a340-500/-600 aircraft characteristics airport and

@AIRBUSA340-500/-600

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: Apr 01/01 Rev: Jul 01/21

@A340-500/-600AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

HIGHLIGHTS

Revision No. 20 - Jul 01/21

LOCATIONS CHGCODE

DESCRIPTIONS OF CHANGE

CHAPTER 2

Section 2-3

Subject 2-3-0

FIGURE Ground Clearances R ADDED A NOTE RELATED TO THEGROUND CLEARANCE VALUES IN THETABLE ARE DEPEND ON THE CGPOSITION AND AIRCRAFT WEIGHT.REPLACED THE VALUE 0.17 BY 0.71 FORMID CG FOR ENGINE/NACELLECONFIGURATION IN THE GROUNDCLEARANCES TABLE.MODIFIED THE HT POSITION IN THEGROUND CLEARANCES.

FIGURE Ground Clearances R ADDED A NOTE RELATED TO THEGROUND CLEARANCE VALUES IN THETABLE ARE DEPEND ON THE CGPOSITION AND AIRCRAFT WEIGHT.

FIGURE Ground Clearances - Ailerons --Up

R ADDED A NOTE RELATED TO THEGROUND CLEARANCE VALUES IN THETABLE ARE DEPEND ON THE CGPOSITION AND AIRCRAFT WEIGHT.

FIGURE Ground Clearances - Ailerons --Down


FIGURE Ground Clearances - Spoilers --Extended


FIGURE Ground Clearances - LeadingEdge Slats -- Extended


HIGHLIGHTSPage 1

Jul 01/21


LOCATIONS CHGCODE


FIGURE Ground Clearances - TrailingEdge Flaps -- Extended


FIGURE Ground Clearances - Flap Tracks-- Extended


FIGURE Ground Clearances - Flap Tracks-- Retracted


FIGURE Ground Clearances - Flap Tracks-- 1 + F


CHAPTER 4

Section 4-1

Subject 4-1-0

General Information R NOTE AMENDED

Section 4-2

Subject 4-2-0

Turning Radii R

FIGURE Turning Radii - (Sheet 1) R MODIFIED PROPERTY OF THE DEGREESYMBOLS IN THE ILLUSTRATION.

FIGURE Turning Radii - (Sheet 1) R MODIFIED PROPERTY OF THE DEGREESYMBOLS IN THE ILLUSTRATION.

Section 4-5

Subject 4-5-0

Runway and Taxiway Turn Paths N

Subject 4-5-1

135˚ Turn - Runway to Taxiway R

FIGURE 135˚ Turn - Runway to Taxiway- Judgemental Oversteering Method

R MODIFIED THE ILLUSTRATION FORJUDGEMENTAL OVERSTEERINGMETHOD.

HIGHLIGHTSPage 2

Jul 01/21


LOCATIONS CHGCODE


FIGURE 135˚ Turn - Runway to Taxiway- TACS Assisted Steering Method

R REPLACED THE ILLUSTRATION FORCOCKPIT OVER CENTERLINE METHODBY TACS ASSISTED STEERING METHOD.ILLUSTRATION REVISED

FIGURE 135˚ Turn - Runway to Taxiway- Cockpit Over Centerline Method

N ADDED AN ILLUSTRATION FOR 135˚TURN - RUNWAY TO TAXIWAY OFCOCKPIT OVER CENTERLINE METHOD.ILLUSTRATION ADDED

FIGURE 135˚ Turn - Runway to Taxiway- Judgemental Oversteering Method


FIGURE 135˚ Turn - Runway to Taxiway- TACS Assisted Steering Method

R REPLACED THE ILLUSTRATION FORCOCKPIT OVER CENTERLINE METHODBY TACS ASSISTED STEERING METHOD.ILLUSTRATION REVISED

FIGURE 135˚ Turn - Runway to Taxiway- Cockpit Over Centerline Method

N ADDED AN ILLUSTRATION FOR 135˚TURN - RUNWAY TO TAXIWAY OFCOCKPIT OVER CENTERLINE METHOD.ILLUSTRATION ADDED

Subject 4-5-2

90˚ Turn - Runway to Taxiway R

FIGURE 90˚ Turn - Runway to Taxiway -Judgemental Oversteering Method


FIGURE 90˚ Turn - Runway to Taxiway -TACS Assisted Steering Method

N ADDED THE ILLUSTRATION FOR TACSASSISTED STEERING METHOD.ILLUSTRATION ADDED

FIGURE 90˚ Turn - Runway to Taxiway -Cockpit Over Centerline Method

R MODIFIED THE ILLUSTRATION FORCOCKPIT OVER CENTERLINE METHOD.

FIGURE 90˚ Turn - Runway to Taxiway -Judgemental Oversteering Method


FIGURE 90˚ Turn - Runway to Taxiway -TACS Assisted Steering Method


FIGURE 90˚ Turn - Runway to Taxiway -Cockpit Over Centerline Method


HIGHLIGHTSPage 3

Jul 01/21


LOCATIONS CHGCODE


Subject 4-5-3

180˚ Turn on a Runway R NOTE AMENDED

FIGURE 180˚ Turn on a Runway R

FIGURE 180˚ Turn on a Runway R

Subject 4-5-4

135˚ Turn - Taxiway to Taxiway R

FIGURE 135˚ Turn - Taxiway to Taxiway- Judgemental Oversteering Method


FIGURE 135˚ Turn - Taxiway to Taxiway- TACS Assisted Steering Method


FIGURE 135˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method








Subject 4-5-5

90˚ Turn - Taxiway to Taxiway R









HIGHLIGHTSPage 4

Jul 01/21


LOCATIONS CHGCODE






Section 4-7

Subject 4-7-0

Minimum Line-Up Distance Corrections R CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETEDNOTE AMENDED

FIGURE Minimum Line-Up DistanceCorrections - 90˚ Turn on Runway Entry

R

FIGURE Minimum Line-Up DistanceCorrections - 180˚ Turn on Runway TurnPad

R

FIGURE Minimum Line-Up DistanceCorrections - 180˚ Turn on RunwayWidth

R

CHAPTER 5

Section 5-4

Subject 5-4-9

Potable Water Servicing R ADDED ”MAXIMUM” TO THE FILLINGPRESSURE FOR THE POTABLE WATERTANK.

Potable Water Servicing R ADDED ”MAXIMUM” TO THE FILLINGPRESSURE FOR THE POTABLE WATERTANK.

CHAPTER 7 R

Section 7-1

Subject 7-1-0

General Information R CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

Section 7-2

Subject 7-2-0

HIGHLIGHTSPage 5

Jul 01/21


LOCATIONS CHGCODE


Landing Gear Footprint R

FIGURE Landing Gear Footprint R

FIGURE Landing Gear Footprint R

Section 7-3

Subject 7-3-0

Maximum Pavement Loads R

FIGURE Maximum Pavement Loads R

FIGURE Maximum Pavement Loads R

Section 7-4

Subject 7-4-0

Landing Gear Loading on Pavement R CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

Section 7-5

Subject 7-5-0

Flexible Pavement Requirements - USArmy Corps of Engineers Design Method

R

Section 7-6

Subject 7-6-0

Flexible Pavement Requirements - LCNConversion

R

Section 7-7

Subject 7-7-0

Rigid Pavement Requirements - PortlandCement Association Design Method

R

Section 7-8

Subject 7-8-0

Rigid Pavement Requirements - LCNConversion

R

Section 7-9

Subject 7-9-0

Aircraft Classification Number - Flexibleand Rigid Pavements

R NOTE AMENDED

HIGHLIGHTSPage 6

Jul 01/21


LOCATIONS CHGCODE


FIGURE Aircraft Classification Number -ACN Table

R

FIGURE Aircraft Classification Number -ACN Table

R

Section 7-10 N

Subject 7-10-0 N

ACR/PCR Reporting System - Flexibleand Rigid Pavements

N

FIGURE ACR Table N ILLUSTRATION ADDED

FIGURE ACR Table N ILLUSTRATION ADDED

HIGHLIGHTSPage 7

Jul 01/21


LIST OF EFFECTIVE CONTENT

Revision No. 20 - Jul 01/21

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 Apr 01/20

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 R Jul 01/21

FIGURE Ground Clearances R Jul 01/21

FIGURE Ground Clearances - Ailerons -- Up R Jul 01/21

FIGURE Ground Clearances - Ailerons -- Down R Jul 01/21

FIGURE Ground Clearances - Spoilers -- Extended R Jul 01/21

FIGURE Ground Clearances - Leading Edge Slats -- Extended R Jul 01/21

FIGURE Ground Clearances - Trailing Edge Flaps -- Extended R Jul 01/21

FIGURE Ground Clearances - Flap Tracks -- Extended R Jul 01/21

FIGURE Ground Clearances - Flap Tracks -- Retracted R Jul 01/21

FIGURE Ground Clearances - Flap Tracks -- 1 + F R Jul 01/21

Subject 2-4-1

Interior Arrangements - Plan View Jan 01/17

L.E.C.Page 1

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

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


Jan 01/14


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 - Mid Passenger/Crew Doors Oct 01/15

FIGURE Door Clearances - Emergency Exits 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

L.E.C.Page 2

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

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

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 - TRENT 500 Jan 01/14

FIGURE Engine and Nacelle - Nacelle Dimensions - TRENT 500 Jan 01/14

FIGURE Engine and Nacelle - Fan Cowls - TRENT 500 Jan 01/14

L.E.C.Page 3

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Engine and Nacelle - Thrust Reverser Cowls - TRENT 500 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

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 - CLG Jacking Point Heights Oct 01/15

FIGURE Jacking of the Landing Gear - NLG Jacking Point Loads -(WV 001)

Oct 01/15


Oct 01/15

L.E.C.Page 4

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Jacking of the Landing Gear - MLG Jacking Point Loads -(WV 001)

Oct 01/15


Oct 01/15

FIGURE Jacking of the Landing Gear - CLG Jacking Point Loads -(WV 001)

Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15

Subject 2-14-2

Support of Aircraft Jan 01/14

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 - RB 211 TRENT 556engine

Oct 01/15

L.E.C.Page 5

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Payload / Range - ISA Conditions - RB 211 TRENT 553engine

Oct 01/15

Subject 3-3-1

Take-Off Weight Limitation - ISA Conditions Oct 01/15

FIGURE Take-Off Weight Limitation - ISA Conditions -- RB 211TRENT 556 engine

Oct 01/15

FIGURE Take-Off Weight Limitation - ISA Conditions -- RB 211TRENT 553 engine

Oct 01/15

Subject 3-3-2

Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions Oct 01/15

FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- RB 211 TRENT 556 engine

Oct 01/15

FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- RB 211 TRENT 553 engine

Oct 01/15

Subject 3-4-1

Landing Field Length - ISA Conditions Oct 01/15

FIGURE Landing Field Length - ISA Conditions -- RB 211 TRENT556 engine

Oct 01/15

FIGURE Landing Field Length - ISA Conditions -- RB 211 TRENT553 engine

Oct 01/15

Subject 3-5-0

Final Approach Speed Jan 01/14

CHAPTER 4

Subject 4-1-0

General Information R Jul 01/21

Subject 4-2-0

Turning Radii R Jul 01/21

FIGURE Turning Radii - (Sheet 1) R Jul 01/21

FIGURE Turning Radii - (Sheet 1) R Jul 01/21

Subject 4-3-0

Minimum Turning Radii Jan 01/17

L.E.C.Page 6

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

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 N Jul 01/21

Subject 4-5-1

135˚ Turn - Runway to Taxiway R Jul 01/21

FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod

R Jul 01/21

FIGURE 135˚ Turn - Runway to Taxiway - TACS Assisted SteeringMethod

R Jul 01/21

FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod

N Jul 01/21


R Jul 01/21


R Jul 01/21


N Jul 01/21

Subject 4-5-2

90˚ Turn - Runway to Taxiway R Jul 01/21


R Jul 01/21


N Jul 01/21


R Jul 01/21


R Jul 01/21

L.E.C.Page 7

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE


N Jul 01/21


R Jul 01/21

Subject 4-5-3

180˚ Turn on a Runway R Jul 01/21

FIGURE 180˚ Turn on a Runway R Jul 01/21

FIGURE 180˚ Turn on a Runway R Jul 01/21

Subject 4-5-4

135˚ Turn - Taxiway to Taxiway R Jul 01/21

FIGURE 135˚ Turn - Taxiway to Taxiway - JudgementalOversteering Method

R Jul 01/21

FIGURE 135˚ Turn - Taxiway to Taxiway - TACS Assisted SteeringMethod

N Jul 01/21

FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod

R Jul 01/21

FIGURE 135˚ Turn - Taxiway to Taxiway - JudgementalOversteering Method

R Jul 01/21


N Jul 01/21


R Jul 01/21

Subject 4-5-5

90˚ Turn - Taxiway to Taxiway R Jul 01/21

FIGURE 90˚ Turn - Taxiway to Taxiway - Judgemental OversteeringMethod

R Jul 01/21


N Jul 01/21


R Jul 01/21

FIGURE 90˚ Turn - Taxiway to Taxiway - Judgemental OversteeringMethod

R Jul 01/21


N Jul 01/21

L.E.C.Page 8

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE


R Jul 01/21

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 R Jul 01/21

FIGURE Minimum Line-Up Distance Corrections - 90˚ Turn onRunway Entry

R Jul 01/21

FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn onRunway Turn Pad

R Jul 01/21

FIGURE Minimum Line-Up Distance Corrections - 180˚ Turn onRunway Width

R Jul 01/21

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

L.E.C.Page 9

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

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

FIGURE Ground Service Connections Layout Oct 01/15

Subject 5-4-2

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

L.E.C.Page 10

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

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

Subject 5-4-8

Oil Servicing Oct 01/15

FIGURE Ground Service Connections - Engine Oil Tank - RR TRENT500 Series Engine

Oct 01/15

FIGURE Ground Service Connections - IDG Oil Tank - RR TRENT500 Series Engine

Oct 01/15

FIGURE Ground Service Connections - Starter Oil Tank - RR TRENT500 Series 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 R Jul 01/21

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 R Jul 01/21

FIGURE Ground Service Connections - Potable-Water Ground ServicePanels

Oct 01/15

FIGURE Ground Service Connections - Potable-Water Tanks Location Oct 01/15

L.E.C.Page 11

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

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 Engine Starting Pneumatic Requirements Jan 01/14

Subject 5-5-1

Low Ambient Temperatures Jan 01/14

FIGURE Engine Starting Pneumatic Requirements - Low AmbientTemperature -40˚C (-40˚F) -- RB 211 TRENT 500 series engine

Jan 01/14

Subject 5-5-2

Medium Ambient Temperatures Jan 01/14

FIGURE Engine Starting Pneumatic Requirements - Medium AmbientTemperature +15˚C (+59˚F) -- RB 211 TRENT 500 series engine

Jan 01/14

Subject 5-5-3

High Ambient Temperatures Jan 01/14

FIGURE Engine Starting Pneumatic Requirements - High AmbientTemperature +50˚C (+122˚F) -- RB 211 TRENT 500 series engine

Jan 01/14

Subject 5-6-0

Ground Pneumatic Power Requirements Oct 01/15

FIGURE Ground Pneumatic Power Requirements - Heating Oct 01/15

FIGURE Ground Pneumatic Power Requirements - Cooling Oct 01/15

Subject 5-7-0

Preconditioned Airflow Requirements Oct 01/15

L.E.C.Page 12

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Preconditioned Airflow Requirements Oct 01/15

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 - RR TRENT500 series 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 - RRTRENT 500 series engine

Jan 01/14

Subject 6-1-3

Engine Exhaust Velocities Contours - Breakaway Power Jan 01/14

FIGURE Engine Exhaust Velocities - Breakaway Power - RR TRENT500 series engine

Jan 01/14

Subject 6-1-4

Engine Exhaust Temperatures Contours - Breakaway Power Jan 01/14

FIGURE Engine Exhaust Temperatures - Breakaway Power - RRTRENT 500 series engine

Jan 01/14

Subject 6-1-5

Engine Exhaust Velocities Contours - Takeoff Power Jan 01/14

FIGURE Engine Exhaust Velocities - Takeoff Power - RR TRENT 500series engine

Jan 01/14

Subject 6-1-6

L.E.C.Page 13

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

Engine Exhaust Temperatures Contours - Takeoff Power Jan 01/14

FIGURE Engine Exhaust Temperatures - Takeoff Power - RR TRENT500 series engine

Jan 01/14

Subject 6-3-0

Danger Areas of Engines Aug 01/19

Subject 6-3-1

Ground Idle Power Oct 01/15

FIGURE Danger Areas of Engines - RR TRENT 500 series engine Jan 01/14

Subject 6-3-2

Breakaway Power Oct 01/15


Subject 6-3-3

Takeoff Power Oct 01/15


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 GTCP331-600 (A)

Jan 01/14

CHAPTER 7

Subject 7-1-0

General Information R Jul 01/21

Subject 7-2-0

Landing Gear Footprint R Jul 01/21

FIGURE Landing Gear Footprint R Jul 01/21

FIGURE Landing Gear Footprint R Jul 01/21

Subject 7-3-0

Maximum Pavement Loads R Jul 01/21

L.E.C.Page 14

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Maximum Pavement Loads R Jul 01/21

FIGURE Maximum Pavement Loads R Jul 01/21

Subject 7-4-0

Landing Gear Loading on Pavement R Jul 01/21

Subject 7-5-0

Flexible Pavement Requirements - US Army Corps of EngineersDesign Method

R Jul 01/21

Subject 7-6-0

Flexible Pavement Requirements - LCN Conversion R Jul 01/21

Subject 7-7-0

Rigid Pavement Requirements - Portland Cement Association DesignMethod

R Jul 01/21

Subject 7-8-0

Rigid Pavement Requirements - LCN Conversion R Jul 01/21

Subject 7-9-0

Aircraft Classification Number - Flexible and Rigid Pavements R Jul 01/21

FIGURE Aircraft Classification Number - ACN Table R Jul 01/21

FIGURE Aircraft Classification Number - ACN Table R Jul 01/21

Subject 7-10-0

ACR/PCR Reporting System - Flexible and Rigid Pavements N Jul 01/21

FIGURE ACR Table N Jul 01/21

FIGURE ACR Table N Jul 01/21

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

L.E.C.Page 15

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

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

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

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

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

L.E.C.Page 16

Jul 01/21


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Structural Break-in Points Jan 01/14

L.E.C.Page 17

Jul 01/21


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


4-2-0 Turning Radii

4-3-0 Minimum Turning Radii

T.O.C.Page 1

Jul 01/21


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


4-5-3 180˚ Turn on a Runway

4-5-4 135˚ 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

5-5-1 Low Ambient Temperatures

5-5-2 Medium Ambient Temperatures

5-5-3 High Ambient Temperatures

5-6-0 Ground Pneumatic Power Requirements

5-7-0 Preconditioned Airflow Requirements

5-8-0 Ground Towing Requirements

5-9-0 De-Icing and External Cleaning

T.O.C.Page 2

Jul 01/21


6 OPERATING CONDITIONS

6-1-0 Engine Exhaust Velocities and Temperatures

6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power

6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power

6-1-3 Engine Exhaust Velocities Contours - Breakaway Power

6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power

6-1-5 Engine Exhaust Velocities Contours - Takeoff Power

6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power

6-3-0 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


7-2-0 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

7-10-0 ACR/PCR Reporting System - Flexible And Rigid Pavement

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

Jul 01/21


SCOPE

1-1-0 Purpose

**ON A/C A340-500 A340-600

Introduction

1. GeneralThe A340-500/-600 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCEPLANNING (AC) manual is issued for the A340-500 and A340-600 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

Jul 01/21


1-2-1 Glossary

**ON A/C A340-500 A340-600

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

1-2-1Page 1

Jul 01/21


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.

1-2-1Page 2

Jul 01/21


AIRCRAFT DESCRIPTION

2-1-1 General Aircraft Characteristics Data

**ON A/C A340-500 A340-600

General Aircraft Characteristics Data

**ON A/C A340-600

1. The following table provides characteristics of A340-600 Models, these data are specific to eachWeight Variant:

Aircraft CharacteristicsWV000 WV001

Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)

366 200 kg(807 333 lb)

369 200 kg(813 946 lb)

Maximum Take-Off Weight(MTOW)

365 000 kg(804 687 lb)

368 000 kg(811 301 lb)

Maximum Landing Weight (MLW)256 000 kg(564 383 lb)

259 000 kg(570 997 lb)

Maximum Zero Fuel Weight(MZFW)

242 000 kg(533 519 lb)

245 000 kg(540 132 lb)

195 010 l(51 516 US gal)Usable Fuel Capacity

(density = 0.785 kg/l) 153 082 kg(337 488 lb)

Aircraft CharacteristicsWV101 WV102 WV103

Maximum Taxi Weight (MTW)Maximum Ramp Weight (MRW)

381 200 kg(840 402 lb)

369 200 kg(813 946 lb)

366 200 kg(807 333 lb)


380 000 kg(837 756 lb)

368 000 kg(811 301 lb)

365 000 kg(804 687 lb)

Maximum Landing Weight (MLW)265 000 kg(584 225 lb)

259 000 kg(570 997 lb)

265 000 kg(584 225 lb)


251 000 kg(553 360 lb)

245 000 kg(540 132 lb)

251 000 kg(553 360 lb)

2-1-1Page 1

Jul 01/21



198 139 l (1) - 208 939 l (2)(52 343 US gal (1) - 55 196 US gal (2))Usable Fuel Capacity

(density = 0.785 kg/l) 155 539 kg (1) - 164 017 kg (2)(342 905 lb (1) - 361 595 lb (2))

(1) Without forward ACT(2) With forward ACT

2. The following table provides characteristics of A340-600 Models, these data are common to eachWeight Variant:

Aircraft CharacteristicsStandard SeatingCapacity

384

Pressurized FuselageVolume (A/C nonequipped)

1 305 m3

(46 086 ft3)

Passenger CompartmentVolume

557 m3

(19 670 ft3)

Cockpit Volume12 m3

(424 ft3)

Usable Volume, FWD CC(Based on LD3)

104 m3

(3 672 ft3)

Usable Volume, AFT CC(Based on LD3)

78 m3

(2 754 ft3)

Usable Volume, Bulk CC19.7 m3

(695 ft3)

Water Volume, FWD CC143 m3

(5 050 ft3)

Water Volume, AFT CC102.3 m3

(3 612 ft3)

Water Volume, Bulk CC22.7 m3

(802 ft3)

2-1-1Page 2

Jul 01/21


**ON A/C A340-500

3. The following table provides characteristics of A340-500 Models, these data are specific to eachWeight Variant:

Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004

Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)

369 200 kg(813 946 lb)

373 200 kg(822 765 lb)

373 200 kg(822 765 lb)

375 200 kg(827 174 lb)

375 200 kg(827 174 lb)


368 000 kg(811 301 lb)

372 000 kg(820 119 lb)

372 000 kg(820 119 lb)

374 000 kg(824 529 lb)

374 000 kg(824 529 lb)

Maximum Landing Weight(MLW)

240 000 kg(529 109 lb)

243 000 kg(535 723 lb)

243 000 kg(535 723 lb)

231 000 kg(509 268 lb)

243 000 kg(535 723 lb)


225 000 kg(496 040 lb)

230 000 kg(507 063 lb)

229 000 kg(504 858 lb)

218 000 kg(480 608 lb)

218 000 kg(480 608 lb)

214 808 l(56 746 US

gal)

215 108 l * - 223 078 l **(56 826 US gal * - 58 931

US gal **)

214 066 l * - 222 036 l **(56 550 US gal * - 58 656

US gal **)Usable Fuel Capacity(density = 0.785 kg/l)

168 624 kg(371 752 lb)

168 859 kg * - 175 116 kg**

(372 270 lb * - 386 065 lb**)

168 041 kg * - 174 298 kg**

(370 467 lb * - 384 261 lb** )


Maximum Taxi Weight(MTW)Maximum Ramp Weight(MRW)

381 200 kg(840 402 lb)

373 200 kg(822 765 lb)

373 200 kg(822 765 lb)


380 000 kg(837 756 lb)

372 000 kg(820 119 lb)

372 000 kg(820 119 lb)

Maximum Landing Weight(MLW)

246 000 kg(542 337 lb)

243 000 kg(535 723 lb)

246 000 kg(542 337 lb)


232 000 kg(511 472 lb)

230 000 kg(507 063 lb)

232 000 kg(511 472 lb)

2-1-1Page 3

Jul 01/21



214 066 l * - 222 036 l**

(56 550 US gal * - 58656 US gal **)

216 622 l * - 223 210 l **(57 225 US gal * - 58 966 US gal **)

Usable Fuel Capacity(density = 0.785 kg/l) 168 041 kg * - 174 298

kg **(370 467 lb * - 384 261

lb **)

170 048 kg * - 175 219 kg **(374 892 lb * - 386 292 lb **)

* (Production model) RCT = 5 frames** (Optional model) RCT = 7 frames

4. The following table provides characteristics of A340-500 Models, these data are common to eachWeight Variant:

Aircraft CharacteristicsStandard Seating Capacity 313

Pressurized Fuselage Volume(A/C non equipped)

1 120 m3

(39 552 ft3)

Passenger CompartmentVolume

490 m3

(17 304 ft3)

Cockpit Volume12 m3

(424 ft3)

Usable Volume, FWD CC(Based on LD3)

78 m3

(2 754 ft3)

Usable Volume, AFT CC(Based on LD3)

52 m3

(1 836 ft3)

Usable Volume, Bulk CC19.7 m3

(695 ft3)

Water Volume, FWD CC107.1 m3

(3 782 ft3)

Water Volume, AFT CC73.9 m3

(2 610 ft3)

Water Volume, Bulk CC22.7 m3

(802 ft3)

2-1-1Page 4

Jul 01/21


2-2-0 General Aircraft Dimensions

**ON A/C A340-500 A340-600

General Aircraft Dimensions

1. This section provides general aircraft dimensions.

2-2-0Page 1

Jul 01/21


**ON A/C A340-600

(28.31 ft)8.63 m

(28.15 ft)8.58 m

(206.82 ft)63.04 m

(241.01 ft)73.46 m

(245.31 ft)74.77 m

(21.59 ft)6.58 m

(129.46 ft)39.46 m − MLG

(131.92 ft)40.21 m − CLG

(18.5 ft)5.64 m

(28.87 ft)8.8 m

(10.17 ft)3.1 m

(208.17 ft)63.45 m

(74.11 ft)22.59 m

(3.87 ft)1.18 m

(35.04 ft)10.68 m

(41.37 ft)12.61 m

(61.48 ft)18.74 m

(126.44 ft)38.54 m

(2.66 ft)0.81 m

NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. F_AC_020200_1_0090101_01_01

General Aircraft Dimensions(Sheet 1 of 2)

FIGURE-2-2-0-991-009-A01

2-2-0Page 2

Jul 01/21


**ON A/C A340-600

(89.63 ft)27.32 m

(111.38 ft)33.95 m

(165.26 ft)50.37 m

(154.3 ft)47.03 m

(239.27 ft)72.93 m

(247.24 ft)75.36 m

(8.76 ft)2.67 m

(7.97 ft)2.43 m

(24.67 ft)7.52 m

(39.96 ft)12.18 m

(35.63 ft)10.86 m

7.45 m(24.44 ft)

(46.

52ft)

14.1

8 m

17.6

2 m

(57.

81 ft

)

NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.

F_AC_020200_1_0090102_01_00


FIGURE-2-2-0-991-009-A01

2-2-0Page 3

Jul 01/21


**ON A/C A340-500

(28.31 ft)8.63 m

(28.15 ft)8.58 m

(182.41 ft)55.6 m

(216.63 ft)66.03 m

(220.9 ft)67.33 m

(21.59 ft)6.58 m

(112.07 ft)34.16 m − MLG

(114.53 ft)34.91 m − CLG

(18.5 ft)5.64 m

(28.87 ft)8.8 m

(10.17 ft)3.1 m

(3.87 ft)1.18 m

(35.04 ft)10.68 m

(41.37 ft)12.61 m

(61.48 ft)18.74 m

(126.44 ft)38.54 m

(2.66 ft)0.81 m

(208.17 ft)63.45 m

(74.11 ft)22.59 m

NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. F_AC_020200_1_0100101_01_01


FIGURE-2-2-0-991-010-A01

2-2-0Page 4

Jul 01/21


**ON A/C A340-500

NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.

(72.24 ft)22.02 m

(94.03 ft)28.66 m

(147.87 ft)45.07 m

(136.91 ft)41.73 m

(214.9 ft)65.5 m

(222.87 ft)67.93 m

(8.76 ft)2.67 m

(24.67 ft)7.52 m

(7.97 ft)2.43 m

(39.96 ft)12.18 m

(35.63 ft)10.86 m

7.45 m(24.44 ft)

(46.

52ft)

14.1

8 m

17.6

2 m

(57.

81 ft

)

F_AC_020200_1_0100102_01_00


FIGURE-2-2-0-991-010-A01

2-2-0Page 5

Jul 01/21


2-3-0 Ground Clearances

**ON A/C A340-500 A340-600

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 7.20 m (23.62 ft).

NOTE : Passenger and cargo door ground clearances are measured from the center of the door silland from floor level.

