking for Maintenance
**ON A/C A340-200 A340-300
Jacking for Maintenance
1. Aircraft Jacking Points for Maintenance
A. General
(1) The A340-200/-300 can be jacked:- At not more than 152 000 kg (335 103 lb),- Within the limits of the permissible wind speed when the aircraft is jacked outside a
closed environment.
B. Primary Jacking Points
(1) The aircraft are provided with three primary jacking points:- One located under the forward fuselage (after FR10A),- Two located under the wings (one under each wing), at the intersection of RIB10 and
the rear of the spar-datum.
(2) Three jack adapters (ground equipment) are used as intermediary parts between theaircraft jacking points and the jacks:- One male spherical jack adapter at the forward fuselage,- Two female spherical jack pad adapters at the wings (one at each wing).
C. Auxiliary Jacking Point (Safety Stay)
(1) When the aircraft is on jacks, a safety stay is placed under the fuselage at FR85 to preventtail tipping caused by accidental displacement of the aircraft center of gravity.
(2) The safety point must not be used for lifting the aircraft.
(3) One male spherical stay adapter (ground equipment) is used as an intermediary partbetween the aircraft safety point and the stay.
2. Jacks and Safety Stay
A. Jack Design
(1) The maximum eligible loads given in the table (Ref. FIGURE 2-14-0-991-008-AFIGURE2-14-0-991-008-B) are the maximum loads applicable on jack fittings.
(2) In fully retracted position (jack stroke at minimum), the height of the jack is such that thejack may be placed beneath the aircraft under the most adverse conditions, namely, tiresdeflated and shock absorbers depressurized, with sufficient clearance between the aircraftjacking point and the jack upper end.
(3) The lifting jack stroke enables the aircraft to be jacked up so that the Fuselage Datum line(FDL) may be positioned up to 7.2 m (23.62 ft) from the ground to allow all requiredmaintenance procedures and in particular, the removal/installation of the landing-gearshock absorbers.
2-14-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B. Safety StayThe stay stroke enables the aircraft tail to be supported up to the Fuselage Datum Line (FDL)positioned 7.2 m (23.62 ft) from the ground.
2-14-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
SAFETY STAY
WING JACKINGPOINT
C
B’
B
FORWARD FUSELAGEJACKING POINT A
3.58 11.75 0
8.51
−8.51
0
0
27.92
−27.92
0
MAXIMUMLOAD ELIGIBLE
m ft daN
YX
m ft
29.41
29.41
51.54
96.49
96.49
169.09
12 300
80 982
80 982
4 500
FWD JACKINGPOINT
SAFETYSTAY
Y
B’
B
WING JACKINGPOINT
X
NOTE:SAFETY STAY IS NOT USED FOR JACKING.
CA
WING JACKINGPOINT
F_AC_021400_1_0080101_01_00
Jacking for MaintenanceJacking Points Location
FIGURE-2-14-0-991-008-A01
2-14-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
SAFETY STAY
WING JACKINGPOINT
C
B’
B
FORWARD FUSELAGEJACKING POINT A
3.58
31.55
31.55
55.81
11.75
103.51
103.51
183.1
0
8.51
−8.51
0
0
27.92
−27.92
0
MAXIMUMLOAD ELIGIBLE
m ft
12 300
daN
YX
81 084
81 084
4 500
m ft
FWD JACKINGPOINT B’
B
NOTE:SAFETY STAY IS NOT USED FOR JACKING.
Y
X
A C
SAFETYSTAY
WING JACKINGPOINT
WING JACKINGPOINT
F_AC_021400_1_0080201_01_00
Jacking for MaintenanceJacking Points Location
FIGURE-2-14-0-991-008-B01
2-14-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
Z−2157.8
Z−2136
SPHERICALRADIUS 19 mm (0.75 in)
A
FR10A
FR10AA
FWD
B
ADAPTOR −JACK NOSE
B
F_AC_021400_1_0090101_01_00
Jacking for MaintenanceForward Jacking Point
FIGURE-2-14-0-991-009-A01
2-14-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
LOWER SURFACE
EXAMPLE
Z −790.3
Z −700.6
SPHERICALRADIUS 32 mm (1.26 in)
JACKING PADSET−WING
OUTER SKIN
RIB10OUTER SKIN
B
B
A
DATUM INTERSECTIONAT MID REAR SPAR DATUM
RIB10
RIB10
A
A
F_AC_021400_1_0100101_01_00
Jacking for MaintenanceWing Jacking Points
FIGURE-2-14-0-991-010-A01
2-14-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
ADAPT−SUPP, AFT JACK
SPHERICALRADIUS 19 mm (0.75 in)
Z −474.0
Z −440.7
A
FR85
B
B
FWD
FR85
A
F_AC_021400_1_0110101_01_00
Jacking for MaintenanceAuxiliary Jacking Point - Safety Stay
FIGURE-2-14-0-991-011-A01
2-14-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
L
AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 152 000 kg (335 103 lb)
2.61 m(8.56 ft)
4.46 m(14.63 ft)
5.36 m(17.59 ft)
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES
2.2 m(7.22 ft)
4.11 m(13.48 ft)
4.77 m(15.65 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6.5 m (21.33 ft) FOR LANDINGGEARS EXTENSION/RETRACTION
4.37 m(14.34 ft)
5.8 m(19.03 ft)
6.06 m(19.88 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7.2 m (23.62 ft) FOR LANDINGGEARS REMOVAL/INSTALLATION
5.07 m(16.63 ft)
6.5 m(21.33 ft)
6.76 m(22.18 ft)
L M N
AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 127 000 kg (279 987 lb)
2.62 m(8.6 ft)
4.51 m(14.8 ft)
5.43 m(17.81 ft)
FUSELAGE
N
DATUM LINE
M
F_AC_021400_1_0120101_01_00
Jacking for MaintenanceJacking Dimensions
FIGURE-2-14-0-991-012-A01
2-14-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
L
AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 152 000 kg (335 103 lb)
2.52 m(8.27 ft)
4.46 m(14.63 ft)
5.38 m(17.65 ft)
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES
2.2 m(7.22 ft)
4.1 m(13.45 ft)
4.77 m(15.65 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6.5 m (21.33 ft) FOR LANDINGGEARS EXTENSION/RETRACTION
4.37 m(14.34 ft)
5.8 m(19.03 ft)
6.06 m(19.88 ft)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7.2 m (23.62 ft) FOR LANDINGGEARS REMOVAL/INSTALLATION
5.07 m(16.63 ft)
6.5 m(21.33 ft)
6.76 m(22.18 ft)
L M N
AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 131 215 kg (279 279 lb)
2.58 m(8.47 ft)
4.51 m(14.8 ft)
5.39 m(17.68 ft)
FUSELAGE
N
DATUM LINE
M
F_AC_021400_1_0120201_01_00
Jacking for MaintenanceJacking Dimensions
FIGURE-2-14-0-991-012-B01
2-14-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
80
90
100
110
120
130
140
150
0 6 8 10 12 14 16 18 20
80
90
100
110
120
130
140
150
160
170 40
2520
1510
45 20 30 40 50 60 70
5
2 4
160
170
LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1 000)
LOA
D O
N W
ING
JA
CK
ING
PO
INT
S (
kg x
1 0
00)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
kg x
1 0
00)
PERMISSIBLE WIND SPEED (km/h)
AIRCRAFT CG (%RC)
EXAMPLE:
AT 22.8% RC . THE REACTION AT THE WING JACKING POINTS IS 137 000 kg(68 500 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINT
IS 8 000 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT
ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 145 000 kg AND CENTER OF GRAVITYAB
CD
BE IN EXCESS OF 50 km/h.
A
D
C
TIP UPSECURITYMARGIN
B
3035
F_AC_021400_1_0130101_01_00
Jacking for MaintenanceLoad at the Aircraft Jacking Points
FIGURE-2-14-0-991-013-A01
2-14-0Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
0 6 8 10 12 14 16 18 20
80
90
100
110
120
130
140
150
160
170 4035
2520
1510
45 20 30 40 50 60 70
50
2 4
80
90
100
110
120
130
140
150
160
170
EXAMPLE:
AT 22.8% RC . THE REACTION AT THE WING JACKING POINTS IS 136 000 kg(68 000 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINT
IS 9 000 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT
ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 145 000 kg AND CENTER OF GRAVITYAB
CD
BE IN EXCESS OF 60 km/h.
TIP UPSECURITYMARGIN
LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1 000)
LOA
D O
N W
ING
JA
CK
ING
PO
INT
S (
kg x
1 0
00)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
kg x
1 0
00)
PERMISSIBLE WIND SPEED (km/h)
30
A
B
D
C
AIRCRAFT CG (%RC)
F_AC_021400_1_0130201_01_00
Jacking for MaintenanceLoad at the Aircraft Jacking Points
FIGURE-2-14-0-991-013-B01
2-14-0Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-1 Jacking of the Landing Gear
**ON A/C A340-200 A340-300
Jacking of the Landing Gear
1. GeneralLanding gear jacking will be required to lift the landing gear wheels off the ground.
NOTE : You can lift the aircraft at Maximum Ramp Weight (MRW).
NOTE : The load at each jacking position is the load required to give 25.4 mm (1 in) clearancebetween the ground and the tire.
2. Main Gear JackingThe 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. Nose Gear JackingFor nose gear jacking, a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shock-absorber 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.
4. Center Gear JackingFor center gear jacking, a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shock-absorber 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.
2-14-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
AFT WHEELS JACKED UPFWD WHEELS INSTALLED AND INFLATED
FWD WHEELS JACKED UPAFT WHEELS INSTALLED AND INFLATED
JACKING POINT570 mm
(22.44 in)
MAX DIAMETER1 443.7 mm(56.84 in)
25.4 mm(1 in)
NORMAL ATTITUDE
JACKING POINT376 mm(14.8 in)
25.4 mm(1 in)
FWD
FWD
FWD
JACKING POINT376 mm(14.8 in)
JACKING POINT570 mm
(22.44 in)
F_AC_021401_1_0050102_01_00
Jacking of the Landing GearMLG Jacking Point Heights (Sheet 1 of 3)
FIGURE-2-14-1-991-005-A01
2-14-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
FWD AXLEBOTH TIRES SHREDDED OR DEFLATED
AFT AXLEBOTH TIRES SHREDDED OR DEFLATED
FWD AND AFT AXLEBOTH TIRES SHREDDED OR DEFLATED
JACKING POINT376 mm(14.8 in)JACKING POINT
145.9 mm(5.74 in)
JACKING POINT376 mm(14.8 in) JACKING POINT
145.5 mm(5.73 in)
JACKING POINT157 mm(6.18 in)
JACKING POINT157 mm(6.18 in)
FWD
FWD
FWD
F_AC_021401_1_0050103_01_00
Jacking of the Landing GearMLG Jacking Point Heights (Sheet 2 of 3)
FIGURE-2-14-1-991-005-A01
2-14-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
AFT AXLEBOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
JACKING POINT376 mm(14.8 in) JACKING POINT
118.8 mm(4.68 in)
FWD
FWD AND AFT AXLESTIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
JACKING POINT130 mm(5.12 in)
JACKING POINT130 mm(5.12 in)
FWD
JACKING POINT376 mm(14.8 in)JACKING POINT
118.8 mm(4.68 in)
FWD
FWD AXLEBOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN
F_AC_021401_1_0050104_01_00
Jacking of the Landing GearMLG Jacking Point Heights (Sheet 3 of 3)
FIGURE-2-14-1-991-005-A01
2-14-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
1 FLAT TIRE110 mm(4.33 in)180 mm MAX
(7.09 in)
(1 in)25.4 mm
400 mm
(15.75 in)
170 mm(6.69 in) FWD
F_AC_021401_1_0060101_01_00
Jacking of the Landing GearJacking of the NLG (Sheet 1 of 2)
FIGURE-2-14-1-991-006-A01
2-14-1Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
1 083 mm(42.64 in)
270 mm(10.63 in)
NORMAL ATTITUDE
TWO TIRES DEFLATED OR SHREDDED
HEIGHT OF JACKING POINT TO GROUNDTO CHANGE/REPLACE THE WHEEL ASSEMBLY
297.5 mm(11.71 in)
JACKING POINT290 mm
(11.42 in)
JACKING POINT148.5 mm(5.85 in)
JACKING POINT400 mm
(15.75 in)
25.4 mm(1 in)
FWD
FWD
FWD
F_AC_021401_1_0060102_01_00
Jacking of the Landing GearNLG Jacking Point Heights (Sheet 2 of 2)
FIGURE-2-14-1-991-006-A01
2-14-1Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
640 mm(25.19 in)
235 mm(9.25 in) FWD
300 mm(11.81 in)
94° 15’
F_AC_021401_1_0070101_01_00
Jacking of the Landing GearJacking of the CLG (Sheet 1 of 2)
FIGURE-2-14-1-991-007-A01
2-14-1Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
TWO TIRES DEFLATED OR SHREDDED
HEIGHT OF JACKING POINT TO GROUNDTO CHANGE/REPLACE THE WHEEL ASSEMBLY
NORMAL ATTITUDE
343 mm(13.5 in)
JACKING POINT480.7 mm(18.93 in)
363 mm(14.29 in)
FWD
JACKING POINT236.4 mm(9.31 in)FWD
FWD
1 443.7 mm(56.84 in)
JACKING POINT641.2 mm(25.24 in)
25.4 mm(1 in)
F_AC_021401_1_0070102_01_00
Jacking of the Landing GearCLG Jacking Point Heights (Sheet 2 of 2)
FIGURE-2-14-1-991-007-A01
2-14-1Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
AIRCRAFT GROSS WEIGHT
280 320 360 400 440 480 520
120 140 160 180 200 220 24020
50
70
90
120
260
560
(x 1 000 kg)
(x 1 000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
280
600
30
40
60
80
100
110
260
250
240
230
220
210
200
190
180
170
160
150
140
130
120
110
100
90
80
70
60
50
100
240
35% MAC25% MAC18% MAC
42% MACCG POSITION
F_AC_021401_1_0080101_01_00
Jacking of the Landing GearMLG Jacking Point Loads
FIGURE-2-14-1-991-008-A01
2-14-1Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
35% MAC25% MAC20% MAC
41% MACCG POSITION
AIRCRAFT GROSS WEIGHT
280 320 360 400 440 480 520
120 140 160 180 200 220 24040
50
60
70
80
90
100
110
120
260
560
(x 1 000 kg)
(x 1 000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
280
600
100
90
F_AC_021401_1_0080201_01_00
Jacking of the Landing GearMLG Jacking Point Loads
FIGURE-2-14-1-991-008-B01
2-14-1Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
120 140 160 180 200 220 240 260
AIRCRAFT GROSS WEIGHT
280 320 360 400 440 480 520
2
22
30
560
(x 1 000 kg)
(x 1 000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
280
600
6
26
100
240
55
45
35
25
15
65
4
8
20
24
18
16
14
12
10
28
10
5
20
30
40
50
60
25% MAC35% MAC42% MAC
18% MACCG POSITION
F_AC_021401_1_0090101_01_00
Jacking of the Landing GearNLG Jacking Point Loads
FIGURE-2-14-1-991-009-A01
2-14-1Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
AIRCRAFT GROSS WEIGHT
280 320 360 400 440 480 520
120 140 160 180 200 220 2400
5
10
15
20
25
30
35
40
260
560
(x 1 000 kg)
(x 1 000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
10
20
30
40
50
60
70
80
280
600
0
25% MAC35% MAC41% MAC
20% MACCG POSITION
F_AC_021401_1_0090201_01_00
Jacking of the Landing GearNLG Jacking Point Loads
FIGURE-2-14-1-991-009-B01
2-14-1Page 12
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
280 320 360 400 440 480 520 560 600240
AIRCRAFT GROSS WEIGHT
120 140 160 180 200 220 2400
6
10
14
260(x 1 000 kg)
(x 1 000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
280
2
4
8
12
1000
25
20
15
10
5
30
35% MAC25% MAC18% MAC
42% MACCG POSITION
F_AC_021401_1_0100101_01_00
Jacking of the Landing GearCLG Jacking Point Loads
FIGURE-2-14-1-991-010-A01
2-14-1Page 13
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
AIRCRAFT GROSS WEIGHT
120 140 160 180 200 220 2400
5
15
20
25
30
260(x 1 000 kg)
(x 1 000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x 1
000
lb)
280
10
35
40
45
10
20
30
40
50
60
70
80
90
0
35% MAC25% MAC20% MAC
41% MACCG POSITION
280 320 360 400 440 480 520 560 600
F_AC_021401_1_0100201_01_00
Jacking of the Landing GearCLG Jacking Point Loads
FIGURE-2-14-1-991-010-B01
2-14-1Page 14
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-2 Support of Aircraft
**ON A/C A340-200 A340-300
Support of Aircraft
1. Support of AircraftWhen it is necessary to support the aircraft in order to relieve the loads on the structure for theaccomplishment of modifications or major work, it is advisable to provide adapters under the wingsand the fuselage for an alternative means of lifting.
The aircraft must not be lifted or supported by the wings or fuselage alone. It is important to supportthe aircraft fuselage and wings at the same time to prevent structural damage.
A. Shoring CradlesShoring 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 in) square, are positioned atfour locations under each wing.
The adjustable pads are faced with thin rubber and are in contact with the wing profile at thedatum intersections of the ribs and the front and rear spars (F/S and R/S).
2-14-2Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
(SAFETY STAY)FR85FR80
FR72
FR26
FR17
FR11
RIB6 RIB6
NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
FR58
RIB16RIB21
RIB31
FR53.2
RIB31
RIB21RIB16
F_AC_021402_1_0020101_01_00
Support of AircraftLocation of Shoring Cradles (Sheet 1 of 2)
FIGURE-2-14-2-991-002-A01
2-14-2Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
FR7
FR17
FR20
FR26.1
FR32
FR39.1 FR53.8 FR59 FR76
A
LH SHOWN
(9.02 ft)2.75 m
(15.09 ft)4.6 m
(6.89 ft)2.1 m
EXAMPLE
A
B
RH SYMMETRICAL
B B
F_AC_021402_1_0020102_01_00
Support of AircraftLocation of Auxiliary Jacking Points (Sheet 2 of 2)
FIGURE-2-14-2-991-002-A01
2-14-2Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FR80
FR72
FR26
FR17
FR11
(SAFETY STAY)FR85
NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
RIB6 RIB6
RIB31
RIB21RIB16
FR58
FR53.2
RIB16RIB21
RIB31
F_AC_021402_1_0020201_01_00
Support of AircraftLocation of Shoring Cradles (Sheet 1 of 2)
FIGURE-2-14-2-991-002-B01
2-14-2Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FR7
FR17 FR20
FR26.1
FR59 FR76FR39.1FR36 FR53.8
A
LH SHOWN
(9.02 ft)2.75 m
(15.09 ft)4.6 m
(6.89 ft)2.1 m
EXAMPLE
A
B
RH SYMMETRICAL
B B
F_AC_021402_1_0020202_01_00
Support of AircraftLocation of Auxiliary Jacking Points (Sheet 2 of 2)
FIGURE-2-14-2-991-002-B01
2-14-2Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0 General Information
**ON A/C A340-200 A340-300
General Information
1. Standard day temperatures for the altitude 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 1220 44.7 7.16000 1830 37.6 3.18000 2440 30.5 -0.8
3-1-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1 Payload / Range - ISA Conditions
**ON A/C A340-200 A340-300
Payload / Range - ISA Conditions
1. This section gives the payload / range at ISA conditions.
3-2-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
0
10
20
30
40
50
60
70
80
90
100
110
120
3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500
160007000 8000 9000 10000 11000 12000 13000 14000 15000
270
280
290
300
310
320
330
340
350
360
370
380
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE: MAX TAKE−OFF WEIGHTZFW
(x 1000 lb)PAYLOAD(x 1000 lb)
RANGE(nm)
RANGE(km)
MAX STRUCTURAL PAYLOAD
MAX PASSENGER PAYLOAD
CRUISE CONDITIONSISA 39000 ft M = 0.82
F_AC_030201_1_0110101_01_01
Payload / Range - ISA ConditionsCFM56-5C2 engine
FIGURE-3-2-1-991-011-A01
3-2-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
0
10
20
30
40
50
60
70
80
90
100
110
120
3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500
160007000 8000 9000 10000 11000 12000 13000 14000 15000
270
280
290
300
310
320
330
340
350
360
370
380
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE: MAX TAKE−OFF WEIGHTZFW
(x 1000 lb)PAYLOAD(x 1000 lb)
RANGE(nm)
RANGE(km)
MAX PASSENGER PAYLOAD
MAX STRUCTURAL PAYLOAD
CRUISE CONDITIONSISA 39000 ft M = 0.82
F_AC_030201_1_0120101_01_01
Payload / Range - ISA ConditionsCFM56-5C2 engine
FIGURE-3-2-1-991-012-A01
3-2-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
0
10
20
30
40
50
60
70
80
90
100
110
120
3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500
160007000 8000 9000 10000 11000 12000 13000 14000 15000
270
280
290
300
310
320
330
340
350
360
370
380
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE: MAX TAKE−OFF WEIGHTZFW
(x 1000 lb)PAYLOAD(x 1000 lb)
RANGE(nm)
RANGE(km)
MAX PASSENGER PAYLOAD
MAX STRUCTURAL PAYLOAD
CRUISE CONDITIONSISA 39000 ft M = 0.82
F_AC_030201_1_0130101_01_01
Payload / Range - ISA ConditionsCFM56-5C3 engine
FIGURE-3-2-1-991-013-A01
3-2-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
0
10
20
30
40
50
60
70
80
90
100
110
120
3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500
160007000 8000 9000 10000 11000 12000 13000 14000 15000
270
280
290
300
310
320
330
340
350
360
370
380
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE: MAX TAKE−OFF WEIGHTZFW
(x 1000 lb)PAYLOAD(x 1000 lb)
RANGE(nm)
RANGE(km)
MAX PASSENGER PAYLOAD
MAX STRUCTURAL PAYLOAD
CRUISE CONDITIONSISA 39000 ft M = 0.82
F_AC_030201_1_0140101_01_01
Payload / Range - ISA ConditionsCFM56-5C3 engine
FIGURE-3-2-1-991-014-A01
3-2-1Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
0
10
20
30
40
50
60
70
80
90
100
110
120
3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500
160007000 8000 9000 10000 11000 12000 13000 14000 15000
270
280
290
300
310
320
330
340
350
360
370
380
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE: MAX TAKE−OFF WEIGHTZFW
(x 1000 lb)PAYLOAD(x 1000 lb)
RANGE(nm)
RANGE(km)
BASIC AIRCRAFT257 000 kg MTOW
NOMINAL PERFORMANCE LEVEL
MAX STRUCTURAL PAYLOAD
MAX PASSENGER PAYLOAD
CRUISE CONDITIONSISA 39000 ft M = 0.82
F_AC_030201_1_0150101_01_01
Payload / Range - ISA ConditionsCFM56-5C4 engine
FIGURE-3-2-1-991-015-A01
3-2-1Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
0
10
20
30
40
50
60
70
80
90
100
110
120
3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500
160007000 8000 9000 10000 11000 12000 13000 14000 15000
270
280
290
300
310
320
330
340
350
360
370
380
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE: MAX TAKE−OFF WEIGHTZFW
(x 1000 lb)PAYLOAD(x 1000 lb)
RANGE(nm)
RANGE(km)
MAX PASSENGER PAYLOAD
MAX STRUCTURAL PAYLOAD
CRUISE CONDITIONSISA 39000 ft M = 0.82
F_AC_030201_1_0160101_01_01
Payload / Range - ISA ConditionsCFM56-5C4 engine
FIGURE-3-2-1-991-016-A01
3-2-1Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
0
10
20
30
40
50
60
70
80
90
100
110
120
4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500
160007000 8000 9000 10000 11000 12000 13000 14000 15000
270
280
290
300
310
320
330
340
350
360
370
380
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE: MAX TAKE−OFF WEIGHTZFW
(x 1000 lb)PAYLOAD(x 1000 lb)
RANGE(nm)
RANGE(km)
BASIC AIRCRAFT271 000 kg AND 275 000 kg MTOWNOMINAL PERFORMANCE LEVEL
275 000 kg
271 000 kg
MAX STRUCTURAL PAYLOAD
MAX PASSENGER PAYLOAD
CRUISE CONDITIONSISA 39000 ft M = 0.82
F_AC_030201_1_0170101_01_01
Payload / Range - ISA ConditionsCFM56-5C4 engine
FIGURE-3-2-1-991-017-A01
3-2-1Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1 Take-Off Weight Limitation - ISA Conditions
**ON A/C A340-200 A340-300
Take-Off Weight Limitation - ISA Conditions
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
TAKE−OFF WEIGHT1000 lb1000 kg
RUNWAY LENGHT(1000 ft)
RUNWAY LENGHT(1000 m)
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
THES CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
640
145
165
185
205
225
245
265
285
FLAPS 3 FLAPS 1
0
F_AC_030301_1_0040101_01_00
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
2
4
6
8
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA Conditions -- CFM56-5C2 engine
FIGURE-3-3-1-991-004-A01
3-3-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
TAKE−OFF WEIGHT1000 lb1000 kg
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
0
FLAPS 2
580
600
620
640
145
165
185
205
225
245
265
285
FLAPS 3 FLAPS 1
NOTE: THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
2
F_AC_030301_1_0050101_01_00
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
4
6
8
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA Conditions -- CFM56-5C2 engine
FIGURE-3-3-1-991-005-A01
3-3-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
TAKE−OFF WEIGHT1000 lb1000 kg
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
RUNWAY LENGTH(1000 m)
RUNWAY LENGTH(1000 ft)
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
8
0
4
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
6
2
BRAKE ENERGY
V.M.C
LIMITATION
F_AC_030301_1_0060101_01_00
Take-Off Weight LimitationISA Conditions -- CFM56-5C3 engine
FIGURE-3-3-1-991-006-A01
3-3-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
1000 lb1000 kg
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
F_AC_030301_1_0070101_01_00
TAKE−OFF WEIGHT
0
2
4
6
8 AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA Conditions -- CFM56-5C3 engine
FIGURE-3-3-1-991-007-A01
3-3-1Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
1000 lb1000 kg
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
F_AC_030301_1_0080101_01_00
TAKE−OFF WEIGHT
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)0
2
4
6
8
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA Conditions -- CFM56-5C4 engine
FIGURE-3-3-1-991-008-A01
3-3-1Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
1000 lb1000 kg
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
F_AC_030301_1_0090101_01_00
TAKE−OFF WEIGHT
8
6
4
2
0
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA Conditions -- CFM56-5C4 engine
FIGURE-3-3-1-991-009-A01
3-3-1Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2 Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions
**ON A/C A340-200 A340-300
Take-Off Weight Limitation - 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
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
1000 lb1000 kg
RUNWAY LENGHT(1000 ft)
RUNWAY LENGHT(1000 m)
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
THES CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
640
145
165
185
205
225
245
265
285
FLAPS 3 FLAPS 1
F_AC_030302_1_0040101_01_00
TAKE−OFF WEIGHT
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)0
2
4
6
8
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56-5C2 engine
FIGURE-3-3-2-991-004-A01
3-3-2Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
1000 lb1000 kg
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
640
145
165
185
205
225
245
265
285
FLAPS 3 FLAPS 1
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
F_AC_030302_1_0050101_01_00
TAKE−OFF WEIGHT
0
2
4
6
8
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56-5C2 engine
FIGURE-3-3-2-991-005-A01
3-3-2Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
1000 lb1000 kg
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 m)
RUNWAY LENGTH(1000 ft)
F_AC_030302_1_0060101_01_00
TAKE−OFF WEIGHT
0
2
4
6
8 AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56-5C3 engine
FIGURE-3-3-2-991-006-A01
3-3-2Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
F_AC_030302_1_0070101_01_00
1000 lb1000 kgTAKE−OFF WEIGHT
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
0
2
4
6
8
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56-5C3 engine
FIGURE-3-3-2-991-007-A01
3-3-2Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
F_AC_030302_1_0080101_01_00
1000 lb1000 kgTAKE−OFF WEIGHT
0
2
4
6
8
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56-5C4 engine
FIGURE-3-3-2-991-008-A01
3-3-2Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
NOTE:
320
340
360
380
400
420
440
460
480
500
520
540
560
4 6 8 10 12 14 16
1 1.5 2 2.5 3 3.5 4 4.5 5
FLAPS 2
580
600
620
145
165
185
205
225
245
265
FLAPS 3 FLAPS 1
640
660
285
680305
THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT
RUNWAY LENGTH(1000 ft)
RUNWAY LENGTH(1000 m)
F_AC_030302_1_0090101_01_00
1000 lb1000 kgTAKE−OFF WEIGHT
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)0
2
4
6
8
BRAKE ENERGY
V.M.C
LIMITATION
Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56-5C4 engine
FIGURE-3-3-2-991-009-A01
3-3-2Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1 Landing Field Length - ISA Conditions
