A340-200/-300 AIRCRAFT CHARACTERISTICS AIRPORT AND ... · FIGURE Jacking for Maintenance - Load at the Aircraft Jacking Points Jan 01/14 Subject 2-14-1 Jacking of the Landing Gear

@AIRBUSA340-200/-300

AIRCRAFT CHARACTERISTICSAIRPORT AND MAINTENANCE PLANNING

AC

The content of this document is the property of Airbus.It is supplied in confidence and commercial security on its contents must be maintained.It must not be used for any purpose other than that for which it is supplied, nor mayinformation contained in it be disclosed to unauthorized persons.It must not be reproduced in whole or in part without permission in writing from the owners ofthe copyright. Requests for reproduction of any data in this document and the media authorizedfor it must be addressed to Airbus.

© AIRBUS S.A.S. 2005. All rights reserved.

AIRBUS S.A.S.Customer Services

Technical Data Support and Services31707 Blagnac Cedex

FRANCE

Issue: Jul 30/92 Rev: Aug 01/19

@A340-200/-300AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

HIGHLIGHTS

Revision No. 26 - Aug 01/19

LOCATIONS CHGCODE

DESCRIPTIONS OF CHANGE

CHAPTER 6

Section 6-3

Subject 6-3-0

Danger Areas of Engines R NOTE AMENDED

HIGHLIGHTSPage 1

Aug 01/19


LIST OF EFFECTIVE CONTENT

Revision No. 26 - Aug 01/19

CONTENT CHGCODE

LAST REVISIONDATE

CHAPTER 1

Subject 1-1-0

Introduction Jan 01/17

Subject 1-2-1

Glossary Jan 01/17

CHAPTER 2

Subject 2-1-1

General Aircraft Characteristics Data Jan 01/14

Subject 2-2-0

General Aircraft Dimensions Jan 01/17

FIGURE General Aircraft Dimensions Jan 01/14

FIGURE General Aircraft Dimensions Jan 01/14

Subject 2-3-0

Ground Clearances Jan 01/17

FIGURE Ground Clearances Oct 01/15


FIGURE Ground Clearances - Ailerons -- Up Oct 01/15

FIGURE Ground Clearances - Ailerons -- Down Oct 01/15

FIGURE Ground Clearances - Spoilers -- Extended Oct 01/15

FIGURE Ground Clearances - Leading Edge Slats -- Extended Oct 01/15

FIGURE Ground Clearances - Trailing Edge Flaps -- Extended Oct 01/15

FIGURE Ground Clearances - Flap Tracks -- Extended Oct 01/15

FIGURE Ground Clearances - Flap Tracks -- Retracted Oct 01/15

FIGURE Ground Clearances - Flap Tracks -- 1 + F Oct 01/15

Subject 2-4-1

Interior Arrangements - Plan View Jan 01/17

L.E.C.Page 1

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Interior Arrangements - Plan View - Typical Configuration Jan 01/17



Subject 2-5-0

Interior Arrangements - Cross Section Jan 01/14

FIGURE Interior Arrangements - Cross Section - TypicalConfiguration

Jan 01/14

Subject 2-6-1

Lower Deck Cargo Compartments Oct 01/15

FIGURE Lower Deck Cargo Compartments - Location and Dimensions Jan 01/14

FIGURE Lower Deck Cargo Compartments - Loading Combinations Oct 01/15

FIGURE Lower Deck Cargo Compartments - Loading Combinations Oct 01/15

Subject 2-7-0

Door Clearances Oct 01/15

FIGURE Door Clearances - Door Identification Jul 01/18

FIGURE Door Clearances - Door Identification Jul 01/18

FIGURE Door Clearances - Forward Passenger/Crew Doors Oct 01/15

FIGURE Door Clearances - Mid Passenger/Crew Doors Oct 01/15

FIGURE Door Clearances - Emergency Exits Oct 01/15

FIGURE Door Clearances - Aft Passenger/Crew Doors Oct 01/15

FIGURE Door Clearances - Forward Cargo Compartment Door Oct 01/15

FIGURE Door Clearances - Aft Cargo Compartment Door Oct 01/15

FIGURE Door Clearances - Bulk Cargo Compartment Door Oct 01/15

FIGURE Door Clearances - Radome Oct 01/15

FIGURE Door Clearances - Main and Center Landing Gear Doors Oct 01/15

FIGURE Door Clearances - APU and Nose Landing Gear Doors Oct 01/15

FIGURE Door Clearances - APU and Nose Landing Gear Doors Oct 01/15

Subject 2-8-0

Escape Slides Oct 01/15

L.E.C.Page 2

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Escape Slides - Location Oct 01/15