2-3-0Page 1

Jul 01/21


**ON A/C A340-600

ENGINE/NACELLE

FUSELAGE

D1D2D3D4D5C1C2C3F1F2F3F4F5BFCPW1W2HTAPVTN1N2

4.604.824.965.125.502.703.313.401.992.172.477.818.271.665.727.565.968.397.0417.730.521.56

15.0815.8116.2716.7918.038.8610.8411.146.537.118.0925.6127.125.4618.7724.8119.5527.5423.1158.171.715.12

4.734.885.005.095.422.823.253.332.112.232.447.878.191.705.877.535.938.266.92

17.600.561.58

15.5316.0316.4016.6917.779.27

10.6610.926.937.337.9925.8326.865.57

19.2724.7019.4627.1022.7157.741.855.18

4.785.005.155.315.692.883.503.592.172.352.667.998.471.855.907.766.158.607.2517.930.711.75

15.6716.4116.9017.4218.689.4611.4911.797.127.718.7226.2227.776.0719.3525.4520.1828.2123.7858.842.325.75

7.037.037.087.037.255.095.145.194.384.384.3810.0210.023.788.209.467.889.988.6619.322.663.62

23.0723.0723.2423.0723.7816.7116.8617.0314.3714.3714.3732.8732.8712.4026.9031.0425.8732.7428.4163.398.73

11.89

WINGS

TAILPLANE

DOORS

A/C CONFIGURATIONMRW

FWD CG AFT CGm ft m ft

MID CGm ft m ft

176 000 kg(380 013 lb) A/C JACKED

FDL = 7.20 m (23.62 ft)

CP D1 D2

N1

D3

N2

D4 W2 W1 D5 AP

VT

F5 C3 C2 F3 BF F2 F4 C1 F1

HT

THE VALUES GIVEN IN THE TABLE DEPEND ON THE POSITION OFTHE CENTER OF GRAVITY (CG) AND ON THE AIRCRAFT WEIGHT.

NOTE:PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.

F_AC_020300_1_0120101_01_04

Ground ClearancesFIGURE-2-3-0-991-012-A01

2-3-0Page 2

Jul 01/21


**ON A/C A340-500

ENGINE/NACELLE

FUSELAGE

D1D2D3D4C1C2C3F1F2F3F4F5BFCPW1W2HTAPVTN1N2

4.534.755.085.582.653.363.461.942.102.107.748.351.635.637.626.018.537.18

17.380.481.56

14.8515.5816.6618.318.7011.0111.356.366.896.8925.3827.405.3618.4825.0119.7027.9723.5757.011.585.10

4.634.805.055.492.743.293.382.032.152.077.798.261.655.757.575.968.387.0517.230.511.55

15.1815.7416.5718.008.98

10.7911.096.647.046.79

25.5427.095.42

18.8624.8319.5627.4823.1256.531.665.10

4.764.965.275.752.883.533.632.162.312.297.958.521.845.877.816.198.687.3417.530.691.75

15.6116.2817.2818.869.4411.5911.927.107.587.51

26.0827.956.03

19.2525.6120.3128.4724.0857.512.255.75

7.037.037.037.255.095.145.194.384.384.0510.0210.023.788.209.467.889.968.6618.822.663.62

23.0723.0723.0723.7816.7116.8617.0314.3714.3713.3032.8732.8712.4026.9031.0425.8732.6828.4161.758.73

11.89

WINGS

TAILPLANE

DOORS

A/C CONFIGURATIONMRW

FWD CG AFT CGm ft m ft

MID CGm ft m ft

171 000 kg(376 990 lb) A/C JACKED

FDL = 7.20 m (23.62 ft)

CP D1 D2 D3 D4W2 W1 AP

VT HT


NOTE:PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.

N1 N2

F5 C2 F3C3 BF F2 F4 C1 F1

F_AC_020300_1_0120201_01_02

Ground ClearancesFIGURE-2-3-0-991-012-B01

2-3-0Page 3

Jul 01/21


**ON A/C A340-500 A340-600

m ft m ft m ft

A

B

C

MRWFWD CG

A/C IN MAINTENANCECONFIGURATION

MID CGDESCRIPTION

AILERON 1 INBD

AILERON 1 OUTBD

AILERON 2 INBD

20.33

20.63

20.38

6.20

6.29

6.21

6.00

6.09

6.02

19.68

19.99

19.75

5.99

6.07

6.00

19.64

19.92

19.68

AILERONS UP

MRWAFT CG

AILERON 2 OUTBD D 21.016.40 6.21 20.37 6.18 20.28

D C B A


NOTE:

F_AC_020300_1_0130101_01_04

Ground ClearancesAilerons -- Up

FIGURE-2-3-0-991-013-A01

2-3-0Page 4

Jul 01/21


**ON A/C A340-500 A340-600

D C B A

m ft m ft m ft

A

B

C

MRWFWD CG


MID CGDESCRIPTION

AILERON 1 INBD

AILERON 1 OUTBD

AILERON 2 INBD

17.24

18.38

18.16

5.26

5.60

5.53

5.06

5.41

5.34

16.61

17.74

17.53

5.05

5.39

5.32

16.56

17.67

17.45

AILERONS DOWN

MRWAFT CG

AILERON 2 OUTBD D 19.385.91 5.71 18.74 5.68 18.65


NOTE:

F_AC_020300_1_0240101_01_02

Ground ClearancesAilerons -- Down

FIGURE-2-3-0-991-024-A01

2-3-0Page 5

Jul 01/21


**ON A/C A340-500 A340-600

m ft m ft m ft

B

C 5.75

5.89

5.87

5.56

5.70

5.68

5.57

5.70

5.68

18.88 18.25 18.26

19.33

19.26

18.70

18.63

18.70

18.63

SPOILERS EXTENDED

D

E

F

G

6.03

6.16

5.84

5.97

5.84

5.96

19.79 19.16 19.16

20.20 19.57 19.55

A 4.78

5.29

4.58

5.10

4.59

5.10

15.67 15.04 15.05

17.36 16.74 16.75

MRWAFT CG

MRWFWD CG


MID CG

SPOILER 1 OUTBD

SPOILER 2 INBD

SPOILER 2 OUTBD

SPOILER 3 INBD

SPOILER 3/4

SPOILER 6 OUTBD

SPOILER 1 INBD

DESCRIPTION

J 6.35 6.16 6.1520.84 20.21 20.17

SPOILER 4/5

H 6.27 6.07 6.0620.56 19.93 19.90SPOILER 5/6

ABCDEFGHJ


NOTE:

F_AC_020300_1_0250101_01_02

Ground ClearancesSpoilers -- Extended

FIGURE-2-3-0-991-025-A01

2-3-0Page 6

Jul 01/21


**ON A/C A340-500 A340-600

m ft m ft m ft

B

C 4.34

4.66

4.91

4.14

4.46

4.72

4.15

4.46

4.71

14.25 13.58 13.63

15.29

16.12

14.64

15.47

14.64

15.46

LEADING EDGE SLATS EXTENDED

D

E

F

G

5.14

5.22

4.94

5.02

4.93

5.01

16.85 16.21 16.17

17.12 16.48 16.44

A 3.58

4.31

3.37

4.11

3.40

4.12

11.74 11.06 11.15

14.14 13.47 13.53

MRWAFT CG

MRWFWD CG


MID CG

SLAT 1 OUTBD

SLAT 2 INBD

SLAT 2/3

SLAT 3/4

SLAT 4 OUTBD

SLAT 6/7

SLAT 1 INBD

DESCRIPTION

J 5.61 5.42 5.3918.39 17.78 17.68

SLAT 5 INBD

H 5.41 5.22 5.2017.75 17.12 17.05SLAT 5/6

SLAT 7 OUTBD K 5.91 5.73 5.6819.39 18.79 18.65

A B C D E F G H J K


NOTE:

F_AC_020300_1_0260101_01_02

Ground ClearancesLeading Edge Slats -- Extended

FIGURE-2-3-0-991-026-A01

2-3-0Page 7

Jul 01/21


**ON A/C A340-500 A340-600

m ft m ft m ft

A

B

C

MRWFWD CG


MID CGDESCRIPTION

FLAP 1 INBD

FLAP 1 OUTBD

FLAP 2 INBD

9.06

12.99

12.95

2.76

3.96

3.95

2.57

3.77

3.76

8.43

12.36

12.32

2.57

3.76

3.75

8.43

12.35

12.31

FLAP EXTENDED

MRWAFT CG

FLAP 2 OUTBD D 15.804.82 4.62 15.17 4.61 15.11

D C B A


NOTE:

F_AC_020300_1_0270101_01_02

Ground ClearancesTrailing Edge Flaps -- Extended

FIGURE-2-3-0-991-027-A01

2-3-0Page 8

Jul 01/21


**ON A/C A340-500 A340-600

m ft m ft m ft

A

B

C

MRWFWD CG


MID CGDESCRIPTION

FLAP TRACK 2

FLAP TRACK 3

FLAP TRACK 4

9.12

10.66

11.34

2.78

3.25

3.46

2.59

3.06

3.27

8.50

10.03

10.71

2.58

3.05

3.25

8.47

10.00

10.67

FLAP TRACKS EXTENDED

MRWAFT CG

FLAP TRACK 5 D 12.213.72 3.53 11.58 3.51 11.52

D C B A


NOTE:

F_AC_020300_1_0280101_01_02

Ground ClearancesFlap Tracks -- Extended

FIGURE-2-3-0-991-028-A01

2-3-0Page 9

Jul 01/21


**ON A/C A340-500 A340-600

m ft m ft m ft

A

B

C

MRWFWD CG


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

12.60

14.16

14.30

3.84

4.31

4.36

3.65

4.12

4.17

11.97

13.53

13.67

FLAP TRACKS RETRACTED

MRWAFT CG

D 15.654.77 4.58 15.01

AIRCRAFTTYPE

A340−600

A

B

C

12.66

14.20

14.35

3.86

4.33

4.37

3.67

4.13

4.18

12.03

13.57

13.71

3.65

4.12

4.16

11.96

13.52

13.66

D 15.744.80 4.61 15.13 4.58 15.01

A340−500

3.65

4.13

4.17

11.97

13.54

13.69

4.56 14.97

D C B A


NOTE:

F_AC_020300_1_0310101_01_01

Ground ClearancesFlap Tracks -- Retracted

FIGURE-2-3-0-991-031-A01

2-3-0Page 10

Jul 01/21


**ON A/C A340-500 A340-600

m ft m ft m ft

A

B

C

MRWFWD CG


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

11.38

12.93

13.09

3.47

3.94

3.99

3.28

3.75

3.80

10.76

12.30

12.47

FLAP TRACKS 1+F

MRWAFT CG

D 13.784.20 4.21 13.81

AIRCRAFTTYPE

A340−600

A

B

C

11.45

12.99

13.12

3.49

3.96

4.00

3.30

3.76

3.81

10.83

12.34

12.50

3.28

3.75

3.79

10.76

12.30

12.43

D 14.534.43 4.24 13.91 4.21 13.81

A340−500

3.28

3.76

3.80

10.76

12.34

12.47

4.19 13.75

D C B A


NOTE:

F_AC_020300_1_0340101_01_01

Ground ClearancesFlap Tracks -- 1 + F

FIGURE-2-3-0-991-034-A01

2-3-0Page 11

Jul 01/21


2-4-1 Interior Arrangements - Plan View

**ON A/C A340-500 A340-600

Interior Arrangements - Plan View

1. This section provides the typical interior configuration.

2-4-1Page 1

Jul 01/21


**ON A/C A340-600

FWD PASSENGER/CREW DOOR 1 LH

ATTENDANT SEATVCC VIDEO

LAVATORY

COAT STOWAGE

FWD PASSENGER/CREW DOOR 1 RH

GALLEY

ATTENDANT SEAT

LAVATORY

FIRST CLASS SEATS

BUSINESSCLASS SEATS

COAT STOWAGE

ATTENDANT SEAT

MID PASSENGER/CREW DOOR 2 RH

LAVATORYLAVATORY

ECONOMYCLASS SEATS

EMERGENCY EXITDOOR 3 RHLAVATORY

ATTENDANT SEATATTENDANT SEAT

ECONOMYCLASS SEATS

LAVATORY

AFT PASSENGER/CREW DOOR 4 LH

AFT PASSENGER/CREW DOOR 4 RH

GALLEY

STOWAGEGALLEYGALLEY

STOWAGE

STOWAGEATTENDANT SEAT

ATTENDANT SEAT ATTENDANT SEAT

54 BUSINESS CLASS SEATS

314 ECONOMY CLASS SEATS

ATTENDANT SEATS 12

COAT STOWAGES 3

GALLEYS 10

PASSENGER SEATS (380 TOTAL)

12 FIRST CLASS SEATS

LAVATORIES 11

STOWAGES 3

VCC VIDEO 1

COAT STOWAGE

MID PASSENGER/CREW DOOR 2 LH

EMERGENCY EXITDOOR 3 LH

GALLEY

GALLEY

GALLEY

F_AC_020401_1_0060101_01_01

Interior Arrangements - Plan ViewTypical Configuration

FIGURE-2-4-1-991-006-A01

2-4-1Page 2

Jul 01/21


**ON A/C A340-500

36 BUSINESS CLASS SEATS

265 ECONOMY CLASS SEATS

ATTENDANT SEATS 12

COAT STOWAGES 2

GALLEYS 11

PASSENGER SEATS (313 TOTAL)

12 FIRST CLASS SEATS

LAVATORIES 10

STOWAGES 3

VCC VIDEO 1

VCC VIDEO

GALLEY

ATTENDANT SEAT

FWD PASSENGER/CREW DOOR 1 RH

LAVATORY

FIRST CLASS SEATS

FWD PASSENGER/CREW DOOR 1 LH

ATTENDANT SEAT

LAVATORY

COAT STOWAGE

BUSINESSCLASS SEATS

MID PASSENGER/CREW DOOR 2 LH

LAVATORY

GALLEY

ATTENDANT SEATMID PASSENGER/CREW DOOR 2 RH

COAT STOWAGEATTENDANT SEAT

LAVATORYGALLEY

ECONOMYCLASS SEATS

EMERGENCY EXITDOOR 3 RHLAVATORY

ATTENDANT SEAT

LAVATORY

EMERGENCY EXITDOOR 3 LH

ECONOMYCLASS SEATS

AFT PASSENGER/CREW DOOR 4 LH

STOWAGEGALLEY

ATTENDANT SEAT

GALLEYGALLEY

AFT PASSENGER/CREW DOOR 4 RH

ATTENDANT SEAT

STOWAGE

GALLEY

STOWAGEATTENDANT SEAT

LAVATORY

F_AC_020401_1_0070101_01_01

Interior Arrangements - Plan ViewTypical Configuration

FIGURE-2-4-1-991-007-A01

2-4-1Page 3

Jul 01/21


2-5-0 Interior Arrangements - Cross Section

**ON A/C A340-500 A340-600

Interior Arrangements - Cross Section

1. This section gives the typical configuration of A340-500/-600 models.

2-5-0Page 1

Jul 01/21


**ON A/C A340-500 A340-600

1006 mm(39.61 in)

450 mm(17.72 in)

2462 mm(96.93 in)

5287 mm(208.15 in)

1827

mm

(71.

92 in

)

1650

mm

(64.

96 in

)

1006 mm(39.61 in)

128.8 mm(5.07 in)

2402 mm(94.56 in)

2222 mm(87.48 in)

1371.6 mm(54.00 in)

533.4 mm(21.00 in)

1371.6 mm(54.00 in)

F_AC_020500_1_0030101_01_00

Interior Arrangements - Cross SectionTypical Configuration

FIGURE-2-5-0-991-003-A01

2-5-0Page 2

Jul 01/21


**ON A/C A340-500 A340-600

1783 mm(70.20 in)

2401 mm(94.52 in)1006 mm

(39.61 in)450 mm

(17.72 in)

2462 mm(96.93 in)

5287 mm(208.15 in)

1827

mm

(71.

92 in

)

1650

mm

(64.

96 in

)

1006 mm(39.61 in)

128.8 mm(5.07 in)

1371.6 mm(54.00 in)

533.4 mm(21.00 in)

1371.6 mm(54.00 in)

F_AC_020500_1_0040101_01_00


FIGURE-2-5-0-991-004-A01

2-5-0Page 3

Jul 01/21


**ON A/C A340-500 A340-600

482.6 mm(19.00 in)

1006 mm(39.61 in)

450 mm(17.72 in)

2462 mm(96.93 in)

5287 mm(208.15 in)

1783 mm(70.20 in)

2401 mm(94.52 in)

1827

mm

(71.

92 in

)

1650

mm

(64.

96 in

)

1054.1 mm(41.50 in)

503 mm(19.80 in)

503 mm(19.80 in)

135.2 mm(5.32 in)

(41.50 in)1054.1 mm

F_AC_020500_1_0050101_01_00


FIGURE-2-5-0-991-005-A01

2-5-0Page 4

Jul 01/21


2-6-1 Lower Deck Cargo Compartments

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-500 A340-600

LOWER DECKFWD CARGO

COMPARTMENT

LOWER DECKAFT CARGO

COMPARTMENT

LOWER DECKBULK CARGO

COMPARTMENT

2.75 m(9.02 ft)

2.78 m(9.12 ft)

0.95 m(3.12 ft)

20.3 m(66.6 ft)

15.27 m(50.1 ft)

4.04 m(13.25 ft)

A340−600

15.1 m(49.54 ft)

10.37 m(34.02 ft)

4.04 m(13.25 ft)

A340−500

FR20 FR39.1 FR53.2 FR65 FR73

NOTE:APPROXIMATE DIMENSIONS DEPENDING ON AIRCRAFT CONFIGURATION.

F_AC_020601_1_0070101_01_01

Lower Deck Cargo CompartmentsLocation and Dimensions

FIGURE-2-6-1-991-007-A01

2-6-1Page 2

Jul 01/21


**ON A/C A340-500

18 LD3 60.4 in X 61.5 in 12 LD3 60.4 in X 61.5 in

6 PALLETS 96 in X 125 in




F_AC_020601_1_0080101_01_03

Lower Deck Cargo CompartmentsLoading Combinations

FIGURE-2-6-1-991-008-A01

2-6-1Page 3

Jul 01/21


**ON A/C A340-600

24 LD3 60.4 in X 61.5 in



18 LD3 60.4 in X 61.5 in



F_AC_020601_1_0080201_01_02

Lower Deck Cargo CompartmentsLoading Combinations

FIGURE-2-6-1-991-008-B01

2-6-1Page 4

Jul 01/21


2-7-0 Door Clearances

**ON A/C A340-500 A340-600

Door Clearances

1. This section provides door location, identification and clearances.

2-7-0Page 1

Jul 01/21


**ON A/C A340-500

DOOR 1L DOOR 2L DOOR 3L DOOR 4L

DOOR 4RDOOR 3R DOOR 1RDOOR 2R

BULK CARGOCOMPARTMENT

DOOR

FWD CARGOCOMPARTMENT

DOOR AFT CARGOCOMPARTMENT

DOOR

F_AC_020700_1_0100101_01_01

Door ClearancesDoor Identification (Sheet 1 of 2)

FIGURE-2-7-0-991-010-A01

2-7-0Page 2

Jul 01/21


**ON A/C A340-500

54.14 m(177.62 ft)

37.67 m(123.59 ft)

18.61 m(61.06 ft)

5.85 m(19.19 ft)

50.53 m(165.78 ft)

9.53 m(31.27 ft)

47.55 m(156 ft)

F_AC_020700_1_0100102_01_00

Door ClearancesDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-010-A01

2-7-0Page 3

Jul 01/21


**ON A/C A340-600

DOOR 1LDOOR 2L

OVERWING EXITDOOR L DOOR 3L DOOR 4L

DOOR 4R DOOR 3RDOOR 1RDOOR 2R

OVERWING EXITDOOR R

BULK CARGOCOMPARTMENT

DOOR

FWD CARGOCOMPARTMENT

DOOR AFT CARGO

COMPARTMENTDOOR

F_AC_020700_1_0100201_01_01

Door ClearancesDoor Identification (Sheet 1 of 2)

FIGURE-2-7-0-991-010-B01

2-7-0Page 4

Jul 01/21


**ON A/C A340-600

61.58 m(202.03 ft)

47.46 m(155.71 ft)

34.09 m(111.84 ft)

23.91 m(78.44 ft)5.85 m

(19.19 ft)

57.96 m(190.16 ft)

9.53 m(31.27 ft)

54.98 m(180.38 ft)

F_AC_020700_1_0100202_01_00

Door ClearancesDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-010-B01

2-7-0Page 5

Jul 01/21


**ON A/C A340-500 A340-600

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_0410101_01_00

Door ClearancesForward Passenger/Crew Doors

FIGURE-2-7-0-991-041-A01

2-7-0Page 6

Jul 01/21


**ON A/C A340-500

2.43 m(7.97 ft)

0.75 m(2.46 ft)

1.07 m(3.51 ft)

0.05 m(0.16 ft)

3.40 m(11.16 ft)

SEECHAPTER

2−3

18.61 m(61.06 ft)

(FROM NOSE)

(TOP OF FLOOR)

1.93 m(6.33 ft)

0.64 m(2.10 ft)

A A

FWD

3.41 m(11.19 ft)

A

A

F_AC_020700_1_0420101_01_00

Door ClearancesMid Passenger/Crew DoorsFIGURE-2-7-0-991-042-A01

2-7-0Page 7

Jul 01/21


**ON A/C A340-600

1.93 m(6.33 ft)

A A

(TOP OF FLOOR)

0.64 m(2.10 ft)

3.41 m(11.19 ft)

0.75 m(2.46 ft)

0.75 m(2.46 ft)

FWD

SEECHAPTER

2−3

1.07 m(3.51 ft)

2.43 m(7.97 ft)

(FROM NOSE)

(FROM NOSE)

3.40 m(11.16 ft)

0.05 m(0.16 ft)

47.46 m(155.71 ft)

23.91 m(78.44 ft)

1.07 m(3.51 ft)

2.43 m(7.97 ft)

A

A

4.85 m(15.91 ft)

A

A

F_AC_020700_1_0430101_01_00

Door ClearancesMid Passenger/Crew DoorsFIGURE-2-7-0-991-043-A01

2-7-0Page 8

Jul 01/21


**ON A/C A340-500

SEE

2−3CHAPTER

37.67 m(123.59 ft)(FROM NOSE)

1.66 m(5.45 ft)

3.24 m(10.63 ft)

0.42 m(1.38 ft)

A A

0.03 m(0.10 ft)

A

A

0.52 m(1.71 ft)

1.46 m(4.79 ft)

CL

0.61 m(2.00 ft)

F_AC_020700_1_0440101_01_00

Door ClearancesEmergency Exits

FIGURE-2-7-0-991-044-A01

2-7-0Page 9

Jul 01/21


**ON A/C A340-600

SEE

2−3CHAPTER

34.09 m(111.84 ft)(FROM NOSE)

1.66 m(5.45 ft)

0.38 m(1.25 ft)

3.20 m(10.50 ft)

A A

0.10 m(0.33 ft)

A

A

0.50 m(1.64 ft)

1.47 m(4.82 ft)

CL

0.61 m(2.00 ft)

F_AC_020700_1_0450101_01_00

Door ClearancesEmergency Exits

FIGURE-2-7-0-991-045-A01

2-7-0Page 10

Jul 01/21


**ON A/C A340-500 A340-600

CL

A A

0.05 m(0.16 ft)

A340−600: 61.58 m (202.03 ft)A340−500: 54.14 m (177.62 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)

2.43 m(7.97 ft)

0.75 m(2.46 ft)

CRITICALCLEARANCE

LIMIT

SEE

2−3CHAPTER

(FROM NOSE)

A

A

F_AC_020700_1_0460101_01_00

Door ClearancesAft Passenger/Crew DoorsFIGURE-2-7-0-991-046-A01

2-7-0Page 11

Jul 01/21


**ON A/C A340-500 A340-600

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

2.04 m(6.69 ft)

1.70 m(5.58 ft)

SEECHAPTER

2−3

F_AC_020700_1_0470101_01_00

Door ClearancesForward Cargo Compartment Door

FIGURE-2-7-0-991-047-A01

2-7-0Page 12

Jul 01/21


**ON A/C A340-500 A340-600

A A

2.72 m(8.92 ft)

A

A

A340−500: 47.55 m (156.00 ft)A340−600: 54.98 m (180.38 ft)

(FROM NOSE)

CL

5.19 m(17.03 ft)

1.92 m(6.30 ft) 1.68 m

(5.51 ft)

FWD

SEECHAPTER

2−3

F_AC_020700_1_0480101_01_00

Door ClearancesAft Cargo Compartment DoorFIGURE-2-7-0-991-048-A01

2-7-0Page 13

Jul 01/21


**ON A/C A340-500 A340-600

A

A

0.95 m(3.12 ft) 1.11 m

(3.64 ft)

(FROM NOSE)A340−500: 50.53 m (165.78 ft)A340−600: 57.96 m (190.16 ft)

SEECHAPTER

2−3

FWD

1.41 m(4.63 ft)

A A

1.07 m(3.51 ft)

F_AC_020700_1_0490101_01_00

Door ClearancesBulk Cargo Compartment Door

FIGURE-2-7-0-991-049-A01

2-7-0Page 14

Jul 01/21


**ON A/C A340-500 A340-600

1.32 m(4.33 ft)

1.25 m(4.10 ft)

67?

1.65 m(5.41 ft)

FR1

F_AC_020700_1_0500101_01_00

Door ClearancesRadome

FIGURE-2-7-0-991-050-A01

2-7-0Page 15

Jul 01/21


**ON A/C A340-500

GROUND LINE

A/C

C L

A

A340−500: 31.31 m (102.72 ft)

3.16 m(10.37 ft)

0.05 m(0.16 ft)

1.10 m(3.61 ft)

2.58 m(8.46 ft)

MAX. 0.37 m (1.21 ft)MIN. 0.17 m (0.56 ft)

LH SHOWNRH SYMMETRICAL

NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01

01

2.30 m(7.55 ft)

A

3.96 m(12.99 ft)

81?90?

1.02 m(3.35 ft)

F_AC_020700_1_0510101_01_00

Door ClearancesMain and Center Landing Gear Doors

FIGURE-2-7-0-991-051-A01

2-7-0Page 16

Jul 01/21


**ON A/C A340-600

ALH SHOWN

RH SYMMETRICALNOTE:

DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01

A340−600: 36.71 m (120.44 ft)

GROUND LINE

A/C

C L

3.16 m(10.37 ft)

0.05 m(0.16 ft)

1.10 m(3.61 ft)

2.58 m(8.46 ft)

MAX. 0.37 m (1.21 ft)MIN. 0.17 m (0.56 ft) 01

2.30 m(7.55 ft)

A

3.96 m(12.99 ft)

81?90?

1.02 m(3.35 ft)

F_AC_020700_1_0520101_01_00

Door ClearancesMain and Center Landing Gear Doors

FIGURE-2-7-0-991-052-A01

2-7-0Page 17

Jul 01/21


**ON A/C A340-500

FR94 FR98

FWD

MAX. 2.18 m (7.15 ft)MIN. 1.93 m (6.33 ft) MAX. 1.65 m (5.41 ft)

MIN. 1.41 m (4.63 ft)

NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01

01

01

0101

MAX = 6.11 m (20.05 ft)MIN = 5.82 m (19.09 ft)

MAX. 6.91 m (22.67 ft)MIN. 6.62 m (21.72 ft)

F_AC_020700_1_0530101_01_00

Door ClearancesAPU and Nose Landing Gear Doors

FIGURE-2-7-0-991-053-A01

2-7-0Page 18

Jul 01/21


**ON A/C A340-600

FR94

NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.

FWD

MAX. 6.03 m (19.78 ft)MIN. 5.71 m (18.73 ft)

MAX. 6.82 m (22.38 ft)MIN. 6.50 m (21.33 ft)

MAX. 1.67 m (5.48 ft)MIN. 1.43 m (4.69 ft)

MAX. 2.2 m (7.23 ft)MIN. 1.96 m (6.43 ft) 01

01

01

01

01

FR98

F_AC_020700_1_0540101_01_00

Door ClearancesAPU and Nose Landing Gear Doors

FIGURE-2-7-0-991-054-A01

2-7-0Page 19

Jul 01/21


2-8-0 Escape Slides

**ON A/C A340-500 A340-600

Escape Slides

1. GeneralThis section provides the location of the cabin escape facilities and their related clearances.

**ON A/C A340-500

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.

**ON A/C A340-600

3. 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 dual lane escape slide-raft at each emergency exit door (total two).The slides are installed in a container in the lower part of the door.

B. Off-Wing Escape Facility- One single lane escape slide at each overwing emergency-exit door (total two).The escape slide is installed in the left and right belly fairing above, and AFT of the wingtrailing edge, between FR53.2 and FR53.4.

2-8-0Page 1

Jul 01/21


**ON A/C A340-500

FWD CABIN DUAL−LANEESCAPE SLIDE/RAFT

MID CABIN DUAL−LANEESCAPE SLIDE/RAFT

AFT CABIN DUAL−LANEESCAPE SLIDE/RAFT

COCKPITESCAPE ROPE

EMERGENCY EXITSINGLE−LANEESCAPE SLIDE

NOTE:LH SHOWN, RH SYMMETRICAL. F_AC_020800_1_0050101_01_01

Escape SlidesLocation (Sheet 1 of 2)

FIGURE-2-8-0-991-005-A01

2-8-0Page 2

Jul 01/21


**ON A/C A340-500

GR

ID E

QU

ALS

1 m

(3.

28 ft

) IN

RE

ALI

TY

0 −3

−6

−9

−1

2

−1

5

−2

1

−1

8

−2

4

−2

7

−3

0

−3

3

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_0050102_01_01F_AC_020800_1_0050102_01_01

Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-005-A01

2-8-0Page 3

Jul 01/21


**ON A/C A340-600

COCKPITESCAPE ROPE

FWD CABIN DUAL−LANEESCAPE SLIDE/RAFT

MID CABIN DUAL−LANEESCAPE SLIDE/RAFT

EMERGENCY EXITDUAL−LANE

ESCAPE SLIDE/RAFT

AFT CABIN DUAL−LANEESCAPE SLIDE/RAFT

OFFWING SINGLE−LANEESCAPE SLIDE

NOTE:LH SHOWN, RH SYMMETRICAL. F_AC_020800_1_0050201_01_01

Escape SlidesLocation (Sheet 1 of 2)

FIGURE-2-8-0-991-005-B01

2-8-0Page 4

Jul 01/21


**ON A/C A340-600

GR

ID E

QU

ALS

1 m

(3.