**ON A/C A340-200 A340-300
Landing Field Length - ISA Conditions
1. This section gives the landing field length.
3-4-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
345678
1
1.52
2.5
NO
TE
: 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
.
GR
OS
S W
EIG
HT
(x 1
000
kg)
GR
OS
S W
EIG
HT
(x 1
000
lb)
(x 1
000
m)
(x 1
000
ft)
24
68
10S
EA
LE
VE
L
150
200
250
300
350
400
450
500
7510
012
515
017
520
025
050
225
ISA
CO
ND
ITIO
NS
AIR
FIE
LD E
LEV
AT
ION
(x 1
000
ft)
LAN
DIN
G F
IELD
LE
NG
HT
F_AC_030401_1_0040101_01_01
Landing Field LengthISA Conditions -- CFM56-5C2 engine
FIGURE-3-4-1-991-004-A01
3-4-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
345678
1
1.52
2.5
NO
TE
:T
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
GT
HE
AIR
CR
AF
T.
GR
OS
S W
EIG
HT
(x 1
000
kg)
GR
OS
S W
EIG
HT
(x 1
000
lb)
24
68
10S
EA
LE
VE
L
150
200
250
300
350
400
450
500
7510
012
515
017
520
025
050
225
AIR
FIE
LD E
LEV
AT
ION
(x 1
000
ft)
LAN
DIN
G F
IELD
LE
NG
HT
(x 1
000
m)
(x 1
000
ft)
ISA
CO
ND
ITIO
NS
F_AC_030401_1_0050101_01_01
Landing Field LengthISA Conditions -- CFM56-5C2 engine
FIGURE-3-4-1-991-005-A01
3-4-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
345678
1
1.52
2.5
NO
TE
:T
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
GT
HE
AIR
CR
AF
T.
GR
OS
S W
EIG
HT
(x 1
000
kg)
GR
OS
S W
EIG
HT
(x 1
000
lb)
24
68
10S
EA
LE
VE
L
150
200
250
300
350
400
450
500
7510
012
515
017
520
025
050
225
AIR
FIE
LD E
LEV
AT
ION
(x 1
000
ft)
LAN
DIN
G F
IELD
LE
NG
HT
ISA
CO
ND
ITIO
NS
(x 1
000
m)
(x10
00 ft
)
F_AC_030401_1_0060101_01_01
Landing Field LengthISA Conditions -- CFM56-5C3 engine
FIGURE-3-4-1-991-006-A01
3-4-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
345678
1
1.52
2.5
NO
TE
:T
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
GT
HE
AIR
CR
AF
T.
GR
OS
S W
EIG
HT
(x 1
000
kg)
GR
OS
S W
EIG
HT
(x 1
000
lb)
24
68
10S
EA
LE
VE
L
150
200
250
300
350
400
450
500
7510
012
515
017
520
025
050
225
AIR
FIE
LD E
LEV
AT
ION
(x 1
000
ft)
LAN
DIN
G F
IELD
LE
NG
HT
(x 1
000
m)
(x 1
000
ft)
ISA
CO
ND
ITIO
NS
F_AC_030401_1_0070101_01_01
Landing Field LengthISA Conditions -- CFM56-5C3 engine
FIGURE-3-4-1-991-007-A01
3-4-1Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
345678
1
1.52
2.5
NO
TE
:T
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
GT
HE
AIR
CR
AF
T.
GR
OS
S W
EIG
HT
(x 1
000
kg)
GR
OS
S W
EIG
HT
(x 1
000
lb)
24
68
10S
EA
LE
VE
L
150
200
250
300
350
400
450
500
7510
012
515
017
520
025
050
225
AIR
FIE
LD E
LEV
AT
ION
(x 1
000
ft)
LAN
DIN
G F
IELD
LE
NG
HT
ISA
CO
ND
ITIO
NS
(x 1
000
m)
(x 1
000
ft)
F_AC_030401_1_0080101_01_01
Landing Field LengthISA Conditions -- CFM56-5C4 engine
FIGURE-3-4-1-991-008-A01
3-4-1Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
345678
1
1.52
2.5
NO
TE
:T
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
GT
HE
AIR
CR
AF
T.
GR
OS
S W
EIG
HT
(x 1
000
kg)
GR
OS
S W
EIG
HT
(x 1
000
lb)
24
68
10S
EA
LE
VE
L
150
200
250
300
350
400
450
500
7510
012
515
017
520
025
050
225
AIR
FIE
LD E
LEV
AT
ION
(x 1
000
ft)
LAN
DIN
G F
IELD
LE
NG
HT
(x 1
000
m)
(x 1
000
ft)
ISA
CO
ND
ITIO
NS
F_AC_030401_1_0090101_01_01
Landing Field LengthISA Conditions -- CFM56-5C4 engine
FIGURE-3-4-1-991-009-A01
3-4-1Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0 Final Approach Speed
**ON A/C A340-200 A340-300
Final Approach Speed
**ON A/C A340-200
1. Final Approach Speed
A. This section gives the final approach speed. This is the indicated airspeed at threshold in thelanding configuration, at the certificated maximum flap setting and maximum landing weight, instandard atmospheric conditions. The approach speed is used to classify the aircraft into anAircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.
B. The final approach speed is 136 kt at a Maximum Landing Weight (MLW) of 185 000 kg (407855 lb) and classifies the aircraft into the Aircraft Approach Category C.
NOTE : This value is given for information only.
**ON A/C A340-300
2. Final Approach Speed
A. This section gives the final approach speed. This is the indicated airspeed at threshold in thelanding configuration, at the certificated maximum flap setting and maximum landing weight, instandard atmospheric conditions. The approach speed is used to classify the aircraft into anAircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.
B. The final approach speed is 138 kt at a Maximum Landing Weight (MLW) of 192 000 kg (423287 lb) and classifies the aircraft into the Aircraft Approach Category C.
NOTE : This value is given for information only.
3-5-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A340-200 A340-300
General Information
1. This section provides aircraft 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 airlines in question prior to layout planning
4-1-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0 Turning Radii
**ON A/C A340-200 A340-300
Turning Radii
1. This section provides the turning radii.
4-2-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
62°60°
55°
R6
R4
R5
R3
NOTE:FOR TURNING RADII VALUES, REFER TO SHEET 2.
R2
R1
F_AC_040200_1_0050101_01_02
Turning Radii(Sheet 1)
FIGURE-4-2-0-991-005-A01
4-2-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
19.320
TYPE OFTURN
267.9223
A340−300 TURNING RADII
m
ft78.6258
77.2253
R4WING
102.9338
R5NOSE
79.1260
R6TAIL
87.9288
R1RMLG
R2LMLG
R3NLG
24.125252.3172
62.9206
62.6205
87.3286
65.1214
73.5241
28.930241.5136
52.2171
52.9174
76.7252
56.0184
64.0210
33.735233.7111
44.4146
46.2152
68.9226
49.8163
57.3188
38.440227.791
38.3126
41.3135
62.9206
45.3149
52.4172
43.045222.875
33.5110
37.6123
58.1191
42.0138
48.6159
47.550218.862
29.597
34.8114
54.2178
39.6130
45.7150
51.955215.5
5126.286
32.6107
51.0167
37.7124
43.3142
56.060212.842
23.477
30.9101
48.2158
36.3119
41.5136
59.665210.534
21.270
29.797
46.0151
35.3116
40.1132
62.47028.929
19.564
28.995
44.4146
34.7114
39.1128
51.750115.752
26.487
32.7107
51.1168
37.8124
43.4142
56.555112.4
4123.176
30.7101
47.9157
36.2119
41.3135
61.26019.531
20.266
29.296
45.1148
34.9115
39.5130
65.96517.023
17.758
28.092
42.6140
34.0112
38.0125
70.47014.715
15.350
27.189
40.3132
33.3109
36.8121
m
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ft
m
ftm
ftm
ftm
ftm
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION.TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; AND NO DIFFERENTIAL BRAKING AT ALL.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYINGDIFFERENTIAL BRAKING DURING THE WHOLE TURN.
63.27228.428
19.163
28.794
44.0144
34.5113
38.8127
m
ft
72.27213.812
14.548
26.888
39.5130
33.1109
36.3119
m
ft
F_AC_040200_1_0100101_01_01
Turning Radii(Sheet 2)
FIGURE-4-2-0-991-010-A01
4-2-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
19.120
TYPE OFTURN
262.6205
A340−200 TURNING RADII
m
ft73.3240
71.4234
R4WING
97.6320
R5NOSE
73.4241
R6TAIL
82.2270
R1RMLG
R2LMLG
R3NLG
23.925248.1158
58.8193
57.9190
83.2273
60.4198
68.8226
28.630238.2125
48.9160
49.0161
73.4241
52.1171
60.1197
33.335231.0102
41.7137
42.8140
66.3218
46.4152
53.9177
37.940225.584
36.2119
38.3126
60.8199
42.3139
49.4162
42.445221.169
31.7104
34.9115
56.4185
39.3129
45.9151
46.850217.557
28.192
32.3106
52.9174
37.0121
43.2142
50.955214.548
25.283
30.399
49.9164
35.4116
41.1135
54.860212.039
22.775
28.894
47.5156
34.1112
39.4129
58.065210.133
20.868
27.791
45.7150
33.2109
38.2125
60.37028.929
19.664
27.089
44.4146
32.7107
37.4123
51.350114.247
24.982
30.199
49.7163
35.2115
40.9134
56.155111.337
22.072
28.393
46.8154
33.8111
38.9128
60.76018.729
19.363
26.988
44.2145
32.6107
37.3122
65.36516.321
17.056
25.885
42.0138
31.8104
35.9118
69.77014.214
14.949
25.082
39.9131
31.1102
34.7114
m
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ftm
ft
m
ftm
ftm
ftm
ftm
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION.TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; AND NO DIFFERENTIAL BRAKING AT ALL.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYINGDIFFERENTIAL BRAKING DURING THE WHOLE TURN.
60.87228.628
19.363
26.988
44.2145
32.6107
37.2122
m
ft
71.67213.411
14.146
24.781
39.1128
30.9101
34.3113
m
ft
F_AC_040200_1_0110101_01_01
Turning Radii(Sheet 2)
FIGURE-4-2-0-991-011-A01
4-2-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A340-200 A340-300
Minimum Turning Radii
1. This section provides the minimum turning radii.
4-3-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
NOTE:TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLETURN; AND NO DIFFERENTIAL BRAKING AT ALL.
A(MINIMUM TURNING WIDTH)
65.965 (MAX)
TYPE OFTURN
111.437
A340−300 MINIMUM TURNING RADII
m
ft46.0151
28.092
R4WING
42.6140
R5NOSE
34.0112
R6TAIL
38.0125
R3NLG
59.665 (MAX)214.949
51.2168
29.797
46.0151
35.3116
40.1132
m
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
25.483
25.483
AX Y
Y
R6
R4
OUTSIDE FACEOF TIRE
72 (MAX)
72 (MAX)
2
1
63.2
72.2m
ftm
ft
8.227
41.7137
26.888
39.5130
33.1109
36.3119
12.842
48.1158
28.794
44.0144
34.5113
38.8127
25.483
25.483
R5
R3
X
F_AC_040300_1_0030101_01_02
Minimum Turning RadiiFIGURE-4-3-0-991-003-A01
4-3-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
NOTE:TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLETURN; AND NO DIFFERENTIAL BRAKING AT ALL.
A(MINIMUM TURNING WIDTH)
65.365 (MAX)
TYPE OFTURN
110.735
A340−200 MINIMUM TURNING RADII
m
ft43.2142
25.885
R4WING
42.0138
R5NOSE
31.8104
R6TAIL
35.9118
R3NLG
58.065 (MAX)214.548
48.8160
27.791
45.7150
33.2109
38.2125
m
ft
STEERING ANGLE (deg)EFFECTIVESTEERING
ANGLE (deg)
NOTE:IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
23.276
23.276
AX Y
72 (MAX)
72 (MAX)
2
1
60.8
71.6m
ftm
ft
7.725
39.1128
24.781
39.1128
30.9101
34.3113
13.043
46.5153
26.988
44.2145
32.6107
37.2122
23.276
23.276
R6
R4
R5
R3
Y
OUTSIDE FACEOF TIRE
X
F_AC_040300_1_0040101_01_02
Minimum Turning RadiiFIGURE-4-3-0-991-004-A01
4-3-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A340-200 A340-300
Visibility from Cockpit in Static Position
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
NOT TO BE USED FORLANDING APPROACH VISIBILITY
CAPTAIN FIELD OF VIEW
VISUAL ANGLES IN HORIZONTALPLANE THROUGH PILOTEYE POSITION.
FIRST OFFICERFIELD OF VIEW
25°
20°
13.75 m(45.11 ft)
6.67 m(21.88 ft)
VISUAL ANGLES IN VERTICALPLANE THROUGH PILOTEYE POSITION.
DIMENSIONS ARE APPROXIMATE
2.4 m(7.87 ft)
NOTE:PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
ZONE THAT CANNOT BE SEEN
MAX AFT VISION WITH HEAD TURNEDAROUND SPINAL COLUMN.WING TIP CAN BE SEEN WHEN HEAD IS MOVEDTO THE SIDE.
0.53 m(1.74 ft)
62°
42°
30°36°
30°
VISUAL ANGLES IN PLANEPERPENDICULAR TOLONGITUDINAL AXIS.
62°
42°
WITH HEAD MOVED125 mm (5 in) OUTBOARD
36°
115°
135°
115°
135°
F_AC_040400_1_0040101_01_02
Visibility from Cockpit in Static PositionFIGURE-4-4-0-991-004-A01
4-4-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
CA
PT
AIN
WIN
DS
HIE
LDC
AP
TA
IN S
LID
ING
WIN
DO
WC
AP
TA
INF
IXE
D W
IND
OW
WIN
G T
IPV
ISIB
LE
CA
PT
AIN
’S F
IELD
OF
VIE
W S
HO
WN
, TH
RO
UG
H C
AP
TA
IN W
IND
OW
S O
NLY
.F
IRS
T O
FF
ICE
R F
IELD
OF
VIE
W S
YM
ME
TR
ICA
L.
EX
AM
PLE
: WH
EN
CA
PT
AIN
TU
RN
S H
IS H
EA
D B
Y 8
5° L
EF
T, V
ISIB
ILIT
YW
ILL
BE
43°
UP
AN
D 3
0° D
OW
N T
HR
OU
GH
TH
E S
LID
ING
WIN
DO
W F
RA
ME
.
A33
0/A
340
50°
40°
30°
20°
10°
0°10
°20
°30
°40
°50
°60
°70
°80
°90
°10
0°11
0°12
0°13
0°14
0°
30°
20°
10°
0°10°
20°
30°
40°
43°
PIL
OT
EY
E P
OS
ITIO
N(C
AP
TA
IN P
OS
ITIO
N)
F_AC_040400_1_0080101_01_00
Binocular Visibility Through Windows from Captain Eye PositionFIGURE-4-4-0-991-008-A01
4-4-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A340-200 A340-300
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A340-200 A340-300
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FAA LEAD−IN FILLET
L = 75 m (250 ft)
(15 ft)APPROX 4.5 m
APPROX 11.7 m(39 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
45 m(150 ft)
23 m(75 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
F_AC_040501_1_0030101_01_01
135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-1-991-003-A01
4-5-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
APPROX 2 m(7 ft)
ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
F_AC_040501_1_0080101_01_00
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-008-A01
4-5-1Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
45 m(150 ft)
APPROX 10.8 m(35 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
APPROX 6.4 m(21 ft)
23 m(75 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
F_AC_040501_1_0090101_01_00
135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-1-991-009-A01
4-5-1Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
APPROX 3.4 m(11 ft)
ADDITIONAL FILLET TO MEET
4.5 m (15 ft) EDGE CLEARANCE
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
45 m150 ft
23 m(75 ft)
F_AC_040501_1_0100101_01_00
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
NLG PATH
MLG PATH
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-010-A01
4-5-1Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A340-200 A340-300
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FAA LEAD−IN FILLETL = 75 m (250 ft)
(41 ft)APPROX 12.3 m
(44 ft)APPROX 13.2 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
45 m(150 ft)
F_AC_040502_1_0030101_01_01
23 m(75 ft)
NLG PATH
MLG PATH
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
F_AC_040502_1_0030101_01_01
90˚ Turn - Runway to TaxiwayJudgement Oversteering Method
FIGURE-4-5-2-991-003-A01
4-5-2Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
(18 ft)APPROX 5.4 m
FILLET R = 25.5 m(85 ft)
FAA LEAD−IN FILLETL = 75 m (250 ft)
45 m(150 ft)
TURN R = 45 m(150 ft)
23 m(75 ft)
NLG PATH
MLG PATH
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
F_AC_040502_1_0100101_01_00
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-010-A01
4-5-2Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
45 m(150 ft)
FILLET R = 25.5 m(85 ft)
(44 ft)APPROX 13.3 m
FAA LEAD−IN FILLETL = 75 m (250 ft)
(42 ft)APPROX 12.7 m
TURN R = 45 m(150 ft)
23 m(75 ft)
NLG PATH
MLG PATH
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
F_AC_040502_1_0110101_01_00
90˚ Turn - Runway to TaxiwayJudgement Oversteering Method
FIGURE-4-5-2-991-011-A01
4-5-2Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
FAA LEAD−IN FILLETL = 75 m (250 ft)
(27 ft)APPROX 8 m
FILLET R = 25.5 m(85 ft)
45 m(150 ft)
TURN R = 45 m(150 ft)
23 m(75 ft)
NLG PATH
MLG PATH
RUNWAYCENTERLINE
TAXIWAYCENTERLINE
F_AC_040502_1_0120101_01_00
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-012-A01
4-5-2Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A340-200 A340-300
180˚ Turn on a Runway
1. This section provides the 180˚ turn on a runway.
4-5-3Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
NLG PATH
MLG PATH
NOSE TIP PATH
WING TIP PATH
TAIL TIP PATHNOTE:
TYPE 1 VALUES FOR MAX STEERING ANGLE = 72°.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
50.7 m(166 ft)
41.7 m(137 ft)
4.5 m
20.2 m(66 ft)
14.6 m(48 ft)
0.9 m(3 ft)
4.5 m(15 ft)
R4 = 39.5 m(130 ft)
R6 = 36.3 m(119 ft) R3 = 26.8 m
(88 ft)
R5 = 33.1 m(109 ft)
RUNWAY CENTERLINE
(15 ft)
F_AC_040503_1_0060101_01_03
180˚ Turn on a RunwayFIGURE-4-5-3-991-006-A01
4-5-3Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
NLG PATH
MLG PATH
NOSE TIP PATH
WING TIP PATH
TAIL TIP PATH
NLG PATH
MLG PATH
NOSE TIP PATH
WING TIP PATH
TAIL TIP PATHNOTE:
TYPE 1 VALUES FOR MAX STEERING ANGLE = 72°.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.
R5 = 30.9 m(101 ft)
4.5 m(15 ft)
20.4 m(67 ft)
13.4 m(44 ft)
0.9 m(3 ft)
4.5 m(15 ft)
R3 = 24.7 m(81 ft)
R6 = 34.3 m(113 ft)
R4 = 39.1 m(128 ft)
48.1 m(158 ft)
39.1 m(128 ft)
RUNWAY CENTERLINE
F_AC_040503_1_0070101_01_03
180˚ Turn on a RunwayFIGURE-4-5-3-991-007-A01
4-5-3Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4 135˚ Turn - Taxiway to Taxiway
**ON A/C A340-200 A340-300
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway
4-5-4Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
TURN R = 45 m(150 ft)
FILLET R = 25.5 m(85 ft)
APPROX 12.9 m(43 ft)
APPROX 4.5 m(15 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
TAXIWAY CENTERLINE
TAXIWAY CENTERLINE
NLG PATH
MLG PATH
(75 ft)23 m
23 m(75 ft)
F_AC_040504_1_0090101_01_00
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-4-991-009-A01
4-5-4Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FILLET R = 25.5 m(85 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
APPROX 3.5 m(12 ft)
ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE
TAXIWAY CENTERLINE
TAXIWAY CENTERLINE
23 m(75 ft)
(75 ft)23 m
TURN R = 45 m(150 ft)
NLG PATH
MLG PATH
F_AC_040504_1_0100101_01_00
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-4-991-010-A01
4-5-4Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
APPROX 13 m(43 ft)
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
TAXIWAY CENTERLINE
APPROX 5.1 m(17 ft)
FAA LEAD−IN FILLET
L = 75 m (250 ft)
(75 ft)23 m
TAXIWAY CENTERLINE
NLG PATH
MLG PATH
23 m(75 ft)
F_AC_040504_1_0110101_01_00
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-4-991-011-A01
4-5-4Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
FILLET R = 25.5 m(85 ft)
APPROX 5.2 m(17 ft)
TAXIWAY CENTERLINE
FAA LEAD−IN FILLET
L = 75 m (250 ft)
23 m(75 ft)
TAXIWAY CENTERLINE
(75 ft)23 m
NLG PATH
MLG PATH
TURN R = 45 m(150 ft)
F_AC_040504_1_0120101_01_00
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-4-991-012-A01
4-5-4Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5 90˚ Turn - Taxiway to Taxiway
**ON A/C A340-200 A340-300
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-5Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
(40 ft)APPROX 12 m
FAA LEAD−IN FILLETL = 75 m (250 ft)
TAXIWAY CENTERLINE(43 ft)APPROX 12.9 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
TAXIWAY CENTERLINE
23 m(75 ft)
(75 ft)23 m NLG PATH
MLG PATH
F_AC_040505_1_0050101_01_01
90˚ Turn - Taxiway to TaxiwayJudgement Oversteering Method
FIGURE-4-5-5-991-005-A01
4-5-5Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
FAA LEAD−IN FILLETL = 75 m (250 ft)
(14 ft)APPROX 4.1 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
4.5 m (15 ft) EDGE CLEARANCEADDITIONAL FILLET TO MEET
TAXIWAY CENTERLINE
23 m(75 ft)
TAXIWAY CENTERLINE
(75 ft)23 m
NLG PATH
MLG PATHF_AC_040505_1_0130101_01_00
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-5-991-013-A01
4-5-5Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
(44 ft)APPROX 13.1 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
(41 ft)APPROX 12.4 m
FAA LEAD−IN FILLETL = 75 m (250 ft)
TAXIWAY CENTERLINE
(75 ft)23 m NLG PATH
MLG PATH
23 m(75 ft)
TAXIWAY CENTERLINE
F_AC_040505_1_0060101_01_02
90˚ Turn - Taxiway to TaxiwayJudgement Oversteering Method
FIGURE-4-5-5-991-006-A01
4-5-5Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
FAA LEAD−IN FILLETL = 75 m (250 ft)
(24 ft)APPROX 7.1 m
FILLET R = 25.5 m(85 ft)
TURN R = 45 m(150 ft)
TAXIWAY CENTERLINE
(75 ft)23 m
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
23 m(75 ft)
F_AC_040505_1_0140101_01_00
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-5-991-014-A01
4-5-5Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A340-200 A340-300
Runway Holding Bay (Apron)
1. This section provides the runway holding bay (Apron).
4-6-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
TAXIWAYCENTERLINE
23 m(75 ft)
45 m(150 ft)
RUNWAYCENTERLINE
HOLDINGPOINT6.1 m
(20 ft)
90 m(300 ft)
97.3 m(319 ft)
6.1 m(20 ft)
12.2 m(40 ft)
20° NOSE−WHEEL STEERING ANGLE.COORDINATE WITH USING AIRLINE FOR SPECIFIC PLANNED OPERATING PROCEDURES.