FIGURE Escape Slides - Location Oct 01/15

Subject 2-9-0

Landing Gear Maintenance Pits Jan 01/14

FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes Jan 01/14

FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes Jan 01/14

Landing Gear Jan 01/17

FIGURE Main Landing Gear - General Jan 01/14

FIGURE Centerline Landing Gear - General Jan 01/14

FIGURE Nose Landing Gear - General Jan 01/14

FIGURE Tow Truck Power Jan 01/17

Subject 2-10-0

Exterior Lighting Jan 01/17

FIGURE Exterior Lighting Jan 01/14

FIGURE Exterior Lighting Jan 01/14

Subject 2-11-0

Antennas and Probes Location Jan 01/14

FIGURE Antennas and Probes - Location Jan 01/14

FIGURE Antennas and Probes - Location Jan 01/14

Subject 2-12-0

Engine and Nacelle Jan 01/14

FIGURE Engine and Nacelle - Engine Dimensions - CFM 56-5C Jan 01/14

FIGURE Engine and Nacelle - Nacelle Dimensions - CFM 56-5C Jan 01/14

FIGURE Engine and Nacelle - Fan Cowls - CFM 56-5C Jan 01/14

FIGURE Engine and Nacelle - Thrust Reverser Cowls - CFM 56-5C Jan 01/14

Subject 2-12-1

Auxiliary Power Unit Jan 01/14

FIGURE Auxiliary Power Unit - Access Doors Jan 01/14

Subject 2-13-0

L.E.C.Page 3

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

Leveling, Symmetry and Alignment Jan 01/14

FIGURE Location of Leveling Points Jan 01/14

FIGURE Location of Leveling Points Jan 01/14

Subject 2-14-0

Jacking for Maintenance Jan 01/17

FIGURE Jacking for Maintenance - Jacking Points Location Jan 01/14

FIGURE Jacking for Maintenance - Jacking Points Location Jan 01/14

FIGURE Jacking for Maintenance - Forward Jacking Point Jan 01/14

FIGURE Jacking for Maintenance - Wing Jacking Points Jan 01/14

FIGURE Jacking for Maintenance - Auxiliary Jacking Point - SafetyStay

Jan 01/14

FIGURE Jacking for Maintenance - Jacking Dimensions Jan 01/14

FIGURE Jacking for Maintenance - Jacking Dimensions Jan 01/14

FIGURE Jacking for Maintenance - Load at the Aircraft JackingPoints

Jan 01/14

FIGURE Jacking for Maintenance - Load at the Aircraft JackingPoints

Jan 01/14

Subject 2-14-1

Jacking of the Landing Gear Oct 01/15

FIGURE Jacking of the Landing Gear - MLG Jacking Point Heights Jul 01/18

FIGURE Jacking of the Landing Gear - Jacking of the NLG Oct 01/15

FIGURE Jacking of the Landing Gear - Jacking of the CLG Oct 01/15

FIGURE Jacking of the Landing Gear - MLG Jacking Point Loads Oct 01/15

FIGURE Jacking of the Landing Gear - MLG Jacking Point Loads Oct 01/15

FIGURE Jacking of the Landing Gear - NLG Jacking Point Loads Oct 01/15

FIGURE Jacking of the Landing Gear - NLG Jacking Point Loads Oct 01/15

FIGURE Jacking of the Landing Gear - CLG Jacking Point Loads Oct 01/15

FIGURE Jacking of the Landing Gear - CLG Jacking Point Loads Oct 01/15

Subject 2-14-2

Support of Aircraft Jan 01/14

L.E.C.Page 4

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Support of Aircraft - Location of Shoring Cradles Jan 01/14

FIGURE Support of Aircraft - Location of Shoring Cradles Jan 01/14

CHAPTER 3

Subject 3-1-0

General Information Oct 01/15

Subject 3-2-1

Payload / Range - ISA Conditions Oct 01/15

FIGURE Payload / Range - ISA Conditions - CFM56-5C2 engine Oct 01/15







Subject 3-3-1

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

FIGURE Take-Off Weight Limitation - ISA Conditions -- CFM56-5C2engine

Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15

Subject 3-3-2

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

L.E.C.Page 5

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Take-Off Weight Limitation - ISA +15˚C (+59˚F)Conditions -- CFM56-5C2 engine

Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15


Oct 01/15

Subject 3-4-1

Landing Field Length - ISA Conditions Oct 01/15

FIGURE Landing Field Length - ISA Conditions -- CFM56-5C2 engine Oct 01/15






Subject 3-5-0

Final Approach Speed Jan 01/14

CHAPTER 4

Subject 4-1-0


Subject 4-2-0

Turning Radii Jan 01/17

FIGURE Turning Radii - (Sheet 1) Jan 01/14



L.E.C.Page 6

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

Subject 4-3-0

Minimum Turning Radii Jan 01/17

FIGURE Minimum Turning Radii Jan 01/14

FIGURE Minimum Turning Radii Jan 01/14

Subject 4-4-0

Visibility from Cockpit in Static Position Jul 01/19

FIGURE Visibility from Cockpit in Static Position Jul 01/19

FIGURE Binocular Visibility Through Windows from Captain EyePosition

Jan 01/14

Subject 4-5-0

Runway and Taxiway Turn Paths Jan 01/14

Subject 4-5-1

135˚ Turn - Runway to Taxiway Jan 01/14

FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod

Jan 01/14

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

Jan 01/14

FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod

Jan 01/14


Jan 01/14

Subject 4-5-2

90˚ Turn - Runway to Taxiway Jan 01/14

FIGURE 90˚ Turn - Runway to Taxiway - Judgement OversteeringMethod

Jan 01/14


Jan 01/14

FIGURE 90˚ Turn - Runway to Taxiway - Judgement OversteeringMethod

Jan 01/14


Jan 01/14

Subject 4-5-3

180˚ Turn on a Runway Jan 01/17

L.E.C.Page 7

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE 180˚ Turn on a Runway Jan 01/14

FIGURE 180˚ Turn on a Runway Jan 01/14

Subject 4-5-4

135˚ Turn - Taxiway to Taxiway Jan 01/14

FIGURE 135˚ Turn - Taxiway to Taxiway - JudgementalOversteering Method

Jan 01/14

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

Jan 01/14

FIGURE 135˚ Turn - Taxiway to Taxiway - JudgementalOversteering Method

Jan 01/14


Jan 01/14

Subject 4-5-5

90˚ Turn - Taxiway to Taxiway Jan 01/14

FIGURE 90˚ Turn - Taxiway to Taxiway - Judgement OversteeringMethod

Jan 01/14


Jan 01/14

FIGURE 90˚ Turn - Taxiway to Taxiway - Judgement OversteeringMethod

Jan 01/14


Jan 01/14

Subject 4-6-0

Runway Holding Bay (Apron) Oct 01/15

FIGURE Runway Holding Bay (Apron) Oct 01/15

Subject 4-7-0

Minimum Line-Up Distance Corrections Jan 01/14

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

Jan 01/14

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

Jan 01/14

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

Jan 01/14

L.E.C.Page 8

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

Subject 4-8-0

Aircraft Mooring Oct 01/15

FIGURE Aircraft Mooring Oct 01/15

CHAPTER 5

Subject 5-1-0

Aircraft Servicing Arrangements Jan 01/14

Subject 5-1-1

Symbols Used on Servicing Diagrams Jan 01/14

Subject 5-1-2

Typical Ramp Layout - Open Apron Jan 01/17

FIGURE Typical Ramp Layout - Open Apron Jan 01/14

FIGURE Typical Ramp Layout - Open Apron Jan 01/14

Subject 5-1-3

Typical Ramp Layout - Gate Jan 01/17

FIGURE Typical Ramp Layout - Gate Jan 01/14

FIGURE Typical Ramp Layout - Gate Jan 01/14

Subject 5-2-0

Terminal Operations - Full Servicing Turn Round Time Oct 01/15

FIGURE Full Servicing Turn Round Time Chart Oct 01/15

Terminal Operations - Full Servicing Turn Round Time Oct 01/15

FIGURE Full Servicing Turn Round Time Chart Oct 01/15

Subject 5-3-0

Terminal Operations - Minimum Servicing Turn-Round Time Jan 01/14

FIGURE Minimum Servicing Turn-Round Time Jan 01/14

Terminal Operations - Minimum Servicing Turn-Round Time Jan 01/14

FIGURE Minimum Servicing Turn-Round Time Jan 01/14

Subject 5-4-1

Ground Service Connections Layout Oct 01/15

FIGURE Ground Service Connections Layout Oct 01/15

L.E.C.Page 9

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

Subject 5-4-2

Grounding (Earthing) Points Oct 01/15

FIGURE Ground Service Connections - Grounding (Earthing) Points Oct 01/15

FIGURE Ground Service Connections - Grounding (Earthing) Points Oct 01/15

Subject 5-4-3

Hydraulic Servicing Oct 01/15

FIGURE Ground Service Connections - Green System Ground ServicePanel

Jan 01/14

FIGURE Ground Service Connections - Blue System Ground ServicePanel

Jan 01/14

FIGURE Ground Service Connections - Yellow System Ground ServicePanel

Jan 01/14

FIGURE Ground Service Connections - RAT Oct 01/15

Subject 5-4-4

Electrical Servicing Jan 01/17

FIGURE Ground Service Connections - Electrical Service Panel Oct 01/15

Subject 5-4-5

Oxygen Servicing Jan 01/17

FIGURE Ground Service Connections - Oxygen Servicing Oct 01/15

Subject 5-4-6

Fuel System Jul 01/18

FIGURE Ground Service Connections - Refuel/Defuel Control Panel Oct 01/15

FIGURE Ground Service Connections - Refuel/Defuel Coupling Oct 01/15

FIGURE Ground Service Connections - Overpressure Protector andNACA Flame Arrestor - Wing