28 ft

) IN

RE

ALI

TY

0 −3

−6

−9

−1

2

−1

5

−2

1

−1

8

−2

4

−2

7

−3

0

−3

3

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_0050202_01_01

Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-005-B01

2-8-0Page 5

Jul 01/21


2-9-0 Landing Gear

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-600

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

3.34

m(1

0.96

ft)

8.44

m(2

7.69

ft)

3.89

m(1

2.76

ft)

6.31

m(2

0.7

ft)

5.34

m(1

7.52

ft)

41.5

9 m

(136

.45

ft)

39.0

1 m

(127

.99

ft)

32.8

9 m

(107

.91

ft)

3.55

m(1

1.65

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_0050101_01_00

Landing Gear Maintenance PitsMaintenance Pit Envelopes (Sheet 1 of 2)

FIGURE-2-9-0-991-005-A01

2-9-0Page 2

Jul 01/21


**ON A/C A340-600

MA

IN L

AN

DIN

G G

EA

R

7.2

m(2

3.62

ft)

FU

SE

LAG

E H

OR

IZO

NT

AL

DA

TU

M

(126

.71

ft)38

.62

m

40.4

7 m

(132

.78

ft)

FR

ON

T O

F N

OS

E R

AD

OM

E

6.58

m(2

1.59

ft)

0.98

m

0.86

m

2.01

m(6

.59

ft)

2. IN

BO

AR

D E

DG

E O

F P

IT D

EF

INE

D B

Y T

HE

PO

SIT

ION

OF

TH

E O

PE

N B

ELL

Y F

AIR

ING

DO

OR

.1.

OU

TB

OA

RD

ED

GE

OF

PIT

DE

FIN

ED

BY

ZE

RO

CLE

AR

AN

CE

TO

OU

TB

OA

RD

GR

OW

N T

IRE

S.

3. D

EP

TH

OF

TH

E P

IT IS

TH

E S

AM

E A

S A

340−

300

ME

AS

UR

ED

FR

OM

TH

E F

US

ELA

GE

HO

RIZ

ON

TA

L D

AT

UM

.4.

NO

PIT

IS R

EQ

UIR

ED

FO

R N

OS

E L

AN

DIN

G G

EA

R O

R C

EN

TE

R L

AN

DIN

G G

EA

R.

NO

TE

:

(3.2

2 ft)

(2.8

2 ft)

F_AC_020900_1_0050102_01_00


FIGURE-2-9-0-991-005-A01

2-9-0Page 3

Jul 01/21


**ON A/C A340-500

3.34

m(1

0.96

ft)

8.44

m(2

7.69

ft)

3.89

m(1

2.76

ft)

6.31

m(2

0.7

ft)

5.34

m(1

7.52

ft)

36.2

9 m

(119

.06

ft)

33.7

m(1

10.5

6 ft)

27.5

9 m

(90.

52 ft

)

3.55

m(1

1.65

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_0050201_01_00


FIGURE-2-9-0-991-005-B01

2-9-0Page 4

Jul 01/21


**ON A/C A340-500

MA

IN L

AN

DIN

G G

EA

R

7.2

m(2

3.62

ft)

FU

SE

LAG

E H

OR

IZO

NT

AL

DA

TU

M

(109

.32

ft)33

.32

m

35.1

7 m

(115

.39

ft)

FR

ON

T O

F N

OS

E R

AD

OM

E

6.58

m(2

1.59

ft)

0.98

m

0.86

m

2.01

m(6

.59

ft)(3

.22

ft)

(2.8

2 ft)

2. IN

BO

AR

D E

DG

E O

F P

IT D

EF

INE

D B

Y T

HE

PO

SIT

ION

OF

TH

E O

PE

N B

ELL

Y F

AIR

ING

DO

OR

.1.

OU

TB

OA

RD

ED

GE

OF

PIT

DE

FIN

ED

BY

ZE

RO

CLE

AR

AN

CE

TO

OU

TB

OA

RD

GR

OW

N T

IRE

S.

3. D

EP

TH

OF

TH

E P

IT IS

TH

E S

AM

E A

S A

340−

300

ME

AS

UR

ED

FR

OM

TH

E F

US

ELA

GE

HO

RIZ

ON

TA

L D

AT

UM

.4.

NO

PIT

IS R

EQ

UIR

ED

FO

R N

OS

E L

AN

DIN

G G

EA

R O

R C

EN

TE

R L

AN

DIN

G G

EA

R.

NO

TE

:

F_AC_020900_1_0050202_01_00


FIGURE-2-9-0-991-005-B01

2-9-0Page 5

Jul 01/21


**ON A/C A340-500 A340-600

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 four wheel bogie assembly and related doors,- A Nose Landing Gear (NLG) with twin wheel assembly and related doors.

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 has a four-wheel bogie beam 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

Jul 01/21


- Two hydraulically-operated center doors (each door includes a manually-operated maintenancedoor attached with hinges to the rear of the center door),

- A fairing door attached to the CLG leg, and an articulated door attached with a hinge to thefairing door.

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 service panel, see FIGURE 2-9-0-991-017-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.

8. Landing Gear Control

2-9-0Page 7

Jul 01/21


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-hydraulic free-fall-system. A switch in the cockpit disengage the doors and the landing gear uplocks. The landinggears then extend by free-fall, and lock down.

9. Braking

A. GeneralCarbon multi-disc brakes are installed on each wheel of the MLG and the CLG. Each brakeassembly has two wear 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 and CLG 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,- The Landing GearAMM 32-69-00.

2-9-0Page 8

Jul 01/21


**ON A/C A340-500 A340-600

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_0120101_01_00

Main Landing GearGeneral (Sheet 1 of 3)

FIGURE-2-9-0-991-012-A01

2-9-0Page 9

Jul 01/21


**ON A/C A340-500 A340-600

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_0120102_01_00

Main Landing GearSafety Devices (Sheet 2 of 3)FIGURE-2-9-0-991-012-A01

2-9-0Page 10

Jul 01/21


**ON A/C A340-500 A340-600

SEAL CHANGEOVERVALVE

BLEED/INFLATIONVALVE

D

E

F

FWD

FILL VALVE

GROUND POINT

F_AC_020900_1_0120103_01_00

Main Landing GearServicing (Sheet 3 of 3)

FIGURE-2-9-0-991-012-A01

2-9-0Page 11

Jul 01/21


**ON A/C A340-500 A340-600

CENTER DOORS

OPERATING ROD

FIXED FAIRING

CENTER DOOR

DOOR

BRAKE RODBOGIE BEAM ASSEMBLY

MAIN FITTING

RETRACTION ACTUATOR

BARREL

UPLOCK PIN

TRIANGULATION LINKS

ARTICULATION LINKS

SHOCK ABSORBER

A

A

MAINTENANCE DOOR

(HYDRAULICALLYOPERATED)

TORQUE LINKS

ASSEMBLY


AFT AXLE

FWD AXLE

B

B

C

E

FG

F_AC_020900_1_0130101_01_00

Centerline Landing GearGeneral (Sheet 1 of 3)

FIGURE-2-9-0-991-013-A01

2-9-0Page 12

Jul 01/21


**ON A/C A340-500 A340-600

C

DOWNLOCKSPRING

DOWNLOCKACTUATOR

UPPER DRAGSTAY

BRH SHOWN

LH SYMMETRICAL

D

GROUNDLOCK PIN

WARNINGFLAG

D

SAFETYCOLLAR

QUICK RELEASE PIN

WARNING FLAG

WARNING FLAG

QUICK RELEASE PIN

DOOR ACTUATOR

F_AC_020900_1_0130102_01_00

Centerline Landing GearSafety Devices (Sheet 2 of 3)FIGURE-2-9-0-991-013-A01

2-9-0Page 13

Jul 01/21


**ON A/C A340-500 A340-600

INFLATION VALVE(SECOND STAGE)

DRAIN PLUG

OIL FILL VALVE

SEAL CHANGEOVERVALVE

FWD

INFLATION VALVE(FIRST STAGE)

FWD F

E

G

F_AC_020900_1_0130103_01_00

Centerline Landing GearServicing (Sheet 3 of 3)

FIGURE-2-9-0-991-013-A01

2-9-0Page 14

Jul 01/21


**ON A/C A340-500 A340-600

RETRACTION DOWNLOCKACTUATOR

MAIN FITTING

TORQUE LINKS


TOWING BRACKET

SHOCK ABSORBER

AXLE

NWS ACTUATORS

DRAG STAY

EH

AFT DOOR(MECHANICALLY OPERATED)

FWD DOORS

A

(HYDRAULICALLY

AFT DOOR(MECHANICALLY

A

F

G

OPERATED)

ACTUATOR

C

OPERATED)

DOWNLOCKSPRINGS

D

B

F_AC_020900_1_0140101_01_00

Nose Landing GearGeneral (Sheet 1 of 4)

FIGURE-2-9-0-991-014-A01

2-9-0Page 15

Jul 01/21


**ON A/C A340-500 A340-600

DOWNLOCKACTUATOR

LUGS

DOWNLOCK SPRINGLOCATION

UPPERLOCK LINK

DRAG STAYLOCATION

LOWERLOCK LINK

GROUND LOCK PIN

CWARNING FLAG

BRH SHOWN

LH SYMMETRICAL

SAFETYCOLLAR

QUICK RELEASE PIN

WARNING FLAG

WARNING FLAG

QUICK RELEASE PIN

DOOR ACTUATOR

F_AC_020900_1_0140102_01_00

Nose Landing GearSafety Devices (Sheet 2 of 4)FIGURE-2-9-0-991-014-A01

2-9-0Page 16

Jul 01/21


**ON A/C A340-500 A340-600

TOP CHARGING

BOTTOMCHARGING

VALVE

INFLATION VALVE

E

VALVE

(FIRST STAGE)

D

F_AC_020900_1_0140103_01_00

Nose Landing GearServicing (Sheet 3 of 4)

FIGURE-2-9-0-991-014-A01

2-9-0Page 17

Jul 01/21


**ON A/C A340-500 A340-600

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_0140104_01_00

Nose Landing GearServicing and Steering Disconnection Box (Sheet 4 of 4)

FIGURE-2-9-0-991-014-A01

2-9-0Page 18

Jul 01/21


**ON A/C A340-500 A340-600

5GC

5GCB

TOW−TRUCK POWER CABLE

SAFETY PIN

ELECTRICALDEACTIVATION BOX

WARNING FLAG

CONNECTOR

FOR PIN ALLOCATIONSEE 05−04−04

A

A

F_AC_020900_1_0170101_01_01

Tow Truck PowerFIGURE-2-9-0-991-017-A01

2-9-0Page 19

Jul 01/21


2-10-0 Exterior Lighting

**ON A/C A340-500 A340-600

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)

17 (A340-600 only) FWD TAXI CAMERA LIGHTS

18 (A340-600 only) AFT TAXI CAMERA LIGHTS

2-10-0Page 1

Jul 01/21


**ON A/C A340-500

8

6

4

7

1 RH

2 LH

9

3

10

5

F_AC_021000_1_0060101_01_00

Exterior Lighting(Sheet 1 of 5)

FIGURE-2-10-0-991-006-A01

2-10-0Page 2

Jul 01/21


**ON A/C A340-500

14

13 12 11

NOTE:LIGHTS 13 AND 14 ARE THE SAME, BUT THEY OPERATE WITH DIFFERENT POWER SETTINGS.

F_AC_021000_1_0060102_01_00


FIGURE-2-10-0-991-006-A01

2-10-0Page 3

Jul 01/21


**ON A/C A340-500

21

7

1212

13

14

3

7

F_AC_021000_1_0060103_01_00


FIGURE-2-10-0-991-006-A01

2-10-0Page 4

Jul 01/21


**ON A/C A340-500

10

9 9

8

11 11

8

54

F_AC_021000_1_0060104_01_00


FIGURE-2-10-0-991-006-A01

2-10-0Page 5

Jul 01/21


**ON A/C A340-500

EXAMPLE FOR LIGHT N? 15

CEILING LIGHT

SPOT LIGHT

GROUND

6

6

15 16 15 16

F_AC_021000_1_0060105_01_00


FIGURE-2-10-0-991-006-A01

2-10-0Page 6

Jul 01/21


**ON A/C A340-600

1 RH

LH

6

4

87

9

2

3

10

17

5

18

18

F_AC_021000_1_0070101_01_00


FIGURE-2-10-0-991-007-A01

2-10-0Page 7

Jul 01/21


**ON A/C A340-600

12 11

14

13

NOTE:LIGHTS 13 AND 14 ARE THE SAME, BUT THEY OPERATE WITH DIFFERENT POWER SETTINGS.

F_AC_021000_1_0070102_01_00


FIGURE-2-10-0-991-007-A01

2-10-0Page 8

Jul 01/21


**ON A/C A340-600

21

7

13

12 12

7

14

3

F_AC_021000_1_0070103_01_00


FIGURE-2-10-0-991-007-A01

2-10-0Page 9

Jul 01/21


**ON A/C A340-600

9 9

10

4 5

88

11 11

F_AC_021000_1_0070104_01_00


FIGURE-2-10-0-991-007-A01

2-10-0Page 10

Jul 01/21


**ON A/C A340-600

EXAMPLE FOR LIGHT N? 15

CEILING LIGHT

SPOT LIGHT

GROUND

6

6

15 16 15 16

F_AC_021000_1_0070105_01_00


FIGURE-2-10-0-991-007-A01

2-10-0Page 11

Jul 01/21


**ON A/C A340-600

17

18 18

17

F_AC_021000_1_0070106_01_00


FIGURE-2-10-0-991-007-A01

2-10-0Page 12

Jul 01/21


2-11-0 Antennas and Probes Location

**ON A/C A340-500 A340-600

Antennas and Probes Location

1. This section gives the location of antennas and probes.

2-11-0Page 1

Jul 01/21


**ON A/C A340-500

VH

F(1

)

ELT

VH

F(3

)

TC

AS

TO

P

GP

S(1

)

GP

S(2

)

ST

AT

IC P

RO

BE

(2)

ST

AT

IC P

RO

BE

(1)

TA

T P

RO

BE

AO

A S

EN

SO

R(1

)A

TC

(4)

EM

ER

GE

NC

Y S

TA

TIC

PR

OB

E(3

)H

F

RA

DIO

ALT

IME

TE

R(2

)

RA

DIO

ALT

IME

TE

R(1

)

VH

F(4

)M

AR

KE

R

GLI

DE

TR

AC

K

LOCGLI

DE

CA

PT

UR

ETC

AS

BO

TT

OM

AT

C(1

)

WE

AT

HE

R R

AD

AR

DM

E(1

)

DM

E(2

)

PIT

OT

PR

OB

E(1

)

PIT

OT

PR

OB

E(3

)

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0060101_01_00

Antennas and ProbesLocation (Sheet 1 of 2)

FIGURE-2-11-0-991-006-A01

2-11-0Page 2

Jul 01/21


**ON A/C A340-500

VO

R

AD

F(2

)A

DF

(1)

SA

TC

OM

AO

A S

EN

SO

R(3

) S

TB

Y

ST

AT

IC P

RO

BE

(1)

VH

F(2

)

AT

C(2

)

ST

AT

IC P

RO

BE

(2)

EM

ER

GE

NC

Y S

TA

TIC

PR

OB

E(3

)

TA

T P

RO

BE

PIT

OT

PR

OB

E(2

)

AT

C(3

)

AO

A S

EN

SO

R(2

)

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0060102_01_00


FIGURE-2-11-0-991-006-A01

2-11-0Page 3

Jul 01/21


**ON A/C A340-600

GP

S(1

)

GP

S(2

)

TC

AS

TO

P

VH

F(1

)A

TC

(4)

WE

AT

HE

R R

AD

AR

VH

F(3

)E

LT

HF

RA

DIO

ALT

IME

TE

R(2

)

RA

DIO

ALT

IME

TE

R(1

)

VH

F(4

)M

AR

KE

RD

ME

(2)

DM

E(1

)

AT

C(1

)

PIT

OT

PR

OB

E(3

)

PIT

OT

PR

OB

E(1

)

GLI

DE

CA

PT

UR

E

TA

T P

RO

BE

GLI

DE

TR

AC

K

TC

AS

BO

TT

OM

AO

A S

EN

SO

R(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)

LOC

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0070101_01_00


FIGURE-2-11-0-991-007-A01

2-11-0Page 4

Jul 01/21


**ON A/C A340-600

AD

F(2

)

AD

F(1

)

VO

R

PIT

OT

PR

OB

E(2

)

TA

T P

RO

BE

ST

AT

IC P

RO

BE

(2)

ST

AT

IC P

RO

BE

(1)

VH

F(2

)A

TC

(2)

EM

ER

GE

NC

Y S

TA

TIC

PR

OB

E(3

)

AT

C(3

)

AO

A S

EN

SO

R(3

) S

TB

Y

SA

TC

OM

AO

A S

EN

SO

R(2

)

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0070102_01_00


FIGURE-2-11-0-991-007-A01

2-11-0Page 5

Jul 01/21


2-12-0 Engine and Nacelle

**ON A/C A340-500 A340-600

Engine and Nacelle

1. Engine and Nacelle -- TRENT 500 Engine

A. EngineThe RB211-TRENT 500 engine is a high bypass ratio, triple spool turbofan.The principal modules of the engine are:- The Low Pressure Compressor (LPC) rotor- The Intermediate Pressure (IP) compressor- The intermediate case- The HP system (this includes the High Pressure Compressor (HPC), the combustion system

and the High Pressure Turbine (HPT))- The IP turbine- The external gearbox.

The compressor system has three axial flow compressors in a triple spool configuration. Thecompressors are turned independently by their related turbines, each at its most satisfactoryspeed. The LP system has a single-stage compressor installed at the front of the engine. Ashaft connects the compressor to a five-stage turbine at the rear of the gas generator. Thegas generator also includes an eight-stage IP compressor, a six-stage HPC and a combustionsystem. Each of the compressors in the gas generator is connected to, and turned by, adifferent single-stage turbine. Between the HPC and the HPT is the annular combustionsystem which burns a mixture of fuel and air to supply energy as heat. Behind the LPturbine there is a collector nozzle assembly through which the hot gas exhaust flows. Theexternal gearbox module is installed below the fan case. It has a gear train that decreasesand increases the speed to meet the specified drive requirements of each accessory.

B. NacelleA nacelle gives the engine an aerodynamic shape and supports the thrust reverser system. Eachengine is housed in a nacelle suspended from a pylon attached below the wing. The nacelleconsists of the following major components:

(1) Air Intake Cowl AssemblyThe air intake cowl is an interchangeable aerodynamic cowl installed at the front of theengine. It ducts airflow to the fan and the engine core. The cowl has panels for easy accessto the components. Acoustic materials are used in the manufacture of the cowl to helpdecrease the engine noise.

(2) Fan Cowl AssemblyThe fan cowl assembly has two semicircular panels, the left fan cowl and the right fancowl, that enclose the engine fan case between the air intake cowl and the thrust reverser.There are four assemblies for each aircraft. Each fan cowl panel is interchangeable fromone engine to a different engine, when the strakes are removed or installed.

2-12-0Page 1

Jul 01/21


(3) Thrust ReverserThe thrust reverser is a component of the aircraft engine nacelle. The thrust reverser is aconventional fixed-cascade, translating-cowl type. The thrust reverser provides anaerodynamic flow path and uses the outer mobile structure, which is hydraulically powered,to provide a fan exhaust duct and a nozzle exit. In stow mode, the thrust reverser is anaerodynamic structure. In reverse mode, it is used to deflect and redirect part of the enginefan exhaust air by the blocker doors and in a forward direction through the cascades. Thethrust reverser increases the aircraft wheel braking and the speed braking systems toreduce the landing distance.

(4) Exhaust SystemThe turbine exhaust system consists of one exhaust nozzle and one exhaust plug. Theexhaust nozzle is bolted to the engine low pressure turbine frame flange outer flange. It isacoustically treated. The exhaust plug is bolted to the engine low pressure turbine frameflange inner flange. It is a two-piece conical structure. The turbine exhaust flow path isformed by the inner wall of the exhaust nozzle and the outer wall of the exhaust plug.

2-12-0Page 2

Jul 01/21


**ON A/C A340-500 A340-600

1.29 m(4.23 ft)

SECTIONACCESSORY DRIVE

A

1.15 m(3.77 ft)

NOZZLEEXHAUST

LP TURBINE

HP COMPRESSOR0.67 m(2.2 ft)

LP COMPRESSORIP COMPRESSOR

1.38 m(4.53 ft)

4.59 m(15.06 ft)

PLUG

1.56 m(5.12 ft)

HP TURBINE

IP TURBINE

SECTIONCOMBUSTION

0.73 m(2.4 ft)

NOTE:APPROXIMATE DIMENSIONS

1.03 m(3.38 ft)

0.69 m(2.26 ft)

2.87 m(9.42 ft)

2.62 m(8.6 ft)

A

B

B

FWD

F_AC_021200_1_0210101_01_00

Engine and NacelleEngine Dimensions - TRENT 500

FIGURE-2-12-0-991-021-A01

2-12-0Page 3

Jul 01/21


**ON A/C A340-500 A340-600

D

D

C

C

W

U

V

DISTANCEFROM THE

NOSE

AIR INTAKE

1.64 m

FAN COWL

1.67 m

THRUSTREVERSER

1.69 m

EXHAUSTNOZZLE

1.41 m

PLUG

1.15 m

1.63 m(5.35 ft)

(5.38 ft) (5.48 ft) (5.54 ft) (4.63 ft) (3.77 ft)

W U V

A−A

B−B

C−C

D−D

E−E

1.49 m(4.89 ft)

3.14 m(10.3 ft)

2.69 m(8.83 ft)

1.51 m(4.95 ft)

1.35 m(4.43 ft)

1.34 m(4.4 ft)

0.78 m(2.56 ft)

0.67 m(2.2 ft)

1.63 m(5.35 ft)

0.75 m(2.46 ft)

0.67 m(2.2 ft)

A

A B

B

E

E


DISTANCE FROMTHE NOSE A340−600 A340−500

(89.63 ft)27.32 m

(72.24 ft)22.02 m

(111.38 ft)33.95 m

(94.03 ft)28.66 m

INBOARDENGINE

OUTBOARDENGINE

COWL

3.14 m(10.3 ft)

1.49 m(4.89 ft)

1.63 m(5.35 ft)

1.34 m(4.4 ft)

F_AC_021200_1_0220101_01_00

Engine and NacelleNacelle Dimensions - TRENT 500

FIGURE-2-12-0-991-022-A01

2-12-0Page 4

Jul 01/21


**ON A/C A340-500 A340-600

A/CCONFIGURATION

OEW

MTW

DIM."A"

INBOARD ENG. OUTBOARD ENG.

0.71 m(2.33 ft)

1.75 m(5.74 ft)

INBOARD ENG.

0.52 m(1.71 ft)

1.56 m(5.12 ft)

DIM."B"

55?

38?

55?

DIM."C" DIM."D"

38?

OUTBOARD ENG.

38?

55?

5.41 m(17.75 ft)

6.12 m(20.08 ft)

2.15 m(7.05 ft)

2.78 m(9.12 ft)

1.36 m(4.46 ft)

2.03 m(6.66 ft)

1.17 m(3.84 ft)

1.84 m(6.04 ft)

2.4 m(7.87 ft)

3.07 m(10.07 ft)

2.21 m(7.25 ft)

2.88 m(9.45 ft)

?

?

A

?

GROUND

C

D

B

FOR OTHER VALUES OF DIM. "D" REFER TO CHAPTER 2−3.


F_AC_021200_1_0230101_01_00

Engine and NacelleFan Cowls - TRENT 500

FIGURE-2-12-0-991-023-A01

2-12-0Page 5

Jul 01/21


**ON A/C A340-500 A340-600

A/CCONFIGURATION

OEW

MTW

DIM."A"

INBOARD ENG. OUTBOARD ENG.

0.71 m(2.33 ft)

1.75 m(5.74 ft)

INBOARD ENG.

0.52 m(1.71 ft)

1.56 m(5.12 ft)

45?

33?

45?

DIM."B" DIM."C"

33?

OUTBOARD ENG.

33?

45?

4.92 m(16.14 ft)

5.5 m(18.04 ft)

1.04 m(3.41 ft)

1.4 m(4.59 ft)

0.85 m(2.79 ft)

1.21 m(3.97 ft)

2.08 m(6.82 ft)

2.44 m(8.01 ft)

1.89 m(6.2 ft)

2.25 m(7.38 ft)

?

?

A

?

GROUND

C

FOR OTHER VALUES OF DIM. "C" REFER TO CHAPTER 2−3.


B

F_AC_021200_1_0240101_01_00

Engine and NacelleThrust Reverser Cowls - TRENT 500

FIGURE-2-12-0-991-024-A01

2-12-0Page 6

Jul 01/21


2-12-1 Auxiliary Power Unit

**ON A/C A340-500 A340-600

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) 331-600A 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 APU has a gearbox-driven oil-cooled AC generator.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.

2-12-1Page 1

Jul 01/21


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

Jul 01/21


**ON A/C A340-500 A340-600

Z310

A B FR100

FR99

FR98

FR94

FR93

FR92

FR91 317BL

315AL

313BL

A

316AR

F_AC_021201_1_0020201_01_00

Auxiliary Power UnitAccess Doors (Sheet 1 of 2)FIGURE-2-12-1-991-002-B01

2-12-1Page 3

Jul 01/21


**ON A/C A340-500 A340-600

FR90

FR92

FR94

FR98

FR100

FIRE EXTINGUISHERBOTTLE

AIR INTAKE DUCT

APU

BLEED AIR LINE

OIL COOLER

EXHAUST MUFFLER

FIXED DIVERTERGUTTER

OUTLET

FIRE WALLFORWARD

FIRE WALLREARAIR INTAKE

B

F_AC_021201_1_0020202_01_00

Auxiliary Power UnitGeneral Layout (Sheet 2 of 2)FIGURE-2-12-1-991-002-B01

2-12-1Page 4

Jul 01/21


2-13-0 Levelling, symmetry and Alignment

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-500

FR57 FR58

RIB12

RIB12

FR37.11 FR37.12

2 LH 13

2 RH

12

F_AC_021300_1_0060101_01_00

Location of Leveling PointsFIGURE-2-13-0-991-006-A01

2-13-0Page 2

Jul 01/21


**ON A/C A340-600

FR37.11 FR37.12

FR57.4 FR58

RIB12

RIB12

132 LH

12

2 RH

F_AC_021300_1_0070101_01_00

Location of Leveling PointsFIGURE-2-13-0-991-007-A01

2-13-0Page 3

Jul 01/21


2-14-0 Jacking for Maintenance

**ON A/C A340-500 A340-600

Jacking for Maintenance

1. Aircraft Jacking Points for Maintenance

A. General

(1) The A340-500/-600 can be jacked:- At not more than 200 000 kg (440 924 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 is provided with three primary jacking points:- One located under the forward fuselage (after FR10),- 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 FR87 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 2-14-0-991-015-AFIGURE2-14-0-991-015-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 DatumLine (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

Jul 01/21


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

Jul 01/21


**ON A/C A340-500

SAFETY STAY

WING JACKINGPOINT

C

B’

B

FORWARD FUSELAGEJACKING POINT A

3.34 10.96 0

8.44

−8.44

0

0

27.69

−27.69

0

MAXIMUMLOAD ELIGIBLE

m ft daN

YX

m ft

33.71

33.71

60.05

110.56

110.56

197.01

17 273

95 505

95 505

4 775

FWD JACKINGPOINT

SAFETYSTAY

X

NOTE:SAFETY STAY IS NOT USED FOR JACKING.

BWING JACKING

POINT

B’

WING JACKINGPOINT

Y

CA

F_AC_021400_1_0150101_01_00

Jacking for MaintenanceJacking Points Location

FIGURE-2-14-0-991-015-A01

2-14-0Page 3

Jul 01/21


**ON A/C A340-600

SAFETY STAY

WING JACKINGPOINT

C

B’

B

FORWARD FUSELAGEJACKING POINT A

3.34 10.96 0

8.44

−8.44

0

0

27.69

−27.69

0

MAXIMUMLOAD ELIGIBLE

m ft daN

YX

m ft

39.01

39.01

67.48

127.99

127.99

221.39

17 971

96 105

96 105

4 805

NOTE:SAFETY STAY IS NOT USED FOR JACKING.