190 m(625 ft)
NOTE:
F_AC_040600_1_0030101_01_03
Runway Holding Bay (Apron)FIGURE-4-6-0-991-003-A01
4-6-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0 Minimum Line-Up Distance Corrections
**ON A/C A340-200 A340-300
Minimum Line-Up Distance Corrections
1. The ground maneuvers were performed using asymmetric thrust and differential-only braking toinitiate the turn.TODA: Take-Off Distance AvailableASDA: Acceleration-Stop Distance Available
2. 90˚ Turn on Runway Entry
This section gives the minimum line-up distance correction for a 90˚ turn on runway entry.This maneuver consists in a 90˚ turn at minimum turn radius. It starts with the edge of the MLG ata distance of 4.5 m (15 ft) from the taxiway edge, and finishes with the aircraft aligned on thecenterline of the runway, see FIGURE 4-7-0-991-022-A.During the turn, all the clearances must meet the minimum value of 4.5 m (15 ft) for this category ofaircraft as recommended in ICAO Annex 14.
3. 180˚ Turn on Runway Turn Pad
This section gives the minimum line-up distance correction for a 180˚ turn on the runway turn pad.This maneuver consists in a 180˚ turn at minimum turn radius on a runway turn pad with standardICAO geometry.It starts with the edge of the MLG at a distance of 4.5 m (15 ft) from the pavement edge, and itfinishes with the aircraft aligned on the centerline of the runway, see FIGURE 4-7-0-991-023-A.During the turn, all the clearances must meet the minimum value of 4.5 m (15 ft) for this category ofaircraft as recommended in ICAO Annex 14.
4. 180˚ Turn on Runway Width
This section gives the minimum line-up distance correction for a 180˚ turn on the runway width.For this maneuver, the pavement width is considered to be the runway width, which is a frozenparameter (45 m (150 ft) and 60 m (200 ft)).As per the standard operating procedures for the ”180˚ turn on runway” (described in the FlightCrew Operating Manual), the aircraft is initially angled with respect to the runway centerline whenstarting the 180˚ turn, see FIGURE 4-7-0-991-024-A.The value of this angle depends on the aircraft type and is mentioned in the FCOM.During the turn, all the clearances must meet the minimum value of 4.5 m (15 ft) for this category ofaircraft as recommended in ICAO Annex 14.
4-7-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
TAXIWAYCENTERLINE
RUNWAY
> 4.5 m(15 ft)
TODA
4.5 m(15 ft)
ASDA
CENTERLINE
90° TURN ON RUNWAY ENTRY
AIRCRAFTTYPE
STEERINGANGLE
MAX
45 m (150 ft)/60 m (200 ft) WIDE RUNWAY
MINIMUM LINE−UP DISTANCE CORRECTION
65°A340−200 21.5 m 70 ft 44.7 m 147 ftON TODA ON ASDA
72°A340−200 18.6 m 61 ft 41.8 m 137 ft
NOTE:
ASDA: ACCELERATION−STOP DISTANCE AVAILABLETODA: TAKE−OFF DISTANCE AVAILABLE
65°A340−300 22.2 m 73 ft 47.6 m 156 ft72°A340−300 20.5 m 67 ft 45.9 m 151 ft
F_AC_040700_1_0220101_01_00
Minimum Line-Up Distance Corrections90˚ Turn on Runway EntryFIGURE-4-7-0-991-022-A01
4-7-0Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
NOTE:
ASDA: ACCELERATION−STOP DISTANCE AVAILABLETODA: TAKE−OFF DISTANCE AVAILABLE
TODA
ASDA
MINIMUM PAVEMENT WIDTH
RUNWAY CENTERLINE
180° TURN ON RUNWAY TURNPAD
AIRCRAFTTYPE
STEERINGANGLE
MAX(STANDARD WIDTH)
DISTANCE CORRECTIONMINIMUM LINE−UP
DISTANCE CORRECTIONMINIMUM LINE−UP MINIMUM
REQUIRED
PAVEMENTWIDTH
65°A340−200 100 ft30.5 m 176 ft53.7 m 179 ft54.6 mON TODA ON ASDA
45 m (150 ft) WIDE RUNWAY 60 m (200 ft) WIDE RUNWAY
72°A340−200 97 ft29.5 m 173 ft52.7 m 160 ft48.8 m
ON TODA ON ASDA
65°A340−300 108 ft32.8 m 191 ft58.2 m 184 ft56.0 m72°A340−300 106 ft32.2 m 189 ft57.6 m 173 ft52.7 m104 ft31.7 m 187 ft57.1 m
SAME AS 45 m WIDE RWY
4.5 m(15 ft)
> 4.5 m(15 ft)
4.5 m(15 ft)
F_AC_040700_1_0230101_01_00
Minimum Line-Up Distance Corrections180˚ Turn on Runway Turn Pad
FIGURE-4-7-0-991-023-A01
4-7-0Page 3
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
180° TURN ON RUNWAY WIDTH
AIRCRAFTTYPE
STEERINGANGLE
MAX(STANDARD WIDTH)
DISTANCE CORRECTIONMINIMUM LINE−UP
DISTANCE CORRECTIONMINIMUM LINE−UP
65°A340−200 138 ft42.0 m 214 ft65.2 mON TODA ON ASDA ON TODA ON ASDA
45 m (150 ft) WIDE RUNWAY 60 m (200 ft) WIDE RUNWAY
72°A340−200NOT POSSIBLE
ASDA
TODA
> 4.5 m(15 ft)
20° RUNWAY CENTERLINE
(15 ft)
4.5 m(15 ft)
A340−300A340−300
65°72°
97 ft29.5 m 173 ft52.7 m156 ft47.6 m 239 ft73.0 m104 ft31.7 m 187 ft57.1 m
NOTE:
ASDA: ACCELERATION−STOP DISTANCE AVAILABLETODA: TAKE−OFF DISTANCE AVAILABLE
4.5 m
F_AC_040700_1_0240101_01_00
Minimum Line-Up Distance Corrections180˚ Turn on Runway WidthFIGURE-4-7-0-991-024-A01
4-7-0Page 4
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-8-0 Aircraft Mooring
**ON A/C A340-200 A340-300
Aircraft Mooring
1. This section provides information on aircraft mooring.
4-8-0Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
TOWING FITTING
GROUND ANCHOR
A
TOWING FITTING
B
WARNING FLAG
B
A
F_AC_040800_1_0010101_01_00
Aircraft MooringFIGURE-4-8-0-991-001-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-1-0 Aircraft Servicing Arrangements
**ON A/C A340-200 A340-300
Aircraft Servicing Arrangements
1. This section provides typical ramp layouts, showing the various GSE items in position during typicalturn-round scenarios for passenger aircraft.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for positioning and operation on the ramp.
5-1-0Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A340-200 A340-300
Symbols Used on Servicing Diagrams
1. This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC AIR CONDITIONING UNITAS AIR START UNIT
BULK BULK TRAINCAT CATERING TRUCK
CB CONVEYOR BELTCLEAN CLEANING TRUCK
FUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNIT
LD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLE
PBB PASSENGER BOARDING BRIDGEPS PASSENGER STAIRS
TOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2 Typical Ramp Layout - Open Apron
**ON A/C A340-200 A340-300
Typical Ramp Layout - Open Apron
1. This section provides the typical servicing arrangements on the open apron, for the passenger versionof the aircraft.The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (24.61 ft) fromthe aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheelchocks in position on landing gears).
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
PS CAT
PS
PS CAT
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
AS
GPU
LD CL
LD CL
AC
ULD
FUELFUEL
LV
CB
ULD
BULKWV
TOW
STAND SAFETY LINE
CAT
F_AC_050102_1_0030101_01_02
Typical Ramp LayoutOpen Apron
FIGURE-5-1-2-991-003-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
PS
PS
CAT
CAT
PS CAT
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
TOW
AS
GPU
LD CL
LD CL
AC
ULD
ULD
BULKCBWV
LV
FUELFUEL
STAND SAFETY LINE
F_AC_050102_1_0040101_01_02
Typical Ramp LayoutOpen Apron
FIGURE-5-1-2-991-004-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3 Typical Ramp Layout - Gate
**ON A/C A340-200 A340-300
Typical Ramp Layout - Gate
1. This section provides the typical servicing arrangements in the gate area for the passenger version ofthe aircraft, with two Passenger Boarding Bridges.The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (24.61 ft) fromthe aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheelchocks in position on landing gears).
5-1-3Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
CLEAN
CAT
CAT
CAT
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
TOW
AS
GPU
LD CL
LD CL
AC
ULD
ULD
BULKCB
LV
FUELFUEL
PBB
PBB
WV
STAND SAFETY LINE
F_AC_050103_1_0020101_01_02
Typical Ramp LayoutGate
FIGURE-5-1-3-991-002-A01
5-1-3Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
CLEAN
WV
CAT
CAT
CAT
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
AS
GPU
LD CL
LD CL
AC
ULD
FUELFUEL
LV
CB
ULD
BULK
TOW
PBB
PBB
STAND SAFETY LINE
F_AC_050103_1_0030101_01_02
Typical Ramp LayoutGate
FIGURE-5-1-3-991-003-A01
5-1-3Page 3
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0 Terminal Operations - Full Servicing
**ON A/C A340-300
Terminal Operations - Full Servicing Turn Round Time
1. This section provides a typical turn round time charts showing the typical time for ramp activitiesduring aircraft turn round.Actual times may vary due to each operator’s specific practices, resources, equipment and operatingconditions.
2. Assumptions used for full servicing turn round time chart
A. PASSENGER HANDLING270 pax: 10 F/C + 28 B/C + 232 Y/C.All passengers deplane and board the aircraft.2 Passenger Boarding Bridges (PBB) used at doors L1 and L2.Equipment positioning + opening door = +3 min.Closing door + equipment removal = +3 min.No Passenger with Reduced Mobility (PRM) on board.
Deplaning:- 135 pax at door L1 (10 F/C + 28 B/C + 97 Y/C)- 135 pax at door L2 (135 Y/C)- Deplaning rate = 25 pax/min per door- Priority deplaning for premium passengers.
Boarding:- 135 pax at door L1 (10 F/C + 28 B/C + 97 Y/C)- 135 pax at door L2 (135 Y/C)- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min.
B. CARGO2 cargo loaders + 1 belt loader.Opening door + equipment positioning = +2.5 minEquipment removal + closing door = +2.5 min.
Cargo exchange:- FWD cargo compartment: 12 LD3 + 2 pallets- AFT cargo compartment: 8 LD3 + 2 pallets- Bulk cargo compartment: 1 000 kg (2 205 lb).
LD3 unloading/loading times:- Unloading = 1.2 min/LD3- Loading = 1.4 min/LD3.
5-2-0Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Pallet unloading/loading times:- Unloading = 2.4 min/pallet- Loading = 2.8 min/pallet.
Bulk unloading/loading times:- Unloading = 9.2 min/t- Loading = 10.5 min/t.
C. REFUELINGBlock-fuel quantity for nominal range through 2 nozzles.127 000 l (33 550 US gal) at 50 psi (3.45 bar).Dispenser positioning + connection = +3 min.Disconnection + dispenser removal = +3 min.
D. CLEANINGCleaning is performed in available time.
E. CATERING3 catering trucks for servicing galleys at doors R1, R2 and R4.Equipment positioning + opening door = +5 min.Closing door + equipment removal = +3 min.
Full Size Trolley Equivalent (FSTE) to unload and load: 48 FSTE- 10 FSTE at door R1- 13 FSTE at door R2- 25 FSTE at door R4.Time for trolley exchange = 1.5 min per FSTE.
F. GROUND HANDLING/GENERAL SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min.
Vehicle positioning/removal = +2 min (except for fuel and catering trucks).Ground Power Unit (GPU): up to 2 × 90 kVA.Air conditioning: two hoses.Potable water servicing: 100% uplift, 700 l (185 US gal) at 60 l/min (15.85 US gal/min).Waste water servicing: draining + rinsing.
5-2-0Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
TRT: 62 min
100 20 30 40 50 60 70
DEPLANING/BOARDING AT L1
HEADCOUNTING
CATERING AT R2
CLEANING
CARGO FWD CC
BULK
REFUELING
POTABLE WATER SERVICING
WASTE WATER SERVICING
DEPLANING/BOARDING AT L2
CATERING AT R4
CARGO AFT CC
CATERING AT R1
AVAILABLE TIME
F_AC_050200_1_0040101_01_01
Full Servicing Turn Round Time ChartFIGURE-5-2-0-991-004-A01
5-2-0Page 3
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
Terminal Operations - Full Servicing Turn Round Time
1. This section provides a typical turn round time charts showing the typical time for ramp activitiesduring aircraft turn round.Actual times may vary due to each operator’s specific practices, resources, equipment and operatingconditions.
2. Assumptions used for full servicing turn round time chart
A. PASSENGER HANDLING231 pax: 10 F/C + 42 B/C + 179 Y/C.All passengers deplane and board the aircraft.2 Passenger Boarding Bridges (PBB) used at doors L1 and L2.Equipment positioning + opening door = +3 min.Closing door + equipment removal = +3 min.No Passenger with Reduced Mobility (PRM) on board.
Deplaning:- 116 pax at door L1 (10 F/C + 42 B/C + 64 Y/C)- 115 pax at door L2 (115 Y/C)- Deplaning rate = 25 pax/min per door- Priority deplaning for premium passengers.
Boarding:- 116 pax at door L1 (10 F/C + 42 B/C + 64 Y/C)- 115 pax at door L2 (115 Y/C)- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min.
B. CARGO2 cargo loaders + 1 belt loader.Opening door + equipment positioning = +2.5 min.Equipment removal + closing door = +2.5 min.
Cargo exchange:- FWD cargo compartment: 8 LD3 + 2 pallets- AFT cargo compartment: 6 LD3 + 2 pallets- Bulk cargo compartment: 1 000 kg (2 205 lb).
LD3 unloading/loading times:- Unloading = 1.2 min/LD3- Loading = 1.4 min/LD3.
Pallet unloading/loading times:
5-2-0Page 4
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Unloading = 2.4 min/pallet- Loading = 2.8 min/pallet.
Bulk unloading/loading times:- Unloading = 9.2 min/t- Loading = 10.5 min/t.
C. REFUELINGBlock-fuel quantity for nominal range through 4 nozzles.127 000 l (33 550 US gal) at 50 psi (3.45 bar).Dispenser positioning + connection = +3 min.Disconnection + dispenser removal = +3 min.
D. CLEANINGCleaning is performed in available time.
E. CATERING3 catering trucks for servicing galleys at doors R1, R2 and R4.Equipment positioning + opening door = +5 min.Closing door + equipment removal = +3 min.
Full Size Trolley Equivalent (FSTE) to unload and load: 36 FSTE- 7 FSTE at door R1- 9 FSTE at door R2- 20 FSTE at door R4.Time for trolley exchange = 1.5 min per FSTE.
F. GROUND HANDLING/GENERAL SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min
Vehicle positioning/removal = +2 min (except for fuel and catering trucks).Ground Power Unit (GPU): up to 2 × 90 kVA.Air conditioning: two hoses.Potable water servicing: 100% uplift, 700 l (185 US gal) at 60 l/min (15.85 US gal/min).Waste water servicing: draining + rinsing.
5-2-0Page 5
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
TRT: 52 min
100 20 30 40 50 60 70
DEPLANING/BOARDING AT L1
HEADCOUNTING
CATERING AT R2
CLEANING
CARGO FWD CC
BULK
REFUELING
POTABLE WATER SERVICING
WASTE WATER SERVICING
DEPLANING/BOARDING AT L2
CATERING AT R4
CARGO AFT CC
CATERING AT R1
AVAILABLE TIME
F_AC_050200_1_0050101_01_01
Full Servicing Turn Round Time ChartFIGURE-5-2-0-991-005-A01
5-2-0Page 6
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0 Terminal Operations - Transit
**ON A/C A340-300
Terminal Operations - 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.
2. Assumptions for minimum servicing turn-round time chart
A. PASSENGER HANDLING270 pax (10 F/C + 38 B/C + 222 Y/C)50% of passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board
Deboarding:- 135 pax at door L1- Deboarding rate = 25 pax/min per door
Boarding:- 135 pax at door L1- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min
B. CARGO1 cargo loader + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min
Cargo exchange:- 4 LD3 in AFT cargo compartment- 500 kg (1 102 lb) in bulk cargo compartment
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t
C. REFUELLINGRefuelling through 2 nozzles30% of max capacity at 50 psi (3.45 bar)
5-3-0Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Dispenser positioning/removal = 3 min
D. CLEANINGPerformed in available time
E. CATERING1 catering truck for servicing galleys as requiredEquipment positioning + door opening = 5 minEquipment removal + door closing = 3 minPerformed in available timeTime for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING/SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min
Vehicle positioning/removal = 2 min (except for fuel and catering trucks)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesNo potable water servicingNo toilet servicing
5-3-0Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
TRT: 33 min
50 10 15 20 25 30 35
AT L1DEBOARDING/BOARDING
HEADCOUNTING
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CATERING
CARGO AFT CC
40
AVAILABLE TIME
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
F_AC_050300_1_0050101_01_00
Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-005-A01
5-3-0Page 3
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
Terminal Operations - 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.
2. Assumptions for minimum servicing turn-round time chart
A. PASSENGER HANDLING231 pax (10 F/C + 42 B/C + 179 Y/C)50% of passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board
Deboarding:- 116 pax at door L1- Deboarding rate = 25 pax/min per door
Boarding:- 116 pax at door L1- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min
B. CARGO1 cargo loader + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min
Cargo exchange:- 4 LD3 in AFT cargo compartment- 500 kg (1 102 lb) in bulk cargo compartment
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t
C. REFUELLINGRefuelling through 2 nozzles30% of max capacity at 50 psi (3.45 bar)Dispenser positioning/removal = 3 min
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
D. CLEANINGPerformed in available time
E. CATERING1 catering truck for servicing galleys as requiredEquipment positioning + door opening = 5 minEquipment removal + door closing = 3 minPerformed in available timeTime for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING/SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min
Vehicle positioning/removal = 2 min (except for fuel and catering trucks)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesNo potable water servicingNo toilet servicing
5-3-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
TRT: 31 min
50 10 15 20 25 30 35
AT L1DEBOARDING/BOARDING
HEADCOUNTING
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CATERING
CARGO AFT CC
40
AVAILABLE TIME
GSE POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
F_AC_050300_1_0060101_01_00
Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-006-A01
5-3-0Page 6
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1 Ground Service Connections Layout
**ON A/C A340-200 A340-300
Ground Service Connections Layout
1. This section provides the ground service connections layout.
5-4-1Page 1
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
1 − OXYGEN SERVICING2 − GROUND ELECTRICAL POWER CONNECTORS3 − POTABLE WATER DRAIN4 − LOW PRESSURE AIR PRE−CONDITIONING
AND ENGINE STARTING6 − ENGINE OIL FILLING7 − IDG OIL FILLING8 − PRESSURE REFUEL/DEFUEL COUPLINGS9 − OVERWING REFUEL (IF INSTALLED)
10 − HYDRAULIC GROUND POWER SUPPLY
5 − HIGH PRESSURE AIR PRE−CONDITIONING
12 − HYDRAULIC RESERVOIR AIR PRESSURIZATIONAND GROUND POWER SUPPLY (BLUE)
14 − POTABLE WATER SERVICE PANEL15 − WASTE WATER SERVICE PANEL16 − APU OIL FILLING17 − GROUNDING (EARTHING) POINT
13 − REFUEL/DEFUEL PANEL
11 − HYDRAULIC RESERVOIR FILLING AND GROUNDPOWER SUPPLY (GREEN)
18 − NACA FLAME ARRESTOR19 − OVERPRESSURE PROTECTOR
(YELLOW)
1
217
3
45106 7
12 6
78 6
7
1918
9
17
11
133
1415
16
18 19
179
8
6 719 18
F_AC_050401_1_0030101_01_03
Ground Service Connections LayoutFIGURE-5-4-1-991-003-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2 Grounding Points
**ON A/C A340-200 A340-300
Grounding (Earthing) Points
**ON A/C A340-300
1. Grounding (Earthing) Points
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
On Nose Landing Gearleg:
6.57 m(21.56 ft) On centerline
1.40 m(4.59 ft)
On left Main LandingGear leg:
31.58 m(103.61 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
On right MainLanding Gear leg:
31.58 m(103.61 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
A. The grounding (earthing) stud on each landing gear leg is designed for use with a clip-onconnector (such as Appleton TGR).
B. The grounding (earthing) studs are used to connect the aircraft to an approved ground (earth)connection on the ramp or in the hangar for:- Refuel/defuel operations- Maintenance operations- Bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tire is sufficient.
**ON A/C A340-200
2. Grounding (Earthing) Points
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
On Nose Landing Gearleg:
6.57 m(21.56 ft) On centerline
1.40 m(4.59 ft)
On left Main LandingGear leg:
29.40 m(96.46 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
On right Main LandingGear leg:
29.40 m(96.46 ft)
5.34 m(17.52 ft)
1.50 m(4.92 ft)
A. The grounding (earthing) stud on each landing gear leg is designed for use with a clip-onconnector (such as Appleton TGR).
B. The grounding (earthing) studs are used to connect the aircraft to an approved ground (earth)connection on the ramp or in the hangar for:- Refuel/defuel operations- Maintenance operations- Bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tire is sufficient.