Oct 01/15

FIGURE Ground Service Connections - Overpressure Protector andNACA Flame Arrestor - Trim Tank

Oct 01/15

Subject 5-4-7

Pneumatic Servicing Jan 01/17

FIGURE Ground Service Connections - LP and HP GroundConnectors

Jan 01/14

L.E.C.Page 10

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

Subject 5-4-8

Oil Servicing Oct 01/15

FIGURE Ground Service Connections - Engine Oil Tank - CFM56-5C2Series Engine

Oct 01/15

FIGURE Ground Service Connections - IDG Oil Tank - CFM56-5C2Series Engine

Oct 01/15

FIGURE Ground Service Connections - Starter Oil Tank - CFM56-5C2Series Engine

Oct 01/15

APU Oil Servicing Oct 01/15

FIGURE Ground Service Connections - APU Oil Servicing Oct 01/15

Subject 5-4-9

Potable Water Servicing Oct 01/15

FIGURE Ground Service Connections - Potable-Water Ground ServicePanels

Oct 01/15

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

Potable Water Servicing Oct 01/15

FIGURE Ground Service Connections - Potable-Water Ground ServicePanels

Oct 01/15

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

Subject 5-4-10

Waste Water Servicing Oct 01/15

FIGURE Ground Service Connections - Waste Water Ground ServicePanel

Jan 01/14

FIGURE Ground Service Connections - Waste Tanks Location Oct 01/15

Subject 5-4-11

Cargo Control Panels Oct 01/15

FIGURE Forward Cargo Control Panels Oct 01/15

FIGURE Aft Cargo Control Panels Oct 01/15

Subject 5-5-0

Engine Starting Pneumatic Requirements Jan 01/14

FIGURE Example for Use of the Charts Jan 01/14

L.E.C.Page 11

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Engine Starting Pneumatic Requirements - CFM56-5C2Series