FWD JACKINGPOINT

BWING JACKING

POINT

B’

WING JACKINGPOINT

YSAFETY

STAY

C

X

A

F_AC_021400_1_0150201_01_00

Jacking for MaintenanceJacking Points Location

FIGURE-2-14-0-991-015-B01

2-14-0Page 4

Jul 01/21


**ON A/C A340-500 A340-600

Z −2123.06

Z −2101.26

SPHERICALRADIUS 19 mm (0.75 in)

A

FR10

FWD

A

FR10

B

ADAPTOR −JACK NOSE

B

F_AC_021400_1_0160101_01_00

Jacking for MaintenanceForward Jacking Point

FIGURE-2-14-0-991-016-A01

2-14-0Page 5

Jul 01/21


**ON A/C A340-500 A340-600

LOWER SURFACE

EXAMPLE

Z −816.2

Z −726.5

SPHERICALRADIUS 32 mm

(1.26 in)

JACKING PADSET−WING

OUTER SKIN

RIB10OUTER SKIN

B

B

A

DATUM INTERSECTIONAT MID REAR SPAR DATUM

ARIB10

A

RIB10

F_AC_021400_1_0170101_01_00

Jacking for MaintenanceWing Jacking Points

FIGURE-2-14-0-991-017-A01

2-14-0Page 6

Jul 01/21


**ON A/C A340-500 A340-600

ADAPT−SUPP, AFT JACK

SPHERICALRADIUS 19 mm (0.75 in)

Z −117.72

Z −84.42

A

FR87

B

B

FWD

A

FR87

F_AC_021400_1_0180101_01_00

Jacking for MaintenanceAuxiliary Jacking Point - Safety Stay

FIGURE-2-14-0-991-018-A01

2-14-0Page 7

Jul 01/21


**ON A/C A340-500

L

AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 200 000 kg (440 924 lb)

2.74 m(8.99 ft)

4.56 m(14.96 ft)

5.6 m(18.37 ft)

AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES

2.22 m(7.28 ft)

4.01 m(13.16 ft)

5.04 m(16.54 ft)

AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6.5 m (21.33 ft) FOR LANDINGGEARS EXTENSION/RETRACTION

4.42 m(14.5 ft)

5.77 m(18.93 ft)

6.42 m(21.06 ft)

AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7.2 m (23.62 ft) FOR LANDINGGEARS REMOVAL/INSTALLATION

5.12 m(16.8 ft)

6.47 m(16.8 ft)

7.12 m(16.8 ft)

L M N

AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 175 377 kg (386 640 lb)

2.74 m(8.99 ft)

4.56 m(14.96 ft)

5.6 m(18.37 ft)

FUSELAGE

N

DATUM LINE

M

F_AC_021400_1_0190101_01_00

Jacking for MaintenanceJacking Dimensions

FIGURE-2-14-0-991-019-A01

2-14-0Page 8

Jul 01/21


**ON A/C A340-600

AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 200 000 kg (440 924 lb)

2.75 m(9.02 ft)

4.56 m(14.96 ft)

5.57 m(18.27 ft)

AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES

2.22 m(7.28 ft)

4.01 m(13.16 ft)

5 m(16.4 ft)

AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6.5 m (21.33 ft) FOR LANDINGGEARS EXTENSION/RETRACTION

4.42 m(14.5 ft)

5.77 m(18.93 ft)

6.42 m(21.06 ft)

AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7.2 m (23.62 ft) FOR LANDINGGEARS REMOVAL/INSTALLATION

5.12 m(16.8 ft)

6.47 m(21.23 ft)

7.12 m(23.36 ft)

L M N

AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 181 606 kg (400 373 lb)

2.75 m(9.02 ft)

4.56 m(14.96 ft)

5.46 m(17.91 ft)

FUSELAGE

N

DATUM LINE

M

L

F_AC_021400_1_0190201_01_00

Jacking for MaintenanceJacking Dimensions

FIGURE-2-14-0-991-019-B01

2-14-0Page 9

Jul 01/21


**ON A/C A340-500

130

140

150

160

170

180

190

200

0 6 8 10 12 14 16 18 20

140

150

160

170

180

190

200

210

220

230

3025

20

5020 30 40 50 60 70

2 4

220

230

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 23% RC . THE REACTION AT THE WING JACKING POINTS IS 140 000 kg(70 000 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINTIS 12 000 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT

ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 152 000 kg AND CENTER OF GRAVITYAB

CD

BE IN EXCESS OF 70 km/h.

3540

210

22 24

100

110

120

130

90

80 90

15

A

C

45

TIP UPSECURITYMARGIN

B

D

F_AC_021400_1_0200101_01_00

Jacking for MaintenanceLoad at the Aircraft Jacking Points

FIGURE-2-14-0-991-020-A01

2-14-0Page 10

Jul 01/21


**ON A/C A340-600

130

140

150

160

170

180

190

200

0 6 8 10 12 14 16 18 20

140

150

160

170

180

190

200

210

220

230

3025

20

20 30 40 50 60 70

2 4

220

230

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)

EXAMPLE:

AT 23% RC . THE REACTION AT THE WING JACKING POINTS IS 134 000 kg(67 000 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINTIS 9 600 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT

ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 143 500 kg AND CENTER OF GRAVITYAB

CD

BE IN EXCESS OF 60 km/h.

35

210

22 24100

110

120

130

15

45

10

A

B

D

40AIRCRAFT CG (%RC)50

C

TIP UPSECURITYMARGIN

F_AC_021400_1_0200201_01_00

Jacking for MaintenanceLoad at the Aircraft Jacking Points

FIGURE-2-14-0-991-020-B01

2-14-0Page 11

Jul 01/21


2-14-1 Jacking of the Landing Gear

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-500 A340-600

1

2

3

4A

5A

5B

6A

6B

7

4B

CONFIGURATION

3 DEFLATED TIRES

3 RIMS

4 RIMS

4 INFLATED TIRES

4 DEFLATED TIRES

MAXIMUM JACKING HEIGHTTO CHANGE WHEELS

1 DEFLATED TIREON ANY AXLE

2 DEFLATED TIRES ONDIFFERENT AXLES

2 DEFLATED TIRES ONTHE SAME AXLE

2 RIMS ON THE SAME AXLE

DIM.A DIM.B DIM.C COMMENTS

DIM "A" DEFINED WITHFLANGES WORN BY 50%

WITH 25.4 mm (1 in)GROUND CLEARANCE

ONLY FLAT TIREDATA AVAILABLE




MLG JACKING

NOTE:VALUES WITH 1 400 x 530 R23 TIRES ONLY.

367 mm(14.45 in)

279 mm(10.98 in)

279 mm(10.98 in)

165 mm(6.5 in)

100 mm(3.94 in)

178 mm(7 in)

113 mm(4.45 in)

192 mm(7.56 in)

134 mm(5.28 in)

570 mm(22.44 in)

> 697 mm(27.44 in)

347 mm(13.66 in)

> 697 mm(27.44 in)

> 697 mm(27.44 in)

> 697 mm(27.44 in)

> 697 mm(27.44 in)

> 697 mm(27.44 in)

> 697 mm(27.44 in)

> 697 mm(27.44 in)

> 697 mm(27.44 in)

842 mm(33.15 in)

347 mm(13.66 in)

347 mm(13.66 in)

347 mm(13.66 in)

347 mm(13.66 in)

347 mm(13.66 in)

347 mm(13.66 in)

347 mm(13.66 in)

347 mm(13.66 in)

347 mm(13.66 in)

A

B

C A

F_AC_021401_1_0110102_01_00

Jacking of the Landing GearMLG Jacking Point HeightsFIGURE-2-14-1-991-011-A01

2-14-1Page 2

Jul 01/21


**ON A/C A340-500 A340-600

1 FLAT TIRE137.5 mm(5.41 in)180 mm MAX

(7.09 in)

(1 in)25.4 mm310 mm

(12.2 in) FWD

700 mm(27.56 in)

F_AC_021401_1_0120101_01_00

Jacking of the Landing GearJacking of the NLG (Sheet 1 of 2)

FIGURE-2-14-1-991-012-A01

2-14-1Page 3

Jul 01/21


**ON A/C A340-500 A340-600

CONFIGURATION DIM.A DIM.B COMMENTS



NLG JACKING

ON 2 RIMS

N/A

2 DEFLATED TIRES

1 DEFLATED TIRE

2 INFLATED TIRES340 mm

(13.39 in)1

2

3

4

5

A

B

NOTE:VALUES WITH 45 x 18 R17 TIRES ONLY.

183 mm(7.2 in)

255 mm(10.04 in)

244 mm(9.61 in)

475 mm(18.7 in)

382 mm(15.04 in)

275 mm(10.83 in)

249 mm(9.8 in)

304 mm(11.97 in)


F_AC_021401_1_0120102_01_00

Jacking of the Landing GearNLG Jacking Point Heights (Sheet 2 of 2)

FIGURE-2-14-1-991-012-A01

2-14-1Page 4

Jul 01/21


**ON A/C A340-500 A340-600

C

B

AA

1

2

3

4A

5A

5B

6A

6B

7

4B

CONFIGURATION

3 DEFLATED TIRES

3 RIMS

4 RIMS

4 INFLATED TIRES

4 DEFLATED TIRES


1 DEFLATED TIREON ANY AXLE

2 DEFLATED TIRES ONDIFFERENT AXLES

2 DEFLATED TIRES ONTHE SAME AXLE

2 RIMS ON THE SAME AXLE

DIM.A DIM.B DIM.C COMMENTS







CLG JACKING

380 mm(14.96 in)

292 mm(11.5 in)

199 mm(7.83 in)

134 mm(5.28 in)

212 mm(8.35 in)

147 mm(5.79 in)

226 mm(8.9 in)

168 mm(6.61 in)

653 mm(25.71 in)

> 476 mm(18.74 in)

621 mm(24.45 in)

292 mm(11.5 in)

> 476 mm(18.74 in)

> 476 mm(18.74 in)

> 476 mm(18.74 in)

> 476 mm(18.74 in)

> 476 mm(18.74 in)

> 476 mm(18.74 in)

> 476 mm(18.74 in)

> 476 mm(18.74 in)

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

N/A

NOTE:VALUES WITH 1 400 x 530 R23 TIRES ONLY. F_AC_021401_1_0130101_01_00

Jacking of the Landing GearCLG Jacking Point Heights

FIGURE-2-14-1-991-013-A01

2-14-1Page 5

Jul 01/21


**ON A/C A340-600

AIRCRAFT GROSS WEIGHT

(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)

400 450 500 550 600 650 700 750 800

45

35

15

5

25

10

20

30

40

91

81

71

61

51

41

31

21

11160 180 200 220 240 260 280 300 320 340 360 380

25% MAC34.4% MAC38% MAC

16% MACCG POSITION

F_AC_021401_1_0140101_01_00

Jacking of the Landing GearNLG Jacking Point Loads - (WV 001)

FIGURE-2-14-1-991-014-A01

2-14-1Page 6

Jul 01/21


**ON A/C A340-600


800750700400 450 500 550

160 180 200 220 2405

10

15

20

25

260

600

(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)

21

31

51

61

71

81

91

280

650

11300 320 340 360 380

30

35

45

40

41

25% MAC30.2% MAC38.2% MAC

16% MACCG POSITION

F_AC_021401_1_0150101_01_00


FIGURE-2-14-1-991-015-A01

2-14-1Page 7

Jul 01/21


**ON A/C A340-600


800750700400 450 500 550

160 180 200 220 24055

65

75

85

95

105

115

260

600

(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)

141

161

181

201

221

241

261

280

650

121

125

300 320 340 360 380

25% MAC34.4% MAC38% MAC

16% MACCG POSITION

F_AC_021401_1_0160101_01_00

Jacking of the Landing GearMLG Jacking Point Loads - (WV 001)

FIGURE-2-14-1-991-016-A01

2-14-1Page 8

Jul 01/21


**ON A/C A340-600


800750700400 450 500 550

160 180 200 220 24055

65

75

85

95

105

115

260

600

(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)

141

161

181

201

221

241

261

280

650

121

125

300 320 340 360 380

25% MAC30.2% MAC38.2% MAC

16% MACCG POSITION

F_AC_021401_1_0170101_01_00


FIGURE-2-14-1-991-017-A01

2-14-1Page 9

Jul 01/21


**ON A/C A340-600


800750700400 450 500 550

160 180 200 220 24020

30

40

50

60

70

100

260

600

(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)

64

84

104

124

144

164

184

204

224

280

650

44

110

300 320 340 360 380

25% MAC34.4% MAC38% MAC

16% MACCG POSITION

80

90

F_AC_021401_1_0180101_01_00

Jacking of the Landing GearCLG Jacking Point Loads - (WV 001)

FIGURE-2-14-1-991-018-A01

2-14-1Page 10

Jul 01/21


**ON A/C A340-600


800750700400 450 500 550

160 180 200 220 24020

30

40

50

60

70

100

260

600

(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)

64

84

104

124

144

164

184

204

224

280

650

44

110

300 320 340 360 380

25% MAC30.2% MAC38.2% MAC

16% MACCG POSITION

80

90

F_AC_021401_1_0190101_01_00


FIGURE-2-14-1-991-019-A01

2-14-1Page 11

Jul 01/21


**ON A/C A340-500


800750700400 450 500 550

160 180 200 220 24010

15

20

25

30

260

600

(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)

32

42

52

62

72

82

92

280

650

22300 320 340 360 380

25% MAC30% MAC36.4% MAC

22% MACCG POSITION

35

40

45

F_AC_021401_1_0200101_01_00


FIGURE-2-14-1-991-020-A01

2-14-1Page 12

Jul 01/21


**ON A/C A340-500


800750700400 450 500 550

160 180 200 220 24010

15

20

25

30

260

600

(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)

32

42

52

62

72

82

92

280

650

22300 320 340 360 380

25% MAC30% MAC34.7% MAC

22% MACCG POSITION

35

40

45

36.4% MAC

F_AC_021401_1_0210101_01_00


FIGURE-2-14-1-991-021-A01

2-14-1Page 13

Jul 01/21


**ON A/C A340-500


800750700400 450 500 550

160 180 200 220 24060

70

80

90

100

110

260

600

(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)

152

172

192

212

232

252

280

650

132

120

300 320 340 360 380

25% MAC30% MAC36.4% MAC

22% MACCG POSITION

F_AC_021401_1_0220101_01_00


FIGURE-2-14-1-991-022-A01

2-14-1Page 14

Jul 01/21


**ON A/C A340-500


800750700400 450 500 550

160 180 200 220 24060

70

80

90

100

110

260

600

(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)

152

172

192

212

232

252

280

650

132

120

300 320 340 360 380

25% MAC30% MAC36.4% MAC

22% MACCG POSITION

F_AC_021401_1_0230101_01_00


FIGURE-2-14-1-991-023-A01

2-14-1Page 15

Jul 01/21


**ON A/C A340-500


800550400 450

160 180 200 220 24020

30

40

50

60

70

100

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)

64

84

104

124

144

164

184

204

224

280

500

44

110

300 320 340 360 380

25% MAC30% MAC36.4% MAC

22% MACCG POSITION

80

90

600 650 700 750

F_AC_021401_1_0240101_01_00


FIGURE-2-14-1-991-024-A01

2-14-1Page 16

Jul 01/21


**ON A/C A340-500


800750700400 450 500 550

160 180 200 220 24020

30

40

50

60

70

100

260

600

(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)

64

84

104

124

144

164

184

204

224

280

650

44

110

300 320 340 360 380

25% MAC30% MAC36.4% MAC

22% MACCG POSITION

80

90

F_AC_021401_1_0250101_01_00


FIGURE-2-14-1-991-025-A01

2-14-1Page 17

Jul 01/21


2-14-2 Support of Aircraft

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-500

(SAFETY STAY)FR87

FR26

FR17

RIB6

RIB16

RIB27

RIB35 RIB35

RIB6

NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.

RIB27

RIB16

FR58

F_AC_021402_1_0030101_01_00

Support of AircraftLocation of Shoring Cradles (Sheet 1 of 2)

FIGURE-2-14-2-991-003-A01

2-14-2Page 2

Jul 01/21


**ON A/C A340-500

FR7

FR17 FR20 FR39 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_0030102_01_00

Support of AircraftLocation of Auxiliary Jacking Points (Sheet 2 of 2)

FIGURE-2-14-2-991-003-A01

2-14-2Page 3

Jul 01/21


**ON A/C A340-600

(SAFETY STAY)FR87

FR58

FR26

FR17

NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.

RIB35

RIB27

RIB16

RIB6RIB6

RIB16

RIB27

RIB35

F_AC_021402_1_0030201_01_00

Support of AircraftLocation of Shoring Cradles (Sheet 1 of 2)

FIGURE-2-14-2-991-003-B01

2-14-2Page 4

Jul 01/21


**ON A/C A340-600

FR7

FR17 FR20

FR26.1

FR36 FR39 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_0030202_01_00

Support of AircraftLocation of Auxiliary Jacking Points (Sheet 2 of 2)

FIGURE-2-14-2-991-003-B01

2-14-2Page 5

Jul 01/21


AIRCRAFT PERFORMANCE


**ON A/C A340-500 A340-600

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

Jul 01/21


3-2-1 Payload / Range - ISA Conditions

**ON A/C A340-500 A340-600

Payload / Range - ISA Conditions

1. This section gives the payload / range at ISA conditions.

3-2-1Page 1

Jul 01/21


**ON A/C A340-600

NOTE:

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

0

5

10

15

20

25

30

35

40

45

50

55

1000

185

190

195

200

205

210

215

220

225

60

65

230

235

240

ZFW(x 1000 kg)

PAYLOAD(x 1000 kg)

RANGE(nm)

RANGE(km)

THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.

180

175

70250

3000 5000 7000 9000 11000 13000 15000 17000 19000

CRUISE CONDITIONSISA 39000 ft M = 0.82

MAX PASSENGER PAYLOAD

MAX STRUCTURAL PAYLOAD

F_AC_030201_1_0180101_01_01

Payload / Range - ISA ConditionsRB 211 TRENT 556 engineFIGURE-3-2-1-991-018-A01

3-2-1Page 2

Jul 01/21


**ON A/C A340-500

NOTE:

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

0

5

10

15

20

25

30

35

40

45

50

55225

11000

RANGE(km)

RANGE(nm)


PAYLOAD(x 1000 kg)

ZFW(x 1000 kg)

165

170

175

180

185

190

195

200

205

210

215

220

1000 3000 5000 7000 9000 11000 13000 15000 17000 19000 21000

CRUISE CONDITIONSISA 39000 ft M = 0.82

MAX PASSENGER PAYLOAD

MAX STRUCTURAL PAYLOAD

F_AC_030201_1_0190101_01_01

Payload / Range - ISA ConditionsRB 211 TRENT 553 engineFIGURE-3-2-1-991-019-A01

3-2-1Page 3

Jul 01/21


3-3-1 Take-Off Weight Limitation - ISA Conditions

**ON A/C A340-500 A340-600

Take-Off Weight Limitation - ISA Conditions

1. This section gives the take-off weight limitation at ISA conditions.

3-3-1Page 1

Jul 01/21


**ON A/C A340-600

0

TAKE−OFF WEIGHT

NOTE:

2

4

6

8

1000 kg1000 lb

1.5 2 2.5 3 3.5180

200

220

240

260

280

300

320

340

360

380

400

420

440

4 4.5 5

4 6 8 10 12 14 16 18

350

400

450

500

550

600

650

700

750

800

850

900

950

1000


AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

RUNWAY LENGTH(1000 m)

RUNWAY LENGTH(1000 ft)

F_AC_030301_1_0100101_01_00

BRAKE ENERGY LIMITATIONV.M.C

Take-Off Weight LimitationISA Conditions -- RB 211 TRENT 556 engine

FIGURE-3-3-1-991-010-A01

3-3-1Page 2

Jul 01/21


**ON A/C A340-500

0

TAKE−OFF WEIGHT

NOTE:

2

4

6

8

1000 kg1000 lb

1.5 2 2.5 3 3.5180

200

220

240

260

280

300

320

340

360

380

400

420

440

4 4.5 5

4 6 8 10 12 14 16 18

350

400

450

500

550

600

650

700

750

800

850

900

950

1000


AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

RUNWAY LENGTH(1000 m)


F_AC_030301_1_0110101_01_00

V.M.C

BRAKE ENERGY LIMITATION

Take-Off Weight LimitationISA Conditions -- RB 211 TRENT 553 engine

FIGURE-3-3-1-991-011-A01

3-3-1Page 3

Jul 01/21


3-3-2 Take-Off Weight Limitation - ISA +15˚C (+59˚F) Conditions

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-600

0

TAKE−OFF WEIGHT

NOTE:

2

4

6

8

1000 kg1000 lb

1.5 2 2.5 3 3.5180

200

220

240

260

280

300

320

340

360

380

400

420

440

4 4.5 5

4 6 8 10 12 14 16 18

350

400

450

500

550

600

650

700

750

800

850

900

950

1000


AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

(1000 m)


RUNWAY LENGTH

V.M.CBRAKE ENERGY LIMITATION

F_AC_030302_1_0100101_01_00

Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- RB 211 TRENT 556 engine

FIGURE-3-3-2-991-010-A01

3-3-2Page 2

Jul 01/21


**ON A/C A340-500

0

TAKE−OFF WEIGHT

NOTE:

2

4

6

8

1000 kg1000 lb

1.5 2 2.5 3 3.5180

200

220

240

260

280

300

320

340

360

380

400

420

440

4 4.5 5

4 6 8 10 12 14 16 18

350

400

450

500

550

600

650

700

750

800

850

900

950

1000


AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

(1000 m)


BRAKE ENERGY LIMITATIONV.M.C

RUNWAY LENGTH

F_AC_030302_1_0110101_01_00

Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- RB 211 TRENT 553 engine

FIGURE-3-3-2-991-011-A01

3-3-2Page 3

Jul 01/21


3-4-1 Landing Field Length - ISA Conditions

**ON A/C A340-500 A340-600

Landing Field Length - ISA Conditions

1. This section gives the landing field length.

3-4-1Page 1

Jul 01/21


**ON A/C A340-600

NO

TE

:

2468 GR

OS

S W

EIG

HT

(x 1

000

lb)

GR

OS

S W

EIG

HT

(x 1

000

kg)

(x 1

000

m)

(x 1

000

ft)

1.5

2.0

2.5

3.0

3.5 18

020

022

024

026

028

030

00

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

400

450

350

500

550

600

650

700

4681012

TH

ES

E C

UR

VE

S A

RE

GIV

EN

FO

R IN

FO

RM

AT

ION

ON

LY.

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.

LAN

DIN

G F

IELD

LE

NG

TH

VA

LID

FO

R A

LL T

EM

PE

RA

TU

RE

S

F_AC_030401_1_0100101_01_01

Landing Field LengthISA Conditions -- RB 211 TRENT 556 engine

FIGURE-3-4-1-991-010-A01

3-4-1Page 2

Jul 01/21


**ON A/C A340-500

180

200

220

240

300

260

NO

TE

:

2468

GR

OS

S W

EIG

HT

(x 1

000

lb)

GR

OS

S W

EIG

HT

(x 1

000

kg)

(x 1

000

m)

(x 1

000

ft)

1.5

2.0

2.5

3.0

3.5

0

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

400

450

350

500

550

600

650

700

4681012

TH

ES

E C

UR

VE

S A

RE

GIV

EN

FO

R IN

FO

RM

AT

ION

ON

LY.

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.

LAN

DIN

G F

IELD

LE

NG

TH

280

VA

LID

FO

R A

LL T

EM

PE

RA

TU

RE

S

F_AC_030401_1_0110101_01_01

Landing Field LengthISA Conditions -- RB 211 TRENT 553 engine

FIGURE-3-4-1-991-011-A01

3-4-1Page 3

Jul 01/21


3-5-0 Final Approach Speed

**ON A/C A340-500 A340-600

Final Approach Speed

**ON A/C A340-500

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 146 kt at a Maximum Landing Weight (MLW) of 246 000 kg (542337 lb) and classifies the aircraft into the Aircraft Approach Category D.

NOTE : This value is given for information only.

**ON A/C A340-600

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 153 kt at a Maximum Landing Weight (MLW) of 265 000 kg (584225 lb) and classifies the aircraft into the Aircraft Approach Category D.

NOTE : This value is given for information only.

3-5-0Page 1

Jul 01/21


GROUND MANEUVERING


**ON A/C A340-500 A340-600

General Information

1. This section gives 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, gives for a normal allowance for tire slippage. As such, itreflects 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

NOTE : The following chapter takes into account ICAO Annex 14 to the Convention onInternational Civil Aviation, Aerodromes - Volume I, Aerodrome Design and Operations,Eighth Edition, July 2018.

4-1-0Page 1

Jul 01/21


4-2-0 Turning Radii

**ON A/C A340-500 A340-600

Turning Radii

1. This section gives the turning radii.

4-2-0Page 1

Jul 01/21


**ON A/C A340-600

R6

R4

R5

R3

NOTE:FOR TURNING RADII VALUES, REFER TO SHEET 2.

55

60

65

70

75

F_AC_040200_1_0080101_01_03

Turning Radii(Sheet 1) (Sheet 1 of 2)

FIGURE-4-2-0-991-008-A01

4-2-0Page 2

Jul 01/21


**ON A/C A340-600

98.9325

m

ft124.8409

98.2322

R6TAIL

109.9361

R3NLG

R4WING

R5NOSE

24.62580.2263

104.7344

82.8272

91.1299

29.53067.9223

91299

70.9233

78.6258

34.43559.3195

80.9265

62.8206

69.7229

39.24053

17473.2240

56.9187

63.1207

444548.3159

66.9220

52.6173

58190

48.85044.7147

61.7202

49.3162

53.9177

53.45541.9138

57.4188

46.8154

50.7166

57.96039.8131

53.6176

44.9147

48158

626538.2125

50.5166

43.5143

45.9151

65.67037.1122

48158

42.5139

44.4146

m

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ft

A340−600 TURNING RADII

67.47536.6120

46.8153

42.1138

43.6143

m

ft

19.7

STEERING ANGLEEFFECTIVE

(deg)

STEERINGANGLE(deg)

20

NOTE:SYMMETRIC THRUST− NO BRAKING.

F_AC_040200_1_0080102_01_00


FIGURE-4-2-0-991-008-A01

4-2-0Page 3

Jul 01/21


**ON A/C A340-500

R6

R4

R5

R3

R2

R1

NOTE:FOR TURNING RADII VALUES, REFER TO SHEET 2.

55

60

65

70

F_AC_040200_1_0090101_01_03


FIGURE-4-2-0-991-009-A01

4-2-0Page 4

Jul 01/21


**ON A/C A340-500

19.520

TYPE OFTURN

278.7258

A340−500 TURNING RADII

m

ft84.4277

83.5274

R4WING

110.4362

R5NOSE

85.3280

R6TAIL

94.9311

R1RMLG

R2LMLG

R3NLG

24.325263.1207

67.4221

67.6222

93.5307

70.0230

79.2260

29.130252.9174

55.9183

57.3188

82.0269

60.2198

68.8226

33.935245.9151

47.3155

50.0164

73.6241

53.4175

61.5202

38.740240.8134

40.8134

44.6146

67.1220

48.5159

56.1184

43.445237.1122

35.5116

40.6133

61.9203

44.9147

51.9170

48.050234.3113

31.1102

37.5123

57.6189

42.2138

48.7160

52.655232.3106

27.490

35.1115

53.9177

40.1132

46.0151

57.060230.7101

24.279

33.3109

50.8167

38.6127

43.9144

61.165229.797

21.671

31.8104

48.2158

37.4123

42.2138

64.570229.095

19.564

30.9101

46.2152

36.6120

40.9134

49.350133.7111

30.098

36.8121

56.5185

41.6136

47.9157

54.055131.7104

26.386

34.5113

52.9174

39.6130

45.3149

58.860130.299

23.075

32.6107

49.7163

38.0125

43.1141

63.565129.195

20.166

31.1102

46.8154

36.8121

41.3135

68.070128.493

17.457

30.098

44.2145

35.9118

39.8131

m

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ft

STEERING ANGLE (deg)EFFECTIVESTEERING

ANGLE (deg)

TYPE 1 TURNS USE: ASYMMETRIC THRUST DURING THE WHOLE TURN;AND DIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY.

IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BYAPPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.

TYPE 2 TURNS USE: SYMMETRIC THRUST DURING THE WHOLE TURN;AND NO DIFFERENTIAL BRAKING AT ALL.

NOTE:ABOVE , AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION.50

F_AC_040200_1_0090102_01_01


FIGURE-4-2-0-991-009-A01

4-2-0Page 5

Jul 01/21


4-3-0 Minimum Turning Radii

**ON A/C A340-500 A340-600

Minimum Turning Radii

1. This section provides the minimum turning radii.

4-3-0Page 1

Jul 01/21


**ON A/C A340-600

A(MINIMUM TURNING

WIDTH)

67.4

TYPE OFTURN

213.745

A340−600 MINIMUM TURNING RADII

m

ft56.7186

36.6120

R4WING

46.8154

R5NOSE

42.1138

R6TAIL43.6143

R3NLGSTEERING ANGLE (deg)

EFFECTIVE

NOTE:TYPE 2 TURNS USE:

X

33.2109

AX Y

R6

R4

R5

R3

Y

SYMMETRIC THRUST DURING THE WHOLE TURN;

OF TIREOUTSIDE FACE

AND NO DIFFERENTIAL BRAKING AT ALL.F_AC_040300_1_0050101_01_01

Minimum Turning RadiiFIGURE-4-3-0-991-005-A01

4-3-0Page 2

Jul 01/21


**ON A/C A340-500

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)

68.070 (MAX)

TYPE OFTURN

111.136

A340−500 MINIMUM TURNING RADII

m

ft47.8157

30.098

R4WING

44.2145

R5NOSE

35.9118

R6TAIL39.8131

R3NLG

64.570 (MAX)213.243

50.7166

30.9101

46.2152

36.6120

40.9134

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.

R6

R4

R5

R3

27.691

27.691

AX Y

Y

OUTSIDE FACEOF TIRE

X

F_AC_040300_1_0060101_01_01

Minimum Turning RadiiFIGURE-4-3-0-991-006-A01

4-3-0Page 3

Jul 01/21


4-4-0 Visibility from Cockpit in Static Position

**ON A/C A340-500 A340-600

Visibility from Cockpit in Static Position

1. This section gives the visibility from cockpit in static position.

4-4-0Page 1

Jul 01/21


**ON A/C A340-500 A340-600

25?

20?

14 m(45.93 ft)

6.58 m(21.59 ft)

VISUAL ANGLES IN VERTICALPLANE THROUGH PILOTEYE POSITION.