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Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
NOSE LANDING GEAR MAIN LANDING GEAR
A
A
LANDINGGEAR
A
GROUNDING (EARTHING) POINTGROUNDING (EARTHING) CABLE
TYPICALF_AC_050402_1_0030101_01_01
Ground Service ConnectionsGrounding (Earthing) PointsFIGURE-5-4-2-991-003-A01
5-4-2Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
BFWD
A
A
ALH SHOWN
RH SYMMETRICAL
RIB22
RIB23
B
F_AC_050402_1_0040101_01_01
Ground Service ConnectionsGrounding (Earthing) PointsFIGURE-5-4-2-991-004-A01
5-4-2Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3 Hydraulic System
**ON A/C A340-200 A340-300
Hydraulic Servicing
**ON A/C A340-300
1. Ground Service Panels
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND
Green System:Access Door 197CB
34.90 m(114.50 ft)
1.34 m(4.40 ft)
2.23 m(7.32 ft)
Yellow System:Access Door 196BB
29.00 m(95.14 ft)
1.30 m(4.27 ft)
1.95 m(6.40 ft)
Blue System:Access Door 195BB
28.00 m(91.86 ft)
1.28 m(4.20 ft)
1.94 m(6.36 ft)
**ON A/C A340-200
2. Ground Service Panels
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND
Green System:Access Door 197CB
32.79 m(107.58 ft)
1.34 m(4.40 ft)
2.23 m(7.32 ft)
Yellow System:Access Door 196BB
26.89 m(88.22 ft)
1.30 m(4.27 ft)
1.95 m(6.40 ft)
Blue System:Access Door 195BB
25.90 m(84.97 ft)
1.28 m(4.20 ft)
1.94 m(6.36 ft)
**ON A/C A340-300
3. Reservoir PressurizationOne 1/4 in. self-sealing connection common to the 3 reservoirs.
5-4-3Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHT FROM
GROUNDBlue System GroundService Panel:Access Door 195BB
34.47 m(113.09 ft)
1.41 m(4.63 ft)
1.89 m(6.20 ft)
**ON A/C A340-200
4. Reservoir PressurizationOne 1/4 in. self-sealing connection common to the 3 reservoirs.
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDBlue System GroundService Panel:Access Door 195BB
32.34 m(106.10 ft)
1.41 m(4.63 ft)
1.89 m(6.20 ft)
**ON A/C A340-300
5. Accumulator ChargingFive connections (one for each accumulator):
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDGreen SystemAccumulator:Access Door 197CB
41.52 m(136.22 ft)
1.33 m(4.36 ft)
2.19 m(7.19 ft)
Yellow SystemAccumulator:Access Door 196BB
35.55 m(116.63 ft)
1.43 m(4.69 ft)
1.91 m(6.27 ft)
Blue System Accumulator:Access Door 195BB
34.54 m(113.32 ft)
1.38 m(4.53 ft)
1.90 m(6.23 ft)
5-4-3Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDBlue System BrakeAccumulator:Access Door 195BB
34.54 m(113.32 ft)
1.24 m(4.07 ft)
1.90 m(6.23 ft)
**ON A/C A340-200
6. Accumulator ChargingFive connections (one for each accumulator):
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDGreen SystemAccumulator:Access Door 197CB
39.39 m(129.23 ft)
1.33 m(4.36 ft)
2.19 m(7.19 ft)
Yellow SystemAccumulator:Access Door 196BB
33.42 m(109.65 ft)
1.43 m(4.69 ft)
1.91 m(6.27 ft)
Blue System Accumulator:Access Door 195BB
32.41 m(106.33 ft)
1.38 m(4.53 ft)
1.90 m(6.23 ft)
Blue System BrakeAccumulator:Access Door 195BB
32.41 m(106.33 ft)
1.18 m(3.87 ft)
1.90 m(6.23 ft)
**ON A/C A340-300
7. Reservoir FillingTwo connections (one self-sealing connection for pressurized supply on the Green system groundservice panel).
5-4-3Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDOne handpump fillingconnection:Access Door 197CB
41.31 m(135.53 ft)
1.30 m(4.27 ft)
2.11 m(6.92 ft)
**ON A/C A340-200
8. Reservoir FillingTwo connections (one self-sealing connection for pressurized supply on the Green system groundservice panel).
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDOne handpump fillingconnection:Access Door 197CB
39.18 m(128.54 ft)
1.30 m(4.27 ft)
2.11 m(6.92 ft)
**ON A/C A340-300
9. Reservoir DrainOne 3/8 in. self-sealing connection on the reservoir for:
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND
Green System33.17 m(108.83 ft)
0.70 m(2.30 ft)
3.80 m(12.47 ft)
Yellow System29.03 m(95.24 ft)
2.12 m(6.96 ft)
2.40 m(7.87 ft)
Blue System29.03 m(95.24 ft)
2.12 m(6.96 ft)
2.40 m(7.87 ft)
5-4-3Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
10. Reservoir DrainOne 3/8 in. self-sealing connection on the reservoir for:
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND
Green System31.04 m(101.84 ft)
0.70 m(2.30 ft)
3.80 m(12.47 ft)
Yellow System26.90 m(88.25 ft)
2.12 m(6.96 ft)
2.40 m(7.87 ft)
Blue System26.90 m(88.25 ft)
2.12 m(6.96 ft)
2.40 m(7.87 ft)
**ON A/C A340-300
11. Ground TestThree 1 in. self-sealing connections and three 1-1/2 in. self-sealing connections (one pair per system).
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUNDGreen System GroundService Panel:Access Door 197CB
34.92 m(114.57 ft)
1.35 m(4.43 ft)
2.20 m(7.22 ft)
Yellow System GroundService Panel:Access Door 196BB
29.03 m(95.24 ft)
1.30 m(4.27 ft)
2.00 m(6.56 ft)
Blue System GroundService Panel:Access Door 195BB
28.03 m(91.96 ft)
1.28 m(4.20 ft)
2.00 m(6.56 ft)
**ON A/C A340-200
12. Ground TestThree 1 in. self-sealing connections and three 1-1/2 in. self-sealing connections (one pair per system).
5-4-3Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUNDGreen System GroundService Panel:Access Door 197CB
32.79 m(107.58 ft)
1.35 m(4.43 ft)
2.20 m(7.22 ft)
Yellow System GroundService Panel:Access Door 196BB
26.90 m(88.25 ft)
1.30 m(4.27 ft)
2.00 m(6.56 ft)
Blue System GroundService Panel:Access Door 195BB
25.90 m(84.97 ft)
1.28 m(4.20 ft)
2.00 m(6.56 ft)
**ON A/C A340-300
13. A/C Emergency Generation
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDRAT Safety-PinInstallation:Access Panel 633SL
34.60 m(113.52 ft)
14.20 m(46.59 ft)
4.30 m(14.11 ft)
**ON A/C A340-200
14. A/C Emergency Generation
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDRAT Safety-PinInstallation:Access Panel 633SL
32.40 m(106.30 ft)
14.20 m(46.59 ft)
4.30 m(14.11 ft)
5-4-3Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
MAN SELECTORVALVE−RSVR
FILLING
LEVER HANDPUMP
GND CNCTR−SELFSEALING RSVR
FILLING
HAND PUMPRSVR FILLING
FILTER−RSVRFILLING
RSVRFILLING VALVE
GND CNCTR−SELFSEALING, G SUCTION
GND CNCTR−SELFSEALING, G DELIVERY
VALVE−MANDEPRESS, G−RSVR
HYDRSVR FILLINGADJUSTMENT
INDICATOR
PRESS GAGEG POWER ACCU
GND CNCTRNITROGEN CHARGING
G POWER ACCU
FWD
A
FR53.4 FR53.5197CB
A
F_AC_050403_1_0040101_01_00
Ground Service ConnectionsGreen System Ground Service Panel
FIGURE-5-4-3-991-004-A01
5-4-3Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
PRESS GAGEB POWER ACCU
GND CNCTRNITROGENCHARGING
B POWER ACCU
GND CNCTRSELF−SEALING,
B SUCTION
VALVE−MANDEPRESS, B RSVR
GND CNCTR−SELFSEALING,
B DELIVERY
GND CNCTRSELF−SEALING,
B/Y RSVR PRESS
GND CNCTRSELF−SEALING,G RSVR PRESS
PRESS GAGESPARK BRK ACCU
PARK BRK ACCU
FWD
A
FR44 FR45
A
195BB
F_AC_050403_1_0050101_01_00
Ground Service ConnectionsBlue System Ground Service Panel
FIGURE-5-4-3-991-005-A01
5-4-3Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
SIGHTGLASSCARGO DOOR
SELECTOR MANIFOLD
HAND PUMPCARGO DOORS, Y RAT STOW PANEL
GND CNCTR−SELFSEALING, Y SUCTION
VALVE−MANDEPRESS, Y RSVR
GND CNCTR−SELFSEALING, Y DELIVERY
PRESS GAGEY POWER ACCU
GND CNCTRNITROGEN CHARGING
Y POWER ACCU
FWD
A
FR46FR47
A
196BB
F_AC_050403_1_0060101_01_00
Ground Service ConnectionsYellow System Ground Service Panel
FIGURE-5-4-3-991-006-A01
5-4-3Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
A
633SL
A
Z633
RAT UPLOCK SAFETY−PIN
633GB
RAM AIR TURBINE (RAT)
B
C
RAT RETRACTED
RAT EXTENDED
C
B
F_AC_050403_1_0110101_01_00
Ground Service ConnectionsRAT
FIGURE-5-4-3-991-011-A01
5-4-3Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4 Electrical System
**ON A/C A340-200 A340-300
Electrical Servicing
1. A/C External Power
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUND
A/C External Power:Access Door 121EL
7.01 m(23.00 ft) On centerline
1.98 m(6.50 ft)
NOTE : Distances are approximate.
2. Technical Specifications
A. External Power Receptacles:- Two receptacles according to MS 90362-3 - 90 kVA.
B. Power Supply:- Three-phase, 115 V, 400 Hz.
C. Electrical Connectors for Servicing:- AC outlets: HUBBELL 5258- DC outlets: HUBBELL 7472.
3. Tow Truck Power
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUND
NLG Service Panel: 5GC6.67 m(21.88 ft)
0.50 m(1.64 ft) TBD
NLG Service Panel: 8GH6.67 m(21.88 ft) On centerline TBD
4. Technical Specifications
A. Power Supply:- Two-phase, 115 V, 400 Hz- 28V DC.
B. Electrical Connector for Servicing:- Bernier, 22-11-10-13 Connector.
5-4-4Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
C. Pin Allocation:
Pin IdentificationA 28V DCB 0V DCD 115V ACE 0V ACGH
PWR SPLYINT LOCK
NOTE : The power cable should be extendable in order to guarantee fit and non-interferencewith nose gear nor tow vehicle during the pick-up and the towing process. Theconnector shall be secured against pull-out by means of straps against the nose gear.
5-4-4Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
FR19 FR18
A
A
121EL
B925VU
EXTERNAL POWER RECEPTACLESB
FR18
FR19
TYPICAL
F_AC_050404_1_0020101_01_01
Ground Service ConnectionsElectrical Service Panel
FIGURE-5-4-4-991-002-A01
5-4-4Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5 Oxygen System
**ON A/C A340-200 A340-300
Oxygen Servicing
1. Oxygen Servicing
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUNDOxygen Replenishment(Option 1):Access Door 811
2.50 m(8.20 ft)
0.53 m(1.74 ft)
3.20 m(10.50 ft)
Oxygen Replenishment(Option 2):Access Door 811
2.50 m(8.20 ft)
0.68 m(2.23 ft)
3.20 m(10.50 ft)
- 0 -- Basic: External charging in the avionic compartment- 1 -- Option- 2 -- Option.Zero, one or two MIL-DTL 7891 standard service connections (external charging in the avionicscompartment).
NOTE : Internal charging connection provided.
5-4-5Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
A
B
OXYGENFILLING PORT
TESTPORT
FWD
FR4
FR7
NOTE:THE NUMBER OF OXYGEN CYLINDERS DEPENDS ON THE SYSTEM CONFIGURATION.
B
FR20
FR1
AVIONICS COMPARTMENT DOOR
FR7
FR10
Z120
A
811
F_AC_050405_1_0030101_01_01
Ground Service ConnectionsOxygen Servicing
FIGURE-5-4-5-991-003-A01
5-4-5Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6 Fuel System
**ON A/C A340-200 A340-300
Fuel System
**ON A/C A340-200
1. Refuel/Defuel Control Panel
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel ControlPanel:Access Door 198DB
32.2 m(105.64 ft)
-0.8 m(2.62 ft)
1.9 m(6.23 ft)
A. Flow rate: 1250 l/min (330 US gal/min) per connection.
B. Maximum pressure: 50 psi (3.45 bar).
2. Refuel/Defuel Connectors
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel Coupling,Left:Access Door 522HB
27.8 m(91.21 ft)
12.6 m(41.34 ft)
-5 m(16.4 ft)
Refuel/Defuel Coupling,Right:Access Door 622HB
27.8 m(91.21 ft)
-12.6 m(41.34 ft)
5 m(16.4 ft)
Overwing GravityRefuel Cap
31.2 m(102.36 ft)
17.2 m(56.43 ft)
17.2 m(56.43 ft)
5.8 m(19.03 ft)
A. Four standard 2.5 in. ISO 45 connections.
B. Two service connections (gravity refuel).
5-4-6Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3. Overpressure Protector and NACA Flame Arrestor
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUNDOverpressure Protector(Wing)Access Panel 550EB(650EB)
37.36 m(122.57 ft)
27.17 m(89.14 ft)
27.17 m(89.14 ft)
5.75 m(18.86 ft)
NACA Flame Arrestor(Wing)Access Panel 550EB(650EB)
37 m(121.39 ft)
26.53 m(87.04 ft)
26.53 m(87.04 ft)
5.7 m(18.7 ft)
Overpressure Protector(Trim Tank)Access Panel 346AB
57.4 m(188.32 ft)
8 m(26.25 ft)
8 m(26.25 ft)
5.7 m(18.7 ft)
NACA Flame Arrestor(Trim Tank)Access Panel 346AB
57.4 m(188.32 ft)
8 m(26.25 ft)
8 m(26.25 ft)
5.7 m(18.7 ft)
**ON A/C A340-300
4. Refuel/Defuel Control Panel
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel ControlPanel:Access Door 198DB
34.3 m(112.53 ft)
-0.8 m(2.62 ft)
1.9 m(6.23 ft)
A. Flow rate: 1250 l/min (330 US gal/min) per connection.
B. Maximum pressure: 50 psi (3.45 bar).
5-4-6Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5. Refuel/Defuel Connectors
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUND
Refuel/Defuel Coupling,Left:Access Door 522HB
30 m(98.43 ft)
12.6 m(41.34 ft)
-5 m(16.4 ft)
Refuel/Defuel Coupling,Right:Access Door 622HB
30 m(98.43 ft)
-12.6 m(41.34 ft)
5 m(16.4 ft)
Overwing GravityRefuel Cap
34.5 m(113.19 ft)
17.2 m(56.43 ft)
17.2 m(56.43 ft)
5.8 m(19.03 ft)
A. Four standard 2.5 in. ISO 45 connections.
B. Two service connections (gravity refuel).
6. Overpressure Protector and NACA Flame Arrestor
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUNDOverpressure Protector(Wing)Access Panel 550EB(650EB)
39.48 m(129.53 ft)
27.17 m(89.14 ft)
27.17 m(89.14 ft)
5.75 m(18.86 ft)
NACA Flame Arrestor(Wing)Access Panel 550EB(650EB)
39.12 m(128.35 ft)
26.53 m(87.04 ft)
26.53 m(87.04 ft)
5.7 m(18.7 ft)
Overpressure Protector(Trim Tank)Access Panel 346AB
61.67 m(202.33 ft)
8 m(26.25 ft)
8 m(26.25 ft)
5.7 m(18.7 ft)
NACA Flame Arrestor(Trim Tank)Access Panel 346AB
61.67 m(202.33 ft)
8 m(26.25 ft)
8 m(26.25 ft)
5.7 m(18.7 ft)
5-4-6Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
A
R OUTER TK
R OUTER TKOVERFLOW
INC
LOAD
HI LEVELTEST
TRANSF. VALVE
OPEN
CLOSED
APU EMERG.
SHUTDOWN
PWRSUPPLY
NORM
BAT
L TT R
DEC
REFUEL/DEFUEL VALVESMODE SELECTL OUTER TK L INNER TK CTR TK
L OUTER TK L INNER TK CTR TK TRIM TKHIGH LEVEL
REFUEL
OFFDEFUEL
R INNER TK
R INNER TK
OPENNORMSHUT
L INR. CENTER R INR.
L OUTER R OUTERTRIM ACTUAL
CKPTEND
x 1000
kg1b
PRESELECTED
TRIM TK
198DB FR53.2FR53.4
A
F_AC_050406_1_0140101_01_00
Ground Service ConnectionsRefuel/Defuel Control PanelFIGURE-5-4-6-991-014-A01
5-4-6Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
A
522HB(622HB)
TYPICAL
A
REFUEL/DEFUELCOUPLINGS
REFUEL/DEFUELCOUPLING CAP
REFUEL/DEFUELCOUPLING CAP
F_AC_050406_1_0150101_01_01
Ground Service ConnectionsRefuel/Defuel Coupling
FIGURE-5-4-6-991-015-A01
5-4-6Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
C
OVERPRESSURE PROTECTOR
A
NACA FLAME ARRESTOR
B
A
A
FWD
LH SIDE SHOWNRH SIDE SYMMETRICAL
B
C
RIB36
RIB37
RIB38
550EB(650EB)
550DB(650DB)
F_AC_050406_1_0030101_01_00
Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor - Wing
FIGURE-5-4-6-991-003-A01
5-4-6Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
B
TRIM−TANK NACA VENT
TRIM−TANK OVERPRESSURE
BOTTOM SKIN
A
Z343
346AB
FWD
A
B
RIB19RIB18
F_AC_050406_1_0160101_01_00
Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor - Trim Tank
FIGURE-5-4-6-991-016-A01
5-4-6Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7 Pneumatic System
**ON A/C A340-200 A340-300
Pneumatic Servicing
**ON A/C A340-300
1. High Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND23.9 m(78.41 ft)
0.84 m(2.76 ft)
1.79 m(5.87 ft)HP Connectors:
Access Door 193CB 24.25 m(79.56 ft)
0.84 m(2.76 ft)
1.79 m(5.87 ft)
A. Connectors:- Two standard 3 in. ISO 2026 connections.
2. Low Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND22.48 m(73.75 ft)
0.31 m(1.02 ft)
1.86 m(6.1 ft)LP Connectors:
Access Door 191EB 22.48 m(73.75 ft)
0.76 m(2.49 ft)
1.89 m(6.2 ft)
A. Connectors:- Two standard 8 in. SAE AS4262 connections.
5-4-7Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
3. High Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND21.77 m(71.42 ft)
0.84 m(2.76 ft)
1.79 m(5.87 ft)HP Connectors:
Access Door 193CB 22.12 m(72.57 ft)
0.84 m(2.76 ft)
1.79 m(5.87 ft)
A. Connectors:- Two standard 3 in. ISO 2026 connections.
4. Low Pressure Air Connection
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUND20.35 m(66.77 ft)
0.31 m(1.02 ft)
1.86 m(6.1 ft)LP Connectors:
Access Door 191EB 20.35 m(66.77 ft)
0.76 m(2.49 ft)
1.89 m(6.2 ft)
A. Connectors:- Two standard 8 in. SAE AS4262 connections.
5-4-7Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
193CB
191EB
B
A
FR40
HP CONNECTOR
B
LP CONNECTOR
A
F_AC_050407_1_0020101_01_00
Ground Service ConnectionsLP and HP Ground Connectors
FIGURE-5-4-7-991-002-A01
5-4-7Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8 Oil System
**ON A/C A340-200 A340-300
Oil Servicing
**ON A/C A340-300
1. CFM56-5C2 Series Engine
A. Engine Oil Replenishment:One gravity filling cap and one pressure filling connection per engine.
(1) Engine Oil Gravity Filling
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415BL
31.03 m(101.80 ft)
20.56 m(67.45 ft)
3.47 m(11.38 ft)
Engine 2:Access Door: 425BL
24.46 m(80.25 ft)
10.33 m(33.89 ft)
2.20 m(7.22 ft)
Engine 3:Access Door: 435BL
24.46 m(80.25 ft)
8.41 m(27.59 ft)
2.20 m(7.22 ft)
Engine 4:Access Door: 445BL
31.03 m(101.80 ft)
18.64 m(61.15 ft)
3.47 m(11.38 ft)
(2) Engine Oil Pressure Filling
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415BL
30.90 m(101.38 ft)
20.64 m(67.72 ft)
3.47 m(11.38 ft)
Engine 2:Access Door: 425BL
24.32 m(79.79 ft)
10.41 m(34.15 ft)
2.20 m(7.22 ft)
Engine 3:Access Door: 435BL
24.32 m(79.79 ft)
8.32 m(27.30 ft)
2.20 m(7.22 ft)
5-4-8Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 4:Access Door: 445BL
30.90 m(101.38 ft)
18.56 m(60.89 ft)
3.47 m(11.38 ft)
- Max delivery pressure required: 1.72 bar (25 psi).- Max delivery flow required: 249.84 l/hour (66.00 US gal/hour).
(3) Tank capacity:- Full level: 19.00 l (5.02 US gal).- Usable: 10.68 l (2.82 US gal).
B. IDG Oil Replenishment:One pressure filling connection per engine.
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415AL (416AR)
30.12 m(98.82 ft)
19.40 m(63.65 ft)
2.55 m(8.37 ft)
Engine 2:Access Door: 425AL (426AR)
23.54 m(77.23 ft)
9.17 m(30.09 ft)
1.35 m(4.43 ft)
Engine 3:Access Door: 435AL (436AR)
23.54 m(77.23 ft)
9.57 m(31.40 ft)
1.35 m(4.43 ft)
Engine 4:Access Door: 445AL (446AR)
30.12 m(98.82 ft)
19.80 m(64.96 ft)
2.55 m(8.37 ft)
- Max delivery pressure required: 2.76 bar (40 psi).- Max oil capacity of the IDG: 4.00 l (1.06 US gal).
C. Starter Oil Replenishment:One filling connection per engine.
5-4-8Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415AL (416AR)
30.12 m(98.82 ft)
19.40 m(63.65 ft)
2.55 m(8.37 ft)
Engine 2:Access Door: 425AL (426AR)
23.54 m(77.23 ft)
9.17 m(30.09 ft)
1.35 m(4.43 ft)
Engine 3:Access Door: 435AL (436AR)
23.54 m(77.23 ft)
9.57 m(31.40 ft)
1.35 m(4.43 ft)
Engine 4:Access Door: 445AL (446AR)
30.12 m(98.82 ft)
19.80 m(64.96 ft)
2.55 m(8.37 ft)
- Max oil capacity of the Starter: 0.80 l (0.21 US gal).
**ON A/C A340-200
2. CFM56-5C2 Series Engine
A. Engine Oil Replenishment:One gravity filling cap and one pressure filling connection per engine.
(1) Engine Oil Gravity Filling
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415BL
28.90 m(94.82 ft)
20.56 m(67.45 ft)
3.47 m(11.38 ft)
Engine 2:Access Door: 425BL
22.33 m(73.26 ft)
10.33 m(33.89 ft)
2.20 m(7.22 ft)
Engine 3:Access Door: 435BL
22.33 m(73.26 ft)
8.41 m(27.59 ft)
2.20 m(7.22 ft)
Engine 4:Access Door: 445BL
28.90 m(94.82 ft)
18.64 m(61.15 ft)
3.47 m(11.38 ft)
(2) Engine Oil Pressure Filling
5-4-8Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415BL
28.77 m(94.39 ft)
20.64 m(67.72 ft)
3.47 m(11.38 ft)
Engine 2:Access Door: 425BL
22.19 m(72.80 ft)
10.41 m(34.15 ft)
2.20 m(7.22 ft)
Engine 3:Access Door: 435BL
22.19 m(72.80 ft)
8.32 m(27.30 ft)
2.20 m(7.22 ft)
Engine 4:Access Door: 445BL
28.77 m(94.39 ft)
18.56 m(60.89 ft)
3.47 m(11.38 ft)
- Max delivery pressure required: 1.72 bar (25 psi).- Max delivery flow required: 249.84 l/hour (66.00 US gal/hour).
(3) Tank capacity:- Full level: 19.00 l (5.02 US gal).- Usable: 10.68 l (2.82 US gal).
B. IDG Oil Replenishment:One pressure filling connection per engine.
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415AL (416AR)
27.99 m(91.83 ft)
19.40 m(63.65 ft)
2.55 m(8.37 ft)
Engine 2:Access Door: 425AL (426AR)
21.41 m(70.24 ft)
9.17 m(30.09 ft)
1.35 m(4.43 ft)
Engine 3:Access Door: 435AL (436AR)
21.41 m(70.24 ft)
9.57 m(31.40 ft)
1.35 m(4.43 ft)
Engine 4:Access Door: 445AL (446AR)
27.99 m(91.83 ft)
19.80 m(64.96 ft)
2.55 m(8.37 ft)
- Max delivery pressure required: 2.76 bar (40 psi).- Max oil capacity of the IDG: 4.00 l (1.06 US gal).
5-4-8Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
C. Starter Oil Replenishment:One filling connection per engine.
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEANHEIGHTFROM
GROUNDEngine 1:Access Door: 415AL (416AR)
27.99 m(91.83 ft)
19.40 m(63.65 ft)
2.55 m(8.37 ft)
Engine 2:Access Door: 425AL (426AR)
21.41 m(70.24 ft)
9.17 m(30.09 ft)
1.35 m(4.43 ft)
Engine 3:Access Door: 435AL (436AR)
21.41 m(70.24 ft)
9.57 m(31.40 ft)
1.35 m(4.43 ft)
Engine 4:Access Door: 445AL (446AR)
27.99 m(91.83 ft)
19.80 m(64.96 ft)
2.55 m(8.37 ft)
- Max oil capacity of the Starter: 0.80 l (0.21 US gal).