Jan 01/14

Subject 5-6-0

Ground Pneumatic Power Requirements Oct 01/15

FIGURE Ground Pneumatic Power Requirements - Heating Jan 01/14

FIGURE Ground Pneumatic Power Requirements - Cooling Jan 01/14

Subject 5-7-0

Preconditioned Airflow Requirements Oct 01/15

FIGURE Preconditioned Airflow Requirements Jan 01/14

Subject 5-8-0

Ground Towing Requirements Jul 01/18

FIGURE Ground Towing Requirements Jan 01/14

Subject 5-9-0

De-Icing and External Cleaning Jan 01/17

CHAPTER 6

Subject 6-1-0

Engine Exhaust Velocities and Temperatures Jul 01/18

Subject 6-1-1

Engine Exhaust Velocities Contours - Ground Idle Power Jan 01/14

FIGURE Engine Exhaust Velocities - Ground Idle Power - CFM56-5Cseries engine

Jan 01/14

Subject 6-1-2

Engine Exhaust Temperatures Contours - Ground Idle Power Jan 01/14

FIGURE Engine Exhaust Temperatures - Ground Idle Power -CFM56-5C series engine

Jan 01/14

Subject 6-1-3

Engine Exhaust Velocities Contours - Breakaway Power Jan 01/14

FIGURE Engine Exhaust Velocities - Breakaway Power - CFM56-5Cseries engine

Jan 01/14

Subject 6-1-4

L.E.C.Page 12

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

Engine Exhaust Temperatures Contours - Breakaway Power Jan 01/14

FIGURE Engine Exhaust Temperatures - Breakaway Power -CFM56-5C series engine

Jan 01/14

Subject 6-1-5

Engine Exhaust Velocities Contours - Takeoff Power Jan 01/14

FIGURE Engine Exhaust Velocities - Takeoff Power - CFM56-5Cseries engine

Jan 01/14

Subject 6-1-6

Engine Exhaust Temperatures Contours - Takeoff Power Jan 01/14

FIGURE Engine Exhaust Temperatures - Takeoff Power - CFM56-5Cseries engine

Jan 01/14

Subject 6-3-0

Danger Areas of Engines R Aug 01/19

Subject 6-3-1

Ground Idle Power Oct 01/15

FIGURE Danger Areas of Engines - CFM56-5C series engine Jan 01/14

Subject 6-3-2

Breakaway Power Oct 01/15


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 GTCP331-350

Jan 01/14

CHAPTER 7

Subject 7-1-0

L.E.C.Page 13

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE


Subject 7-2-0

Landing Gear Footprint Oct 01/15

FIGURE Landing Gear Footprint Jan 01/14

FIGURE Landing Gear Footprint Jan 01/14

Subject 7-3-0

Maximum Pavement Loads Oct 01/15

FIGURE Maximum Pavement Loads Jan 01/14

FIGURE Maximum Pavement Loads Jan 01/14

Subject 7-4-0

Landing Gear Loading on Pavement Oct 01/15

FIGURE Landing Gear Loading on Pavement - WV000, MRW 254400 kg, CG 37.7%

Jan 01/14

FIGURE Landing Gear Loading on Pavement - WV021, MRW 275900 kg, CG 37%

Jan 01/14

FIGURE Landing Gear Loading on Pavement - WV000, MRW 254400 kg, CG 38.18%

Jan 01/14

FIGURE Landing Gear Loading on Pavement - WV028, MRW 277400 kg, CG 35%

Jan 01/14

Subject 7-5-0

Flexible Pavement Requirements - US Army Corps of EngineersDesign Method

Jan 01/17

FIGURE Flexible Pavement Requirements - WV000, MRW 254 400kg, CG 37.7%

Jan 01/17

FIGURE Flexible Pavement Requirements - WV000, MRW 254 400kg, CG 38.18%

Jan 01/17

Subject 7-6-0

Flexible Pavement Requirements - LCN Conversion Oct 01/15

Subject 7-7-0

Rigid Pavement Requirements - Portland Cement Association DesignMethod

Oct 01/15

L.E.C.Page 14

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Rigid Pavement Requirements - WV000, MRW 254 400 kg,CG 37.7%

Jan 01/17

FIGURE Rigid Pavement Requirements - WV000, MRW 254 400 kg,CG 38.18%

Jan 01/17

Subject 7-8-0

Rigid Pavement Requirements - LCN Conversion Oct 01/15

Subject 7-9-0

Aircraft Classification Number - Flexible and Rigid Pavements Jan 01/17

FIGURE Aircraft Classification Number - ACN Table Jan 01/14

FIGURE Aircraft Classification Number - Flexible Pavement - WV000,MRW 254 400 kg, CG 37.7%

Jan 01/17

FIGURE Aircraft Classification Number - Flexible Pavement - WV021,MRW 275 900 kg, CG 37%

Jan 01/17

FIGURE Aircraft Classification Number - ACN Table Jan 01/14

FIGURE Aircraft Classification Number - Flexible Pavement - WV000,MRW 254 400 kg, CG 38.18%

Jan 01/17

FIGURE Aircraft Classification Number - Flexible Pavement - WV028,MRW 277 400 kg, CG 35%

Jan 01/17

CHAPTER 8

Subject 8-0-0

Scaled Drawings Jan 01/14

FIGURE Scaled Drawing Jan 01/17

FIGURE Scaled Drawing Jan 01/17

CHAPTER 10

Subject 10-0-0

Aircraft Rescue and Fire Fighting Oct 01/15

FIGURE Front Page Jan 01/17

FIGURE Highly Flammable and Hazardous Materials and Components Oct 01/15

FIGURE Batteries Location and Access Oct 01/15

FIGURE Crew Rest Compartments Location Jan 01/14

L.E.C.Page 15

Aug 01/19


CONTENT CHGCODE

LAST REVISIONDATE

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 Structural Break-in Points Jan 01/14

L.E.C.Page 16

Aug 01/19


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

Aug 01/19


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

5-6-0 Ground Pneumatic Power Requirements

5-7-0 Preconditioned Airflow Requirements

5-8-0 Ground Towing Requirements

5-9-0 De-Icing and External Cleaning

6 OPERATING CONDITIONS

6-1-0 Engine Exhaust Velocities and Temperatures

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

T.O.C.Page 2

Aug 01/19


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

8 SCALED DRAWINGS

8-0-0 SCALED DRAWINGS

10 AIRCRAFT RESCUE AND FIRE FIGHTING

10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING

T.O.C.Page 3

Aug 01/19


SCOPE

1-1-0 Purpose

**ON A/C A340-200 A340-300

Introduction

1. GeneralThe A340-200/-300 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCEPLANNING (AC) manual is issued for the A340-200 and A340-300 basic versions to providenecessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO) for airportand maintenance facilities planning.

This document is not customized and must not be used for training purposes.

The A340 is part of an integrated family sharing the same modern technology as the A330 andmaintaining the commonality that is integrated into the Airbus Fly-by-Wire family. It has undergonea program of continuous improvement and still delivers the value that airline customers expect, as theA340 has over 50 customers and operators with more than 350 A340s flying to over 150 airportsevery week.

The different models of the A340 family can carry from 250 to 440 passengers and are operating onsome of the world’s longest routes.

A stand-out benefit of the four-engine A340 is that it does not require any ETOPS certification. Thisallows quick start-up of long-haul operations. It also has good ’hot and high’ capability at airportsthat would be off-limits to other aircraft.

The A340 has one of the quietest and most comfortable cabins in the sky, with state-of-the-art LED(Light Emitting Diode) lighting, mood styles of lighting and AVOD IFE systems.

The A340 combines good capability, economics and passenger product in one package.