DIMENSIONS ARE APPROXIMATE

2.4 m(7.87 ft)

CAPTAIN FIELD OF VIEW

MAX AFT VISION WITH HEAD TURNEDAROUND SPINAL COLUMN.WING TIP CAN BE SEEN WHEN HEAD IS MOVEDTO THE SIDE.

VISUAL ANGLES IN HORIZONTALPLANE THROUGH PILOTEYE POSITION.

FIRST OFFICERFIELD OF VIEW

NOT TO BE USED FORLANDING APPROACH VISIBILITY

NOTE:PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.

ZONE THAT CANNOT BE SEEN

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_0050101_01_02

Visibility from Cockpit in Static PositionFIGURE-4-4-0-991-005-A01

4-4-0Page 2

Jul 01/21


**ON A/C A340-500 A340-600

CA

PT

AIN

WIN

DS

HIE

LDC

AP

TA

IN S

LID

ING

WIN

DO

WC

AP

TA

INF

IXE

D W

IND

OW

PIL

OT

EY

E P

OS

ITIO

N(C

AP

TA

IN P

OS

ITIO

N)

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?

F_AC_040400_1_0090101_01_00

Binocular Visibility Through Windows from Captain Eye PositionFIGURE-4-4-0-991-009-A01

4-4-0Page 3

Jul 01/21


4-5-0 Runway and Taxiway Turn Paths

**ON A/C A340-500 A340-600

Runway and Taxiway Turn Paths

1. This section gives the runway and taxiway turn paths for the following configurations:- 135˚ Turn - Runway to Taxiway- 90˚ Turn - Runway to Taxiway- 180˚ Turn on a Runway- 135˚ Turn - Taxiway to Taxiway- 90˚ Turn - Taxiway to Taxiway.The turn paths Runway to Taxiway and Taxiway to Taxiway are defined using 3 methods:- Oversteering method,- External and Taxiing Aid Camera System (ETACS) assisted steering method,- Cockpit over centerline method.The 180˚ Turn on runway is defined using the following method:- 180˚ Turn using edge of runway method.

NOTE : The fillet design and the turn radii are as per FAA AC 150/5300-13 Change 18.

4-5-0Page 1

Jul 01/21



**ON A/C A340-500 A340-600

135˚ Turn - Runway to Taxiway

1. This section gives the 135˚ turn - runway to taxiway.

4-5-1Page 1

Jul 01/21


**ON A/C A340-600

45 m(150 ft)

23 m(75 ft)

RUNWAY CENTERLINE

TAXIWAYCENTERLINE

FAA LEAD−IN FILLET

L = 75 m (250 ft)


L = 75 m (250 ft)

(2 ft)APPROX 0.48 m

APPROX 13.15 m(45 ft)

FILLET R = 25.5 m(85 ft)

TURN R = 45 m(150 ft)

NOTE:THE MLG FOLLOWS THE CENTERLINE.THE NLG EDGE MARGIN DECREASES BY 0.6 m (2 ft)

NLG PATH (CENTER)

MLG PATH (EDGE)

F_AC_040501_1_0040101_01_02

135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method

FIGURE-4-5-1-991-004-A01

4-5-1Page 2

Jul 01/21


**ON A/C A340-600

NOTE:THE NLG FOLLOWS THE RH ETACS MARKER.THE NLG EDGE MARGIN DECREASES BY 0.6 m (2 ft).

45 m(150 ft)

23 m(75 ft)

TAXIWAYCENTERLINE

NLG PATH (CENTER)

NLG ETACS MARKER (RH)

MLG PATH (EDGE)

MLG ETACS MARKER (RH)


L = 75 m (250 ft)


L = 75 m (250 ft)

TURN R = 45 m(150 ft)



(16 ft)APPROX 4.86 m

RUNWAY CENTERLINE

F_AC_040501_1_0110101_01_01

135˚ Turn - Runway to TaxiwayTACS Assisted Steering Method

FIGURE-4-5-1-991-011-A01

4-5-1Page 3

Jul 01/21


**ON A/C A340-600

45 m(150 ft)

RUNWAY CENTERLINE

TAXIWAYCENTERLINE

23 m(75 ft)

TURN R = 45 m(150 ft)


APPROX 0.48 m(2 ft)

ADDITIONAL FILLET TO MEET4 m (13 ft) EDGE CLEARANCE


L = 75 m (250 ft)


L = 75 m (250 ft)

APPROX 2.62 m(9 ft)

NLG PATH (CENTER)

MLG PATH (EDGE)

F_AC_040501_1_0150101_01_00

135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method

FIGURE-4-5-1-991-015-A01

4-5-1Page 4

Jul 01/21


**ON A/C A340-500

NOTE:THE MLG FOLLOWS THE CENTERLINE.THE NLG EDGE MARGIN DECREASES BY 0.6 m (2 ft).

45 m(150 ft)


L = 75 m (250 ft)


TAXIWAYCENTERLINE

23 m(75 ft)


TURN R = 45 m(150 ft)



L = 75 m (250 ft)

RUNWAY CENTERLINE

NLG PATH (CENTER)

MLG PATH (EDGE)

F_AC_040501_1_0050101_01_02


FIGURE-4-5-1-991-005-A01

4-5-1Page 5

Jul 01/21


**ON A/C A340-500



L = 75 m (250 ft)


L = 75 m (250 ft)

TURN R = 45 m(150 ft)




23 m(75 ft)

TAXIWAYCENTERLINE

RUNWAY CENTERLINE

45 m(150 ft)

NLG PATH (CENTER)


MLG PATH (EDGE)


F_AC_040501_1_0120101_01_01


FIGURE-4-5-1-991-012-A01

4-5-1Page 6

Jul 01/21


**ON A/C A340-500

45 m(150 ft)

23 m(75 ft)


L = 75 m (250 ft)

TAXIWAYCENTERLINE

RUNWAY CENTERLINE

APPROX 1.37 m(5 ft)


L = 75 m (250 ft)


TURN R = 45 m(150 ft)

ADDITIONAL FILLET TO MEET4.0 m (13 ft) EDGE CLEARANCE

NLG PATH (CENTER)

MLG PATH (EDGE)

F_AC_040501_1_0160101_01_00


FIGURE-4-5-1-991-016-A01

4-5-1Page 7

Jul 01/21



**ON A/C A340-500 A340-600

90˚ Turn - Runway to Taxiway

1. This section gives the 90˚ turn - runway to taxiway.

4-5-2Page 1

Jul 01/21


**ON A/C A340-600

NLG PATH (CENTER)

MLG PATH (EDGE)45 m

(150 ft)

RUNWAY CENTERLINE

23 m(75 ft)

TAXIWAYCENTERLINE

TURN R = 45 m(150 ft)




FAA LEAD−IN FILLETL = 75 m (250 ft)

NOTE:THE MLG FOLLOWS THE CENTERLINE.THE NLG EDGE MARGIN DECREASES BY 0.6 m (2 ft). F_AC_040502_1_0040101_01_02


FIGURE-4-5-2-991-004-A01

4-5-2Page 2

Jul 01/21


**ON A/C A340-600


NLG PATH (CENTER)



23 m(75 ft)

TAXIWAYCENTERLINE

45 m(150 ft)

RUNWAY CENTERLINE

TURN R = 45 m(150 ft)




MLG PATH (EDGE)


F_AC_040502_1_0170101_01_00


FIGURE-4-5-2-991-017-A01

4-5-2Page 3

Jul 01/21


**ON A/C A340-600

45 m(150 ft)

RUNWAY CENTERLINE

TURN R = 45 m(150 ft)


APPROX 0.2 m(1 ft)

4.0 m (13 ft) EDGE CLEARANCEADDITIONAL FILLET TO MEET


23 m(75 ft)

TAXIWAYCENTERLINE

NLG PATH (CENTER)

MLG PATH (EDGE)

F_AC_040502_1_0130101_01_01


FIGURE-4-5-2-991-013-A01

4-5-2Page 4

Jul 01/21


**ON A/C A340-500


NLG PATH (CENTER)

MLG PATH (EDGE)

45 m(150 ft)

RUNWAY CENTERLINE

23 m(75 ft)

TAXIWAYCENTERLINE



TURN R = 45 m(150 ft)



F_AC_040502_1_0050101_01_02


FIGURE-4-5-2-991-005-A01

4-5-2Page 5

Jul 01/21


**ON A/C A340-500


NLG PATH (CENTER)


MLG PATH (EDGE)



23 m(75 ft)

TAXIWAYCENTERLINE

45 m(150 ft)

RUNWAY CENTERLINE

TURN R = 45 m(150 ft)


APPROX 9.1 m(30 ft)


F_AC_040502_1_0180101_01_00


FIGURE-4-5-2-991-018-A01

4-5-2Page 6

Jul 01/21


**ON A/C A340-500

NLG PATH (CENTER)

MLG PATH (EDGE)

45 m(150 ft)

RUNWAY CENTERLINE


TURN R = 45 m(150 ft)



TAXIWAYCENTERLINE

23 m(75 ft)


F_AC_040502_1_0140101_01_01


FIGURE-4-5-2-991-014-A01

4-5-2Page 7

Jul 01/21


4-5-3 180˚ Turn on a Runway

**ON A/C A340-500 A340-600

180˚ Turn on a Runway

1. This section gives the 180˚ turn on a runway.

NOTE : The turns in this section show turns on a runway after landing and are not aimed to resultin good alignment.

4-5-3Page 1

Jul 01/21


**ON A/C A340-600

NLG PATH

MLG PATH

NOSE TIP PATH

WING TIP PATH

TAIL TIP PATH

MLG PATH

NOSE TIP PATH

WING TIP PATH

TAIL TIP PATH

R4 = 46.8 m

64.8 m(213 ft)

(154 ft)

R6 = 43.6 m(143 ft)

56.8 m(186 ft)

4.0 m(13 ft)

22.6 m(74 ft)

19.5 m(64 ft)

6.1 m(20 ft)

1.4 m(5 ft)

4.0 m(13 ft)

R3 = 36.6 m(120 ft)

R5 = 42.1 m(138 ft)

RUNWAY CENTERLINE

NLG PATH (EDGE)

NLG PATH (CENTER)

NOTE:TYPE 2 VALUES FOR MAX STEERING ANGLE = 75 . F_AC_040503_1_0090101_01_04

180˚ Turn on a RunwayFIGURE-4-5-3-991-009-A01

4-5-3Page 2

Jul 01/21


**ON A/C A340-500

R5 = 35.9 m(118 ft)

4.0 m(13 ft)

22.7 m(74 ft)

18 m(59 ft)

10.5 m(34 ft)

1.5 m(5 ft)

4.0 m(13 ft)

R3 = 30 m(98 ft)

R6 = 39.8 m(131 ft)

R4 = 44.2 m(145 ft)

55.8 m(183 ft)

47.8 m(157 ft)

NLG PATH

MLG PATH

NOSE TIP PATH

WING TIP PATH

TAIL TIP PATH

NLG PATH (EDGE)

MLG PATH

NOSE TIP PATH

WING TIP PATH

TAIL TIP PATH

RUNWAY CENTERLINE

NLG PATHNLG PATH (CENTER)

TYPE 1 VALUES FOR MAX STEERING ANGLE = 70 .IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.

NOTE:

F_AC_040503_1_0100101_01_04

180˚ Turn on a RunwayFIGURE-4-5-3-991-010-A01

4-5-3Page 3

Jul 01/21



**ON A/C A340-500 A340-600

135˚ Turn - Taxiway to Taxiway

1. This section gives the 135˚ turn - taxiway to taxiway.

4-5-4Page 1

Jul 01/21


**ON A/C A340-600

23 m(75 ft)

23 m(75 ft)

CENTERLINECENTERLINETAXIWAY

TAXIWAY CENTERLINE

TURN R = 45 m(150 ft)


FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


NLG PATH (CENTER)

MLG PATH (EDGE)


L = 75 m (250 ft)

APPROX 0.49 m(2 ft)


135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method

FIGURE-4-5-4-991-005-A01

4-5-4Page 2

Jul 01/21


**ON A/C A340-600

TAXIWAY CENTERLINE

23 m(75 ft)

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


L = 75 m (250 ft)FILLET R = 25.5 m

(85 ft)



TURN R = 45 m(150 ft)


NLG PATH (CENTER)


MLG PATH (EDGE)


CENTERLINETAXIWAY

23 m(75 ft)

F_AC_040504_1_0170101_01_00

135˚ Turn - Taxiway to TaxiwayTACS Assisted Steering Method

FIGURE-4-5-4-991-017-A01

4-5-4Page 3

Jul 01/21


**ON A/C A340-600

NLG PATH (CENTER)

MLG PATH (EDGE)

TAXIWAY CENTERLINE

23 m(75 ft)

CENTERLINETAXIWAY

23 m(75 ft)

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


L = 75 m (250 ft)FILLET R = 25.5 m

(85 ft)

APPROX 2.63 m(9 ft)

TURN R = 45 m(150 ft)


F_AC_040504_1_0130101_01_01

135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method

FIGURE-4-5-4-991-013-A01

4-5-4Page 4

Jul 01/21


**ON A/C A340-500


23 m(75 ft)

23 m(75 ft)

CENTERLINECENTERLINETAXIWAY

TAXIWAY CENTERLINE

TURN R = 45 m(150 ft)


FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


NLG PATH (CENTER)

MLG PATH (EDGE)


L = 75 m (250 ft)


F_AC_040504_1_0060101_01_02


FIGURE-4-5-4-991-006-A01

4-5-4Page 5

Jul 01/21


**ON A/C A340-500

TAXIWAY CENTERLINE

23 m(75 ft)

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


L = 75 m (250 ft)FILLET R = 25.5 m

(85 ft)



TURN R = 45 m(150 ft)

23 m(75 ft)

CENTERLINETAXIWAY


NLG PATH (CENTER)


MLG PATH (EDGE)


F_AC_040504_1_0180101_01_00


FIGURE-4-5-4-991-018-A01

4-5-4Page 6

Jul 01/21


**ON A/C A340-500

NLG PATH (CENTER)

MLG PATH (EDGE)

TAXIWAY CENTERLINE

23 m(75 ft)

23 m(75 ft)

CENTERLINETAXIWAY

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


L = 75 m (250 ft)FILLET R = 25.5 m

(85 ft)

APPROX 1.36 m(4 ft)

TURN R = 45 m(150 ft)


F_AC_040504_1_0140101_01_01


FIGURE-4-5-4-991-014-A01

4-5-4Page 7

Jul 01/21



**ON A/C A340-500 A340-600

90˚ Turn - Taxiway to Taxiway

1. This section gives the 90˚ turn - taxiway to taxiway.

4-5-5Page 1

Jul 01/21


**ON A/C A340-600

23 m(75 ft)

TAXIWAY CENTERLINE

23 m(75 ft)

TAXIWAYCENTERLINEF

AA

LEA

D−

IN F

ILLET

L = 75 m

(250 ft)





TURN R = 45 m(150 ft)

NLG PATH (CENTER)

MLG PATH (EDGE)



FIGURE-4-5-5-991-008-A01

4-5-5Page 2

Jul 01/21


**ON A/C A340-600

23 m(75 ft)

TAXIWAY CENTERLINE

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


23 m(75 ft)

TAXIWAYCENTERLINE


TURN R = 45 m(150 ft)


NOTE:THE NLG FOLLOWS THE RH ETACS MARKER.THE NLG EDGE MARGIN DECREASES BY 0.6 (2 ft).


NLG PATH (CENTER)


MLG PATH (EDGE)


F_AC_040505_1_0190101_01_00


FIGURE-4-5-5-991-019-A01

4-5-5Page 3

Jul 01/21


**ON A/C A340-600

23 m(75 ft)

TAXIWAY CENTERLINE

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


23 m(75 ft)

TAXIWAYCENTERLINE


TURN R = 45 m(150 ft)

NLG PATH (CENTER)

MLG PATH (EDGE)

APPROX 0.2 m(1 ft)


F_AC_040505_1_0150101_01_01


FIGURE-4-5-5-991-015-A01

4-5-5Page 4

Jul 01/21


**ON A/C A340-500

23 m(75 ft)

TAXIWAY CENTERLINE

23 m(75 ft)

TAXIWAYCENTERLINEF

AA

LEA

D−

IN F

ILLET

L = 75 m

(250 ft)





TURN R = 45 m(150 ft)

NLG PATH (CENTER)

MLG PATH (EDGE)



FIGURE-4-5-5-991-009-A01

4-5-5Page 5

Jul 01/21


**ON A/C A340-500

23 m(75 ft)

TAXIWAY CENTERLINE

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


23 m(75 ft)


TURN R = 45 m(150 ft)

APPROX 9.1 m(30 ft)

NOTE:THE NLG FOLLOWS THE RH ETACS MARKER.THE NLG EDGE MARGIN DECREASES BY 0.6 (2 ft).

NLG PATH (CENTER)


MLG PATH (EDGE)


TAXIWAYCENTERLINE


F_AC_040505_1_0200101_01_00


FIGURE-4-5-5-991-020-A01

4-5-5Page 6

Jul 01/21


**ON A/C A340-500

23 m(75 ft)

TAXIWAY CENTERLINE

FA

A LE

AD

−IN

FILLE

TL =

75 m (250 ft)


23 m(75 ft)

TAXIWAYCENTERLINE


TURN R = 45 m(150 ft)

NLG PATH (CENTER)

MLG PATH (EDGE)



F_AC_040505_1_0160101_01_01


FIGURE-4-5-5-991-016-A01

4-5-5Page 7

Jul 01/21


4-6-0 Runway Holding Bay (Apron)

**ON A/C A340-500 A340-600

Runway Holding Bay (Apron)

1. This section provides the runway holding bay (Apron).

4-6-0Page 1

Jul 01/21


**ON A/C A340-500 A340-600

TAXIWAYCENTERLINE

23 m(75 ft)

45 m(150 ft)

RUNWAYCENTERLINE

HOLDINGPOINT

90 m(300 ft)

6.1 m(20 ft)

6.1 m(20 ft)

12.2 m(40 ft)

100.54 m(329 ft)

190 m(625 ft)

20? NOSE−WHEEL STEERING ANGLE.COORDINATE WITH USING AIRLINE FOR SPECIFIC PLANNED OPERATING PROCEDURES.

NOTE:

F_AC_040600_1_0040101_01_02

Runway Holding Bay (Apron)FIGURE-4-6-0-991-004-A01

4-6-0Page 2

Jul 01/21


4-7-0 Minimum Line-Up Distance Corrections

**ON A/C A340-500 A340-600

Minimum Line-Up Distance Corrections

1. The ground maneuvers were performed using asymmetric thrust and differential-only braking toinitiate the turn.Maneuvers of this section are calculated with turn characteristics as given in chapter 04-02-00.TODA: Take-Off Distance AvailableASDA: Acceleration-Stop Distance Available

2. 90˚ Turn on Runway EntryThis 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 4.0 m (13 ft) from the taxiway edge, and finishes with the aircraft aligned on thecenterline of the runway, see FIGURE 4-7-0-991-025-A.During the turn, all the clearances must meet the minimum value of 4.0 m (13 ft) for this category ofaircraft as recommended in ICAO Annex 14 (Eighth Edition).

3. 180˚ Turn on Runway Turn PadThis 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 4.0 m (13 ft) from the pavement edge, and itfinishes with the aircraft aligned on the centerline of the runway, see FIGURE 4-7-0-991-026-A.During the turn, all the clearances must meet the minimum value of 4.0 m (13 ft) for this category ofaircraft as recommended in ICAO Annex 14 (Eighth Edition).

4. 180˚ Turn on Runway WidthThis 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 (FCOM)), the aircraft is initially angled with respect to the runwaycenterline when starting the 180˚ turn, see FIGURE 4-7-0-991-027-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 4.0 m (13 ft) for this category ofaircraft as recommended in ICAO Annex 14 (Eighth Edition).

NOTE : The minimum line-up distances may need a lower steering angle than maximum steeringangle.

4-7-0Page 1

Jul 01/21


**ON A/C A340-500 A340-600

NOTE:ASDA: ACCELERATION−STOP DISTANCE AVAILABLETODA: TAKE−OFF DISTANCE AVAILABLE

TAXIWAYCENTERLINE

RUNWAY

> 4.0 m(13 ft)

TODA

4.0 m(13 ft)

ASDA

CENTERLINE

AIRCRAFTTYPE

STEERINGANGLE

MAX(STANDARD WIDTH)

45 m (150 ft) WIDE RUNWAY

DISTANCE CORRECTIONMINIMUM LINE−UP


A340−500 76 ft23.1 m 168 ft51.1 m 71 ft21.6 m 163 ft49.6 mON TODA ON ASDA ON TODA ON ASDA

60 m (200 ft) WIDE RUNWAY

A340−600 105 ft32.0 m 214 ft65.2 m 66 ft20.0 m 175 ft53.2 m

90 TURN ON RUNWAY ENTRY

7076

F_AC_040700_1_0250101_01_01

Minimum Line-Up Distance Corrections90˚ Turn on Runway EntryFIGURE-4-7-0-991-025-A01

4-7-0Page 2

Jul 01/21


**ON A/C A340-500 A340-600

AIRCRAFTTYPE

STEERINGANGLE

MAX(STANDARD WIDTH)


MINIMUMREQUIRED

PAVEMENTWIDTH

MINIMUMREQUIRED

PAVEMENTWIDTH


A340−500 192 ft58.5 m116 ft35.3 m 208 ft63.3 m 206 ft62.9 m114 ft34.7 m 206 ft62.7 mON TODA ON ASDA ON TODA ON ASDA

45 m (150 ft) WIDE RUNWAY 60 m (200 ft) WIDE RUNWAY

4.0 m(13 ft)

A340−600 250 ft76.2 m145 ft44.2 m 254 ft77.4 m 196 ft59.7 m129 ft39.2 m 238 ft72.4 m

> 4.0 m(13 ft)

TODA

ASDA

RUNWAY CENTERLINE

4.0 m(13 ft)

MINIMUM PAVEMENT WIDTH


7076


F_AC_040700_1_0260101_01_01

Minimum Line-Up Distance Corrections180˚ Turn on Runway Turn Pad

FIGURE-4-7-0-991-026-A01

4-7-0Page 3

Jul 01/21


**ON A/C A340-500 A340-600

AIRCRAFTTYPE

STEERINGANGLE

MAX(STANDARD WIDTH)



A340−500 154 ft47.0 m 246 ft74.9 mON TODA ON ASDA ON TODA ON ASDA

45 m (150 ft) WIDE RUNWAY 60 m (200 ft) WIDE RUNWAY

A340−600NOT POSSIBLE

ASDA

TODA

> 4.0 m(13 ft)

4.0 m(13 ft)

4.0 m(13 ft)

RUNWAY CENTERLINE



7076 156 ft47.5 m 265 ft80.7 m

20

F_AC_040700_1_0270101_01_01

Minimum Line-Up Distance Corrections180˚ Turn on Runway WidthFIGURE-4-7-0-991-027-A01

4-7-0Page 4

Jul 01/21


4-8-0 Aircraft Mooring

**ON A/C A340-500 A340-600

Aircraft Mooring

1. This section provides information on aircraft mooring.

4-8-0Page 1

Jul 01/21


**ON A/C A340-500 A340-600

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

4-8-0Page 2

Jul 01/21


TERMINAL SERVICING

5-1-0 Aircraft Servicing Arrangements

**ON A/C A340-500 A340-600

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

Jul 01/21


5-1-1 Symbols Used on Servicing Diagrams

**ON A/C A340-500 A340-600

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

5-1-1Page 1

Jul 01/21


5-1-2 Typical Ramp Layout - Open Apron

**ON A/C A340-500 A340-600

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).

5-1-2Page 1

Jul 01/21


**ON A/C A340-600

PS

TOW

AS

GP

U

LD CL

CAT

CATPS

AC

LD CL

CATPS

CAT

ULD

FUELFUEL

WV

LV

ULD

BULKCB

STAND SAFETY LINE

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

F_AC_050102_1_0080101_01_01

Typical Ramp LayoutOpen Apron

FIGURE-5-1-2-991-008-A01

5-1-2Page 2

Jul 01/21


**ON A/C A340-500

PS CAT

CATPS

PS CAT

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

TOW

AS

GP

U

LD CL

AC

LD CL

ULD

FUELFUEL

WV CB BULK

ULD

LV

STAND SAFETY LINE

F_AC_050102_1_0090101_01_01

Typical Ramp LayoutOpen Apron

FIGURE-5-1-2-991-009-A01

5-1-2Page 3

Jul 01/21


5-1-3 Typical Ramp Layout - Gate

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-600

TOW

AS

GP

U

LD CL

CAT

CAT

AC

LD CL

CAT

CLEAN

ULD

FUELFUEL

WV

LV

ULD

BULKCB

PBB

PBB

STAND SAFETY LINE

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

F_AC_050103_1_0040101_01_03

Typical Ramp LayoutGate

FIGURE-5-1-3-991-004-A01

5-1-3Page 2

Jul 01/21


**ON A/C A340-500

CLEAN CAT

CAT

CAT

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

TOW

AS

GP

U

LD CL

AC

LD CL

ULD

FUELFUEL

CB BULK

ULD

LV

PBB

PBB

WV

STAND SAFETY LINE

F_AC_050103_1_0050101_01_03

Typical Ramp LayoutGate

FIGURE-5-1-3-991-005-A01

5-1-3Page 3

Jul 01/21


5-2-0 Terminal Operations - Full Servicing

**ON A/C A340-600

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 HANDLING319 pax: 12 F/C + 42 B/C + 265 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:- 160 pax at door L1 (12 F/C + 42 B/C + 106 Y/C)- 159 pax at door L2 (159 Y/C)- Deplaning rate = 25 pax/min per door- Priority deplaning for premium passengers.

Boarding:- 160 pax at door L1 (12 F/C + 42 B/C + 106 Y/C)- 159 pax at door L2 (159 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: 20 LD3- AFT cargo compartment: 6 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

Jul 01/21


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 4 nozzles.178 000 l (47 023 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 R5.Equipment positioning + opening door = +5 min.Closing door + equipment removal = +3 min.

Full Size Trolley Equivalent (FSTE) to unload and load: 45 FSTE- 9 FSTE at door R1- 9 FSTE at door R2- 27 FSTE at door R5.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

Jul 01/21


**ON A/C A340-600

GSE POSITIONING/REMOVAL

ACTIVITY

CRITICAL PATH

TRT: 68 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


CATERING AT R5

CARGO AFT CC

CATERING AT R1

AVAILABLE TIME

F_AC_050200_1_0060101_01_01

Full Servicing Turn Round Time ChartFIGURE-5-2-0-991-006-A01

5-2-0Page 3

Jul 01/21


**ON A/C A340-500

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 HANDLING246 pax: 8 F/C + 42 B/C + 196 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:- 123 pax at door L1 (8 F/C + 42 B/C + 73 Y/C)- 123 pax at door L2 (123 Y/C)- Deplaning rate = 25 pax/min per door- Priority deplaning for premium passengers.

Boarding:- 123 pax at door L1 (8 F/C + 42 B/C + 73 Y/C)- 123 pax at door L2 (123 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: 16 LD3- AFT cargo compartment: 4 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

Jul 01/21


- 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.191 000 l (50 457 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: 39 FSTE- 8 FSTE at door R1- 9 FSTE at door R2- 22 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

Jul 01/21


**ON A/C A340-500


ACTIVITY

CRITICAL PATH

TRT: 56 min

100 20 30 40 50 60 70


HEADCOUNTING

CATERING AT R2

CLEANING

CARGO FWD CC

BULK

REFUELING


WASTE WATER SERVICING


CATERING AT R4

CARGO AFT CC

CATERING AT R1

AVAILABLE TIME

F_AC_050200_1_0070101_01_01

Full Servicing Turn Round Time ChartFIGURE-5-2-0-991-007-A01

5-2-0Page 6

Jul 01/21


5-3-0 Terminal Operations - Transit

**ON A/C A340-600

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 HANDLING319 pax (12 F/C + 42 B/C + 265 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:- 160 pax at door L1- Deboarding rate = 25 pax/min per door

Boarding:- 160 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:- 6 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

Jul 01/21


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

Jul 01/21


**ON A/C A340-600

TRT: 34 min

50 10 15 20 25 30 35

AT L1DEBOARDING/BOARDING

HEADCOUNTING

CLEANING

CARGO FWD CC

BULK

REFUELLING


TOILET SERVICING

CATERING

CARGO AFT CC

40


ACTIVITY

CRITICAL PATH

AVAILABLE TIME

F_AC_050300_1_0070101_01_00

Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-007-A01

5-3-0Page 3

Jul 01/21


**ON A/C A340-500

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 HANDLING246 pax (8 F/C + 42 B/C + 196 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:- 123 pax at door L1- Deboarding rate = 25 pax/min per door

Boarding:- 123 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

5-3-0Page 4

Jul 01/21


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

Jul 01/21


**ON A/C A340-500

TRT: 32 min

50 10 15 20 25 30 35

AT L1DEBOARDING/BOARDING

HEADCOUNTING

CLEANING

CARGO FWD CC

BULK

REFUELLING


TOILET SERVICING

CATERING

CARGO AFT CC

40


ACTIVITY

CRITICAL PATH

AVAILABLE TIME

F_AC_050300_1_0080101_01_00

Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-008-A01

5-3-0Page 6

Jul 01/21


5-4-1 Ground Service Connections Layout

**ON A/C A340-500 A340-600

Ground Service Connections Layout

1. This section provides the ground service connections layout.

5-4-1Page 1

Jul 01/21


**ON A/C A340-600

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 − HYDRAULIC GROUND POWER SUPPLY

(YELLOW)

5 − HIGH PRESSURE AIR PRE−CONDITIONING

11 − HYDRAULIC RESERVOIR AIR PRESSURIZATIONAND GROUND POWER SUPPLY (BLUE)

13 − POTABLE WATER SERVICE PANEL14 − WASTE WATER SERVICE PANEL15 − APU OIL FILLING16 − GROUNDING (EARTHING) POINT

12 − REFUEL/DEFUEL PANEL

10 − HYDRAULIC RESERVOIR FILLING AND GROUNDPOWER SUPPLY (GREEN)

17 − NACA FLAME ARRESTOR18 − OVERPRESSURE PROTECTOR

1

216

3

46

78 6

7

18

17

5

119

1612 10

16

13

14

15

18 17

1817 6

7 6 78

F_AC_050401_1_0040101_01_04

Ground Service Connections LayoutFIGURE-5-4-1-991-004-A01

5-4-1Page 2

Jul 01/21


**ON A/C A340-500

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 − HYDRAULIC GROUND POWER SUPPLY

(YELLOW)

5 − HIGH PRESSURE AIR PRE−CONDITIONING

11 − HYDRAULIC RESERVOIR AIR PRESSURIZATIONAND GROUND POWER SUPPLY (BLUE)

13 − POTABLE WATER SERVICE PANEL14 − WASTE WATER SERVICE PANEL15 − APU OIL FILLING16 − GROUNDING (EARTHING) POINT

12 − REFUEL/DEFUEL PANEL

10 − HYDRAULIC RESERVOIR FILLING AND GROUNDPOWER SUPPLY (GREEN)

17 − NACA FLAME ARRESTOR18 − OVERPRESSURE PROTECTOR

1

2 163

18

17

6

7

8

6

7

4

5

9 11

16

1012

13

14

15

18 17

16

1718

6

78

6 7

F_AC_050401_1_0050101_01_04

Ground Service Connections LayoutFIGURE-5-4-1-991-005-A01

5-4-1Page 3

Jul 01/21


5-4-2 Grounding Points

**ON A/C A340-500 A340-600

Grounding (Earthing) Points

**ON A/C A340-600

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:

39.45 m(129.43 ft)

5.34 m(17.52 ft)

1.50 m(4.92 ft)

On right Main LandingGear leg:

39.45 m(129.43 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 A340-500

2. Grounding (Earthing) Points




On Nose Landing Gearleg:


1.40 m(4.59 ft)

On left Main LandingGear leg:

34.15 m(112.04 ft)

5.34 m(17.52 ft)

1.50 m(4.92 ft)

5-4-2Page 1

Jul 01/21





On right Main LandingGear leg:

34.15 m(112.04 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.