5-4-8Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
OIL TANKFILLER CAP
A
OIL TANK
OIL
LEVEL
SIGHT CAGE
BFWD
A
415BL425BL435BL445BL
(ENGINE 1)(ENGINE 2)(ENGINE 3)(ENGINE 4)
FULL MARK
B
F_AC_050408_1_0170101_01_00
Ground Service ConnectionsEngine Oil Tank - CFM56-5C2 Series Engine
FIGURE-5-4-8-991-017-A01
5-4-8Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
CASEDRAINPLUG
DUSTCAP
PRESSUREFILL VALVE
OVERFILLDRAINVALVE
A
B
A340OVER
ADDOIL
CFM56−5C2
FULL
ADDOIL
STABLE OIL
B
FWD
A
445AL
415AL425AL435AL
(ENGINE 1)(ENGINE 2)(ENGINE 3)(ENGINE 4)
446AR
416AR426AR436AR
(ENGINE 1)(ENGINE 2)(ENGINE 3)(ENGINE 4)
SIGHT GLASS
F_AC_050408_1_0180101_01_00
Ground Service ConnectionsIDG Oil Tank - CFM56-5C2 Series Engine
FIGURE-5-4-8-991-018-A01
5-4-8Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
PNEUMATICSTARTER
OIL FILLPLUG
OIL LEVELOVERFLOW
PLUG
MAGNETIC CHIPDETECTOR
DRAINPLUG
ACCESSORYGEARBOX
A
445AL
415AL425AL435AL
(ENGINE 1)(ENGINE 2)(ENGINE 3)(ENGINE 4)
446AR
416AR426AR436AR
(ENGINE 1)(ENGINE 2)(ENGINE 3)(ENGINE 4) A
F_AC_050408_1_0270101_01_00
Ground Service ConnectionsStarter Oil Tank - CFM56-5C2 Series Engine
FIGURE-5-4-8-991-027-A01
5-4-8Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
APU Oil Servicing
**ON A/C A340-300
1. APU Oil Servicing:APU oil gravity filling cap.
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
APU OilReplenishment:Access Doors:316AR, 315AL
60.3 m(197.83 ft)
0.4 m(1.31 ft)
8 m(26.25 ft)
A. Tank capacity (usable):- APU Type: 331-350: 7.3 l (1.93 US gal)- APU Type: 331-600: 11 l (2.91 US gal).
**ON A/C A340-200
2. APU Oil Servicing:APU oil gravity filling cap.
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
APU OilReplenishment:Access Doors:316AR, 315AL
56 m(183.73 ft)
0.4 m(1.31 ft)
8 m(26.25 ft)
A. Tank capacity (usable):- APU Type: 331-350: 7.3 l (1.93 US gal)- APU Type: 331-600: 11 l (2.91 US gal).
5-4-8Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
PRESSURE FILLOVERFLOW PORT
PRESSUREFILL PORT
OIL SIGHTGLASS
BFWD
DO NOT REMOVE OILFILLER CAP WHEN OILLEVEL IS ABOVE FULLMARK ON SIGHT GLASS
OIL SCUPPER
GRAVITY FILLPORT
LUBRIFICATION OIL FILTER
GENERATOR SCAVENGE OIL FILTER
OIL PUMPMODULE
A
OIL FILLERCAP
B
FR95
FR101
316AR
315AL
A
F_AC_050408_1_0220101_01_00
Ground Service ConnectionsAPU Oil Servicing
FIGURE-5-4-8-991-022-A01
5-4-8Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9 Potable Water System
**ON A/C A340-300
Potable Water Servicing
1. Potable Water Servicing
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
Potable-WaterService Panel:Access Door 164AR
48.15 m(157.97 ft)
0.51 m(1.67 ft)
3.15 m(10.33 ft)
FWD Drain Panel:Access Door 133BL
14.7 m(48.23 ft)
0.6 m(1.97 ft)
1.92 m(6.30 ft)
AFT Drain Panel:Access Door 154AR
40.18 m(131.82 ft)
0.72 m(2.36 ft)
2.46 m(8.07 ft)
NOTE : Distances are approximate.
2. Technical Specifications
A. Connections
(1) On the potable-water service panel (access door 164AR):- One heated 3/4 in. (ISO 17775) quick release filling connection- One heated 3/4 in. (ISO 17775) overflow and discharge connection- One ground pressurization connection.
(2) On the FWD drain panel (access door 133BL):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control.
(3) On the AFT drain panel (access door 154AR):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control- One standard 3/4 in. (ISO 17775) overflow and discharge connection with back-up
mechanical control.
B. Capacity- 700 l (184.92 US gal) standard- 1050 l (277.38 US gal) standard option.
C. Filling Pressure and Flow Rate
FWD tank:- Filling pressure: 3.45/8.62 bar (50/125 psi)- Flow rate: 45/73 l/min (11.89/19.28 US gal/min).
AFT tank:
5-4-9Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Filling pressure: 3.45/8.62 bar (50/125 psi)- Flow rate: 56/85 l/min (14.79/22.45 US gal/min).
5-4-9Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
164AR
154AR
133BL
DRAIN NIPPLEDRAIN NIPPLE
FWD POTABLE−WATER DRAIN PANELAFT POTABLE−WATER DRAIN PANEL
CB
OVERFLOW NIPPLE
APOTABLE−WATER SERVICE PANEL
CAPASSEMBLY
FILL/DRAINNIPPLE
FR69
FILL/DRAINCONTROL HANDLE
FR70
MAINTENANCE DOORLIMIT−SWITCH
GROUND AIRCONNECTION
DRAIN VALVECONTROL HANDLE
FR29
FR28FR57.1
FR57.2OVERFLOW
NIPPLEDRAIN CONTROL HANDLE(FILLING LINE DRAIN VALVE)
OVERFLOW CONTROL HANDLE(FILL/DRAIN VALVE)
AB
C
F_AC_050409_1_0290101_01_00
Ground Service ConnectionsPotable-Water Ground Service Panels
FIGURE-5-4-9-991-029-A01
5-4-9Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
POTABLE WATERTANK
OVERFLOW LINE
ANOTE:
TYPICAL01
01
POTABLE WATERFILL/DRAIN LINE
FR53.8
FR57
FR73
A
A
AFT CARGO DOOR
BULK CARGO DOOR
Z152
Z172
FR53.2
FR65
FR80Z160
FR72
FR76
F_AC_050409_1_0300101_01_00
Ground Service ConnectionsPotable-Water Tanks LocationFIGURE-5-4-9-991-030-A01
5-4-9Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
Potable Water Servicing
1. Potable Water Servicing
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
Potable-WaterService Panel:Access Door 164AR
43.88 m(143.96 ft)
0.51 m(1.67 ft)
3.13 m(10.27 ft)
FWD Drain Panel:Access Door 133BL
14.7 m(48.23 ft)
0.60 m(1.97 ft)
1.92 m(6.30 ft)
AFT Drain Panel:Access Door 154AR
36.51 m(119.78 ft)
0.72 m(2.36 ft)
2.44 m(8.01 ft)
NOTE : Distances are approximate.
2. Technical Specifications
A. Connections
(1) On the potable-water service panel (access door 164AR):- One heated 3/4 in. (ISO 17775) quick release filling connection- One heated 3/4 in. (ISO 17775) overflow and discharge connection- One ground pressurization connection.
(2) On the FWD drain panel (access door 133BL):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control.
(3) On the AFT drain panel (access door 154AR):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control- One standard 3/4 in. (ISO 17775) overflow and discharge connection with back-up
mechanical control.
B. Capacity- 700 l (184.92 US gal) standard- 1050 l (277.38 US gal) standard option.
C. Filling Pressure and Flow Rate
FWD tank:- Filling pressure: 3.45/8.62 bar (50/125 psi)- Flow rate: 45/73 l/min (11.89/19.28 US gal/min).
AFT tank:- Filling pressure: 3.45/8.62 bar (50/125 psi)
5-4-9Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Flow rate: 56/85 l/min (14.79/22.45 US gal/min).
5-4-9Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
DRAIN NIPPLEDRAIN NIPPLE
FWD POTABLE−WATER DRAIN PANELAFT POTABLE−WATER DRAIN PANEL
CB
OVERFLOW NIPPLE
APOTABLE−WATER SERVICE PANEL
CAPASSEMBLY
FILL/DRAINNIPPLE
FR69
FILL/DRAINCONTROL HANDLE
FR70
MAINTENANCE DOORLIMIT−SWITCH
GROUND AIRCONNECTION
DRAIN VALVECONTROL HANDLE
FR29
FR28
OVERFLOWNIPPLEDRAIN CONTROL HANDLE
(FILLING LINE DRAIN VALVE)
OVERFLOW CONTROL HANDLE(FILL/DRAIN VALVE)
164AR
154AR
133BL
FR56
FR57
B A
C
F_AC_050409_1_0310101_01_00
Ground Service ConnectionsPotable-Water Ground Service Panels
FIGURE-5-4-9-991-031-A01
5-4-9Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
POTABLE WATERTANK
OVERFLOW LINE
ANOTE:
TYPICAL01
01
POTABLE WATERFILL/DRAIN LINE
FR73
A
AFT CARGO DOOR
BULK CARGO DOOR
Z152
Z172
A
FR53.4
FR53.9
Z160
FR53.2
FR65
FR80
FR72
FR76
F_AC_050409_1_0320101_01_00
Ground Service ConnectionsPotable-Water Tanks LocationFIGURE-5-4-9-991-032-A01
5-4-9Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10 Waste Water System
**ON A/C A340-200 A340-300
Waste Water Servicing
**ON A/C A340-300
1. Waste Water Servicing
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUNDWaste Water GroundService Panel:Access Door 171AL
50.00 m(164.04 ft)
0.09 m(0.30 ft)
3.60 m(11.81 ft)
A. Waste water ground service panel comprising:- Standard: One standard 4 in. (ISO 17775) drain connection and two 1 in. (ISO 17775)
flushing connections- Standard option: One standard 4 in. (ISO 17775) drain connection and three 1 in. (ISO
17775) flushing connections.
B. Capacity waste tanks:- Standard: 700 l (184.92 US gal)- Standard option: 1050 l (277.38 US gal).
C. Chemical fluid:- Standard: 36 l (9.51 US gal)- Standard option: 54 l (14.27 US gal).
**ON A/C A340-200
2. Waste Water Servicing
DISTANCEFROM AIRCRAFT CENTERLINE
ACCESSAFT OF NOSE
LH SIDE RH SIDE
MEAN HEIGHTFROM
GROUNDWaste Water GroundService Panel:Access Door 171AL
45.72 m(150.00 ft)
0.09 m(0.30 ft)
3.60 m(11.81 ft)
A. Waste water ground service panel comprising:- Standard: One standard 4 in. (ISO 17775) drain connection and two 1 in. (ISO 17775)
flushing connections
5-4-10Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Standard option: One standard 4 in. (ISO 17775) drain connection and three 1 in. (ISO17775) flushing connections.
B. Capacity waste tanks:- Standard: 700 l (184.92 US gal)- Standard option: 1050 l (277.38 US gal).
C. Chemical fluid:- Standard: 36 l (9.51 US gal)- Standard option: 54 l (14.27 US gal).
5-4-10Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
LIMIT SWITCHWASTE−PANEL
RINSE CONNECTIONTANK 2 FILL AND
TANK 1 FILL ANDRINSE CONNECTION
WASTEDRAIN−LINE VALVE
DRAIN−VALVECONTROL LEVERS
FR75
FR59
FR74 FR73
A171AL
OPEN
CLOSE
LH RH
A
FWD
F_AC_050410_1_0020101_01_00
Ground Service ConnectionsWaste Water Ground Service Panel
FIGURE-5-4-10-991-002-A01
5-4-10Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
FR73
FR65
BULK CARGO DOOR
Z160
Z172162ZW
A
FR76
A
WASTE TANK
FR73
FR76
F_AC_050410_1_0060101_01_00
Ground Service ConnectionsWaste Tanks Location
FIGURE-5-4-10-991-006-A01
5-4-10Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-11 Cargo Control Panels
**ON A/C A340-200 A340-300
Cargo Control Panels
**ON A/C A340-300
1. Cargo Control Panels
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
FWD CLS* Panel:Access Door 122DR
14.17 m(46.49 ft)
2.60 m(8.53 ft)
3.90 m(12.80 ft)
FWD Cargo DoorPanel:Access Door 122CR
13.87 m(45.51 ft)
2.40 m(7.87 ft)
3.30 m(10.83 ft)
AFT CLS* Panel:Access Door152MR
48.95 m(160.60 ft)
2.60 m(8.53 ft)
4.60 m(15.09 ft)
AFT Cargo DoorPanel:Access Door 152NR
48.65 m(159.61 ft)
2.40 m(7.87 ft)
4.00 m(13.12 ft)
NOTE : * CLS - CARGO LOADING SYSTEMS
**ON A/C A340-200
2. Cargo Control Panels
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
FWD CLS* Panel:Access Door 122DR
14.17 m(46.49 ft)
2.60 m(8.53 ft)
3.90 m(12.80 ft)
FWD Cargo DoorPanel:Access Door 122CR
13.87 m(45.51 ft)
2.40 m(7.87 ft)
3.30 m(10.83 ft)
AFT CLS* Panel:Access Door152MR
44.68 m(146.59 ft)
2.60 m(8.53 ft)
4.60 m(15.09 ft)
5-4-11Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
DISTANCEFROM AIRCRAFT CENTERLINEACCESS
AFT OF NOSELH SIDE RH SIDE
MEAN HEIGHTFROM GROUND
AFT Cargo DoorPanel:Access Door 152NR
44.38 m(145.60 ft)
2.40 m(7.87 ft)
4.00 m(13.12 ft)
NOTE : * CLS - CARGO LOADING SYSTEMS
5-4-11Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
PWR ON/OFF SWITCH
JOYSTICK
DOOR SILL LATCHRELEASE LEVER
OUTSIDE CARGO LOADINGSYSTEM CONTROL PANEL
LIGHT SWITCH
INDICATOR LIGHT
DOOR OPERATION LEVER
CARGO DOOR CONTROL PANEL
122DR
122CR
A
B
FR18
FR19
FR20
A
B
FWD CARGO DOOR
F_AC_050411_1_0040101_01_00
Forward Cargo Control PanelsFIGURE-5-4-11-991-004-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
PWR ON/OFF SWITCH
OUTSIDE CARGO LOADINGSYSTEM CONTROL PANEL
DOOR SILL LATCHRELEASE LEVER
JOYSTICK
CARGO DOOR CONTROL PANEL
LIGHT SWITCH
INDICATOR LIGHT
DOOR OPERATION LEVER
152MR
152NR
A
B
FR65
FR53.2
Z150
AFT CARGO DOOR
FR59FR58
A
B
F_AC_050411_1_0050101_01_00
Aft Cargo Control PanelsFIGURE-5-4-11-991-005-A01
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Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A340-200 A340-300
Engine Starting Pneumatic Requirements
1. The purpose of this section is to provide the minimum air data requirements at the aircraftconnection, needed to start the engine within no more than 70 seconds, at sea level (0 feet), for a setof Outside Air Temperatures (OAT).
ABBREVIATION DEFINITION
A/C Aircraft
ASU Air Start Unit
HPGC High Pressure Ground Connection
OAT Outside Air Temperature
A. Air data (discharge temperature, absolute discharge pressure) are given at the HPGC.
B. For the requirements below, the configuration with two HPGC is used. Using one connector only(for a given mass flow rate and discharge pressure from the ASU) will increase the pressure lossin the ducts of the bleed system and therefore lower the performances at the engine starter.
C. For a given OAT the following charts are used to determine an acceptable combination for airdischarge temperature, absolute discharge pressure and mass flow rate.
D. This section is addressing requirements for the ASU only, and is not representative of the startperformance of the aircraft using the APU or engine cross bleed procedure.
E. To protect the A/C, the charts feature, if necessary:- The maximum discharge pressure at the HPGC- The maximum discharge temperature at the HPGC.
5-5-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
AIR
FLO
W (
lb/m
in)
CFM56−5C2 SERIES/SEA LEVELSTARTING TIME: LESS THAN 70 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
OUTSIDE AIR TEMPERATURE OAT (° C)
OUTSIDE AIR TEMPERATURE OAT (° F)0 20 40 60 80 100 120 140−20−40
EXAMPLE:
NOTE:
35
40
45
50
0 10 20 30 40 50 60−10−20−30−40−50
30 35 40 45 5040
45
50
55
60
65
70
75
80
90
100
110
120
130
140
150
160
170
FOR AN OAT OF 20° C (68° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 150° C (302° F) AT HPGC:− THE REQUIRED PRESSURE AT HPGC IS 39 psia− THE REQUIRED AIRFLOW AT HPGC IS 50.5 kg/min.
IN CASE THE ACTUAL DISCHARGE TEMPERATURE OF THE ASU DIFFERS SUBSTANTIALLY FROM THE ONES GIVEN IN THE CHARTS, A SIMPLE INTERPOLATION (LINEAR) IS SUFFICIENT TO DETERMINE THE REQUIRED AIR DATA.
ABSOLUTE PRESSURE (psia)
AIR
FLO
W (
kg/m
in)
AB
SO
LUT
E P
RE
SS
UR
E (
psia
)
220° C (428° F) MAX.150° C (302° F)100° C (212° F)
ASU DISCHARGE TEMPERATURE:
F_AC_050500_1_0020101_01_02
Example for Use of the ChartsFIGURE-5-5-0-991-002-A01
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
AIR
FLO
W (
kg/m
in)
AIR
FLO
W (
lb/m
in)
AB
SO
LUT
E P
RE
SS
UR
E (
psia
)STARTING TIME: LESS THAN 70 s
AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)
OUTSIDE AIR TEMPERATURE OAT (° C)
OUTSIDE AIR TEMPERATURE OAT (° F)0 20 40 60 80 100 120 140−20−40
30 35 40 45 5040
45
50
55
60
65
70
75
80
90
100
110
120
130
140
150
160
170
35
40
45
50
0 10 20 30 40 50 60−10−20−30−40−50
ABSOLUTE PRESSURE (psia)
CFM56−5C2 SERIES/SEA LEVEL
220° C (428° F) MAX.150° C (302° F)100° C (212° F)
ASU DISCHARGE TEMPERATURE:
F_AC_050500_1_0080101_01_01
Engine Starting Pneumatic RequirementsCFM56-5C2 Series
FIGURE-5-5-0-991-008-A01
5-5-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A340-200 A340-300
Ground Pneumatic Power Requirements
1. GeneralThis section describes the required performance for the ground equipment to maintain the cabintemperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for heating cases after boarding(Section 5.7 - steady state), and provides the time needed to cool down or heat up the aircraft cabinto the required temperature (Section 5.6 - dynamic cases with aircraft empty).
ABBREVIATION DEFINITION
A/C Aircraft
AHM Aircraft Handling Manual
GC Ground ConnectionGSE Ground Service Equipment
IFE In-Flight Entertainment
LP Low PressureLPGC Low Pressure Ground ConnectionOAT Outside Air Temperature
PCA Pre-Conditioned Air
A. The air flow rates and temperature requirements for the GSE, provided in Sections 5.6 and 5.7,are given at A/C ground connection.
NOTE : The cooling capacity of the equipment (kW) is only indicative and is not sufficient byitself to ensure the performance (outlet temperature and flow rate combinations arethe requirements needed for ground power).An example of cooling capacity calculation is given in Section 5.7.
B. The air flow rates and temperature requirements for the GSE are given for the A/C in theconfiguration ”2 LP ducts connected”.
NOTE : The maximum air flow is driven by pressure limitation at LPGC.
C. For temperatures at ground connection below +2 ˚C (+35.6 ˚F) (Subfreezing), the groundequipment shall be compliant with the Airbus document ”Subfreezing PCA Carts -- ComplianceDocument for Suppliers” (contact Airbus to obtain this document) defining all the requirementswith which Subfreezing Pre-Conditioning Air equipment must comply to allow its use on Airbusaircraft. These requirements are in addition to the functional specifications included in the IATAAHM997.
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2. Ground Pneumatic Power RequirementsThis section provides the ground pneumatic power requirements for:- Heating (pull up) the cabin, initially at OAT, up to 21 ˚C (69.8 ˚F) (see FIGURE
5-6-0-991-002-A)- Cooling (pull down) the cabin, initially at OAT, down to 27 ˚C (80.6 ˚F) (see FIGURE
5-6-0-991-004-A).
5-6-0Page 2
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@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
30 60 90 120 1500.8
1.2
1.4
1.6
1.8
2.2
2.4
2.0
2.5
3.0
3.5
4.0
4.5
5.0
AIR
FLO
W A
T G
C (
kg/s
)
AIR
FLO
W A
T G
C (
lb/s
)
PULL UP PERFORMANCE
TIME TO HEAT CABIN TO +21° C (+69.8° F) ON GROUND (min)
OAT ISA −38° C (−36.4° F); GC OUTLET +70° C (+158° F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
40 50 70 80 100 110 130 140
MAXIMUM AIR FLOW
1.0
2.0
F_AC_050600_1_0020101_01_00
Ground Pneumatic Power RequirementsHeating
FIGURE-5-6-0-991-002-A01
5-6-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
30 60 90 120 1500.8
1.2
1.4
1.6
1.8
2.2
2.4
2.0
2.5
3.0
3.5
4.0
4.5
5.0
AIR
FLO
W A
T G
C (
kg/s
)
AIR
FLO
W A
T G
C (
lb/s
)
PULL DOWN PERFORMANCE
TIME TO COOL CABIN TO +27° C (+80.6° F) ON GROUND (min)
OAT ISA +23° C (+73.4° F); GC OUTLET +2° C (+35.6° F); EMPTY CABIN; IFE OFF; SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
OAT ISA +23° C (+73.4° F); GC OUTLET −10° C (+14° F); EMPTY CABIN; IFE OFF; SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
40 50 70 80 100 110 130 140
MAXIMUM AIR FLOW
2.0
1.0
F_AC_050600_1_0040101_01_00
Ground Pneumatic Power RequirementsCooling
FIGURE-5-6-0-991-004-A01
5-6-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A340-200 A340-300
Preconditioned Airflow Requirements
1. This section provides the preconditioned airflow rate and temperature needed to maintain the cabintemperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for the heating cases.
These settings are not intended to be used for operation (they are not a substitute for the settingsgiven in the AMM). They are based on theoretical simulations and give the picture of a real steadystate.The purpose of the air conditioning (cooling) operation (described in the AMM) is to maintain thecabin temperature below 27 ˚C (80.6 ˚F) during boarding (therefore it is not a steady state).
5-7-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
AIR
FLO
W A
T G
C (
kg/s
)
−150.8
AIR
FLO
W A
T G
C (
lb/s
)
1.0
1.2
1.4
1.6
1.8
2.0
2.2
2.4
−10 −5 0 5 10 15 20 25 30 35 40 45 50 55 60
2.0
2.5
3.0
3.5
4.0
4.5
5.0
0 10 20 30 40 50 60 70 80
INLET TEMPERATURE AT GC (° C)
INLET TEMPERATURE AT GC (° F)
MAXIMUM AIRFLOW
COOLING/HEATING PERFORMANCE
SETTINGS NOTINTENDED TO BE USED
FOR OPERATION
OAT ISA; EMPTY CABIN; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON; GALLEYS ON
OAT ISA −38° C (−36.4° F); EMPTY CABIN; IFE OFF; LIGHTS ON; NO SOLAR LOAD; RECIRCULATIONFANS ON; GALLEYS OFF
C H
EXAMPLE:COOLING CAPACITY CALCULATION:FOR THE CONDITIONS "C", THE COOLING CAPACITY OF 1.9 kg/s x 1 kJ/(kg.° C) x (27− 5) = 41.8 kW(OR 12.5 TONS COOLING CAPACITY) IS NEEDED TO MAINTAIN THE CABIN TEMPERATURE AT 27° C (80.6° F)(1.9 kg/s AT 5° C (41° F) FOR AIR AT GC INLET).
90 100 110 120 130 140
F_AC_050700_1_0030101_01_01
Preconditioned Airflow RequirementsFIGURE-5-7-0-991-003-A01
5-7-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A340-200 A340-300
Ground Towing Requirements
1. This section provides information on aircraft towing.
The A340-200/-300 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 ISI 09.11.00001.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a towbar attached to the NLG. One towbar fitting is installed at the front of the leg(optional towing fitting for towing from the rear of the NLG available).The main landing gears have attachment points for towing or debogging (for details, refer ARM 07).
This section shows the chart to determine the drawbar pull and tow tractor mass requirements as afunction of the following physical characteristics:- Aircraft weight,- Number of engines at idle,- Slope.
The following chart is applicable to both A340-200 and -300 aircraft.
2. Towbar design guidelines
The aircraft towbar shall comply with the following standards:- ISO 8267-1, ”Aircraft - Towbar Attachment Fitting - Interface Requirements - Part 1: Main Line
Aircraft”,- ISO 9667, ”Aircraft Ground Support Equipment - Towbars”,- IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Towbar”.
A conventional type towbar is required which should be equipped with a damping system (to protectthe NLG against jerks) and with towing shear pins:- A traction shear pin calibrated at 28 620 daN (64 340 lbf),- A torsion pin calibrated at 3 130 m.daN (277 028 lbf.in).The towing head is designed according to ISO 8267-1, cat. III.
5-8-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A340−200 OR −300 AT 270 000 kg,AT 1.5% SLOPE, 2 ENGINES AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (270 000 kg),− 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 = 4,− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED No. OF ENGINES (2),− 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 (21 300 kg),− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (37 300 kg).