Correspondence concerning this publication should be directed to:

AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services1, Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE

1-1-0Page 1

Aug 01/19


1-2-1 Glossary

**ON A/C A340-200 A340-300

Glossary

1. List of Abbreviations

A/C Aircraft

ACN Aircraft Classification NumberAMM Aircraft Maintenance ManualAPU Auxiliary Power Unit

B/C Business Class

C/L Center Line

CBR California Bearing Ratio

CC Cargo Compartment

CG Center of Gravity

CKPT Cockpit

CLG Centerline Landing Gear

E Young’s Modulus

ELEC Electric, Electrical, Electricity

ESWL Equivalent Single Wheel Load

F/C First Class

FAA Federal Aviation AdministrationFDL Fuselage Datum Line

FR FrameFSTE Full Size Trolley Equivalent

FWD ForwardGPU Ground Power UnitGSE Ground Support Equipment

HYD Hydraulic

ICAO International Civil Aviation Organisation

IDG Integrated Drive Generator

ISA International Standard Atmosphere

L Radius of relative stiffnessLCN Load Classification NumberLD Load DeviceLD Lower DeckL/G Landing Gear

LH Left HandLPS Last Pax Seating

1-2-1Page 1

Aug 01/19


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

Aug 01/19


AIRCRAFT DESCRIPTION

2-1-1 General Aircraft Characteristics Data

**ON A/C A340-200 A340-300

General Aircraft Characteristics Data

**ON A/C A340-300

1. The following table provides characteristics of A340-300 Models, these data are specific to eachWeight Variant:

Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004

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

254 400 kg(560 856 lb)

257 900 kg(568 572 lb)

260 900 kg(575 186 lb)

257 900 kg(568 572 lb)

260 900 kg(575 186 lb)

Maximum Take-Off Weight(MTOW)

253 500 kg(558 872 lb)

257 000 kg(566 588 lb)

260 000 kg(573 202 lb)

257 000 kg(566 588 lb)

260 000 kg(573 202 lb)

Maximum Landing Weight(MLW)

186 000 kg(410 060 lb)

186 000 kg(410 060 lb)

186 000 kg(410 060 lb)

188 000 kg(414 469 lb)

188 000 kg(414 469 lb)

Maximum Zero Fuel Weight(MZFW)

174 000 kg(383 604 lb)

174 000 kg(383 604 lb)

174 000 kg(383 604 lb)

178 000 kg(392 423 lb)

178 000 kg(392 423 lb)



271 900 kg(599 437 lb)

275 900 kg(608 255 lb)

262 900 kg(579 595 lb)

275 900 kg(608 255 lb)

260 900 kg(575 186 lb)


271 000 kg(597 453 lb)

275 000 kg(606 271 lb)

262 000 kg(577 611 lb)

275 000 kg(606 271 lb)

260 000 kg(573 202 lb)


190 000 kg(418 878 lb)

190 000 kg(418 878 lb)

190 000 kg(418 878 lb)

192 000 kg(423 287 lb)

190 000 kg(418 878 lb)


178 000 kg(392 423 lb)

178 000 kg(392 423 lb)

178 000 kg(392 423 lb)

180 000 kg(396 832 lb)

178 000 kg(392 423 lb)

2-1-1Page 1

Aug 01/19


Aircraft CharacteristicsWV026 WV027 WV028 WV029


275 900 kg(608 255 lb)

271 900 kg(599 437 lb)

277 400 kg(611 562 lb)

260 900 kg(575 186 lb)


275 000 kg(606 271 lb)

271 000 kg(597 453 lb)

276 500 kg(609 578 lb)

260 000 kg(573 202 lb)


192 000 kg(423 287 lb)

192 000 kg(423 287 lb)

190 000 kg(418 878 lb)

188 000 kg(414 469 lb)


181 000 kg(399 037 lb)

178 000 kg(392 423 lb)

178 000 kg(392 423 lb)

178 000 kg(392 423 lb)



275 900 kg(608 255 lb)

275 900 kg(608 255 lb)

277 400 kg(611 562 lb)

277 400 kg(611 562 lb)

275 900 kg(608 255 lb)


275 000 kg(606 271 lb)

275 000 kg(606 271 lb)

276 500 kg(609 578 lb)

276 500 kg(609 578 lb)

275 000 kg(606 271 lb)


192 000 kg(423 287 lb)

192 000 kg(423 287 lb)

192 000 kg(423 287 lb)

192 000 kg(423 287 lb)

192 000 kg(423 287 lb)


180 000 kg(396 832 lb)

181 000 kg(399 037 lb)

181 000 kg(399 037 lb)

183 000 kg(403 446 lb)

183 000 kg(403 446 lb)

2. The following table provides characteristics of A340-300 Models, these data are common to eachWeight Variant:

Aircraft CharacteristicsStandard Seating Capacity 335

140 640 l(37 153 US gal)Usable Fuel Capacity

(density = 0.785 kg/l) 110 402 kg(243 395 lb)

Pressurized Fuselage Volume(A/C non equipped)

1 056 m3

(37 292 ft3)