5-4-2Page 2

Jul 01/21


**ON A/C A340-500 A340-600

MAIN LANDING GEAR

A

LANDINGGEAR

A

GROUNDING (EARTHING) POINTGROUNDING (EARTHING) CABLE

TYPICAL

NOSE LANDING GEAR

A

F_AC_050402_1_0050101_01_02

Ground Service ConnectionsGrounding (Earthing) PointsFIGURE-5-4-2-991-005-A01

5-4-2Page 3

Jul 01/21


5-4-3 Hydraulic System

**ON A/C A340-500 A340-600

Hydraulic Servicing

**ON A/C A340-600

1. Ground Service Panels

DISTANCEFROM AIRCRAFT CENTERLINE

ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Green System:Access Door 197FB

35.62 m(116.86 ft)

1.50 m(4.92 ft)

2.10 m(6.89 ft)

Yellow System:Access Door 196PB

30.32 m(99.48 ft)

1.70 m(5.58 ft)

1.80 m(5.91 ft)

Blue System:Access Door 195MB

27.82 m(91.27 ft)

1.50 m(4.92 ft)

1.75 m(5.74 ft)

A. Reservoir pressurization

On the Blue ground service panel:- One self-sealing connector - Green reservoir pressurization.- One self-sealing connector - Blue and Yellow reservoir pressurization.

B. Reservoir filling

On the Green ground service panel:- One self-sealing connector - reservoir filling.- One self-sealing connector - reservoir filling (hand pump).

C. Ground test

On each ground service panel:- One self-sealing connector - suction.- One self-sealing connector - delivery.

D. Accumulator charging

On each ground service panel:- One nitrogen charging connector - power accumulator.On the Blue ground service panel:- Two nitrogen charging connectors - parking/ultimate emergency brake accumulators.

5-4-3Page 1

Jul 01/21


NOTE : The nitrogen charging connectors for the normal and alternate braking systems areinstalled on the accumulators located on the main and center landing gear legs.

**ON A/C A340-500

2. Ground Service Panels


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Green System:Access Door 197FB

30.32 m(99.48 ft)

1.50 m(4.92 ft)

2.10 m(6.89 ft)

Yellow System:Access Door 196PB

25.02 m(82.09 ft)

1.70 m(5.58 ft)

1.80 m(5.91 ft)

Blue System:Access Door 195MB

22.47 m(73.72 ft)

1.50 m(4.92 ft)

1.75 m(5.74 ft)

A. Reservoir pressurization

On the Blue ground service panel:- One self-sealing connector - Green reservoir pressurization.- One self-sealing connector - Blue and Yellow reservoir pressurization.

B. Reservoir filling

On the Green ground service panel:- One self-sealing connector - reservoir filling.- One self-sealing connector - reservoir filling (hand pump).

C. Ground test

On each ground service panel:- One self-sealing connector - suction.- One self-sealing connector - delivery.

D. Accumulator charging

On each ground service panel:- One nitrogen charging connector - power accumulator.On the Blue ground service panel:- Two nitrogen charging connectors - parking/ultimate emergency brake accumulators.

5-4-3Page 2

Jul 01/21


NOTE : The nitrogen charging connectors for the normal and alternate braking systems areinstalled on the accumulators located on the main and center landing gear legs.

**ON A/C A340-500 A340-600

3. A/C Emergency Generation




RAT Safety-PinInstallation:Access Panel 633SL

42.00 m(137.80 ft)

14.20 m(46.59 ft)

4.15 m(13.62 ft)

5-4-3Page 3

Jul 01/21


**ON A/C A340-500 A340-600

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

FR53.4 FR53.5

FWD

A

A

197FB

F_AC_050403_1_0070101_01_00

Ground Service ConnectionsGreen System Ground Service Panel

FIGURE-5-4-3-991-007-A01

5-4-3Page 4

Jul 01/21


**ON A/C A340-500 A340-600

GND CNCTR−SELFSEALING,

B DELIVERY

GND CNCTRSELF−SEALING,

B SUCTION

PRESS GAGESPARK BRK ACCU

CHARGESVALVES

PARK BRKACCU

VALVE−MANDEPRESS, B RSVR

GND CNCTRNITROGENCHARGING

B POWER ACCU

PRESS GAGEB POWER ACCU

GND CNCTRSELF−SEALING,G RSVR PRESS

GND CNCTRSELF−SEALING,

B/Y RSVR PRESS

FWD

A

195MB

FR42 FR44

A

F_AC_050403_1_0080101_01_00

Ground Service ConnectionsBlue System Ground Service Panel

FIGURE-5-4-3-991-008-A01

5-4-3Page 5

Jul 01/21


**ON A/C A340-500 A340-600

VALVE−MANDEPRESS, Y RSVR

GND CNCTR−SELFSEALING, Y DELIVERY

PRESS GAGEY POWER ACCU

GND CNCTRNITROGEN CHARGING

Y POWER ACCU

RAT STOW PANELCARGO DOORSELECTOR MANIFOLD

HAND PUMPCARGO DOORS, Y

SIGHTGLASS

GND CNCTR−SELFSEALING, Y SUCTION

FWD

A

196PBFR44 FR47

A

F_AC_050403_1_0090101_01_00

Ground Service ConnectionsYellow System Ground Service Panel

FIGURE-5-4-3-991-009-A01

5-4-3Page 6

Jul 01/21


**ON A/C A340-500 A340-600

633AS

633AP

B

C

RAT UPLOCK SAFETY−PIN

RAT RETRACTED

RAT EXTENDED

RAM AIR TURBINE (RAT)

A

A

633SL

B

Z633

F_AC_050403_1_0120101_01_00

Ground Service ConnectionsRAT

FIGURE-5-4-3-991-012-A01

5-4-3Page 7

Jul 01/21


5-4-4 Electrical System

**ON A/C A340-500 A340-600

Electrical Servicing

1. A/C External Power


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

A/C External Power:Access Door 121EL


2.00 m(6.56 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


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

NLG Service Panel: 5GC6.58 m(21.59 ft)

0.50 m(1.64 ft) TBD


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

Jul 01/21


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

Jul 01/21


**ON A/C A340-500 A340-600

FR19 FR18

A

A

121EL

EXTERNAL POWER RECEPTACLESB

FR18

FR19

B925VU TYPICAL

F_AC_050404_1_0040101_01_01

Ground Service ConnectionsElectrical Service Panel

FIGURE-5-4-4-991-004-A01

5-4-4Page 3

Jul 01/21


5-4-5 Oxygen System

**ON A/C A340-500 A340-600

Oxygen Servicing

1. Oxygen Servicing


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: Replenishment by replacement of oxygen cylinders in the avionic compartment- 1 -- Option: External charging in the avionic compartment- 2 -- Option: External charging in the avionic compartment.One or two MIL-DTL 7891 standard service connections (external charging in the avionicscompartment).

NOTE : Internal charging connection provided.

5-4-5Page 1

Jul 01/21


**ON A/C A340-500 A340-600

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_0040101_01_01

Ground Service ConnectionsOxygen Servicing

FIGURE-5-4-5-991-004-A01

5-4-5Page 2

Jul 01/21


5-4-6 Fuel System

**ON A/C A340-500 A340-600

Fuel System

**ON A/C A340-600

1. Refuel/Defuel Control Panel


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel ControlPanel:Access Door 198FB

42.5 m(139.44 ft)

-1.4 m(4.59 ft)

2 m(6.56 ft)

A. Refuel/Defuel pressure/suction:- Maximum pressure: 50 psi (3.45 bar)- Maximum suction: 11 psi (0.76 bar).

B. Flow rate:- 2 couplings (total/min): 1576 l (416 US gal)- 4 couplings (total/min): 1438 l (380 US gal).

2. Refuel/Defuel Connectors


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel Coupling,Left:Access Door 522HB

37.1 m(121.72 ft)

-12.6 m(41.34 ft)

5 m(16.4 ft)

Refuel/Defuel Coupling,Right:Access Door 622HB

37.1 m(121.72 ft)

12.6 m(41.34 ft)

-5 m(16.4 ft)

A. Refuel/Defuel couplings:- Four standard 2.5 in. ISO 45 connections.

5-4-6Page 1

Jul 01/21


3. Overpressure Protector and NACA Flame Arrestor


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDOverpressure Protector(Wing)Access Panel 550DB(650DB)

47.03 m(154.3 ft)

28.7 m(94.16 ft)

28.7 m(94.16 ft)

5.75 m(18.86 ft)

NACA Flame Arrestor(Wing)Access Panel 550DB(650DB)

47.03 m(154.3 ft)

28.1 m(92.19 ft)

28.1 m592.19 ft)

5.7 m(18.7 ft)

Overpressure Protector(Trim Tank)Access Panel 346AB

72.93 m(239.27 ft)

7.10 m(23.29 ft)

7.10 m(23.29 ft)

5.7 m(18.7 ft)

NACA Flame Arrestor(Trim Tank)Access Panel 346AB

72.93 m(239.27 ft)

7.10 m(23.29 ft)

7.10 m(23.29 ft)

5.7 m(18.7 ft)

**ON A/C A340-500

4. Refuel/Defuel Control Panel


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel ControlPanel:Access Door 198FB

37.2 m(122.05 ft)

-1.4 m(4.59 ft)

2 m(6.56 ft)

A. Refuel/Defuel pressure/suction:- Maximum pressure: 50 psi (3.45 bar)- Maximum suction: 11 psi (0.76 bar).

B. Flow rate:- 2 couplings (total/min): 1576 l (416 US gal)- 4 couplings (total/min): 1438 l (380 US gal).

5-4-6Page 2

Jul 01/21


5. Refuel/Defuel Connectors


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel Coupling,Left:Access Door 522HB

31.4 m(103.02 ft)

12.6 m(41.34 ft)

-5 m(16.4 ft)

Refuel/Defuel Coupling,Right:Access Door 622HB

31.4 m(103.02 ft)

-12.6 m(41.34 ft)

5 m(16.4 ft)

A. Refuel/Defuel couplings:- Four standard 2.5 in. ISO 45 connections.

6. Overpressure Protector and NACA Flame Arrestor


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDOverpressure Protector(Wing)Access Panel 550DB(650DB)

41.73 m(136.91 ft)

28.7 m(94.16 ft)

28.7 m(94.16 ft)

5.75 m(18.86 ft)

NACA Flame Arrestor(Wing)Access Panel 550DB(650DB)

41.73 m(136.91 ft)

28.1 m(92.19 ft)

28.1 m592.19 ft)

5.7 m(18.7 ft)

Overpressure Protector(Trim Tank)Access Panel 346AB

65.5 m(214.9 ft)

7.10 m(23.29 ft)

7.10 m(23.29 ft)

5.7 m(18.7 ft)

NACA Flame Arrestor(Trim Tank)Access Panel 346AB

65.5 m(214.9 ft)

7.10 m(23.29 ft)

7.10 m(23.29 ft)

5.7 m(18.7 ft)

5-4-6Page 3

Jul 01/21


**ON A/C A340-500 A340-600

A

198DB

ON A/C A340−50001

ON A/C A340−60002

NOTE:

01

02

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 ACT 2ACT 1

ACT 2ACT 1

ACTCTR

ACT 1

CTR

FQI DISPLAY

REFUEL/DEFUEL VALVES

LOUTER INNER 1 INNER 2 INNER 3 INNER 4 ROUTEROPEN

SHUT

REFUEL/DEFUEL VALVES

TRIM CTR RCT

MANUALREFUEL

DEFUEL

AUTOREFUEL

OFF

MODE SELECT

APU EMERGENCY

OPEN

SHUT

HIGH LEVEL TEST

SHUTDOWNTRANSFER

DECREASE

INCREASE

PRESELECT

NORMAL

BATTERY

POWERSUPPLY

OVERFLOWFAULT

PRESELECT (PFQ)

ACTUAL (FOB)

STATUS

LOUTER INNER 1 INNER 2 INNER 3

HILEVEL >

HILEVEL >

TRIM CTR RCT

INNER 4 ROUTER

kg

kg

FR53.2FR53.4

A

F_AC_050406_1_0170101_01_00

Ground Service ConnectionsRefuel/Defuel Control PanelFIGURE-5-4-6-991-017-A01

5-4-6Page 4

Jul 01/21


**ON A/C A340-500 A340-600

522HB(622HB)

A

TYPICAL

A

REFUEL/DEFUELCOUPLINGS

REFUEL/DEFUELCOUPLING CAP

REFUEL/DEFUELCOUPLING CAP

F_AC_050406_1_0190101_01_01

Ground Service ConnectionsRefuel/Defuel Coupling

FIGURE-5-4-6-991-019-A01

5-4-6Page 5

Jul 01/21


**ON A/C A340-500 A340-600

C

OVERPRESSURE PROTECTOR

A

NACA FLAME ARRESTOR

B

A

A

FWD

LH SIDE SHOWNRH SIDE SYMMETRICAL

C

B

RIB37

RIB38

RIB39

550CB(650CB)

550DB(650DB)

F_AC_050406_1_0040101_01_00

Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor - Wing

FIGURE-5-4-6-991-004-A01

5-4-6Page 6

Jul 01/21


**ON A/C A340-500 A340-600

B

TRIM−TANK NACA VENT

TRIM−TANK OVERPRESSURE

BOTTOM SKIN

A

Z343

346AB

FWD

A

B

RIB19RIB18

F_AC_050406_1_0200101_01_00

Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor - Trim Tank

FIGURE-5-4-6-991-020-A01

5-4-6Page 7

Jul 01/21


5-4-7 Pneumatic System

**ON A/C A340-500 A340-600

Pneumatic Servicing

**ON A/C A340-600

1. High Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

HP Connectors:Access Door 193DB

29.71 m(97.47 ft)

0.35 m(1.15 ft)

1.75 m(5.74 ft)

A. Connectors:- Two standard 3 in. ISO 2026 connections.

2. Low Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

LP Connector:Access Door 193BB


1.8 m(5.91 ft)

LP Connector:Access Door 193GB

28.75 m(94.32 ft)

0.63 m(2.07 ft)

1.8 m(5.91 ft)

A. Connectors:- Two standard 8 in. SAE AS4262 connections.

5-4-7Page 1

Jul 01/21


**ON A/C A340-500

3. High Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

HP Connectors:Access Door 193DB

23.41 m(76.8 ft)

0.35 m(1.15 ft)

1.75 m(5.74 ft)

A. Connectors:- Two standard 3 in. ISO 2026 connections.

4. Low Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

LP Connector:Access Door 193BB


1.8 m(5.91 ft)

LP Connector:Access Door 193GB

23.45 m(76.94 ft)

0.63 m(2.07 ft)

1.8 m(5.91 ft)

A. Connectors:- Two standard 8 in. SAE AS4262 connections.

5-4-7Page 2

Jul 01/21


**ON A/C A340-500 A340-600

B

193DB

193GB

193BB A

B

FR40

AHP CONNECTOR

LP CONNECTOR

F_AC_050407_1_0030101_01_00

Ground Service ConnectionsLP and HP Ground Connectors

FIGURE-5-4-7-991-003-A01

5-4-7Page 3

Jul 01/21


5-4-8 Oil System

**ON A/C A340-500 A340-600

Oil Servicing

**ON A/C A340-600

1. RR TRENT 500 Series Engine

A. Engine Oil Replenishment:One gravity filling cap and one pressure filling connection per engine.


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Engine 1:Access Door: 416BR

36.30 m(119.09 ft)

17.85 m(58.56 ft)

3.15 m(10.33 ft)


29.70 m(97.44 ft)

7.95 m(26.08 ft)

1.60 m(5.25 ft)


29.70 m(97.44 ft)

10.80 m(35.43 ft)

1.60 m(5.25 ft)


36.30 m(119.09 ft)

20.70 m(67.91 ft)

3.15 m(10.33 ft)

(1) Approximate tank capacity:- Full level: 23.70 l (6.26 US gal).- Usable: 15.90 l (4.20 US gal).

B. IDG Oil Replenishment:One pressure filling connection per engine.


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Engine 1:Access Door: 415CL

36.97 m(121.29 ft)

19.66 m(64.50 ft)

1.85 m(6.07 ft)

5-4-8Page 1

Jul 01/21



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND


30.36 m(99.61 ft)

9.76 m(32.02 ft)

0.80 m(2.62 ft)


30.36 m(99.61 ft)

8.98 m(29.46 ft)

0.80 m(2.62 ft)


36.97 m(121.29 ft)

18.87 m(61.91 ft)

1.85 m(6.07 ft)

(1) IDG oil replenishment:- one ozone self-sealing pressure fill and overfill connector.

(2) Max delivery pressure:- 2.41 bar (34.95 psi).

(3) Approximate max oil capacity of the IDG:- 6.80 l (1.80 US gal).

C. Starter Oil Replenishment:One filling connection per engine.


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDEngine 1:Access Door: 415AL (416AR)

36.30 m(119.09 ft)

19.72 m(64.70 ft)

1.80 m(5.91 ft)

Engine 2:Access Door: 425AL (426AR)

29.70 m(97.44 ft)

9.82 m(32.22 ft)

0.77 m(2.53 ft)


29.70 m(97.44 ft)

8.92 m(29.27 ft)

0.77 m(2.53 ft)


36.30 m(119.09 ft)

18.82 m(61.75 ft)

1.80 m(5.91 ft)

(1) Pneumatic starter, oil replenishment:- one gravity filling plug.

5-4-8Page 2

Jul 01/21


(2) Approximate max oil capacity of the starter:- 0.40 l (0.11 US gal).

**ON A/C A340-500

2. RR TRENT 500 Series Engine

A. Engine Oil Replenishment:One gravity filling cap and one pressure filling connection per engine.


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND


31.00 m(101.71 ft)

17.85 m(58.56 ft)

3.15 m(10.33 ft)


24.42 m(80.12 ft)

7.95 m(26.08 ft)

1.60 m(5.25 ft)


24.42 m(80.12 ft)

10.80 m(35.43 ft)

1.60 m(5.25 ft)


31.00 m(101.71 ft)

20.70 m(67.91 ft)

3.15 m(10.33 ft)

(1) Approximate tank capacity:- Full level: 23.70 l (6.26 US gal).- Usable: 15.90 l (4.20 US gal).

B. IDG Oil Replenishment:One pressure filling connection per engine.


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND


31.66 m(103.87 ft)

19.66 m(64.50 ft)

1.85 m(6.07 ft)


25.05 m(82.19 ft)

9.76 m(32.02 ft)

0.80 m(2.62 ft)

5-4-8Page 3

Jul 01/21



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND


25.05 m(82.19 ft)

8.98 m(29.46 ft)

0.80 m(2.62 ft)


31.66 m(103.87 ft)

18.87 m(61.91 ft)

1.85 m(6.07 ft)

(1) IDG oil replenishment:- one ozone self-sealing pressure fill and overfill connector.

(2) Max delivery pressure:- 2.41 bar (34.95 psi).

(3) Approximate max oil capacity of the IDG:- 6.80 l (1.80 US gal).

C. Starter Oil Replenishment:One filling connection per engine.


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDEngine 1:Access Door: 415AL (416AR)

31.00 m(101.71 ft)

19.72 m(64.70 ft)

1.80 m(5.91 ft)


24.42 m(80.12 ft)

9.82 m(32.22 ft)

0.77 m(2.53 ft)


24.42 m(80.12 ft)

8.92 m(29.27 ft)

0.77 m(2.53 ft)


31.00 m(101.71 ft)

18.82 m(61.75 ft)

1.80 m(5.91 ft)

(1) Pneumatic starter, oil replenishment:- one gravity filling plug.

(2) Approximate max oil capacity of the starter:- 0.40 l (0.11 US gal).

5-4-8Page 4

Jul 01/21


**ON A/C A340-500 A340-600

A

SIGHT GLASS

B

FULL FULL

LIT

RE

S R

EQ

UIR

ED

US

QU

AR

TS

RE

QU

IRE

D

5

4

3

2

1

5

4

3

2

1

FWD

OILFILLER

CAP

OILTANK

BA

416BR426BR436BR446BR

(ENGINE 1)(ENGINE 2)(ENGINE 3)(ENGINE 4)

F_AC_050408_1_0190101_01_00

Ground Service ConnectionsEngine Oil Tank - RR TRENT 500 Series Engine

FIGURE-5-4-8-991-019-A01

5-4-8Page 5

Jul 01/21


**ON A/C A340-500 A340-600

OVERFILL DRAINCONNECTOR

PRESSUREFILL CONNECTOR

B

B

A340

OVER FULL

ADDOIL

ADDOIL

A

STABLE OIL

FWD

A

445CL

415CL425CL435CL


SIGHT GLASS

F_AC_050408_1_0200101_01_00

Ground Service ConnectionsIDG Oil Tank - RR TRENT 500 Series Engine

FIGURE-5-4-8-991-020-A01

5-4-8Page 6

Jul 01/21


**ON A/C A340-500 A340-600

OIL FILLPLUG

EXTERNALGEARBOXMODULE

OIL LEVELOVERFLOW

PLUGMAGNETIC CHIPDETECTOR

DRAINPLUG

PNEUMATICSTARTER

A

A

445AL

415AL425AL435AL


446AR

416AR426AR436AR


F_AC_050408_1_0210101_01_00

Ground Service ConnectionsStarter Oil Tank - RR TRENT 500 Series Engine

FIGURE-5-4-8-991-021-A01

5-4-8Page 7

Jul 01/21


**ON A/C A340-500 A340-600

APU Oil Servicing

**ON A/C A340-600

1. APU Oil Servicing:APU oil gravity filling cap.




APU OilReplenishment:Access Doors:316AR, 315AL

71 m(232.94 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 A340-500

2. APU Oil Servicing:APU oil gravity filling cap.




APU OilReplenishment:Access Doors:316AR, 315AL

63.5 m(208.33 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 8

Jul 01/21


**ON A/C A340-500 A340-600

OIL RESERVOIRGRAVITY FILL

PORT

PRESSUREFILL PORT

OIL SIGHTGLASS

FR98

FR94

A

A

316AR

315AL

F_AC_050408_1_0230101_01_00

Ground Service ConnectionsAPU Oil Servicing

FIGURE-5-4-8-991-023-A01

5-4-8Page 9

Jul 01/21


5-4-9 Potable Water System

**ON A/C A340-600

Potable Water Servicing

1. Potable Water Servicing




Potable-WaterService Panel:Access Door 154BR

58.75 m(192.75 ft)

0.5 m(1.64 ft)

3.5 m(11.48 ft)



A. Connectors- Roylin, 3/4 in. (ISO 17775).

B. Capacity- 1 070 l (282.66 US gal).

C. Filling Pressure and Flow Rate- Maximum filling pressure: 1.72/2.07 bar (25/30 psi)- Flow rate: 87.5 l/min (23.12 US gal/min).

5-4-9Page 1

Jul 01/21


**ON A/C A340-600

OVERFLOW NIPPLE

DRAIN NIPPLE

B

A

FILL/DRAINCONTROL HANDLE

MAINTENANCE DOORLIMIT−SWITCH

CONTROL HANDLE

FILL/DRAINNIPPLE

CAPASSEMBLY

POTABLE−WATER SERVICE PANEL

INDICATIONPANEL

FWD POTABLE−WATER DRAIN PANEL

DRAIN VALVECONTROL HANDLE

154BR

A

B

133BL

FR63

FR64

FR26.1

FR26.2

F_AC_050409_1_0330101_01_00

Ground Service ConnectionsPotable-Water Ground Service Panels

FIGURE-5-4-9-991-033-A01

5-4-9Page 2

Jul 01/21


**ON A/C A340-600

POTABLE WATERTANK

OVERFLOW LINE

ANOTE:

TYPICAL01

01

POTABLE WATERFILL/DRAIN LINE

FR59

FR73A

A

A

Z152

Z160

Z172

AFT CARGO DOOR

BULK CARGO DOOR

FR57

FR53.2 FR65

FR80

FR76

FR72

FR56.2

FR57.1

F_AC_050409_1_0340101_01_00

Ground Service ConnectionsPotable-Water Tanks LocationFIGURE-5-4-9-991-034-A01

5-4-9Page 3

Jul 01/21


**ON A/C A340-500

Potable Water Servicing

1. Potable Water Servicing




Potable-WaterService Panel:Access Door 154BR

51.32 m(168.37 ft)

0.5 m(1.64 ft)

3.5 m(11.48 ft)



A. Connectors- Roylin, 3/4 in. (ISO 17775)

B. Capacity- 700 l (184.92 US gal).

C. Filling Pressure and Flow Rate- Maximum filling pressure: 1.72/2.07 bar (25/30 psi)- Flow rate: 87.5 l/min (23.12 US gal/min).