30
25
20
15
10
5
00 10 20 30 40 50 60 70 80 0 1 2 3 4 0 0.5 1.0 1.5 2.0
280255230205180155130
21.3
37.3
2 ENGINES ON1.5% SLOPE 270
ICE = 0.05
HARD SNOW = 0.2
DR
Y C
ON
CR
ETE
= 0.
8
DR
AW
BA
R P
ULL
(x
1 00
0 kg
)
A/C
WE
IGH
T (
x 1
000
kg)
TOTAL TRACTION WHEEL LOAD (x 1 000 kg) No. OF ENGINES AT IDLE SLOPE ( % )
WET
CO
NC
RET
E
= 0
.57
BREAKAWAY RESISTANCE 4%# OF ENGINES ON FOR PB: 2ENGINE THRUST 500 daN
F_AC_050800_1_0060101_01_01
Ground Towing RequirementsFIGURE-5-8-0-991-006-A01
5-8-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0 De-Icing and External Cleaning
**ON A/C A340-200 A340-300
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 17 m (56 ft).
2. De-Icing
AIRCRAFT TYPEWing Top Surface
(Both Sides)
Wingtip Devices(Both Inside andOutside Surfaces)
(Both Sides)
HTP Top Surface(Both Sides)
VTP(Both Sides)
A340-200306 m2
(3 294 ft2)11 m2
(118 ft2)65 m2
(700 ft2)91 m2
(980 ft2)
A340-300306 m2
(3 294 ft2)11 m2
(118 ft2)65 m2
(700 ft2)91 m2
(980 ft2)
AIRCRAFT TYPEFuselage Top Surface
(Top Third - 120˚ Arc)
Nacelle and Pylon(Top Third - 120˚ Arc)
(All Engines)Total De-Iced Area
A340-200294 m2
(3 165 ft2)55 m2
(592 ft2)821 m2
(8 837 ft2)
A340-300319 m2
(3 434 ft2)55 m2
(592 ft2)847 m2
(9 117 ft2)
NOTE : Dimensions are approximate.
3. External Cleaning
AIRCRAFTTYPE
Wing TopSurface
(Both Sides)
Wing LowerSurface
(Including FlapTrack Fairing)(Both Sides)
Wingtip Devices(Both Insideand OutsideSurfaces)
(Both Sides)
HTP TopSurface
(Both Sides)
HTP LowerSurface
(Both Sides)
A340-200306 m2
(3 294 ft2)340 m2
(3 660 ft2)11 m2
(118 ft2)65 m2
(700 ft2)65 m2
(700 ft2)
A340-300306 m2
(3 294 ft2)340 m2
(3 660 ft2)11 m2
(118 ft2)65 m2
(700 ft2)65 m2
(700 ft2)
5-9-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT TYPEVTP
(Both Sides)Fuselage andBelly Fairing
Nacelle and Pylon(All Engines) Total Cleaned Area
A340-20091 m2
(980 ft2)896 m2
(9 644 ft2)200 m2
(2 153 ft2)1 982 m2
(21 334 ft2)
A340-30091 m2
(980 ft2)971 m2
(10 452 ft2)200 m2
(2 153 ft2)2 057 m2
(22 141 ft2)
NOTE : Dimensions are approximate.
5-9-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A340-200 A340-300
Engine Exhaust Velocities and Temperatures
1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway and Maximum Takeoff conditions.
6-1-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A340-200 A340-300
Engine Exhaust Velocities Contours - Ground Idle Power
1. This section gives engine exhaust velocities contours at ground idle power.
6-1-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_060101_1_0040101_01_00
FE
ET
ME
TE
RS
50
GR
OU
ND
PLA
NE
AIR
PLA
NE
ELE
VA
TIO
N
100
150
200
250
300
350
400
1530
4560
7590
105
120
C L
ftm
00
V =
40
m/s
V =
20
m/s
V =
12
m/s
V =
40
m/s
V =
20
m/s
V =
12
m/s
30 121824 6
100 406080 20
030 121824 6
GR
OU
ND
IDLE
INC
LUD
ES
: (W
OR
ST
CA
SE
) G
RO
UN
D P
LAN
E P
RO
XIM
ITY
HE
AD
WIN
D (
20 K
NT
S)
PLA
N
ftm
0
100 406080 20
00
Engine Exhaust VelocitiesGround Idle Power - CFM56-5C series engine
FIGURE-6-1-1-991-004-A01
6-1-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A340-200 A340-300
Engine Exhaust Temperatures Contours - Ground Idle Power
1. This section gives engine exhaust temperatures contours at ground idle power.
6-1-2Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
FEET
METERS
50
GROUND PLANE
AIRPLANE
100
15 30
CL
ftm
0
12
18
6
60
ftm
0
30
12
18
24
6
100
45
150
60
200
GROUND IDLE
INCLUDES: (WORST CASE) GROUND PLANE PROXIMITY HEADWIND (20 KNTS)
306°F152°C
207°F97°C
108°F42°C
306°F 207°F 108°F152°C 97°C 42°C
PLAN0
40
60
80
20
ELEVATION0
40
20
0
0
F_AC_060102_1_0040101_01_00
Engine Exhaust TemperaturesGround Idle Power - CFM56-5C series engine
FIGURE-6-1-2-991-004-A01
6-1-2Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A340-200 A340-300
Engine Exhaust Velocities Contours - Breakaway Power
1. This section gives engine exhaust velocities contours at breakaway power.
6-1-3Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_060103_1_0040101_01_00
FE
ET
ME
TE
RS
50
GR
OU
ND
PLA
NE
AIR
PLA
NE
ELE
VA
TIO
N 100
150
200
250
300
350
400
1530
4560
7590
105
120
C L
135
150
165
180
195
ftm
450
500
550
650
600
00
V =
40
m/s
V =
20
m/s
V =
12
m/s
4−E
NG
INE
BR
EA
KA
WA
Y
INC
LUD
ES
: (W
OR
ST
CA
SE
) G
RO
UN
D P
LAN
E P
RO
XIM
ITY
HE
AD
WIN
D (
20 K
NT
S)
V =
40
m/s
V =
20
m/s
V =
12
m/s
30 121824 6
100 406080 20
ftm
030 121824 6
PLA
N0
100 406080 20
00
Engine Exhaust VelocitiesBreakaway Power - CFM56-5C series engine
FIGURE-6-1-3-991-004-A01
6-1-3Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A340-200 A340-300
Engine Exhaust Temperatures Contours - Breakaway Power
1. This section gives engine exhaust temperatures contours at breakaway power.
6-1-4Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_060104_1_0040101_01_00
GROUND PLANE
AIRPLANE
ELEVATION
PLAN CL
ftm
0 0
12
18
6
40
60
20
ftm
0 0
30
12
18
24
6
100
40
60
80
20
240°F116°C
140°F60°C
100°F38°C
240°F116°C
140°F60°C
100°F38°C
FEET
METERS
50 100
15 30 45
150
60
2000
0
Engine Exhaust TemperaturesBreakaway Power - CFM56-5C series engine
FIGURE-6-1-4-991-004-A01
6-1-4Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A340-200 A340-300
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power.
6-1-5Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_060105_1_0040101_01_00
FE
ET
ME
TE
RS
GR
OU
ND
PLA
NE
AIR
PLA
NE
ELE
VA
TIO
N
PLA
N
100
200
300
C L
ftm 0
0
30 121824 6
100
406080 20
3060
9012
015
018
021
024
027
030
033
036
039
0
400
500
700
800
600
900
1000
1100
1200
1300
ftm 0
0
30 121824 6
100
406080 20
V =
40
m/s
V =
20
m/s
V =
12
m/s
V =
40
m/s
V =
20
m/s
V =
12
m/s
TA
KE
OF
F P
OW
ER
INC
LUD
ES
: (W
OR
ST
CA
SE
) G
RO
UN
D P
LAN
E P
RO
XIM
ITY
HE
AD
WIN
D (
20 K
NT
S)
00
Engine Exhaust VelocitiesTakeoff Power - CFM56-5C series engine
FIGURE-6-1-5-991-004-A01
6-1-5Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A340-200 A340-300
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power.
6-1-6Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_060106_1_0040101_01_00
FEET
METERS
50
GROUND PLANE
AIRPLANE
ELEVATION
PLAN
100
15 30
CL
ftm
0 0
30
12
18
24
6
100
40
60
80
20
45
150
306°F152°C
207°F97°C
108°F42°C
60
200 250
75 90
300
0 0
30
12
18
24
6
100
40
60
80
108°F42°C
306°F152°C
207°F97°C
TAKEOFF POWER
INCLUDES: (WORST CASE) GROUND PLANE PROXIMITY HEADWIND (20KNTS)
ftm
20
0
0
Engine Exhaust TemperaturesTakeoff Power - CFM56-5C series engine
FIGURE-6-1-6-991-004-A01
6-1-6Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A340-200 A340-300
Danger Areas of Engines
1. Danger Areas of the Engines.
NOTE : Areas with exhaust velocities of more than 56 km/h (35 mph, 50 ft/s or 15 m/s) aredefined as areas where injury to persons and/or damage to machinery can occur.
6-3-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1 Ground Idle Power
**ON A/C A340-200 A340-300
Ground Idle Power
1. This section provides danger areas of the engines at ground idle power conditions.
6-3-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_060301_1_0040101_01_00F_AC_060301_1_0040101_01_00
NOT TO SCALE
RADIUS = 9.7 ft
4.7 ft45°
CLOSE ENTRYCORRIDOR FOR
WIND DIRECTION>90 DEGREES
AB
CNO ENTRY 105 ft (32 m)AFT OF NOZZLE EXIT
GMM−1137912−00−B
AREA
A 210−145(338−233)
B 145−105(233−169)
C
D 65−20(105−32)
105−65(169−105)
E < 20 (32) BEYOND DANGER AREA.
INLET SUCTIONDANGER AREA
ENTRYCORRIDOR
EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR LESS
APPROX. WINDVELOCITYmph (km/h)
LIGHT TO MODERATE DAMAGE TO TRANSPORT − TYPE AIRCRAFT.
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE", VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV 1951.
D
EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR GREATER
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR;COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE − ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING; CORRUGATED STEEL STRUCTURES LESS SEVERELY.
MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AIR TRANSPORT− TYPE AIRCRAFT.
171 ft (52 m)WIDTH
TO 417 ft (127 m)E
(3.0 m)
(1.4 m)
INLET DANGER AREASINCLUDE:(WORST CASE)
GROUND PLANE PROXIMITYHEADWIND/CROSSWIND (20 kts)
EXHAUST DANGER AREASINCLUDE (WORST CASE):
GROUND PLANE PROXIMITYHEADWIND (20 kts)
INLET HAZARD DIMENSIONSBASED ON 40 ft/SEC
CRITICAL VELOCITY WITH A3 ft CONTINGENCY ADDED
Danger Areas of EnginesCFM56-5C series engine
FIGURE-6-3-1-991-004-A01
6-3-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2 Breakaway Power
**ON A/C A340-200 A340-300
Breakaway Power
1. This section provides danger areas of the engines at breakaway conditions.
6-3-2Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
AREA
A 210−145(338−233)
B 145−105(233−169)
C
D 65−20(105−32)
105−65(169−105)
E < 20 (32) BEYOND DANGER AREA.
APPROX. WINDVELOCITYmph (km/h)
LIGHT TO MODERATE DAMAGE TO TRANSPORT − TYPE AIRCRAFT.
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE", VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV 1951.
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR;COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE − ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING; CORRUGATED STEEL STRUCTURES LESS SEVERELY.
MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AIR TRANSPORT− TYPE AIRCRAFT.
INLET SUCTIONDANGER AREA
ENTRYCORRIDOR
EXHAUST WAKE DANGERAREA 65 Mph (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 Mph (105 km/h)OR LESS
RADIUS = 13.9 ft(4.2 m)
NOT TO SCALE
NO ENTRY 198 ft (60 m)AFT OF NOZZLE EXIT
TO 750 ft (229 m)
A
B
C
D
E
INLET DANGER AREASINCLUDE:(WORST CASE)
GROUND PLANE PROXIMITYHEADWIND/CROSSWIND (20 kts)
EXHAUST DANGER AREASINCLUDE (WORST CASE):
GROUND PLANE PROXIMITYHEADWIND (20 kts)
INLET HAZARD DIMENSIONSBASED ON 40 ft/SEC
CRITICAL VELOCITY WITH A3 ft CONTINGENCY ADDED
214 ft (65 m)
WIDTH
6.3 ft(1.9 m)
F_AC_060302_1_0040101_01_02
Danger Areas of EnginesCFM56-5C series engine
FIGURE-6-3-2-991-004-A01
6-3-2Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-3 Takeoff Power
**ON A/C A340-200 A340-300
Takeoff Power
1. This section provides danger areas of the engines at max takeoff conditions.
6-3-3Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
RADIUS = 34 ft
NOT TO SCALE
13.4 ft
AREA
A 210−145(338−233)
B 145−105(233−169)
C
D 65−20(105−32)
105−65(169−105)
E < 20 (32) BEYOND DANGER AREA.
INLET SUCTIONDANGER AREA
ENTRYCORRIDOR
EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR LESS
APPROX. WINDVELOCITYmph (km/h)
LIGHT TO MODERATE DAMAGE TO TRANSPORT − TYPE AIRCRAFT.
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE", VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV 1951.
EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR GREATER
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR;COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE − ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING; CORRUGATED STEEL STRUCTURES LESS SEVERELY.
MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AIR TRANSPORT − TYPE AIRCRAFT.
GMM−1137913−00−B
A
B
C
D
295 ft (90 m)
TO 1460 ft (445 m)
WIDTH
E
(10.4 m)
(4.1 m)
NO ENTRY 830 ft (253 m)AFT OF NOZZLE EXIT
INLET DANGER AREASINCLUDE:(WORST CASE)
GROUND PLANE PROXIMITYHEADWIND/CROSSWIND (20 kts)
EXHAUST DANGER AREASINCLUDE (WORST CASE):
GROUND PLANE PROXIMITYHEADWIND (20 kts)
INLET HAZARD DIMENSIONSBASED ON 40 ft/SEC
CRITICAL VELOCITY WITH A3 ft CONTINGENCY ADDED
F_AC_060303_1_0040101_01_01
Danger Areas of EnginesCFM56-5C series engine
FIGURE-6-3-3-991-004-A01
6-3-3Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A340-200 A340-300
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1 APU
**ON A/C A340-200 A340-300
APU - GARRETT
1. This section gives APU exhaust velocities and temperatures.
6-4-1Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_060401_1_0020101_01_00
20
METERS
0
5 10 15
FEET
0
10 20 30 40 50
0
60
0
10
5
10
20
30
40
METERS FEET
20
METERS
FD
0
5 10 15
FEET
0
10 20 30 40 50
0
60
0
10
5
10
20
30
40
METERS FEET
121°C
93°C
204°C260°C
315.5°C427°C
15 m/s
18 m/s
24 m/s
FD
149°C177°C
61 m/s46 m/s
30.5 m/s
Exhaust Velocities and TemperaturesGARRETT GTCP 331-350FIGURE-6-4-1-991-002-A01
6-4-1Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A340-200 A340-300
General Information
1. A brief description of the pavement charts that follow will help in airport planning.
To aid in the interpolation between the discrete values shown, each aircraft configuration is shownwith a minimum range of five loads on the Main Landing Gear (MLG).
All curves on the charts represent data at a constant specified tire pressure with:- The aircraft loaded to the Maximum Ramp Weight (MRW),- The CG at its maximum permissible aft position.
Pavement requirements for commercial aircraft are derived from the static analysis of loads imposedon the MLG struts.
Landing Gear Footprint:Section 07-02-00 presents basic data on the landing gear footprint configuration, MRW and tire sizesand pressures.
Maximum Pavement Loads:Section 07-03-00 shows maximum vertical and horizontal pavement loads for certain criticalconditions at the tire-ground interfaces.
Landing Gear Loading on Pavement:Section 07-04-00 contains charts to find these loads throughout the stability limits of the aircraft atrest on the pavement.These MLG loads are used as the point of entry to the pavement design charts which follow,interpolating load values where necessary.
Flexible Pavement Requirements - US Army Corps of Engineers Design Method:Section 07-05-00 uses procedures in Instruction Report No. S-77-1 ”Procedures for Development ofCBR Design 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.The report was prepared by the ”U.S. Army Corps Engineers Waterways Experiment Station, Soilsand Pavement Laboratory, Vicksburg, Mississippi”.The line showing 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).
Flexible Pavement Requirements - LCN Conversion Method:
7-1-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The Load Classification Number (LCN) curves are no longer provided in section 07-06-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983. For questions regarding the LCN system, contact Airbus.
Rigid Pavement Requirements - PCA (Portland Cement Association) Design Method:Section 07-07-00 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 Portland Cement Associationpublications, ”Design of Concrete Airport Pavement”, 1973 and ”Computer Program for AirportPavement Design” (Program PDILB), 1967 both by Robert G. Packard.
Rigid Pavement Requirements - LCN Conversion:The Load Classification Number (LCN) curves are no longer provided in section 07-08-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983. For questions regarding the LCN system, contact Airbus.
ACN/PCN Reporting System:Section 07-09-00 provides ACN data prepared according to the ACN/PCN system as referenced inICAO Annex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations” Fourth Edition, July2004, incorporating Amendments 1 to 6.The ACN/PCN system provides a standardized international aircraft/pavement rating systemreplacing the various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world.ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.An aircraft having an ACN less than or equal to 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 load is defined as the load on a single tire inflated to 1.25 MPa (181 psi)that would 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 pressure limit T - Technical
F - Flexible B - MediumX - High pressure limited to1.75 MPa (254 psi)
U - Using Aircraft
C - LowY - Medium pressure limited to1.25 MPa (181 psi)
7-1-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PCNPAVEMENT
TYPESUBGRADECATEGORY
TIRE PRESSURE CATEGORY EVALUATION METHOD
D - Ultra LowZ - Low pressure limited to 0.5MPa (73 psi)
For flexible pavements, the four subgrade categories (CBR) are:
- A. High Strength CBR 15
- B. Medium Strength CBR 10
- C. Low Strength CBR 6
- D. Ultra Low Strength CBR 3
For rigid pavements, the four subgrade categories (k) are:
- A. High Strength k = 150 MN/m3 (550 pci)
- B. Medium Strength k = 80 MN/m3 (300 pci)
- C. Low Strength k = 40 MN/m3 (150 pci)
- D. Ultra Low Strength k = 20 MN/m3 (75 pci)
7-1-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A340-200 A340-300
Landing Gear Footprint
1. This section provides data about the landing gear footprint in relation to the aircraft MRW and tiresizes and pressures.The landing-gear footprint information is given for all the operational weight variants of the aircraft.
7-2-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
0.71
0 m
(2.3
29 ft
)
25.3
75 m
(83.
251
ft)
10.6
84 m
(35.
052
ft)
0.96
5 m
(3.1
66 ft
)
1.39
7 m
(4.5
83 ft
)1.
981
m(6
.499
ft)
26.3
72 m
(86.
522
ft)
CE
NT
RA
L G
EA
RT
IRE
SIZ
E
1400
x530
R23
OR
54x2
1−23
(bi
as)
10.9
bar
(158
psi
)
CE
NT
RA
LG
EA
RT
IRE
PR
ES
SU
RE
WE
IGH
TV
AR
IAN
TM
AX
IMU
MR
AM
PW
EIG
HT
PE
RC
EN
TA
GE
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
P
NO
SE
GE
AR
TIR
EP
RE
SS
UR
EM
AIN
GE
AR
TIR
ES
IZE
MA
IN G
EA
RT
IRE
PR
ES
SU
RE
A34
0−30
0W
V00
125
7 90
0 kg
(568
575
lb)
94.7
%11
.6 b
ar(1
68 p
si)
1400
x530
R23
OR
54x2
1−23
(bi
as)
A34
0−30
0W
V00
2
A34
0−30
0W
V00
3
A34
0−30
0W
V00
4
13.2
bar
(191
psi
)10
50x3
95R
16
1050
x395
R16
1050
x395
R16
NO
SE
GE
AR
TIR
E S
IZE
1050
x395
R16
A34
0−30
0W
V02
010
50x3
95R
16
260
900
kg(5
75 1
75 lb
)93
.8%
11.6
bar
(168
psi
)13
.2 b
ar(1
91 p
si)
257
900
kg(5
68 5
75 lb
)94
.7%
11.6
bar
(168
psi
)13
.2 b
ar(1
91 p
si)
260
900
kg(5
75 1
75 lb
)93
.8%
11.6
bar
(168
psi
)13
.2 b
ar(1
91 p
si)
271
900
kg(5
99 4
25 lb
)94
.6%
12.1
bar
(175
psi
)14
.2 b
ar(2
06 p
si)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
10.4
bar
(151
psi
)A
340−
300
WV
000
254
400
kg(5
60 8
50 lb
)94
.7%
11.4
bar
(165
psi
)14
00x5
30R
23 O
R54
x21−
23 (
bias
)13
.1 b
ar(1
90 p
si)
1050
x395
R16
F_AC_070200_1_0290101_01_04
Landing Gear Footprint(Sheet 1 of 2)
FIGURE-7-2-0-991-029-A01
7-2-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
CE
NT
RA
L G
EA
RT
IRE
SIZ
E
CE
NT
RA
LG
EA
RT
IRE
PR
ES
SU
RE
WE
IGH
TM
AX
IMU
MP
ER
CE
NT
AG
EN
OS
EM
AIN
GE
AR
TIR
EM
AIN
GE
AR
RA
MP
WE
IGH
T
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
PG
EA
R T
IRE
PR
ES
SU
RE
SIZ
ET
IRE
PR
ES
SU
RE
VA
RIA
NT
NO
SE
GE
AR
TIR
E S
IZE
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
A34
0−30
0W
V02
6
A34
0−30
0W
V02
7
A34
0−30
0W
V02
8
A34
0−30
0W
V02
9
A34
0−30
0W
V05
0
275
900
kg(6
08 2
50 lb
)94
.6%
12.1
bar
(175
psi
)
A34
0−30
0W
V05
1
271
900
kg(5
99 4
25 lb
)94
.6%
12.1
bar
(175
psi
)
A34
0−30
0W
V05
2
277
400
kg(6
11 5
50 lb
)93
.8%
12.1
bar
(175
psi
)
A34
0−30
0W
V05
3
260
900
kg(5
75 1
75 lb
)94
.7%
12.1
bar
(175
psi
)
A34
0−30
0W
V05
4
275
900
kg(6
08 2
50 lb
)94
.6%
12.1
bar
(175
psi
)
275
900
kg(6
08 2
50 lb
)94
.6%
277
400
kg(6
11 5
50 lb
)93
.8%
277
400
kg(6
11 5
50 lb
)93
.8%
275
900
kg(6
08 2
50 lb
)94
.6%
12.1
bar
(175
psi
)
12.1
bar
(175
psi
)
12.1
bar
(175
psi
)
12.1
bar
(175
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1050
x395
R16
A34
0−30
0W
V02
526
0 90
0 kg
(575
175
lb)
94.7
%12
.1 b
ar(1
75 p
si)
14.2
bar
(206
psi
)10
.9 b
ar(1
58 p
si)
A34
0−30
0W
V02
1
1400
x530
R23
OR
54x2
1−23
(bi
as)
1050
x395
R16
1050
x395
R16
1050
x395
R16
1050
x395
R16
A34
0−30
0W
V02
3
A34
0−30
0W
V02
4
A34
0−30
0W
V02
5
275
900
kg(6
08 2
50 lb
)94
.6%
12.1
bar
(175
psi
)14
.2 b
ar(2
06 p
si)
262
900
kg(5
79 6
00 lb
)94
.7%
12.1
bar
(175
psi
)
275
900
kg(6
08 2
50 lb
)94
.6%
12.1
bar
(175
psi
)
260
900
kg(5
75 1
75 lb
)94
.7%
12.1
bar
(175
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
14.2
bar
(206
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)(C
G 3
8.02
%)
(CG
38%
)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
F_AC_070200_1_0300101_01_03F_AC_070200_1_0290102_01_00
Landing Gear Footprint(Sheet 2 of 2)
FIGURE-7-2-0-991-029-A01
7-2-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
0.71
0 m
(2.3
29 ft
)
23.2
41 m
(76.
249
ft)
24.2
35 m
(79.
510
ft)
10.6
84 m
(35.
052
ft)
0.96
5 m
(3.1
66 ft
)
1.39
7 m
(4.5
83 ft
)1.