Passenger CompartmentVolume

372 m3

(13 137 ft3)

2-1-1Page 2

Aug 01/19


Aircraft Characteristics

Cockpit Volume12 m3

(424 ft3)

Usable Volume, FWD CC(Based on LD3)

78 m3

(2 754 ft3)

Usable Volume, AFT CC(Based on LD3)

60.7 m3

(2 142 ft3)

Usable Volume, Bulk CC19.7 m3

(695 ft3)

Water Volume, FWD CC107 m3

(3 789 ft3)

Water Volume, AFT CC85.7 m3

(3 026 ft3)

Water Volume, Bulk CC22.7 m3

(802 ft3)

**ON A/C A340-200

3. The following table provides characteristics of A340-200 Models, these data are specific to eachWeight Variant:

Aircraft CharacteristicsWV000 WV001 WV002 WV021


254 400 kg(560 856 lb)

257 900 kg(568 572 lb)

260 900 kg(575 186 lb)

275 900 kg(608 255 lb)


253 500 kg(558 872 lb)

257 000 kg(566 588 lb)

260 000 kg(573 202 lb)

275 000 kg(606 271 lb)


181 000 kg(399 037 lb)

181 000 kg(399 037 lb)

181 000 kg(399 037 lb)

185 000 kg(407 855 lb)


169 000 kg(372 581 lb)

169 000 kg(372 581 lb)

169 000 kg(372 581 lb)

173 000 kg(381 400 lb)

4. The following table provides characteristics of A340-200 Models, these data are common to eachWeight Variant:

Aircraft CharacteristicsStandard Seating Capacity 303

2-1-1Page 3

Aug 01/19


Aircraft Characteristics140 640 l

(37 153 US gal)Usable Fuel Capacity(density = 0.785 kg/l) 110 402 kg

(243 395 lb)

Pressurized Fuselage Volume(A/C non equipped)

946 m3

(33 408 ft3)

Passenger CompartmentVolume

345 m3

(12 184 ft3)

Cockpit Volume12 m3

(424 ft3)

Usable Volume, FWD CC(Based on LD3)

60.7 m3

(2 142 ft3)

Usable Volume, AFT CC(Based on LD3)

52 m3

(1 836 ft3)

Usable Volume, Bulk CC19.7 m3

(695 ft3)

Water Volume, FWD CC84.6 m3

(2 988 ft3)

Water Volume, AFT CC71.1 m3

(2 511 ft3)

Water Volume, Bulk CC22.7 m3

(802 ft3)

2-1-1Page 4

Aug 01/19


2-2-0 General Aircraft Dimensions

**ON A/C A340-200 A340-300

General Aircraft Dimensions

1. This section provides general aircraft dimensions.

2-2-0Page 1

Aug 01/19


**ON A/C A340-300

(126.44 ft)38.54 m

(3.18 ft)0.97 m

(35.04 ft)10.68 m

(41.37 ft)12.61 m

(61.48 ft)18.74 m

(2.33 ft)0.71 m

(197.83 ft)60.3 m

(63.65 ft)19.4 m

(26.71 ft)8.14 m

(25.52 ft)7.78 m

(171.98 ft)52.42 m

(206.17 ft)62.84 m

(208.86 ft)63.66 m

(21.88 ft)6.67 m

(105.15 ft)32.05 m − MLG

(108.4 ft)33.04 m − CLG

(18.5 ft)5.64 m

(27.23 ft)8.3 m

(10.17 ft)3.1 m

NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT. F_AC_020200_1_0070101_01_02

General Aircraft Dimensions(Sheet 1 of 2)

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

2-2-0Page 2

Aug 01/19


**ON A/C A340-300

(73.46 ft)22.39 m

(95.01 ft)28.96 m

(138.52 ft)42.22 m

(128.28 ft)39.1 m

(202.33 ft)61.67 m

(208.96 ft)63.69 m

(34.45 ft)10.5 m

(8.2 ft)2.5 m

(6.63 ft)2.02 m

(21.1 ft)6.43 m

(35.7 ft)10.88 m

7.46 m

(46.

62 ft

)14

.21

m

(57.

91 ft

)17

.65

m

(24.48 ft)

NOTE:RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.

F_AC_020200_1_0070102_01_00


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

2-2-0Page 3

Aug 01/19


**ON A/C A340-200

(3.18 ft)0.97 m

(35.04 ft)10.68 m

(41.37 ft)12.61 m

(61.48 ft)18.74 m

(128.61 ft)39.2 m

(2.33 ft)0.71 m

(197.83 ft)60.3 m

(63.65 ft)19.4 m

(26.7 ft)8.14 m

(25.59 ft)7.8 m

(157.97 ft)48.15 m

(192.16 ft)58.57 m

(194.85 ft)59.39 m

(21.88 ft)6.67 m

(98.13 ft)29.91 m − MLG

(101.41 ft)30.91 m − CLG

(27.23 ft)8.3 m


(10.17 ft)3.1 m

(18.5 ft)5.64 m

F_AC_020200_1_0080101_01_02


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

2-2-0Page 4

Aug 01/19


**ON A/C A340-200


(66.44 ft)20.25 m

(88.02 ft)26.83 m

(132.22 ft)40.3 m

(121.29 ft)36.97 m

(188.32 ft)57.4 m

(194.95 ft)59.42 m

(34.45 ft)10.5 m

(8.43 ft)2.57 m

(6.63 ft)2.02 m

(21.1 ft)6.43 m

(35.7 ft)10.88 m

7.46 m(24.48 ft)

(57.