5-4-9Page 4

Jul 01/21


**ON A/C A340-500

OVERFLOW NIPPLE

DRAIN NIPPLE

B

A

FILL/DRAINCONTROL HANDLE

MAINTENANCE DOORLIMIT−SWITCH

CONTROL HANDLE

FILL/DRAINNIPPLE

CAPASSEMBLY

POTABLE−WATER SERVICE PANEL

INDICATIONPANEL

FWD POTABLE−WATER DRAIN PANEL

DRAIN VALVECONTROL HANDLE

FR63

FR64

133BL

154BR

A

FR33

FR34

B

F_AC_050409_1_0350101_01_00

Ground Service ConnectionsPotable-Water Ground Service Panels

FIGURE-5-4-9-991-035-A01

5-4-9Page 5

Jul 01/21


**ON A/C A340-500

POTABLE WATERTANK

OVERFLOW LINE

ANOTE:

TYPICAL01

01

POTABLE WATERFILL/DRAIN LINE

FR59

FR73

Z152

Z160

Z172

AFT CARGO DOOR

BULK CARGO DOOR

FR56.3

A

A

FR80

FR53.2FR65

A

FR72

FR76

FR56.4

FR54

F_AC_050409_1_0360101_01_00

Ground Service ConnectionsPotable-Water Tanks LocationFIGURE-5-4-9-991-036-A01

5-4-9Page 6

Jul 01/21


5-4-10 Waste Water System

**ON A/C A340-500 A340-600

Waste Water Servicing

**ON A/C A340-600

1. Waste Water Servicing


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDWaste Water GroundService Panel:Access Door 171AL

60.61 m(198.85 ft)

0.10 m(0.33 ft)

4.00 m(13.12 ft)

A. Connectors:- Flushing and filling: Roylin, 1 in. (ISO 17775).- Draining: Roylin, 4 in. (ISO 17775).

B. Capacity (four tanks - basic configuration):- 1050 l (277.38 US gal).

C. Operating pressure:- 0.07 bar (1.02 psi)/0.70 bar (10.15 psi).

D. Flow rate:- 87.5 l/min (23.1 US gal/min).

**ON A/C A340-500

2. Waste Water Servicing


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDWaste Water GroundService Panel:Access Door 171AL

53.18 m(174.48 ft)

0.10 m(0.33 ft)

4.00 m(13.12 ft)

A. Connectors:- Flushing and filling: Roylin, 1 in. (ISO 17775).- Draining: Roylin, 4 in. (ISO 17775).

5-4-10Page 1

Jul 01/21


B. Capacity (four tanks - basic configuration):- 1050 l (277.38 US gal).

C. Operating pressure:- 0.07 bar (1.02 psi)/0.70 bar (10.15 psi).

D. Flow rate:- 87.5 l/min (23.1 US gal/min).

5-4-10Page 2

Jul 01/21


**ON A/C A340-500 A340-600

OPEN

CLOSE

DRAIN−VALVECONTROL LEVERS

WASTEDRAIN−LINE VALVE

TANK 1 FILLAND RINSE

CONNECTION


CONNECTION


CONNECTION


CONNECTION LIMIT SWITCHWASTE−PANEL

A

FWD

FR75

FR59

A171AL

FR74 FR73

LH RH

F_AC_050410_1_0030101_01_00

Ground Service ConnectionsWaste Water Ground Service Panel

FIGURE-5-4-10-991-003-A01

5-4-10Page 3

Jul 01/21


**ON A/C A340-500 A340-600

FR73

FR65

BULK CARGO DOOR

Z160

Z172

161AZ

A

FR76

WASTE TANK

FR73

FR76

AF_AC_050410_1_0070101_01_00

Ground Service ConnectionsWaste Tanks Location

FIGURE-5-4-10-991-007-A01

5-4-10Page 4

Jul 01/21


5-4-11 Cargo Control Panels

**ON A/C A340-500 A340-600

Cargo Control Panels

**ON A/C A340-600

1. Cargo Control Panels




FWD CLS* Panel:Access Door 122DR

14.17 m(46.49 ft)

2.60 m(8.53 ft)

3.10 m(10.17 ft)

FWD Cargo DoorPanel:Access Door 122CR

13.87 m(45.51 ft)

2.40 m(7.87 ft)

3.50 m(11.48 ft)

AFT CLS* Panel:Access Door152MR

59.60 m(195.54 ft)

2.60 m(8.53 ft)

4.70 m(15.42 ft)

AFT Cargo DoorPanel:Access Door 152NR

59.20 m(194.23 ft)

2.40 m(7.87 ft)

4.10 m(13.45 ft)

NOTE : * CLS - CARGO LOADING SYSTEMS

**ON A/C A340-500

2. Cargo Control Panels




FWD CLS* Panel:Access Door 122DR

14.17 m(46.49 ft)

2.60 m(8.53 ft)

3.10 m(10.17 ft)

FWD Cargo DoorPanel:Access Door 122CR

13.87 m(45.51 ft)

2.40 m(7.87 ft)

3.50 m(11.48 ft)

AFT CLS* Panel:Access Door152MR

51.94 m(170.41 ft)

2.60 m(8.53 ft)

4.70 m(15.42 ft)

5-4-11Page 1

Jul 01/21





AFT Cargo DoorPanel:Access Door 152NR

51.64 m(169.42 ft)

2.40 m(7.87 ft)

4.10 m(13.45 ft)

NOTE : * CLS - CARGO LOADING SYSTEMS

5-4-11Page 2

Jul 01/21


**ON A/C A340-500 A340-600

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_0060101_01_00

Forward Cargo Control PanelsFIGURE-5-4-11-991-006-A01

5-4-11Page 3

Jul 01/21


**ON A/C A340-500 A340-600

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_0070101_01_00

Aft Cargo Control PanelsFIGURE-5-4-11-991-007-A01

5-4-11Page 4

Jul 01/21


5-5-0 Engine Starting Pneumatic Requirements

**ON A/C A340-500 A340-600

Engine Starting Pneumatic Requirements

1. Engine Starting Pneumatic Requirements.To determinate the airflow required at ground connection, refer to the example given in FIGURE5-5-0-991-003-A.

For engine starting pneumatic requirements for:- Low ambient temperatures, refer to 05-05-01,- Medium ambient temperatures, refer to 05-05-02,- High ambient temperatures, refer to 05-05-03.

5-5-0Page 1

Jul 01/21


**ON A/C A340-500 A340-600

EXAMPLE TO DETERMINATE THE AIRFLOW REQUIRED AT THE FUSELAGE CONNECTION:−FOR AN AIR START UNIT DELIVERING 60 PSIA (4.14 BARS) AIR PRESSURE AT THE

FUSELAGE CONNECTOR

1. DRAW AN HORIZONTAL LINE FROM THE SUPPLIED AIR PRESSURE (60 PSIA (4.14 BARS)).2. FROM THE INTERSECTION WITH THE AIR SUPPLY TEMPERATURE AT FUSELAGE

CONNECTION (220?C (428?F)), DRAW A VERTICAL LINE.3. THE INTERSECTION WITH THE HORIZONTAL AXIS GIVES THE REQUIRED AIRFLOW AT GROUND

CONNECTION (125 kg/min (2.08 kg/s)).

−AT A SUPPLIED AIR TEMPERATURE OF 220?C (428?F) AT THE FUSELAGE CONNECTOR

2.5

5

4.5

4

3.5

3

40

50

60

70

PSI

GROUND CART FLOW(Kg/s)

BARSGROUND CART PRESSURE

AIR TEMPERATUREGROUND CART OUTLET

0?C 85?C 100?C

220?C180?C150?C

STARTING TIME = 90 Sec



0.50 1.00 3.503.002.502.001.50 kg/s

30 60 12090 kg/min210180150


F_AC_050500_1_0030101_01_00

Engine Starting Pneumatic RequirementsFIGURE-5-5-0-991-003-A01

5-5-0Page 2

Jul 01/21


5-5-1 Low Ambient Temperatures

**ON A/C A340-500 A340-600

Low Ambient Temperatures

1. This section provides the engine starting pneumatic requirements for a temperature of -40˚C(-40˚F).

5-5-1Page 1

Jul 01/21


**ON A/C A340-500 A340-600

0.52.5

1 2 2.5 3 3.5

5

4.5

4

3.5

3

40

50

60

70

PSI



F_AC_050501_1_0050101_01_00

1.5






0?C 85?C 100?C

220?C180?C150?C

Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- RB 211 TRENT 500 series engine

FIGURE-5-5-1-991-005-A01

5-5-1Page 2

Jul 01/21


5-5-2 Medium Ambient Temperatures

**ON A/C A340-500 A340-600

Medium Ambient Temperatures

1. This section provides the engine starting pneumatic requirements for a temperature of +15˚C(+59˚F).

5-5-2Page 1

Jul 01/21


**ON A/C A340-500 A340-600

20.5

2.5

1 1.5 2 2.5 3 3.5

5

4.5

4

3.5

3

30

40

50

60

70

PSI



F_AC_050502_1_0050101_01_00





0?C 85?C

180?C150?C

100?C

220?C


Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- RB 211 TRENT 500 series engine

FIGURE-5-5-2-991-005-A01

5-5-2Page 2

Jul 01/21


5-5-3 High Ambient Temperatures

**ON A/C A340-500 A340-600

High Ambient Temperatures

1. This section provides the engine starting pneumatic requirements for a temperature upper +50˚C(+122˚F).

5-5-3Page 1

Jul 01/21


**ON A/C A340-500 A340-600

20.5

2.5

1 1.5 2 2.5 3 3.5

5

4.5

4

3.5

3

30

40

50

60

70

PSI



F_AC_050503_1_0050101_01_00






85?C 100?C 150?C

180?C 220?C

Engine Starting Pneumatic RequirementsHigh Ambient Temperature +50˚C (+122˚F) -- RB 211 TRENT 500 series engine

FIGURE-5-5-3-991-005-A01

5-5-3Page 2

Jul 01/21


5-6-0 Ground Pneumatic Power Requirements

**ON A/C A340-500 A340-600

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 Connection

GSE Ground Service Equipment

IFE In-Flight Entertainment

LP Low PressureLPGC Low Pressure Ground Connection

OAT 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.

5-6-0Page 1

Jul 01/21


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

5-6-0-991-005-A)- Cooling (pull down) the cabin, initially at OAT, down to 27 ˚C (80.6 ˚F) (see FIGURE

5-6-0-991-006-A).

5-6-0Page 2

Jul 01/21


**ON A/C A340-500 A340-600

AIR

FLO

W A

T G

C (

kg/s

)

AIR

FLO

W A

T G

C (

lb/s

)

PULL UP PERFORMANCE

1.2

1.4

1.6

1.8

2.0

2.2

2.4

2.6

2.8

3.0

3.2

3.4

3.6

30 6040 50 70 90 12080 100 110

3.0

3.5

4.0

4.5

5.0

5.5

6.0

6.5

7.0

7.5

TIME TO HEAT CABIN TO +21? C (+69.8? F) ON GROUND (min)

MAXIMUM AIR FLOW

OAT ISA −38? C (−36.4? F); GC INLET +70? C (+158? F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON

F_AC_050600_1_0050101_01_00

Ground Pneumatic Power RequirementsHeating

FIGURE-5-6-0-991-005-A01

5-6-0Page 3

Jul 01/21


**ON A/C A340-500 A340-600

AIR

FLO

W A

T G

C (

kg/s

)

AIR

FLO

W A

T G

C (

lb/s

)

1.2

1.4

1.6

1.8

2.0

2.2

2.4

2.6

2.8

3.0

3.2

3.4

3.6

0 30 90 150

3.0

3.5

4.0

4.5

5.0

5.5

6.0

6.5

7.0

7.5

60

MAXIMUM AIR FLOW

OAT ISA +23? C (+73.4? F); GC INLET +2? C (+35.6? F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON

OAT ISA +23? C (+73.4? F); GC INLET −10? C (+14? F); EMPTY CABIN; IFE OFF; NO SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON

120

PULL DOWN PERFORMANCE

TIME TO COOL CABIN TO +27? C (+80.6? F) ON GROUND (min)

F_AC_050600_1_0060101_01_00

Ground Pneumatic Power RequirementsCooling

FIGURE-5-6-0-991-006-A01

5-6-0Page 4

Jul 01/21


5-7-0 Preconditioned Airflow Requirements

**ON A/C A340-500 A340-600

Preconditioned Airflow Requirements

1. This section provides the preconditioned airflow rate and temperature needed to maintain the cabintemperature at 24 ˚C (75.2 ˚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

Jul 01/21


**ON A/C A340-500 A340-600

1.4

1.6

1.8

2.0

2.2

2.4

2.6

2.8

3.0

3.2

3.4

SETTINGS NOTINTENDED TO BE USED

FOR OPERATION

MAXIMUM AIRFLOW

0 5 10 15 20 25 30 35 40 45 50 55 60

COOLING/HEATING PERFORMANCE

AIR

FLO

W A

T G

C (

kg/s

)

AIR

FLO

W A

T G

C (

lb/s

)

INLET TEMPERATURE AT GC (? C)

30 40 50 60 70 80

INLET TEMPERATURE AT GC (? F)

90 100 110 120 130 140

3.5

4.0

4.5

5.0

5.5

6.0

6.5

7.0

OAT ISA; EMPTY CABIN; IFE ON; LIGHTS ON; NO 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

EXAMPLE:COOLING CAPACITY CALCULATION:FOR THE CONDITIONS "C", THE COOLING CAPACITY OF 1.6 kg/s x 1 kJ/(kg.? C) x (24 − 10) = 22.4 kW(OR 6.7 TONS COOLING CAPACITY) IS NEEDED TO MAINTAIN THE CABIN TEMPERATURE AT 24? C (75.2? F)(1.6 kg/s AT 10? C (50? F) FOR AIR AT GC INLET).

C H

F_AC_050700_1_0040101_01_01

Preconditioned Airflow RequirementsFIGURE-5-7-0-991-004-A01

5-7-0Page 2

Jul 01/21


5-8-0 Ground Towing Requirements

**ON A/C A340-500 A340-600

Ground Towing Requirements

1. This section provides information on aircraft towing.

The A340-500/-600 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 A340-500 and -600 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 40 400 daN (90 823 lbf),- A torsion pin calibrated at 4 800 m.daN (424 836 lbf.in).The towing head is designed according to ISO 8267-1, cat. IV.

5-8-0Page 1

Jul 01/21


**ON A/C A340-500 A340-600

EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A340−500 OR −600 AT 380 000 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 (380 000 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 (30 300 kg),− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (53 100 kg).

40

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

390

350

310

270

230

190

150

TOTAL TRACTION WHEEL LOAD (x 1 000 kg) No. OF ENGINES AT IDLE SLOPE ( % )

ICE = 0.05WET C

ONCRETE

= 0.

57

DR

Y C

ON

CR

ETE

=

0.8

35

30

1.5% SLOPE 3802 ENGINES ON30.3

53.1

BREAKAWAY RESISTANCE 4%# OF ENGINES ON FOR PB: 2ENGINE THRUST 876.3 daN

HARD SNOW = 0.2

DR

AW

BA

R P

ULL

(x

1 00

0 kg

)

A/C

WE

IGH

T (

x 1

000

kg)

F_AC_050800_1_0100101_01_01

Ground Towing RequirementsFIGURE-5-8-0-991-010-A01

5-8-0Page 2

Jul 01/21


5-9-0 De-Icing and External Cleaning

**ON A/C A340-500 A340-600

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)

A340-500373 m2

(4 015 ft2)11 m2

(118 ft2)90 m2

(969 ft2)103 m2

(1 109 ft2)

A340-600373 m2

(4 015 ft2)11 m2

(118 ft2)90 m2

(969 ft2)103 m2

(1 109 ft2)

AIRCRAFT TYPEFuselage Top Surface

(Top Third - 120˚ Arc)

Nacelle and Pylon(Top Third - 120˚ Arc)

(All Engines)Total De-Iced Area

A340-500338 m2

(3 638 ft2)83 m2

(893 ft2)998 m2

(10 742 ft2)

A340-600382 m2

(4 112 ft2)83 m2

(893 ft2)1 042 m2

(11 216 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)

A340-500373 m2

(4 015 ft2)412 m2

(4 435 ft2)11 m2

(118 ft2)90 m2

(969 ft2)90 m2

(969 ft2)

A340-600373 m2

(4 015 ft2)412 m2

(4 435 ft2)11 m2

(118 ft2)90 m2

(969 ft2)90 m2

(969 ft2)

5-9-0Page 1

Jul 01/21


AIRCRAFT TYPEVTP

(Both Sides)Fuselage andBelly Fairing

Nacelle and Pylon(All Engines) Total Cleaned Area

A340-500103 m2

(1 109 ft2)1 024 m2

(11 022 ft2)244 m2

(2 626 ft2)2 363 m2

(25 435 ft2)

A340-600103 m2

(1 109 ft2)1 156 m2

(12 443 ft2)244 m2

(2 626 ft2)2 494 m2

(26 845 ft2)

NOTE : Dimensions are approximate.

5-9-0Page 2

Jul 01/21


OPERATING CONDITIONS

6-1-0 Engine Exhaust Velocities and Temperatures

**ON A/C A340-500 A340-600

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

Jul 01/21


6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power

**ON A/C A340-500 A340-600

Engine Exhaust Velocities Contours - Ground Idle Power

1. This section gives engine exhaust velocities contours at ground idle power.

6-1-1Page 1

Jul 01/21


**ON A/C A340-500 A340-600

150 fps 100 fps 50 fps

FEET

METERS

50 100 150

15 30 450

0



m ft

10

5

40

30

20

10

m ft

10

5

40

30

10

20

0

0

PLAN

ELEVATION

LOW IDLE POWER (100 fps = 68 mph = 109 kmph)

F_AC_060101_1_0050101_01_00

Engine Exhaust VelocitiesGround Idle Power - RR TRENT 500 series engine

FIGURE-6-1-1-991-005-A01

6-1-1Page 2

Jul 01/21


6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power

**ON A/C A340-500 A340-600

Engine Exhaust Temperatures Contours - Ground Idle Power

1. This section gives engine exhaust temperatures contours at ground idle power.

6-1-2Page 1

Jul 01/21


**ON A/C A340-500 A340-600

LOW IDLE POWER

50?C(122?F)

40?C(104?F)

30?C(86?F)

FEET

METERS

50 100 150

15 30 450

0

ft

m ft

10

5

40

30

10

20

0

PLAN

ELEVATION

40?C

30?C(86?F)

40?C(104?F)

30?C(86?F)

50?C(122?F)

F_AC_060102_1_0050101_01_00

50?C(122?F)

(104?F)

40

30

20

10

0

10

5

m

Engine Exhaust TemperaturesGround Idle Power - RR TRENT 500 series engine

FIGURE-6-1-2-991-005-A01

6-1-2Page 2

Jul 01/21


6-1-3 Engine Exhaust Velocities Contours - Breakaway Power

**ON A/C A340-500 A340-600

Engine Exhaust Velocities Contours - Breakaway Power

1. This section gives engine exhaust velocities contours at breakaway power.

6-1-3Page 1

Jul 01/21


**ON A/C A340-500 A340-600

50 fps100 fps

ELEVATION

20

80m ft

20

60

15

10

5

m ft40

10

5

0

METERS

FEET

0 15 30 45

15010050

60 75 90

200 250 300

BREAKAWAY POWER (100 fps = 60 mph = 109 Kmph)

PLAN

F_AC_060103_1_0050101_01_00

150 fps 50 fps100 fps

150 fps

40

20

0

0

Engine Exhaust VelocitiesBreakaway Power - RR TRENT 500 series engine

FIGURE-6-1-3-991-005-A01

6-1-3Page 2

Jul 01/21


6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power

**ON A/C A340-500 A340-600

Engine Exhaust Temperatures Contours - Breakaway Power

1. This section gives engine exhaust temperatures contours at breakaway power.

6-1-4Page 1

Jul 01/21


**ON A/C A340-500 A340-600

40?C(104?F)

30?C(86?F)

50?C(122?F)

0

METERS

FEET

0 15 30

10050

ELEVATION

BREAKAWAY POWER

PLAN

50?C(122?F)

40?C(104?F) (86?F)

F_AC_060104_1_0050101_01_00

m ft40

10

5

m

15

10

5

0

20

0

30?C

20

60

40

ft

Engine Exhaust TemperaturesBreakaway Power - RR TRENT 500 series engine

FIGURE-6-1-4-991-005-A01

6-1-4Page 2

Jul 01/21


6-1-5 Engine Exhaust Velocities Contours - Takeoff Power

**ON A/C A340-500 A340-600

Engine Exhaust Velocities Contours - Takeoff Power

1. This section gives engine exhaust velocities contours at takeoff power.

6-1-5Page 1

Jul 01/21


**ON A/C A340-500 A340-600

MA

X T

AK

E−

OF

F P

OW

ER

(10

0 fp

s =

68

mph

= 1

09 k

mph

)

105

350

90 300

75 250

60 200

45 150

30 100

15 50

0 0

ME

TE

RS

FE

ET

mft 80 60 40 20

5101520

(162

0 ft)

494

mT

O

(600

ft)

183

mT

O

50 fp

s10

0 fp

s15

0 fp

s

PLA

N

F_AC_060105_1_0050101_01_00

0

Engine Exhaust VelocitiesTakeoff Power - RR TRENT 500 series engine

FIGURE-6-1-5-991-005-A01

6-1-5Page 2

Jul 01/21


6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power

**ON A/C A340-500 A340-600

Engine Exhaust Temperatures Contours - Takeoff Power

1. This section gives engine exhaust temperatures contours at takeoff power.

6-1-6Page 1

Jul 01/21


**ON A/C A340-500 A340-600

m ft

20

40

60

15

10

5

0

METERS

FEET

0 15 30 45

15010050

60 75 90

200 250 300

(122?F)

PLAN

50?C(104?F)

40?C(86?F)30?C

MAX TAKE−OFF POWER

0

F_AC_060106_1_0050101_01_00

Engine Exhaust TemperaturesTakeoff Power - RR TRENT 500 series engine

FIGURE-6-1-6-991-005-A01

6-1-6Page 2

Jul 01/21


6-3-0 Danger Areas of Engines

**ON A/C A340-500 A340-600

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

Jul 01/21


6-3-1 Ground Idle Power

**ON A/C A340-500 A340-600

Ground Idle Power

1. This section provides danger areas of the engines at ground idle power conditions

6-3-1Page 1

Jul 01/21


**ON A/C A340-500 A340-600

(25 ft)7,6 m

(3 ft 8 in)1,1 m

30?TO 48,8 m (160 ft) AFT OF EXHAUST NOZZLES

INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER

EXHAUST DANGER AREA

ENTRY CORRIDOR

DEF0004201A

F_AC_060301_1_0050101_01_00

Danger Areas of EnginesRR TRENT 500 series engineFIGURE-6-3-1-991-005-A01

6-3-1Page 2

Jul 01/21


6-3-2 Breakaway Power

**ON A/C A340-500 A340-600

Breakaway Power

1. This section provides danger areas of the engines at breakaway conditions.

6-3-2Page 1

Jul 01/21


**ON A/C A340-500 A340-600

(25 ft)7,6 m

30?TO 82.3 m (270 ft) AFT OF EXHAUST NOZZLES

INTAKE SUCTION DANGER AREA BREAKWAY POWER

EXHAUST DANGER AREA

F_AC_060302_1_0050101_01_00


6-3-2Page 2

Jul 01/21


6-3-3 Takeoff Power

**ON A/C A340-500 A340-600

Takeoff Power

1. This section provides danger areas of the engines at max takeoff conditions.

6-3-3Page 1

Jul 01/21


**ON A/C A340-500 A340-600

(25 ft)7,6 m

30?TO 490,7 m (1610 ft) AFT OF EXHAUST NOZZLES

INTAKE SUCTION DANGER AREA MAX TAKE−OFF

EXHAUST DANGER AREA

F_AC_060303_1_0050101_01_00


6-3-3Page 2

Jul 01/21


6-4-0 APU Exhaust Velocities and Temperatures

**ON A/C A340-500 A340-600

APU Exhaust Velocities and Temperatures

1. APU Exhaust Velocities and Temperatures.

6-4-0Page 1

Jul 01/21


6-4-1 APU

**ON A/C A340-500 A340-600

APU - GARRETT

1. This section gives APU exhaust velocities and temperatures.

6-4-1Page 1

Jul 01/21


**ON A/C A340-500 A340-600

20

METERS

0

5 10 15FEET

0

10 20 30 40 50

0

60

0

20

METERS

0

5 10 15FEET

0

10 20 30 40 50

0

60

0

10

5

10

20

30

40

METERS FEET50

15 m/s(50 ft/s)18 m/s

(60 ft/s)24 m/s(80 ft/s)

30.5 m/s(100 ft/s)

46 m/s(150 ft/s)

61 m/s(200 ft/s)

10

5

10

20

30

40

METERS FEET50

93?C(200?F)121?C

(250?F)

149?C(300?F)

177?C(350?F)

204?C(400?F)

260?C(500?F)

315.5?C(600?F)

427?C(800?F)

15

15

F_AC_060401_1_0030101_01_00

Exhaust Velocities and TemperaturesGARRETT GTCP 331-600 (A)

FIGURE-6-4-1-991-003-A01

6-4-1Page 2

Jul 01/21


PAVEMENT DATA


**ON A/C A340-500 A340-600

General Information

1. A brief description of the pavement charts that follow will help in the 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 permitted 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 gives basic data on the landing-gear footprint configuration, MRW, tire dimensionsand pressures.Maximum Pavement Loads:Section 07-03-00 shows maximum vertical and horizontal pavement loads for specific criticalconditions at the tire-ground interfaces.Landing Gear Loading on Pavement:The curves related to the landing gear loading on pavement are not given in section 07-04-00.Because the relationship between the aircraft weight, the center of gravity and the landing gearloading on the pavement is not strictly linear, it cannot be shown in chart format.But you can find in section 07-03-00 the maximum vertical and horizontal pavement loads for somecritical conditions at the tire/ground interfaces for all the operational weight variants of the aircraft.For questions that are related to landing gear loading on pavement, contact Airbus.Flexible Pavement Requirements - US Army Corps of Engineers Design Method:The flexible pavement-requirements curves as per as U.S. Army Corps of Engineers Design Methodare not given in section 07-05-00 since the related data is available through free software.Sections 07-02-00 and 07-03-00 gives all the inputs data required for the use of such software.For questions that are related to the flexible pavement requirements, contact Airbus.Flexible Pavement Requirements - LCN Conversion Method:The Load Classification Number (LCN) curves are not given in section 07-06-00 since the LCNsystem for the reporting pavement strength is old and are replaced by the ICAO recommendedACN/PCN system in 1983 and ACR/PCR system in 2020.For questions that are related to the LCN system, contact Airbus.Rigid Pavement Requirements - PCA (Portland Cement Association) Design Method:The rigid-pavement requirements curves as per as Portland Cement Association Design Method arenot given in section 07-07-00 since the related data is available through free software.Sections 07-02-00 and 07-03-00 gives all the inputs data required for the use of such software.For questions that are related to the rigid pavement requirements, contact Airbus.

7-1-0Page 1

Jul 01/21


Rigid Pavement Requirements - LCN Conversion:The Load Classification Number (LCN) curves are not given in section 07-08-00 since the LCNsystem for the reporting pavement strength is old and are replaced by the ICAO recommendedACN/PCN system in 1983 and ACR/PCR system in 2020.For questions that are related to the LCN system, contact Airbus.ACN/PCN Reporting System:Section 07-09-00 gives ACN data prepared according to the ACN/PCN system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations”.Eighth Edition July 2018, incorporating Amendments 1 to 14 and ICAO doc 9157, ”AerodromeDesign Manual”, part 3 ”Pavements” Second Edition 1983.The ACN/PCN system is applicable until November 2024.ACN is the Aircraft Classification Number and PCN is the related Pavement Classification Number.An aircraft with 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 calculated as the load on a single tire inflated to 1.25 MPa (181 psi)that can have the same pavement requirements as the aircraft.Computationally the ACN/PCN system uses the PCA program PDILB for rigid pavements and S-77-1for flexible pavements to calculate ACN values.The airport authority must select the method of pavement analysis.The results of their analysis should be reported with the following format:

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 Limitedto 1.25 MPa (181 psi)

D - Ultra LowZ - Low Pressure Limited to0.5 MPa (73 psi)

Section 07-09-00 shows the aircraft ACN values.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:

7-1-0Page 2

Jul 01/21


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)

ACR/PCR Reporting System:Section 07-10-00 gives ACR data prepared according to the ACR/PCR system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations”.Eight Edition July 2018, incorporating Amendments 1 to 15 and ICAO doc 9157, ”Aerodrome DesignManual”, part 3 ”Pavements” Third Edition 2021.The ACR/PCR system is effective from November 2020 and will be applicable in November 2024.ACR is the Aircraft Classification Rating and PCR is the related Pavement Classification Rating.An aircraft with an ACR less than or equal to the PCR can operate without restriction on thepavement.Numerically the ACR is two times the derived single-wheel load expressed in hundreds of kilograms.The derived single-wheel load is calculated as the load on a single tire inflated to 1.50 Mpa (218 psi)that can have the same pavement requirements as the aircraft.Computationally the ACR/PCR system relies on the Linear Elastic Analysis (LEA). The ACR arecomputed with the official ICAO-ACR software.States can start their own methods for PCR determination, which agree with the overall parametersof the ACR/PCR method.The results of their analysis should be reported with the following format:

PCR

PAVEMENT TYPESUBGRADECATEGORY

TIRE PRESSURECATEGORY

EVALUATIONMETHOD

R - Rigid A - High W - No Pressure Limit T - Technical

F - Flexible B - Medium

X - High PressureLimited to 1.75 MPa(254 psi)

U - Using Aircraft

C - Low

Y - Medium PressureLimited to 1.25 MPa(181 psi)

D - Ultra LowZ - Low Pressure Limitedto 0.5 MPa (73 psi)

Section 07-10-00 shows the aircraft ACR values.For flexible and rigid pavement, the four subgrade categories are defined based on the subgrademodulus of elasticity (E):

A. High Strength E = 200 MPa (29 008 psi)

B. Medium Strength E = 120 MPa (17 405 psi)

7-1-0Page 3

Jul 01/21


C. Low Strength E = 80 MPa (11 603 psi)

D. Ultra Low Strength E = 50 MPa (7 252 psi)

7-1-0Page 4

Jul 01/21


7-2-0 Landing Gear Footprint

**ON A/C A340-500 A340-600

Landing Gear Footprint

1. This section gives data about the landing gear footprint in relation to the aircraft MRW, tire sizesand pressures.The landing-gear footprint information is given for all the operational weight variants of the aircraft.

7-2-0Page 1

Jul 01/21


**ON A/C A340-600

0.81

4 m

(2.6

71 ft

)

10.6

84 m

(35.