981
m(6
.499
ft)
CE
NT
RA
L G
EA
RT
IRE
SIZ
E
1400
x530
R23
OR
54x2
1−23
(bi
as)
10.3
bar
(149
psi
)
10.9
bar
(158
psi
)
10.9
bar
(158
psi
)
CE
NT
RA
LG
EA
RT
IRE
PR
ES
SU
RE
10.9
bar
(158
psi
)
WE
IGH
TM
AX
IMU
MP
ER
CE
NT
AG
EN
OS
E G
EA
RM
AIN
GE
AR
TIR
EM
AIN
GE
AR
RA
MP
WE
IGH
T
OF
WE
IGH
TO
N M
AIN
GE
AR
GR
OU
PT
IRE
PR
ES
SU
RE
SIZ
ET
IRE
PR
ES
SU
RE
VA
RIA
NT
A34
0−20
0W
V00
025
4 40
0 kg
(560
850
lb)
93.8
%11
.4 b
ar(1
65 p
si)
1400
x530
R23
OR
54x2
1−23
(bi
as)
A34
0−20
0W
V00
125
7 90
0 kg
(568
575
lb)
93.7
%11
.6 b
ar(1
68 p
si)
A34
0−20
0W
V00
226
0 90
0 kg
(575
175
lb)
93.7
%11
.6 b
ar(1
68 p
si)
A34
0−20
0W
V02
127
5 90
0 kg
(608
250
lb)
93.6
%13
.1 b
ar(1
90 p
si)
13 b
ar(1
89 p
si)
13.2
bar
(191
psi
)
13.2
bar
(191
psi
)
14.2
bar
(206
psi
)
1050
x395
R16
1050
x395
R16
1050
x395
R16
NO
SE
GE
AR
TIR
E S
IZE
1050
x395
R16
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
1400
x530
R23
OR
54x2
1−23
(bi
as)
F_AC_070200_1_0380101_01_02
Landing Gear FootprintFIGURE-7-2-0-991-038-A01
7-2-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A340-200 A340-300
Maximum Pavement Loads
1. This section provides maximum vertical and horizontal pavement loads for some critical conditions atthe tire-ground interfaces.The maximum pavement loads are given for all the operational weight variants of the aircraft.
7-3-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
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
WD
CG
V(N
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MA
X A
FT
CG
V(N
G)
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
V(C
G)
MA
XIM
UM
VE
RT
ICA
L C
EN
TE
R G
EA
R G
RO
UN
D L
OA
D A
T M
AX
AF
T C
G
V(M
G)
H
V(C
G)
12
34
57
H (
PE
R S
TR
UT
)
MO
DE
LM
AX
IMU
MR
AM
PW
EIG
HT
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
BR
AK
ING
ST
AT
IC
AT
10
ft/s²
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GB
RA
KIN
GA
T 1
0 ft/
s²D
EC
ELE
RA
TIO
N
ST
EA
DY
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
AT
6
ST
AT
IC L
OA
D A
TM
AX
AF
T C
G
A34
0−30
0W
V00
0(5
60 8
50 lb
)25
4 40
0 kg
(56
375
lb)
25 5
70 k
g(8
3 92
5 lb
)38
070
kg
(220
975
lb)
100
230
kg(8
7 15
0 lb
)39
530
kg
(d)
(88
350
lb)
40 0
80 k
g(d
)
(89
400
lb)
40 5
50 k
g(d
)
(88
350
lb)
40 0
80 k
g(d
)
(89
400
lb)
40 5
50 k
g(d
)
(93
150
lb)
42 2
50 k
g(d
)
(94
525
lb)
42 8
80 k
g(d
)
MA
C18
% (b)
MA
C38
.18
%
(a)
(89
300
lb)
40 5
10 k
g(1
76 7
75 lb
)80
180
kg
(d)
(179
275
lb)
81 3
20 k
g(d
)
(179
875
lb)
81 5
90 k
g(d
)
(179
275
lb)
81 3
20 k
g(d
)
(179
875
lb)
81 5
90 k
g(d
)
(189
950
lb)
86 1
60 k
g(d
)
(193
050
lb)
87 5
70 k
g(d
)
MA
C38
.18
%
(a)
A34
0−30
0W
V00
1
A34
0−30
0W
V00
2
A34
0−30
0W
V00
3
A34
0−30
0W
V00
4
A34
0−30
0W
V02
0
A34
0−30
0W
V02
1
(568
575
lb)
257
900
kg(5
6 37
5 lb
)25
570
kg
(83
875
lb)
38 0
50 k
g(2
24 0
75 lb
)10
1 64
0 kg
MA
C38
.05
%
(a)
(90
200
lb)
40 9
10 k
g
(575
175
lb)
260
900
kg(5
6 37
5 lb
)25
570
kg
(83
725
lb)
37 9
80 k
g(2
24 8
25 lb
)10
1 98
0 kg
MA
C35
% (a)
(90
050
lb)
40 8
50 k
g
(568
575
lb)
257
900
kg(5
6 37
5 lb
)25
570
kg
(83
875
lb)
38 0
50 k
g(2
24 0
75 lb
)10
1 64
0 kg
MA
C38
.05
%
(a)
(90
200
lb)
40 9
10 k
g
(575
175
lb)
260
900
kg(5
6 37
5 lb
)25
570
kg
(84
025
lb)
38 1
10 k
g(2
24 8
25 lb
)10
1 98
0 kg
MA
C35
% (a)
(90
050
lb)
40 8
50 k
g
(599
425
lb)
271
900
kg(6
0 57
5 lb
)27
480
kg
(93
075
lb)
42 2
20 k
g(2
37 4
50 lb
)10
7 70
0 kg
MA
C37
.63
%
(a)
(92
150
lb)
41 8
00 k
g
(608
250
lb)
275
900
kg(6
0 72
5 lb
)27
550
kg
(93
675
lb)
42 4
90 k
g(2
41 3
25 lb
)10
9 46
0 kg
MA
C37
.5 %
(a)
(92
575
lb)
41 9
90 k
g
MA
C38
.05
%
(a)
MA
C38
.05
%
(c)
MA
C38
.05
%
(a)
MA
C(c
)
38.0
5 %
MA
C37
.63
%
(a)
MA
C37
.5 %
(a)
MA
C18
% (b)
MA
C18
% (b)
MA
C18
% (b)
MA
C18
% (b)
MA
C21
.5 %
(a)
MA
C21
.9 %
(a)
NO
TE
:(a
) L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
.(b
) L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T 2
31 0
00 k
g (5
09 2
75 lb
).
(d)
BR
AK
ED
MA
IN G
EA
R.
LOA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T 2
57 0
00 k
g (5
66 6
00 lb
).(c
)
(PE
R S
TR
UT
)V
(MG
)V
(NG
)(P
ER
ST
RU
T)
V(C
G)
F_AC_070300_1_0070101_01_05
Maximum Pavement Loads(Sheet 1 of 2)
FIGURE-7-3-0-991-007-A01
7-3-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
WV
023
A34
0−30
0(5
79 6
00 lb
)26
2 90
0 kg
(60
250
lb)
27 3
30 k
g
(58
875
lb)
26 7
10 k
g
(60
125
lb)
27 2
70 k
g
(60
725
lb)
27 5
50 k
g
(60
725
lb)
27 5
50 k
g
(60
575
lb)
27 4
80 k
g
(60
550
lb)
27 4
60 k
g
(60
125
lb)
27 2
70 k
g
(60
725
lb)
27 5
50 k
g
(60
725
lb)
27 5
50 k
g
(60
550
lb)
27 4
60 k
g
(60
550
lb)
27 4
60 k
g
(60
725
lb)
27 5
50 k
g
(91
725
lb)
41 6
10 k
g(2
28 8
50 lb
)10
3 80
0 kg
(90
075
lb)
40 8
60 k
g(d
)
(89
400
lb)
40 5
50 k
g(d
)
(89
400
lb)
40 5
50 k
g(d
)
(94
525
lb)
42 8
80 k
g(d
)
(94
525
lb)
42 8
80 k
g(d
)
(93
150
lb)
42 2
50 k
g(d
)
(95
050
lb)
43 1
10 k
g(d
)
(89
400
lb)
40 5
50 k
g(d
)
(94
525
lb)
42 8
80 k
g(d
)
(94
525
lb)
42 8
80 k
g(d
)
(95
050
lb)
43 1
10 k
g(d
)
(95
050
lb)
43 1
10 k
g(d
)
(94
525
lb)
42 8
80 k
g(d
)
MA
C20
.5 %
(a)
MA
C37
.9 %
(a)
(90
950
lb)
41 2
50 k
g(1
83 0
75 lb
)83
040
kg
(d)
(181
575
lb)
82 3
70 k
g(d
)
(181
575
lb)
82 3
70 k
g(d
)
(193
050
lb)
87 5
70 k
g(d
)
(193
050
lb)
87 5
70 k
g(d
)
(189
950
lb)
86 1
60 k
g(d
)
(192
575
lb)
87
350
kg(d
)
(181
575
lb)
82 3
60 k
g(d
)
(193
050
lb)
87 5
70 k
g(d
)
(193
050
lb)
87 5
70 k
g(d
)
(192
575
lb)
87 3
50 k
g(d
)
(192
575
lb)
87 3
50 k
g(d
)
(193
050
lb)
87 5
70 k
g(d
)
MA
C37
.9 %
(a)
WV
025
A34
0−30
0
(CG
38
%)(5
75 1
75 lb
)26
0 90
0 kg
(87
775
lb)
39 8
10 k
g(2
26 9
75 lb
)10
2 95
0 kg
(226
975
lb)
102
960
kg
(241
325
lb)
109
460
kg
(241
325
lb)
109
460
kg
107
700
kg(2
37 4
50 lb
)
(240
725
lb)
109
190
kg
(226
975
lb)
102
950
kg
(241
325
lb)
109
460
kg
(241
325
lb)
109
460
kg
(240
725
lb)
109
190
kg
(240
725
lb)
109
190
kg
(241
325
lb)
109
460
kg
MA
C18
% (e)
MA
C38
% (a)
(90
650
lb)
41 1
20 k
g
WV
025
A34
0−30
0
(CG
38.0
2 %
)(5
75 1
75 lb
)26
0 90
0 kg
(91
375
lb)
41 4
50 k
gM
AC
38.0
2 %
(a)
(90
650
lb)
41 1
20 k
g
A34
0−30
0W
V02
4
A34
0−30
0W
V02
6
A34
0−30
0W
V02
7
A34
0−30
0W
V02
8
A34
0−30
0W
V02
9
A34
0−30
0W
V05
0
A34
0−30
0W
V05
1
A34
0−30
0W
V05
2
A34
0−30
0W
V05
3
A34
0−30
0W
V05
4
(608
250
lb)
275
900
kg(9
3 67
5 lb
)42
490
kg
MA
C37
.5 %
(a)
(92
575
lb)
41 9
90 k
g
(608
250
lb)
275
900
kg(9
3 67
5 lb
)42
490
kg
MA
C37
.5 %
(a)
(92
575
lb)
41 9
90 k
g
(599
425
lb)
271
900
kg(9
3 07
5 lb
)42
220
kg
MA
C37
.63
%
(a)
(92
150
lb)
41 8
00 k
g
(611
550
lb)
277
400
kg(9
3 35
0 lb
)42
340
kg
MA
C35
% (a)
(92
475
lb)
41 9
50 k
g
(575
175
lb)
260
900
kg(9
1 37
5 lb
)41
450
kg
MA
C38
% (a)
(90
650
lb)
41 1
20 k
g
(608
250
lb)
275
900
kg(9
3 67
5 lb
)42
490
kg
MA
C37
.5 %
(a)
(92
575
lb)
41 9
90 k
g
(608
250
lb)
275
900
kg(9
3 67
5 lb
)42
490
kg
MA
C37
.5 %
(a)
(92
575
lb)
41 9
90 k
g
(611
550
lb)
277
400
kg(9
3 35
0 lb
)42
340
kg
MA
C35
% (a)
(92
475
lb)
41 9
50 k
g
(611
550
lb)
277
400
kg(9
3 35
0 lb
)42
340
kg
MA
C35
% (a)
(92
475
lb)
41 9
50 k
g
(608
250
lb)
275
900
kg(9
3 67
5 lb
)42
490
kg
MA
C37
.5 %
(a)
(92
575
lb)
41 9
90 k
g
MA
C37
.5 %
(a)
MA
C37
.5 %
(a)
MA
C37
.63
%
(a)
MA
C37
.5 %
(f)
MA
C38
% (a)
MA
C37
.5 %
(a)
MA
C37
.5 %
(a)
MA
C37
.5 %
(f)
37.5
%M
AC
(f)
MA
C37
.5 %
(a)
MA
C38
.02
%
(a)
MA
C38
% (a)
MA
C21
.9 %
(a)
MA
C20
.3 %
(a)
MA
C21
.9 %
(a)
MA
C21
.9 %
(f)
MA
C21
.9 %
(a)
MA
C21
.9 %
(a)
MA
C21
.9 %
(f)
MA
C21
.9 %
(f)
MA
C21
.9 %
(a)
MA
C21
.5 %
(a)
MA
C20
.3 %
(a)
NO
TE
:(a
) L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
.(e
) L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T 2
41 0
00 k
g (5
31 3
25 lb
).(f
)
LOA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T 2
75 0
00 k
g (6
06 2
75 lb
).
12
34
56
(PE
R S
TR
UT
)
V(M
G)
H (
PE
R S
TR
UT
)
MO
DE
LM
AX
IMU
MR
AM
PW
EIG
HT
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC B
RA
KIN
GA
T 1
0 ft/
s²D
EC
ELE
RA
TIO
N
ST
AT
IC L
OA
D A
TM
AX
AF
T C
G
ST
EA
DY
BR
AK
ING
AT
10
ft/s²
DE
CE
LER
AT
ION
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
V(N
G)
7
(d)
BR
AK
ED
MA
IN G
EA
R.
(PE
R S
TR
UT
)
V(C
G)
ST
AT
IC L
OA
D A
TM
AX
AF
T C
G
F_AC_070300_1_0070102_01_02
Maximum Pavement Loads(Sheet 2 of 2)
FIGURE-7-3-0-991-007-A01
7-3-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
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
WD
CG
V(N
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MA
X A
FT
CG
V(N
G)
V(M
G)
H
A34
0−20
0W
V00
025
4 40
0 kg
(560
850
lb)
27 3
30 k
g(6
0 25
0 lb
)40
730
kg
(89
800
lb)
99 4
10 k
g(2
19 1
50 lb
)39
700
kg
(87
525
lb)
39 5
30 k
g(8
7 15
0 lb
)(c
)
40 0
80 k
g(8
8 35
0 lb
)(c
)
40 5
50 k
g(8
9 40
0 lb
)(c
)
42 8
80 k
g(9
4 52
5 lb
)(c
)
20 %
MA
C(b
)
37.7
%M
AC
(a)
A34
0−20
0W
V00
125
7 90
0 kg
(568
575
lb)
27 3
30 k
g(6
0 25
0 lb
)40
720
kg
(89
775
lb)
100
730
kg(2
22 0
75 lb
)40
240
kg
(88
725
lb)
20 %
MA
C(b
)
37.6
%M
AC
(a)
A34
0−20
0W
V00
226
0 90
0 kg
(575
175
lb)
27 3
30 k
g(6
0 25
0 lb
)40
700
kg
(89
725
lb)
101
950
kg(2
24 7
50 lb
)40
550
kg
(89
400
lb)
20 %
MA
C(b
)
37.5
%M
AC
(a)
37 %
MA
C(a
)A
340−
200
WV
021
275
900
kg(6
08 2
50 lb
)30
030
kg
(66
200
lb)
46 2
10 k
g(1
01 8
75 lb
)10
8 22
0 kg
(238
575
lb)
41 6
90 k
g(9
1 90
0 lb
)
23.7
%M
AC
(a)
79 5
30 k
g(1
75 3
25 lb
)(c
)
80 5
90 k
g(1
77 6
75 lb
)(c
)
81 5
60 k
g(1
79 8
00 lb
)(c
)
86 5
80 k
g(1
90 8
75 lb
)(c
)
37.7
%M
AC
(a)
37.6
%M
AC
(a)
37.5
%M
AC
(a)
37 %
MA
C(a
)
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
V(C
G)
MA
XIM
UM
VE
RT
ICA
L C
EN
TE
R G
EA
R G
RO
UN
D L
OA
D A
T M
AX
AF
T C
G
V(C
G)
12
34
57
MO
DE
LM
AX
IMU
MR
AM
PS
TA
TIC
LO
AD
AT
MO
ST
FW
D C
GB
RA
KIN
G
DE
CE
LER
AT
ION
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GB
RA
KIN
GA
T 1
0 ft/
s²D
EC
ELE
RA
TIO
N
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
WE
IGH
T
6
ST
AT
IC L
OA
D A
TM
AX
AF
T C
G
AT
ST
AT
ICS
TE
AD
Y
V(N
G)
(PE
R S
TR
UT
)
V(M
G)
H (
PE
R S
TR
UT
)(P
ER
ST
RU
T)
V(C
G)
AT
10
ft/s²
NO
TE
:(a
) L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T M
RW
.(b
) L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
CR
AF
T A
T 2
27 0
00 k
g (5
00 4
50 lb
).B
RA
KE
D M
AIN
GE
AR
(c)
F_AC_070300_1_0090101_01_04
Maximum Pavement LoadsFIGURE-7-3-0-991-009-A01
7-3-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A340-200 A340-300
Landing Gear Loading on Pavement
1. This section provides data about the landing gear loading on pavement.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN (and LCN) and the highest ACN(and LCN) for each type of aircraft.
2. MLG Loading on PavementExample, see FIGURE 7-4-0-991-005-A (Sheet 1), calculation of the total weight on the MLG for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- The aircraft gross weight is 200 000 kg (440 925 lb),- A percentage of weight on the MLG of 93.76% (percentage of weight on the MLG at MRW and
maximum aft CG at MRW).The total weight on the MLG group is 187 510 kg (413 400 lb).
3. Main Gear and Center Gear Loading on PavementThe MLG group consists of two main gears (4-wheel bogies) plus one center gear (twin-wheel).
Example, see FIGURE 7-4-0-991-005-A (Sheet 2), calculation of the total weight on the MLG for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- The aircraft gross weight is 200 000 kg (440 925 lb),- A percentage of weight on the MLG of 93.85% (percentage of weight on the MLG at 200 000 kg
(440 925 lb) and maximum aft CG at MRW).The load on the two main gears is 162 720 kg (358 725 lb) and the load on the center gear is 24 980kg (55 050 lb).The total weight on the MLG group is 187 690 kg (413 800 lb).
NOTE : The CG in the figure title is the CG used for ACN/LCN calculation.
7-4-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
84 86 88 90 92 94 96 98 100
(x 1
000
kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1 00
0 kg
)
PERCENTAGE OF WEIGHT ON MAIN GEAR
250
300
350
400
450
500
550
600
(x 1
000
lb)
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CG FOR ACNCALCULATION
37.7% MAC
MTOW − 253 500 kg
24.2% MAC
MLW
MZFW
LANDING
TAKE OFF
F_AC_070400_1_0050101_01_01
Landing Gear Loading on PavementWV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)
FIGURE-7-4-0-991-005-A01
7-4-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
100
200
300
400
500
300
280
260
240
220
200
180
160
140
120
100
020406080100
120
140
160
180
200
220
240
300
400
500
600
LOAD ON CENTER GEAR OR LOAD ON MAIN GEARS (x 1000 Kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
x 10
00 K
g)
(x 1
000
lb)
MA
IN G
EA
RS
CE
NT
ER
LIN
E G
EA
R
(x 1000 lb)
F_AC_070400_1_0050102_01_00
Landing Gear Loading on PavementWV000, MRW 254 400 kg, CG 37.7% (Sheet 2 of 2)
FIGURE-7-4-0-991-005-A01
7-4-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
84 86 88 90 92 94 96 98 100
(x 1
000
Kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
250
300
350
400
450
500
550
600
(x 1
000
lb)
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
AIR
CR
AF
T G
RO
SS
WE
IGH
T
MTOW − 275 000 kg
TAKE OFF
MZFW
CG FOR ACNCALCULATION
37% MAC
23.7% MAC
MLW
LANDING
F_AC_070400_1_0060101_01_00
Landing Gear Loading on PavementWV021, MRW 275 900 kg, CG 37% (Sheet 1 of 2)
FIGURE-7-4-0-991-006-A01
7-4-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
100
200
300
400
500
300
280
260
240
220
200
180
160
140
120
100
020406080100
120
140
160
180
200
220
240
300
400
500
600
LOAD ON CENTER GEAR OR LOAD ON MAIN GEARS (x 1000 Kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
x 10
00 K
g)
(x 1
000
lb)
MA
IN G
EA
RS
CE
NT
ER
LIN
E G
EA
R
(x 1000 lb)
F_AC_070400_1_0060102_01_00
Landing Gear Loading on PavementWV021, MRW 275 900 kg, CG 37% (Sheet 2 of 2)
FIGURE-7-4-0-991-006-A01
7-4-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
84 86 88 90 92 94 96 98 100
(x 1
000
Kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
250
300
350
400
450
500
550
600
(x 1
000
lb)
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CG FOR ACNCALCULATION38.18% MAC
MTOW − 253 500 kg
22% MAC
MLW
MZFW
TAKE OFF
LANDING
F_AC_070400_1_0070101_01_00
Landing Gear Loading on PavementWV000, MRW 254 400 kg, CG 38.18% (Sheet 1 of 2)
FIGURE-7-4-0-991-007-A01
7-4-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
100
200
300
400
500
300
280
260
240
220
200
180
160
140
120
100
020406080100
120
140
160
180
200
220
240
300
400
500
600
LOAD ON CENTER GEAR OR LOAD ON MAIN GEARS (x 1000 Kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
x 10
00 K
g)
(x 1
000
lb)
MA
IN G
EA
RS
CE
NT
ER
LIN
E G
EA
R
(x 1000 lb)
F_AC_070400_1_0070102_01_00
Landing Gear Loading on PavementWV000, MRW 254 400 kg, CG 38.18% (Sheet 2 of 2)
FIGURE-7-4-0-991-007-A01
7-4-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
84 86 88 90 92 94 96 98 100
(x 1
000
Kg)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
(x
1000
Kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
250
300
350
400
450
500
550
600
(x 1
000
lb)
110
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
270
280
AIR
CR
AF
T G
RO
SS
WE
IGH
T
CG FOR ACNCALCULATION
35% MACMTOW − 276 500 kg
24% MAC
MLW
MZFW
TAKE OFF
LANDING
F_AC_070400_1_0080101_01_00
Landing Gear Loading on PavementWV028, MRW 277 400 kg, CG 35% (Sheet 1 of 2)
FIGURE-7-4-0-991-008-A01
7-4-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
100
200
300
400
500
300
280
260
240
220
200
180
160
140
120
100
020406080100
120
140
160
180
200
220
240
300
400
500
600
LOAD ON CENTER GEAR OR LOAD ON MAIN GEARS (x 1000 Kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T (
x 10
00 K
g)
(x 1
000
lb)
MA
IN G
EA
RS
CE
NT
ER
LIN
E G
EA
R
(x 1000 lb)
F_AC_070400_1_0080102_01_00
Landing Gear Loading on PavementWV028, MRW 277 400 kg, CG 35% (Sheet 2 of 2)
FIGURE-7-4-0-991-008-A01
7-4-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A340-200 A340-300
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
1. This section provides data about the flexible pavement requirements.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN for each typeof aircraft.They are calculated with the US Army Corps of Engineers Design Method.To find a flexible pavement thickness, you must know the Subgrade Strength (CBR), the annualdeparture level and the weight on one MLG.The line that shows 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).The procedure that follows is used to develop flexible pavement design curves:- With the scale for pavement thickness at the bottom and the scale for CBR at the top, a random
line is made to show 10 000 coverages,- A plot is then made of the incremental values of the weight on the MLG,- Annual departure lines are made based on the load lines of the weight on the MLG that is shown
on the graph.
Example, see FIGURE 7-5-0-991-005-A (Sheet 1), calculation of the thickness of the flexiblepavement for MLG:- An aircraft with a MRW of 254 400 kg (560 850 lb),- A ”CBR” value of 10,- An annual departure level of 3 000,- The load on one MLG of 80 000 kg (176 375 lb).The required flexible pavement thickness is 59.2 cm (23 in).