052

ft)

1.17

6 m

(3.8

58 ft

)

1.39

7 m

(4.5

83 ft

)1.98

1 m

(6.4

99 ft

)

15 b

ar(2

18 p

si)

CE

NT

RA

LG

EA

RT

IRE

PR

ES

SU

RE

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

A340−

600

WV

000

366

200

kg(8

07 3

25 lb

)93

.5%

13.7

bar

(199

psi

)16

.1 b

ar(2

34 p

si)

45x1

80R

17 3

6PR

NO

SE

GE

AR

TIR

E S

IZE

1400

x530

R23

40P

R14

00x5

30R

23 4

0PR

CE

NT

RA

LG

EA

RT

IRE

SIZ

E

15 b

ar(2

18 p

si)

A340−

600

WV

001

369

200

kg(8

13 9

50 lb

)93

.4%

13.7

bar

(199

psi

)

16.1

bar

(234

psi

)A

340−

600

WV

101

381

200

kg(8

40 4

00 lb

)92

.3%

13.9

bar

(202

psi

)

A340−

600

WV

102

369

200

kg(8

13 9

50 lb

)93

.4%

13.9

bar

(202

psi

)

A340−

600

WV

103

366

200

kg(8

07 3

25 lb

)93

.5%

13.9

bar

(202

psi

)

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)14

00x5

30R

23 4

0PR

16.1

bar

(234

psi

)14

00x5

30R

23 4

0PR

16.1

bar

(234

psi

)14

00x5

30R

23 4

0PR

16.1

bar

(234

psi

)14

00x5

30R

23 4

0PR

33.6

37 m

(110

.358

ft)

32.8

89 m

(107

.904

ft)

1.98

1 m

(6.4

99 ft

)

F_AC_070200_1_0320101_01_03

Landing Gear FootprintFIGURE-7-2-0-991-032-A01

7-2-0Page 2

Jul 01/21


**ON A/C A340-500

15 b

ar(2

18 p

si)

CE

NT

RA

LG

EA

RT

IRE

PR

ES

SU

RE

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

A340−

500

WV

000

369

200

kg(8

13 9

50 lb

)92

.7%

14.1

bar

(205

psi

)16

.1 b

ar(2

34 p

si)

45x1

80R

17 3

6PR

NO

SE

GE

AR

TIR

E S

IZE

A340−

500

WV

001

373

200

kg(8

22 7

75 lb

)92

.7%

A340−

500

WV

002

373

200

kg(8

22 7

75 lb

)92

.7%

A340−

500

WV

003

375

200

kg(8

27 1

75 lb

)92

.2%

A340−

500

WV

004

375

200

kg(8

27 1

75 lb

)92

.2%

A340−

500

WV

101

381

200

kg(8

40 4

00 lb

)92

.1%

A340−

500

WV

102

373

200

kg(8

22 7

75 lb

)92

.6%

16.1

bar

(234

psi

)A

340−

500

WV

103

373

200

kg(8

22 7

75 lb

)92

.6%

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

45x1

80R

17 3

6PR

14.1

bar

(205

psi

)

14.1

bar

(205

psi

)

14.1

bar

(205

psi

)

14.1

bar

(205

psi

)

14.1

bar

(205

psi

)

14.1

bar

(205

psi

)

14.1

bar

(205

psi

)

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

1400

x530

R23

40P

R

16.1

bar

(234

psi

)

16.1

bar

(234

psi

)

15 b

ar(2

18 p

si)

15 b

ar(2

18 p

si)

15 b

ar(2

18 p

si)

15 b

ar(2

18 p

si)

CE

NT

RA

LG

EA

RT

IRE

SIZ

E

0.81

4 m

(2.6

71 ft

)

10.6

84 m

(35.

052

ft)

1.17

6 m

(3.8

58 ft

)

1.39

7 m

(4.5

83 ft

)1.98

1 m

(6.4

99 ft

)

28.3

37 m

(92.

969

ft)

27.5

89 m

(90.

515

ft)

1.98

1 m

(6.4

99 ft

)

F_AC_070200_1_0440101_01_02

Landing Gear FootprintFIGURE-7-2-0-991-044-A01

7-2-0Page 3

Jul 01/21


7-3-0 Maximum Pavement Loads

**ON A/C A340-500 A340-600

Maximum Pavement Loads

1. This section gives maximum vertical and horizontal pavement loads for some critical conditions at thetire-ground interfaces.The maximum pavement loads are given for all the operational weight variants of the aircraft.

7-3-0Page 1

Jul 01/21


**ON A/C A340-600

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

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)

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 3

54 6

00 k

g (7

81 7

50 lb

).B

RA

KE

D M

AIN

GE

AR

.(d

) B

RA

KE

D C

EN

TE

R G

EA

R.

(c)

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 10

ft/s

?D

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

A340−

600

WV

000

366

200

kg(8

07 3

25 lb

)40

320

kg

(88

900

lb)

55 2

50 k

g(1

21 8

00 lb

)11

7 95

0 kg

(260

025

lb)

106

570

kg(2

34 9

50 lb

)

39 2

00 k

g(8

6 42

5 lb

)35

420

kg

(78

075

lb)

(c)

(d)

35 %

MA

C(a

)

94 3

60 k

g(2

08 0

25 lb

)85

260

kg

(187

950

lb)

(c)

(d)

16 %

MA

C(b

)

35 %

MA

C(a

)

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

/s?

F_AC_070300_1_0110101_01_04

Maximum Pavement Loads(Sheet 1 of 2)

FIGURE-7-3-0-991-011-A01

7-3-0Page 2

Jul 01/21


**ON A/C A340-600

A340−

600

WV

001

369

200

kg(8

13 9

50 lb

)40

320

kg

(88

900

lb)

55 2

50 k

g(1

21 8

00 lb

)11

8 93

0 kg

(262

200

lb)

106

880

kg(2

35 6

25 lb

)

39 5

90 k

g(8

7 27

5 lb

)35

580

kg

(78

425

lb)

(c)

(d)

34.4

3 %

MA

C(a

)

30.2

%M

AC

(a)

34.4

3 %

MA

C(a

)

35 %

MA

C(a

)

95 1

40 k

g(2

09 7

50 lb

)85

500

kg

(188

500

lb)

(c)

(d)

A340−

600

WV

101

381

200

kg(8

40 4

00 lb

)40

330

kg

(88

900

lb)

55 0

80 k

g(1

21 4

25 lb

)12

1 02

0 kg

(266

800

lb)

109

720

kg(2

41 9

00 lb

)

40 7

60 k

g(8

9 87

5 lb

)36

960

kg

(81

475

lb)

(c)

(d)

96 8

10 k

g(2

13 4

25 lb

)87

780

kg

(193

500

lb)

(c)

(d)

A340−

600

WV

102

369

200

kg(8

13 9

50 lb

)40

330

kg

(88

900

lb)

118

160

kg(2

60 5

00 lb

)10

8 34

0 kg

(238

850

lb)

39 3

40 k

g(8

6 72

5 lb

)36

070

kg

(79

525

lb)

(c)

(d)

94 5

30 k

g(2

08 4

00 lb

)86

670

kg

(191

075

lb)

(c)

(d)

A340−

600

WV

103

366

200

kg(8

07 3

25 lb

)40

330

kg

(88

900

lb)

55 1

20 k

g(1

21 5

25 lb

)11

7 27

0 kg

(258

525

lb)

107

850

kg(2

37 7

75 lb

)

38 9

80 k

g(8

5 95

0 lb

)35

850

kg

(79

050

lb)

(c)

(d)

93 8

20 k

g(2

06 8

25 lb

)86

280

kg

(190

200

lb)

(c)

(d)

16 %

MA

C(b

)

16 %

MA

C(b

)

16 %

MA

C(b

)

16 %

MA

C(b

)

34.4

3 %

MA

C(a

)

30.2

%M

AC

(a)

34.4

3 %

MA

C(a

)

35 %

MA

C(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 3

54 6

00 k

g (7

81 7

50 lb

).B

RA

KE

D M

AIN

GE

AR

.(d

) B

RA

KE

D C

EN

TE

R G

EA

R.

(c)

INS

TA

NT

AN

EO

US

BR

AK

ING

CO

EF

FIC

IEN

T =

0.8

AT

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 10

ft/s

?D

EC

ELE

RA

TIO

NW

EIG

HT

6

ST

AT

IC L

OA

D A

TM

AX

AF

T C

G

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

/s?

55 0

70 k

g(1

21 4

25 lb

)

F_AC_070300_1_0110102_01_02


FIGURE-7-3-0-991-011-A01

7-3-0Page 3

Jul 01/21


**ON A/C A340-500

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

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 10

ft/s

?D

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

A340−

500

WV

000

369

200

kg(8

13 9

50 lb

)41

160

kg

(90

750

lb)

58 5

00 k

g(1

28 9

75 lb

)11

7 99

0 kg

(260

125

lb)

106

240

kg(2

34 2

25 lb

)

39 5

60 k

g(8

7 22

5 lb

)35

620

kg

(78

525

lb)

(c)

(d)

36.5

%M

AC

(a)

94 3

90 k

g(2

08 1

00 lb

)84

990

kg

(187

375

lb)

(c)

(d)

A340−

500

WV

001

41 1

60 k

g(9

0 75

0 lb

)58

500

kg

(128

975

lb)

119

540

kg(2

63 5

25 lb

)10

6 76

0 kg

(235

350

lb)

40 0

90 k

g(8

8 40

0 lb

)35

810

kg

(78

950

lb)

(c)

(d)

95 6

30 k

g(2

10 8

25 lb

)85

410

kg

(188

275

lb)

(c)

(d)

373

200

kg(8

22 7

75 lb

)

36.4

%M

AC

(a)

22 %

MA

C(b

)

22 %

MA

C(b

)

36.5

%M

AC

(a)

36.4

%M

AC

(a)

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

/s?

NO

TE

:(a

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T M

RW

(b)

LO

AD

S C

ALC

ULA

TE

D U

SIN

G A

IRC

RA

FT

AT

349

200

kg

(769

850

lb)

BR

AK

ED

MA

IN G

EA

R(d

) B

RA

KE

D C

EN

TE

R G

EA

R(c

)

F_AC_070300_1_0130101_01_05


FIGURE-7-3-0-991-013-A01

7-3-0Page 4

Jul 01/21


**ON A/C A340-500

A340−

500

WV

002

A340−

500

WV

003

A340−

500

WV

004

A340−

500

WV

101

A340−

500

WV

102

A340−

500

WV

103

40 3

30 k

g(8

8 90

0 lb

)35

960

kg

(79

275

lb)

(c)

(d)

40 6

90 k

g(8

9 70

0 lb

)37

110

kg

(81

800

lb)

(c)

(d)

39 7

40 k

g(8

7 60

0 lb

)36

520

kg

(80

500

lb)

(c)

(d)

40 0

90 k

g(8

8 40

0 lb

)35

810

kg

(78

950

lb)

(c)

(d)

40 3

30 k

g(8

8 90

0 lb

)35

960

kg

(79

275

lb)

(c)

(d)

39 7

40 k

g(8

7 60

0 lb

)36

520

kg

(80

500

lb)

(c)

(d)

95 7

40 k

g(2

11 0

75 lb

)85

380

kg

(188

250

lb)

(c)

(d)

96

470

kg(2

12 6

75 lb

)87

990

kg

(193

975

lb)

(c)

(d)

94 7

50 k

g(2

08 9

00 lb

)87

070

kg

(191

975

lb)

(c)

(d)

95 6

30 k

g(2

10 8

25 lb

)85

410

kg

(188

275

lb)

(c)

(d)

95 7

40 k

g(2

11 0

75 lb

)85

380

kg

(188

250

lb)

(c)

(d)

94 7

50 k

g(2

08 9

00 lb

)87

070

kg

(191

975

lb)

(c)

(d)

INS

TA

NT

AN

EO

US

BR

AK

ING

CO

EF

FIC

IEN

T =

0.8

AT

41 1

50 k

g(9

0 72

5 lb

)58

440

kg

(128

825

lb)

109

980

kg(2

42 4

75 lb

)38

1 20

0 kg

(840

400

lb)

118

440

kg(2

61 1

25 lb

)37

3 20

0 kg

(822

775

lb)

34.7

%M

AC

(a)

36.4

%M

AC

(a)

41 1

60 k

g(9

0 75

0 lb

)58

500

kg

(128

975

lb)

119

540

kg(2

63 5

25 lb

)10

6 76

0 kg

(235

350

lb)

373

200

kg(8

22 7

75 lb

)

36.4

%M

AC

(a)

41 1

50 k

g(9

0 72

5 lb

)

41 1

50 k

g(9

0 72

5 lb

)

375

200

kg(8

27 1

75 lb

)41

160

kg

(90

750

lb)

41 1

60 k

g(9

0 75

0 lb

)37

5 20

0 kg

(827

175

lb)

373

200

kg(8

22 7

75 lb

)

119

680

kg(2

63 8

50 lb

)

119

680

kg(2

63 8

50 lb

)

120

590

kg(2

65 8

50 lb

)

118

440

kg(2

61 1

25 lb

)

106

730

kg(2

35 3

00 lb

)

106

730

kg(2

35 3

00 lb

)

108

840

kg(2

39 9

50 lb

)

108

840

kg(2

39 9

50 lb

)

35.0

1 %

MA

C(a

)

35.0

1 %

MA

C(a

)

36.4

%M

AC

(a)

22 %

MA

C(b

)

22 %

MA

C(b

)

22 %

MA

C(b

)

22 %

MA

C(b

)

22 %

MA

C(b

)

22 %

MA

C(b

)

36.4

%M

AC

(a)

35.0

1 %

MA

C(a

)

35.0

1 %

MA

C(a

)

34.7

%M

AC

(a)

36.4

%M

AC

(a)

36.4

%M

AC

(a)

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 10

ft/s

?D

EC

ELE

RA

TIO

NW

EIG

HT

6

ST

AT

IC L

OA

D A

TM

AX

AF

T C

G

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

/s?

NO

TE

:(a

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T M

RW

(b)

LO

AD

S C

ALC

ULA

TE

D U

SIN

G A

IRC

RA

FT

AT

349

200

kg

(769

850

lb)

BR

AK

ED

MA

IN G

EA

R(d

) B

RA

KE

D C

EN

TE

R G

EA

R(c

)

58 5

00 k

g(1

28 9

75 lb

)

58 5

00 k

g(1

28 9

75 lb

)

58 4

40 k

g(1

28 8

25 lb

)

58 4

40 k

g(1

28 8

25 lb

)

F_AC_070300_1_0130102_01_02


FIGURE-7-3-0-991-013-A01

7-3-0Page 5

Jul 01/21


7-4-0 Landing Gear Loading on Pavement

**ON A/C A340-500 A340-600

Landing Gear Loading on Pavement

1. The curves related to the landing gear loading on pavement are not given in section 07-04-00.Because the relationship between the aircraft weight, the center of gravity and the landing gearloading on the pavement is not strictly linear, it cannot be shown in chart format. But you can find insection 07-03-00 the maximum vertical and horizontal pavement loads for some critical conditions atthe tire/ground interfaces for all the operational weight variants of the aircraft.For questions related to the landing gear loading on pavement, contact Airbus.

7-4-0Page 1

Jul 01/21


7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method

**ON A/C A340-500 A340-600

Flexible Pavement Requirements - US Army Corps of Engineers Design Method

1. The flexible-pavement requirements curves by U.S. Army Corps of Engineers Design Method are notgiven in section 07-05-00 since the related data is available through free software.Sections 07-02-00 and 07-03-00 give all the inputs data required for the use of such software.

NOTE : The U.S. Army Corps of Engineers Design Method for flexible pavements is being graduallysuperseded by mechanistic-empirical design methods mostly relying on Linear ElasticAnalysis (LEA). The number of parameters considered by such methods is not applicablefor a chart format and the use of dedicated pavement-design software is necessary.

For questions related to the flexible pavement requirements, contact Airbus.

7-5-0Page 1

Jul 01/21


7-6-0 Flexible Pavement Requirements - LCN Conversion

**ON A/C A340-500 A340-600

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 and ACR/PCR system in 2020.For questions related to the LCN system, contact Airbus.

7-6-0Page 1

Jul 01/21


7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method

**ON A/C A340-500 A340-600

Rigid Pavement Requirements - Portland Cement Association Design Method

1. The rigid-pavement requirements curves by Portland Cement Association Design Method are notgiven in section 07-07-00 since the related data is available through free software.Sections 07-02-00 and 07-03-00 give all the inputs data required for the use of such software.

NOTE : The Portland Cement Association Design Method for rigid pavements is being graduallysuperseded by mechanistic-empirical design methods mostly relying on Finite ElementAnalysis (FEM). The number of parameters considered by such methods is not applicablefor a chart format and the use of dedicated pavement-design software is necessary.

For questions related to the rigid pavement requirements, contact Airbus.

7-7-0Page 1

Jul 01/21


7-8-0 Rigid Pavement Requirements - LCN Conversion

**ON A/C A340-500 A340-600

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 and ACR/PCR system in 2020.For questions related to the LCN system, contact Airbus.

7-8-0Page 1

Jul 01/21


7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements

**ON A/C A340-500 A340-600

Aircraft Classification Number - Flexible and Rigid Pavements

1. This section gives data about the Aircraft Classification Number (ACN) for an aircraft gross weight inrelation 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).

2. Aircraft Classification Number - ACN tableThe tables in FIGURE 7-9-0-991-006-A and FIGURE 7-9-0-991-007-A gives ACN data in tabularformat 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 - 180 000 kg)/(MRW - 180 000

kg)Please note that the interpolation error can reach 5% to 10%.

As an approximation, use a linear interpolation in order to get the aircraft weight at the pavementPCN using the following equation:- Operating weight = 180 000 kg + (MRW - 180 000 kg) x (PCN - ACN min)/(ACN max - ACN

min)Please note that the interpolation error can reach up to 5%.

With ACN max = ACN calculated at the MRW in the table and with ACN min = ACN calculated at180 000 kg.

7-9-0Page 1

Jul 01/21


**ON A/C A340-500

AIRCRAFT TYPEALL UP

MASS (kg)

LOAD ONONE MAINGEAR LEG

(%)

TIREPRESSURE

(Mpa)

ACN FOR

High150

RIGID PAVEMENTSUBGRADES − MN/m?

Medium80

Low40

Ultral−low20

ACN FOR

High15

FLEXIBLE PAVEMENTSUBGRADES − CBR

Medium10

Low6

Ultral−low3

A340−500WV000

369 200 32.037.4

1.61

WV001

WV002

WV003

A340−500

A340−500

A340−500

WV004A340−500

WV101A340−500

WV102A340−500

WV103A340−500

373 200 32.037.4

373 200 32.037.4

375 200 31.937.3

375 200 31.937.3

381 200 31.636.3

373 200 31.736.4

373 200 31.736.4

180 000

180 000

180 000

180 000

180 000

180 000

180 000

180 000

1.61

1.61

1.61

1.61

1.61

1.61

1.61

6133

7135

8339

9645

6432

6934

8037

10847

62 72 85 98 65 70 81 110

62 72 85 98 65 70 81 110

63 72 85 98 65 70 82 110

63 72 85 98 65 70 82 110

6332

7334

86 99 66 71 83 111

62 71 84 97 64 69 80 108

62 71 8438

9744

6431

6933

8036

10845

33

33

33

33

33

33

35

35

35

35

34

34

38

38

39

39

39

39

44

44

45

45

45

45

31

31

32

32

32

32

33

33

34

34

34

34

36

36

37

37

37

37

45

45

47

47

47

47

F_AC_070900_1_0060101_01_01

Aircraft Classification NumberACN Table

FIGURE-7-9-0-991-006-A01

7-9-0Page 2

Jul 01/21


**ON A/C A340-600

AIRCRAFT TYPEALL UP

MASS (kg)


(%)

TIREPRESSURE

(Mpa)

ACN FOR

High150

RIGID PAVEMENTSUBGRADES − MN/m?

Medium80

Low40

Ultral−low20

ACN FOR

High15

FLEXIBLE PAVEMENTSUBGRADES − CBR

Medium10

Low6

Ultral−low3

6133

7135

8339

9645

6432

6934

8037

10847

A340−600WV000

32.2 1.61

WV001

WV101

WV102

WV103

37.5A340−600

A340−600

A340−600

A340−600

32.237.531.736.332.036.632.036.6

1.61

1.61

1.61

1.61

366 200180 000369 200

381 200

369 200

366 200

180 000

180 000

180 000

180 000

6332

7334

8638

10044

6631

7133

8336

11245

6233

7135

8440

9745

6432

6934

8137

10947

6233

7134

8338

9644

6432

6933

8036

10846

6133

7034

8238

9544

6332

6833

7936

10746

F_AC_070900_1_0070101_01_01

Aircraft Classification NumberACN Table

FIGURE-7-9-0-991-007-A01

7-9-0Page 3

Jul 01/21


7-10-0 ACR/PCR Reporting System - Flexible And Rigid Pavement

**ON A/C A340-500 A340-600

ACR/PCR Reporting System - Flexible and Rigid Pavements

1. The ACR/PCR system has been developed by the ICAO to overcome the deficiencies of theACN/PCN system. Significant advances in pavement design methods had occurred since itsdevelopment in the late 1970s early 1980s, leading to inconsistencies with the pavement-strength-rating system.The ACR/PCR system entails new procedures for the determination of both the ACR and the PCRthat are consistent with the current pavement design procedures. This allows to capture the effects ofthe improved characteristics of new pavement materials as well as modern landing gearconfigurations, thus leading to an improved accuracy.This section gives data about the Aircraft Classification Rating (ACR) for the maximum ramp weightin relation with standard subgrade strength values for flexible and rigid pavement.To determine the ACR at other aircraft gross weight, use the official ICAO-ACR software.

NOTE : An aircraft with an ACR equal to or less than the reported PCR can operate on thatpavement, subject to any limitation on the tire pressure. (Ref: ICAO Aerodrome DesignManual, Part 3, Third Edition 2020).

2. Aircraft Classification Rating - ACR TableThe table FIGURE 7-10-0-991-008-A and FIGURE 7-10-0-991-009-A give ACR data in tabular formatfor all the operational weight variants of the aircraft.For questions or specific calculation related to ACR/PCR reporting system, contact Airbus.

7-10-0Page 1

Jul 01/21


**ON A/C A340-500

ALL UPMASS

(kg)


(%)

TIREPRESSURE

(MPa) HIGH200

MEDIUM120

LOW80

HIGH200

MEDIUM120

LOW80

ACR FORRIGID PAVEMENT

SUBGRADES − MPa

ULTRA−LOW

50

ULTRA−LOW

50

ACR FORFLEXIBLE PAVEMENTSUBGRADES − MPaAIRCRAFT

TYPE

A340−500WV000 369 200

32 (WLG)28.8 (CLG) 1.61 690 790 880 990 620 640 710 870

A340−500WV001 373 200

32 (WLG)28.6 (CLG) 1.61 710 810 900 1 010 630 650 720 890

A340−500WV002 373 200

32 (WLG)28.6 (CLG) 1.61

A340−500WV003 375 200

31.9 (WLG)28.4 (CLG) 1.61

A340−500WV004 375 200 1.61

A340−500WV101 381 200

31.6 (WLG)28.9 (CLG) 1.61 710 820 910 1 020 640 660 730 900

A340−500WV102 373 200

31.7 (WLG)29.2 (CLG) 1.61 700 800 890 1 000 620 650 710 870

A340−500WV103 373 200

31.7 (WLG)29.2 (CLG) 1.61

31.9 (WLG)28.4 (CLG)

710 810 900 1 010 630 650 720 890

710 810 900 1 010 630 660 720 890

710 810 900 1 010 630 660 720 890

700 800 890 1 000 620 650 710 870

F_AC_071000_1_0080101_01_00

ACR TableFIGURE-7-10-0-991-008-A01

7-10-0Page 2

Jul 01/21


**ON A/C A340-600

ALL UPMASS

(kg)


(%)

TIREPRESSURE

(MPa) HIGH200

MEDIUM120

LOW80

HIGH200

MEDIUM120

LOW80

ACR FORRIGID PAVEMENT

SUBGRADES − MPa

ULTRA−LOW

50

ULTRA−LOW

50

ACR FORFLEXIBLE PAVEMENTSUBGRADES − MPaAIRCRAFT

TYPE

A340−600WV000 366 200

32.2 (WLG)29.1 (CLG) 1.61 690 790 880 990 620 640 710 870

369 200 1.61 700 800 890 1 000 630 650 720 880

381 200 1.61 720 820 920 1 030 640 660 730 900

369 200 1.61 700 790 890

366 200 1.61 690 790 880 980 620 640 700 860

990 620 650 710 870

A340−600WV001

A340−600WV101

A340−600WV102

A340−600WV103

32.2 (WLG)28.9 (CLG)31.7 (WLG)28.8 (CLG)32 (WLG)

29.3 (CLG)32 (WLG)

29.5 (CLG)

F_AC_071000_1_0090101_01_00

ACR TableFIGURE-7-10-0-991-009-A01

7-10-0Page 3

Jul 01/21


SCALED DRAWINGS

8-0-0 SCALED DRAWINGS

**ON A/C A340-500 A340-600

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

Jul 01/21


**ON A/C A340-500

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_0040101_01_01

Scaled DrawingFIGURE-8-0-0-991-004-A01

8-0-0Page 2

Jul 01/21


**ON A/C A340-600

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_0040201_01_01

Scaled DrawingFIGURE-8-0-0-991-004-B01

8-0-0Page 3

Jul 01/21


AIRCRAFT RESCUE AND FIRE FIGHTING

10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING

**ON A/C A340-500

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

Jul 01/21


**ON A/C A340-500

JAN

UA

RY

201

7

F_AC_100000_1_0400101_01_03

Front PageFIGURE-10-0-0-991-040-A01

10-0-0Page 2

Jul 01/21


**ON A/C A340-500

F_AC_100000_1_0410101_01_01

Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-041-A01

10-0-0Page 3

Jul 01/21


**ON A/C A340-500

FR

73F

R20

FR

1F

R67

FR

64

FR

65B

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F_AC_100000_1_0700101_01_01

Batteries Location and AccessFIGURE-10-0-0-991-070-A01

10-0-0Page 4

Jul 01/21


**ON A/C A340-500

F_AC_100000_1_0420101_01_00

Crew Rest Compartments LocationFIGURE-10-0-0-991-042-A01

10-0-0Page 5

Jul 01/21


**ON A/C A340-500

F_AC_100000_1_0430101_01_00

Wheel/Brake OverheatWheel Safety Area (Sheet 1 of 2)

FIGURE-10-0-0-991-043-A01

10-0-0Page 6

Jul 01/21


**ON A/C A340-500

F_AC_100000_1_0430102_01_00

Wheel/Brake OverheatRecommendations (Sheet 2 of 2)

FIGURE-10-0-0-991-043-A01

10-0-0Page 7

Jul 01/21


**ON A/C A340-500

Car

bon

Fib

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Composite Materials LocationFIGURE-10-0-0-991-044-A01

10-0-0Page 8

Jul 01/21


**ON A/C A340-500

BA

B

C

C

A

F_AC_100000_1_0450101_01_00

Ground Lock Safety DevicesFIGURE-10-0-0-991-045-A01

10-0-0Page 9

Jul 01/21


**ON A/C A340-500

0 −3

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Emergency Evacuation DevicesFIGURE-10-0-0-991-046-A01

10-0-0Page 10

Jul 01/21


**ON A/C A340-500

F_AC_100000_1_0470101_01_00

Pax/Crew Doors and Emergency ExitsFIGURE-10-0-0-991-047-A01

10-0-0Page 11

Jul 01/21


**ON A/C A340-500

122C

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FW

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F_AC_100000_1_0480101_01_00

FWD and AFT Lower Deck Cargo DoorsFIGURE-10-0-0-991-048-A01

10-0-0Page 12

Jul 01/21


**ON A/C A340-500

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43

21

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F_AC_100000_1_0490101_01_00

Control PanelsFIGURE-10-0-0-991-049-A01

10-0-0Page 13

Jul 01/21


**ON A/C A340-500

A

315A

L

316A

R

A

F_AC_100000_1_0500101_01_00

APU Compartment AccessFIGURE-10-0-0-991-050-A01

10-0-0Page 14

Jul 01/21


**ON A/C A340-500

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F_AC_100000_1_0510101_01_01


10-0-0Page 15

Jul 01/21


**ON A/C A340-500

F_AC_100000_1_0520101_01_00

Structural Break-in PointsFIGURE-10-0-0-991-052-A01

10-0-0Page 16

Jul 01/21


**ON A/C A340-600

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 17

Jul 01/21


**ON A/C A340-600

JAN

UA

RY

201

7

F_AC_100000_1_0530101_01_03

Front PageFIGURE-10-0-0-991-053-A01

10-0-0Page 18

Jul 01/21


**ON A/C A340-600

F_AC_100000_1_0540101_01_01

Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-054-A01

10-0-0Page 19

Jul 01/21


**ON A/C A340-600

FR

73F

R20

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1

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F_AC_100000_1_0710101_01_01

Batteries Location and AccessFIGURE-10-0-0-991-071-A01

10-0-0Page 20

Jul 01/21


**ON A/C A340-600

F_AC_100000_1_0550101_01_00

Crew Rest Compartments LocationFIGURE-10-0-0-991-055-A01

10-0-0Page 21

Jul 01/21


**ON A/C A340-600

F_AC_100000_1_0560101_01_00

Wheel/Brake OverheatWheel Safety Area (Sheet 1 of 2)

FIGURE-10-0-0-991-056-A01

10-0-0Page 22

Jul 01/21


**ON A/C A340-600

F_AC_100000_1_0560102_01_00

Wheel/Brake OverheatRecommendations (Sheet 2 of 2)

FIGURE-10-0-0-991-056-A01

10-0-0Page 23

Jul 01/21


**ON A/C A340-600

Car

bon

Fib

er R

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orce

d P

last

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CF

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)

Gla

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Composite Materials LocationFIGURE-10-0-0-991-057-A01

10-0-0Page 24

Jul 01/21


**ON A/C A340-600

BA

B

C

C

A

F_AC_100000_1_0580101_01_00

Ground Lock Safety DevicesFIGURE-10-0-0-991-058-A01

10-0-0Page 25

Jul 01/21


**ON A/C A340-600

EM

ER

GE

NC

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F_AC_100000_1_0590101_01_02

Emergency Evacuation DevicesFIGURE-10-0-0-991-059-A01

10-0-0Page 26

Jul 01/21


**ON A/C A340-600

F_AC_100000_1_0600101_01_00

Pax/Crew Doors and Emergency ExitsFIGURE-10-0-0-991-060-A01

10-0-0Page 27

Jul 01/21


**ON A/C A340-600

122C

R

FW

D

7155

JE 196B

B

152N

R/

197C

B

F_AC_100000_1_0610101_01_00

FWD and AFT Lower Deck Cargo DoorsFIGURE-10-0-0-991-061-A01

10-0-0Page 28

Jul 01/21


**ON A/C A340-600

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Control PanelsFIGURE-10-0-0-991-062-A01

10-0-0Page 29

Jul 01/21


**ON A/C A340-600

A

315A

L

316A

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F_AC_100000_1_0630101_01_00

APU Compartment AccessFIGURE-10-0-0-991-063-A01

10-0-0Page 30

Jul 01/21


**ON A/C A340-600

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**ON A/C A340-600

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Structural Break-in PointsFIGURE-10-0-0-991-065-A01

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a340-500/-600 aircraft characteristics airport and

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