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-5-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
SUBGRADE STRENGTH − CBR
8060403020151063
8060403020151063
FLEXIBLE PAVEMENT THICKNESS
10 15 20 30 40 60 80 100 120 150 180(cm)
(in)
10 000 COVERAGES USEDFOR ACN CALCULATIONSALPHA FACTOR = 0.8
99 410 kg (219 150 lb)WEIGHT ON ONE MAIN LANDING GEAR
80 000 kg (176 375 lb)70 000 kg (154 325 lb)
(110 225 lb)(132 275 lb)60 000 kg
50 000 kg
MAXIMUM POSSIBLEMAIN LANDING GEARLOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
1400 x 530R23 OR 54 x 21−23 (bias) TIRES
TIRE PRESSURE CONSTANT AT 13 bar (189 psi)
1 2003 0006 00015 000
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
F_AC_070500_1_0050101_01_01
Flexible Pavement RequirementsWV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)
FIGURE-7-5-0-991-005-A01
7-5-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
SUBGRADE STRENGTH − CBR
8060403020151063
80604020151063
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 OR 54 x 21−23 (bias) TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
10 15 20 30 40 60 80 100 120 150 180(cm)
(in)
10 000 COVERAGES USEDFOR ACN CALCULATIONSALPHA FACTOR = 0.8
MAXIMUM POSSIBLEMAIN LANDING GEARLOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
108 220 kg (238 575 lb)WEIGHT ON ONE MAIN LANDING GEAR
90 000 kg (198 425 lb)80 000 kg (176 375 lb)
(132 275 lb)(154 325 lb)70 000 kg
60 000 kg
30
1 2003 0006 00015 000
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
F_AC_070500_1_0050102_01_01
Flexible Pavement RequirementsWV021, MRW 275 900 kg, CG 37% (Sheet 2 of 2)
FIGURE-7-5-0-991-005-A01
7-5-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
SUBGRADE STRENGTH − CBR
8060403020151063
80604020151063
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 OR 54 x 21−23 (bias) TIRES
TIRE PRESSURE CONSTANT AT 13.1 bar (190 psi)
10 15 20 30 40 60 80 100 120 150 180(cm)
(in)
10 000 COVERAGES USEDFOR ACN CALCULATIONSALPHA FACTOR = 0.8
MAXIMUM POSSIBLEMAIN LANDING GEARLOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
100 230 kg (220 975 lb)WEIGHT ON ONE MAIN LANDING GEAR
90 000 kg (198 425 lb)80 000 kg (176 375 lb)
(132 275 lb)(154 325 lb)70 000 kg
60 000 kg
30
1 2003 0006 00015 000
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
F_AC_070500_1_0060101_01_01
Flexible Pavement RequirementsWV000, MRW 254 400 kg, CG 38.18% (Sheet 1 of 2)
FIGURE-7-5-0-991-006-A01
7-5-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
SUBGRADE STRENGTH − CBR
8060403020151063
80604020151063
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 OR 54 x 21−23 (bias) TIRES
TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
10 15 20 30 40 60 80 100 120 150 180(cm)
(in)
10 000 COVERAGES USEDFOR ACN CALCULATIONSALPHA FACTOR = 0.8
MAXIMUM POSSIBLEMAIN LANDING GEARLOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG
109 190 kg (240 725 lb)WEIGHT ON ONE MAIN LANDING GEAR
90 000 kg (198 425 lb)80 000 kg (176 375 lb)
(132 275 lb)(154 325 lb)70 000 kg
60 000 kg
30
1 2003 0006 00015 000
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE25 000
F_AC_070500_1_0060102_01_01
Flexible Pavement RequirementsWV028, MRW 277 400 kg, CG 35% (Sheet 2 of 2)
FIGURE-7-5-0-991-006-A01
7-5-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A340-200 A340-300
Flexible Pavement Requirements - LCN Conversion
1. The Load Classification Number (LCN) curves are no longer provided in section 07-06-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983.For questions regarding the LCN system, contact Airbus.
7-6-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A340-200 A340-300
Rigid Pavement Requirements - Portland Cement Association Design Method
1. This section provides data about the rigid pavement requirements for the PCA (Portland CementAssociation) design method.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN for each typeof aircraft.To find a rigid pavement thickness, you must know the Subgrade Modulus (k), the permitted workingstress and the weight on one MLG.The procedure that follows is used to develop rigid pavement design curves:- With the scale for pavement thickness on the left and the scale for permitted working stress on
the right, a random load line is made. This represents the MLG maximum weight to be shown,- A plot is then made of all values of the subgrade modulus (k values),- More load lines for the incremental values of the weight on the MLG are made based on the
curve for k = 80 MN/m3, which is already shown on the graph.
Example, see FIGURE 7-7-0-991-004-A (sheet 1), calculation of the thickness of the rigid pavementfor the MLG:- An aircraft with a MRW of 254 400 kg (560 850 lb),- A k value of 80 MN/m3 (300 lb/in3),- A permitted working stress of 35.15 kg/cm2 (500 lb/in2),- The load on one MLG is 80 000 kg (176 375 lb).The required rigid pavement thickness is 242 mm (10 in).
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-7-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 13 bar (189 psi)
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
8
13
18
23
28
33
38
43
48
53
58
63
60 000 kg (132 275 lb)70 000 kg (154 325 lb)80 000 kg (176 375 lb)99 410 kg (219 150 lb)LANDING GEARWEIGHT ON ONE MAIN
50 000 kg (110 225 lb)
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
F_AC_070700_1_0040101_01_00
Rigid Pavement RequirementsWV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)
FIGURE-7-7-0-991-004-A01
7-7-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
8
13
18
23
28
33
38
43
48
53
58
63
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)108 220 kg (238 575 lb)LANDING GEARWEIGHT ON ONE MAIN
60 000 kg (132 275 lb)
F_AC_070700_1_0040201_01_00F_AC_070700_1_0040102_01_00
Rigid Pavement RequirementsWV021, MRW 275 900 kg, CG 37% (Sheet 2 of 2)
FIGURE-7-7-0-991-004-A01
7-7-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 13.1 bar (190 psi)
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
8
13
18
23
28
33
38
43
48
53
58
63
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)100 230 kg (220 975 lb)LANDING GEARWEIGHT ON ONE MAIN
60 000 kg (132 275 lb)
F_AC_070700_1_0050101_01_00
Rigid Pavement RequirementsWV000, MRW 254 400 kg, CG 38.18% (Sheet 1 of 2)
FIGURE-7-7-0-991-005-A01
7-7-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)
100
200
300
400
500
600
700
800
90015
14
38
36
34
32
13
1230
28 11
26
24
22
10
9
20
18 7
8
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(c
m)
(in)
FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:
THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.
PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:
ASSOCIATION.
(kg/
cm²)
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
(lb/in
²)
8
13
18
23
28
33
38
43
48
53
58
63
K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³
RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN
70 000 kg (154 325 lb)80 000 kg (176 375 lb)90 000 kg (198 425 lb)109 190 kg (240 725 lb)LANDING GEARWEIGHT ON ONE MAIN
60 000 kg (132 275 lb)
F_AC_070700_1_0050201_01_00F_AC_070700_1_0050102_01_00
Rigid Pavement RequirementsWV028, MRW 277 400 kg, CG 35% (Sheet 2 of 2)
FIGURE-7-7-0-991-005-A01
7-7-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-0 Rigid Pavement Requirements - LCN Conversion
**ON A/C A340-200 A340-300
Rigid Pavement Requirements - LCN Conversion
1. The Load Classification Number (LCN) curves are no longer provided in section 07-08-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983.For questions regarding the LCN system, contact Airbus.
7-8-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements
**ON A/C A340-200 A340-300
Aircraft Classification Number - Flexible and Rigid Pavements
1. This section provides data about the Aircraft Classification Number (ACN) for an aircraft grossweight in relation to a subgrade strength value for flexible and rigid pavement.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN for each typeof aircraft.To find the ACN of an aircraft on flexible and rigid pavement, you must know the aircraft grossweight and the subgrade strength.
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).
Example, see FIGURE 7-9-0-991-014-A (sheet 1), calculation of the ACN for flexible pavement for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- An aircraft gross weight of 200 000 kg (440 925 lb),- A medium subgrade strength (code B).The ACN for flexible pavement is 42.
Example, see FIGURE 7-9-0-991-014-A (sheet 2), calculation of the ACN for rigid pavement for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- An aircraft gross weight of 200 000 kg (440 925 lb),- A medium subgrade strength (code B).The ACN for rigid pavement is 40.
2. Aircraft Classification Number - ACN tableThe tables in FIGURE 7-9-0-991-004-A and FIGURE 7-9-0-991-005-A provide ACN data in tabularformat similar to the one used by ICAO in the ”Aerodrome Design Manual Part 3, Pavements -Edition 1983” for all the operational weight variants of the aircraft.As an approximation, use a linear interpolation in order to get the ACN at the required operatingweight using the following equation:- ACN = ACN min + (ACN max - ACN min) x (Operating weight - 130 000 kg)/(MRW - 130 000
kg)As an approximation, also use a linear interpolation in order to get the aircraft weight at thepavement PCN using the following equation:- Operating weight = 130 000 kg + (MRW - 130 000 kg) x (PCN - ACN min) / (ACN max - ACN
min)With ACN max = ACN calculated at the MRW in the table and with ACN min = ACN calculated at130 000 kg.
7-9-0Page 1
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOTE : The CG in the figure title is the CG used for ACN calculation.
7-9-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
AIRCRAFT TYPEALL UP
MASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
4528
ACN FOR
High150
RIGID PAVEMENTSUBGRADES − MN/m³
5228
Medium80
6232
Low40
7337
Ultral−low20
5028
ACN FOR
High15
FLEXIBLE PAVEMENTSUBGRADES − CBR
5429
Medium10
6232
Low6
8439
Ultral−low3
A340−200WV000
254 400130 000
39.146.1
1.30
WV001
WV002
WV021
A340−200
A340−200
A340−200
257 900130 000
39.146.1
1.32
260 900130 000
39.146.1
1.32
275 900130 000
39.246.0
1.42
4628
5328
6332
7437
5128
5529
6332
8639
4728
5428
6432
7637
5228
5629
6532
8739
5229
6029
7133
8338
5628
6129
7032
9539
F_AC_070900_1_0040101_01_00
Aircraft Classification NumberACN Table
FIGURE-7-9-0-991-004-A01
7-9-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3 ba
r (1
89 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
SS
EE
SE
CT
ION
7−
4−0
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0140101_01_00
Aircraft Classification NumberFlexible Pavement - WV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)
FIGURE-7-9-0-991-014-A01
7-9-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3 ba
r (1
89 p
si)
1400
x530
R23
OR
54x
21−
23 (
bias
) T
IRE
SS
EE
SE
CT
ION
7−
4−0
CH
AP
TE
R 1
. SE
CO
ND
ED
ITIO
N 1
983.
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
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)
F_AC_070900_1_0140102_01_00
Aircraft Classification NumberRigid Pavement - WV000, MRW 254 400 kg, CG 37.7% (Sheet 2 of 2)
FIGURE-7-9-0-991-014-A01
7-9-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0C
HA
PT
ER
1. S
EC
ON
D E
DIT
ION
198
3.IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3A
CN
WA
S D
ET
ER
MIN
ED
AS
RE
FE
RE
NC
ED
IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0150101_01_00
Aircraft Classification NumberFlexible Pavement - WV021, MRW 275 900 kg, CG 37% (Sheet 1 of 2)
FIGURE-7-9-0-991-015-A01
7-9-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0C
HA
PT
ER
1. S
EC
ON
D E
DIT
ION
198
3.IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3A
CN
WA
S D
ET
ER
MIN
ED
AS
RE
FE
RE
NC
ED
IN
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
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)
F_AC_070900_1_0150102_01_00
Aircraft Classification NumberRigid Pavement - WV021, MRW 275 900 kg, CG 37% (Sheet 2 of 2)
FIGURE-7-9-0-991-015-A01
7-9-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
AIRCRAFT TYPEALL UP
MASS (kg)
LOAD ONONE MAINGEAR LEG
(%)
TIREPRESSURE
(Mpa)
4628
ACN FOR
High150
RIGID PAVEMENTSUBGRADES − MN/m³
5328
Medium80
6332
Low40
7437
Ultral−low20
5128
ACN FOR
High15
FLEXIBLE PAVEMENTSUBGRADES − CBR
55
Medium10
63
Low6
8540
Ultral−low3
A340−300 254 400130 000
39.446.2
1.31WV000
260 900
257 900
260 900
271 900
275 900
262 900
275 900
260 900
260 900
275 900
271 900
277 400
260 900
275 900
275 900
277 400
277 400
275 900
39.446.2
1.32WV001
39.146.0
1.32WV002
39.446.2
1.32WV003
39.146.0
1.32WV004
39.646.2
1.42WV020
39.746.2
1.42WV021
39.546.2
1.42WV023
39.746.2
1.42WV024
39.5
46.21.42WV025
39.5
46.21.42WV025
39.746.2WV02639.646.2WV02739.446.0WV02839.546.2WV02939.746.2WV05039.746.2WV05139.446.0WV05239.446.0WV05339.746.2WV054
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
A340−300
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
130 000
257 900
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
1.42
(CG 38.02%)
(CG 38%)
28
28
28
28
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
47
47
47
47
52
53
49
53
48
48
53
52
53
48
53
53
53
53
53
54 64 75 52 56 64 87
54 64 76 52 56 65 8739
54 64 75 52 56 64 8740
54 64 76 52 56 65 8739
6029
7133
8338
56 61 70 9440
61 73 85 57 62 72 9740
57 67 79 54 58 66 9040
61 73 85 57 62 72 9740
29 33 38 28 29 32 40
29 33 38 28 29 32 40
56 67 78 53 57 66 88
56 67 78 53 57 66 88
61 73 85 57 62 72 9740
60 71 83 56 61 70 9440
61 72 84 57 62 71 9639
56 67 78 53 57 66 88
61 73 85 57 62 72 97
61 73 85 57 62 72 97
61 72 84 57 62 71 9639
61 72 84 57 62 71 9639
61 73 85 57 62 72 9740
28
28
28
28
29
29
29
29
29
29
29
29
29
29
29
29
32
32
32
32
33
33
33
33
33
33
33
33
33
33
33
33
37
37
37
37
38
38
38
38
38
38
38
38
38
38
38
38
28
28
28
28
28
28
28
28
28
28
28
28
28
28
28
28
28
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
29
32
32
32
32
32
32
32
32
32
32
32
32
32
32
32
32
32
32
40
40
40
40
F_AC_070900_1_0050101_01_00
Aircraft Classification NumberACN Table
FIGURE-7-9-0-991-005-A01
7-9-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(190
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0C
HA
PT
ER
1. S
EC
ON
D E
DIT
ION
198
3.IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3A
CN
WA
S D
ET
ER
MIN
ED
AS
RE
FE
RE
NC
ED
IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0160101_01_00
Aircraft Classification NumberFlexible Pavement - WV000, MRW 254 400 kg, CG 38.18% (Sheet 1 of 2)
FIGURE-7-9-0-991-016-A01
7-9-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.1
bar
(190
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0C
HA
PT
ER
1. S
EC
ON
D E
DIT
ION
198
3.IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3A
CN
WA
S D
ET
ER
MIN
ED
AS
RE
FE
RE
NC
ED
IN
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
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)
F_AC_070900_1_0160102_01_00
Aircraft Classification NumberRigid Pavement - WV000, MRW 254 400 kg, CG 38.18% (Sheet 2 of 2)
FIGURE-7-9-0-991-016-A01
7-9-0Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0C
HA
PT
ER
1. S
EC
ON
D E
DIT
ION
198
3.IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3A
CN
WA
S D
ET
ER
MIN
ED
AS
RE
FE
RE
NC
ED
IN
ALP
HA
FA
CT
OR
= 0
.8
D −
CB
R
3 (
ULT
RA
LO
W)
SU
BG
RA
DE
ST
RE
NG
TH
C −
CB
R
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
F_AC_070900_1_0170101_01_00
Aircraft Classification NumberFlexible Pavement - WV028, MRW 277 400 kg, CG 35% (Sheet 1 of 2)
FIGURE-7-9-0-991-017-A01
7-9-0Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
300
400
500
600
0102030405060708090100
110
120
100
150
200
250
300
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
100
0 lb
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.2
bar
(206
psi
)14
00x5
30R
23 O
R 5
4x21
−23
(bi
as)
TIR
ES
SE
E S
EC
TIO
N 7
−4−
0C
HA
PT
ER
1. S
EC
ON
D E
DIT
ION
198
3.IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3A
CN
WA
S D
ET
ER
MIN
ED
AS
RE
FE
RE
NC
ED
IN
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
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)
F_AC_070900_1_0170102_01_00
Aircraft Classification NumberRigid Pavement - WV028, MRW 277 400 kg, CG 35% (Sheet 2 of 2)
FIGURE-7-9-0-991-017-A01
7-9-0Page 12
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
**ON A/C A340-200 A340-300
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
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
NOTE:WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.
F_AC_080000_1_0030101_01_01
Scaled DrawingFIGURE-8-0-0-991-003-A01
8-0-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-300
NOTE:WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
F_AC_080000_1_0030201_01_01
Scaled DrawingFIGURE-8-0-0-991-003-B01
8-0-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A340-200 A340-300
Aircraft Rescue and Fire Fighting
1. Aircraft Rescue and Fire Fighting ChartsThis sections provides 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
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
JAN
UA
RY
201
7
F_AC_100000_1_0270101_01_03
Front PageFIGURE-10-0-0-991-027-A01
10-0-0Page 2
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_100000_1_0280101_01_01
Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-028-A01
10-0-0Page 3
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
FR
73F
R67
FR
65
BF
R20
FR
1
A
BA
T−
2BA
T−
1
AC
CE
SS
VIA
AC
CE
SS
DO
OR
811
AC
CE
SS
DO
OR
132
AZ
VIA
FW
D C
AR
GO
DO
OR
ELT
FR
65
C
FR
64
D
FR
64
A
Z12
0Z
160
D
DIV
IDE
R N
ET
AC
CE
SS
VIA
AF
T C
AR
GO
BA
T−
AP
UA
CC
ES
S V
IAB
ULK
CA
RG
O D
OO
R 8
23
B
FR
67F
R66
FR
65
FR
64
C
ELT
AN
TE
NN
A
F_AC_100000_1_0690101_01_01
Batteries Location and AccessFIGURE-10-0-0-991-069-A01
10-0-0Page 4
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_100000_1_0290101_01_00
Crew Rest Compartments LocationFIGURE-10-0-0-991-029-A01
10-0-0Page 5
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_100000_1_0300101_01_00
Wheel/Brake OverheatWheel Safety Area (Sheet 1 of 2)
FIGURE-10-0-0-991-030-A01
10-0-0Page 6
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_100000_1_0300102_01_00
Wheel/Brake OverheatRecommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-030-A01
10-0-0Page 7
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
Car
bon
Fib
er R
einf
orce
d P
last
ic (
CF
RP
)
Gla
ss F
iber
Rei
nfor
ced
Pla
stic
(G
FR
P)
Ara
mid
Fib
er R
einf
orce
d P
last
ic (
AF
RP
)
Hyb
rid (
GF
RP
+ C
FR
P)
CO
MP
OS
ITE
MA
TE
RIA
LS
F_AC_100000_1_0310101_01_01
Composite Materials LocationFIGURE-10-0-0-991-031-A01
10-0-0Page 8
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
BA
AB
C
C
F_AC_100000_1_0320101_01_00
Ground Lock Safety DevicesFIGURE-10-0-0-991-032-A01
10-0-0Page 9
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
EM
ER
GE
NC
Y D
ES
CE
NT
TH
RO
UG
H T
HE
WIN
DO
WO
PE
NIN
G W
ITH
TH
E E
SC
AP
E R
OP
E
0 −3
−6
−9
−12
−15
GR
ID E
QU
ALS
1 m
(3.
28 ft
) IN
RE
ALI
TY
− *
TH
E S
ING
LE−
LAN
E E
SC
AP
E S
LID
E S
HO
WN
IS F
OR
A T
YP
E "
1" D
OO
R.
A D
UA
L−LA
NE
ES
CA
PE
SLI
DE
/RA
FT
IS A
VA
ILA
BLE
FO
R A
IRC
RA
FT
FIT
TE
D W
ITH
A T
YP
E "
A"
DO
OR
.
− D
IME
NS
ION
S A
RE
AP
PR
OX
IMA
TE
.
NO
TE
:−
LH
SH
OW
N, R
H S
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ME
TR
ICA
L.
FW
D C
AB
IN D
UA
L−LA
NE
ES
CA
PE
SLI
DE
/RA
FT
CO
CK
PIT
ES
CA
PE
RO
PE
AF
T C
AB
IN D
UA
L−LA
NE
ES
CA
PE
SLI
DE
/RA
FT
EM
ER
GE
NC
Y E
XIT
SIN
GLE
−LA
NE
ES
CA
PE
SLI
DE
*
MID
CA
BIN
DU
AL−
LAN
EE
SC
AP
E S
LID
E/R
AF
T
F_AC_100000_1_0330101_01_02
Emergency Evacuation DevicesFIGURE-10-0-0-991-033-A01
10-0-0Page 10
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
F_AC_100000_1_0340101_01_00
Pax/Crew Doors and Emergency ExitsFIGURE-10-0-0-991-034-A01
10-0-0Page 11
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
122C
R
FW
D
7155
JE 196B
B
152N
R/
197C
B
F_AC_100000_1_0350101_01_00
FWD and AFT Lower Deck Cargo DoorsFIGURE-10-0-0-991-035-A01
10-0-0Page 12
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
CA
B F
AN
SE
XTR
AC
TA
VN
CS
BTL
2
BTL
1
TES
TD
ISC
HA
FT A
GE
NT
FWD
AG
EN
T
SMO
KE
SQU
IBSM
OK
ESQ
UIB
OFF
FAU
LT
OFF
FAU
LT
OFF
FAU
LT
OFF
FAU
LT
CA
RG
O A
IR C
ON
DFW
DA
FTB
ULK
ISO
L V
ALV
ES
ISO
L V
ALV
ES
ISO
L V
ALV
ES
HO
T A
IR
A U T O
CA
RG
O S
MO
KE
VE
NTI
LATI
ON
OVR
D
FAU
LTSM
OK
E
FAU
LTO
FF/R
FAU
LTO
FF/R
FAU
LTO
FF/R
PR
IM 2
PR
IM 3
SE
C 2
FLT
CTL
212V
U
OFF
NO
RM
MA
X
CO
OLI
NG
CO
LDH
OT
CO
LDH
OT
WIP
ER
RA
IN R
PLN
TO
FFS
LOW
FAS
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OFF
42
13
MA
N S
TAR
TE
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ON
ON
ON
ON
B CA
R O
UTE
R T
K
R O
UTE
R T
KO
VE
RFL
OW
INC
LOAD
HI
LE
VE
LT
ES
TTR
AN
SF.
VA
LVE
OP
EN
CLO
SE
D
AP
U E
ME
RG
.
SH
UT
DOW
N
PW
RS
UP
PLY NO
RM
BAT
LTT
R
DEC
RE
FU
EL
/DE
FU
EL
VA
LV
ES
MO
DE
SE
LE
CT
L O
UTE
R T
KL
INN
ER
TK
CT
R T
K
L O
UTE
R T
KL
INN
ER
TK
CT
R T
KTR
IM T
KH
IGH
LE
VE
L
REF
UEL
OFF
DEF
UEL
R IN
NE
R T
K
R IN
NE
R T
K
OP
EN
NORM
SH
UT
L IN
R.
CE
NT
ER
R IN
R.
L O
UT
ER
R O
UT
ER
TR
IMA
CT
UA
L
CK
PT
EN
D
x 10
00kg1b
PR
ES
ELE
CT
ED
TRIM
TK
C
E
B
D
A
D
43
21
E
F_AC_100000_1_0360101_01_00
Control PanelsFIGURE-10-0-0-991-036-A01
10-0-0Page 13
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
A
315A
L
316A
R
A
F_AC_100000_1_0370101_01_00
APU Compartment AccessFIGURE-10-0-0-991-037-A01
10-0-0Page 14
Aug 01/19
@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A340-200 A340-300
DIM
EN
SIO
NS
AR
E R
ELA
TE
D T
O A
IRC
RA
FT
WE
IGH
T A
ND
CG
CO
NF
IGU
RA
TIO
N
VT
AP
D4
F5
C3
C2
F3
D3
BF
F2
D2
F4
C1
F1
D1
CP
N2
HT
RN
1F
T1
FT
2F
T3
FT
4W
2W
1
NO
TE
:P
AS
SE
NG
ER
AN
D C
AR
GO
DO
OR
GR
OU
ND
CLE
AR
AN
CE
S A
RE
ME
AS
UR
ED
FR
OM
TH
E C
EN
TE
R O
F T
HE
DO
OR
SIL
L A
ND
FR
OM
FLO
OR
LE
VE
L.
125
000
kg(2
75 5
78 lb
)A
FT
CG
(31
.9%
)
DO
OR
SA/C
CO
NF
IGU
RA
TIO
Nm
ftD
1D
2D
3D
4C
1C
2C
3
4.59
4.84
5.31
5.70
2.73
3.44
3.58
15.0
615
.88
17.4
218
.70
8.96
11.2
911
.75
TA
ILP
LAN
E17
.00
8.14
7.30
55.7
726
.71
23.9
5
VT
HT
AP
FU
SE
LAG
E
A/C
CO
NF
IGU
RA
TIO
Nm
ftF
1F
2F
3F
4F
5B
FC
P
2.13
2.27
2.37
7.76
8.42
2.02
5.62
6.99
7.45
7.78
25.4
627
.62
6.63
18.4
4E
NG
INE
/N
AC
ELL
E1.
422.
594.
668.
50N
1N
2
A/C
CO
NF
IGU
RA
TIO
N
WIN
GS
mft
FT
1F
T2
FT
3F
T4
W1
W2 R
3.85
4.31
4.59
4.90
7.91
6.35
3.40
12.6
314
.14
15.0
616
.08
25.9
520
.83
11.1
5
125
000
kg(2
75 5
78 lb
)A
FT
CG
(31
.9%
)
125
000
kg(2
75 5
78 lb
)A
FT
CG
(31
.9%
)
F_AC_100000_1_0380101_01_01
Ground ClearancesFIGURE-10-0-0-991-038-A01
10-0-0Page 15
Aug 01/19