91 ft

)17

.65

m

(46.

62 ft

)14

.21

m

F_AC_020200_1_0080102_01_00


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

2-2-0Page 5

Aug 01/19


2-3-0 Ground Clearances

**ON A/C A340-200 A340-300

Ground Clearances

1. This section provides the height of various points of the aircraft, above the ground, for differentaircraft configurations.Dimensions in the tables are approximate and will vary with tire type, weight and balance and otherspecial conditions.

The dimensions are given for:- A light weight, for an A/C in maintenance configuration with a mid CG,- An aircraft at Maximum Ramp Weight with a FWD CG and an AFT CG,- Aircraft on jacks, FDL at 6.50 m (21.33 ft).

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

2-3-0Page 1

Aug 01/19


**ON A/C A340-300

CP D1 D2N1 N2

D3 W2 W1 D4 AP

VTF5

C3 C2 F3BF

F2F4

C1 F1HT

ENGINE/NACELLE

FUSELAGE

D1D2D3D4C1C2C3F1F2F3F4F5BFCPW1W2HTAPVTN1N2

4.454.725.145.492.583.273.431.842.062.457.548.301.825.237.556.008.047.1916.881.252.35

14.5915.5016.8618.018.4610.7311.256.036.758.0324.7327.235.97

17.1524.7619.6826.3723.5855.364.107.70

4.604.795.105.362.713.183.321.982.132.397.668.181.835.417.485.947.836.98

16.671.282.35

15.0915.7116.7317.588.8810.4310.896.496.987.83

25.1226.836.0017.7424.5419.4825.6822.8954.684.207.70

4.594.845.315.702.733.443.582.132.272.377.768.422.02

7.916.358.147.3016.991.422.59

15.0515.8717.4218.698.9511.2811.746.987.447.7725.4527.626.62

25.9420.8326.7023.9455.724.658.49

6.326.326.326.534.144.244.393.683.683.689.329.323.267.108.967.559.238.1017.622.793.98

20.7320.7320.7321.4213.5813.9114.4012.0712.0712.0730.5830.5810.7023.3029.4024.7730.2826.5757.819.15

13.06

WINGS

TAILPLANE

DOORS

A/C CONFIGURATIONMRW

FWD CG AFT CGm ft m ft

MID CGm ft m ft

125 000 kg(275 578 lb) A/C JACKED

FDL = 6.50 m (21.33 ft)

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

F_AC_020300_1_0050101_01_03

Ground ClearancesFIGURE-2-3-0-991-005-A01

2-3-0Page 2

Aug 01/19


**ON A/C A340-200

ENGINE/NACELLE

FUSELAGE

D1D2D3D4C1C2C3F1F2F3F4F5BFCPW1W2HTAPVTN1N2

4.444.715.135.492.583.413.411.832.082.467.548.291.865.217.576.018.057.2016.901.222.34

14.5615.4516.8318.018.4611.1811.186.006.828.0624.7327.196.10

17.0924.8319.7126.4123.6155.434.007.67

4.564.775.105.382.683.183.331.952.132.417.648.191.855.367.505.967.887.02

16.721.262.34

14.9515.6516.7317.648.7910.4310.926.406.987.90

25.0626.866.0717.5824.6019.5525.8423.0254.854.137.67

4.584.865.325.702.733.453.582.142.262.667.788.432.02

7.956.378.187.3317.031.412.60

15.0215.9417.4518.698.9511.3111.747.027.418.7225.5227.656.62

26.0820.8926.8324.0455.864.628.53

6.326.326.326.534.144.244.393.683.683.689.329.323.267.108.967.559.238.1017.622.793.98

20.7320.7320.7321.4213.5813.9114.4012.0712.0712.0730.5830.5810.7023.3029.4024.7730.2826.5757.819.15

13.06

WINGS

TAILPLANE

DOORS

A/C CONFIGURATIONMRW

FWD CG AFT CGm ft m ft

MID CGm ft m ft

124 000 kg(273 373 lb) A/C JACKED

FDL = 6.50 m (21.33 ft)

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

CP D1 D2N1 N2

D3 W2 W1 D4 AP

VT C3 C2 F3BF

F2F4

C1 F1HTF5

F_AC_020300_1_0050201_01_01

Ground ClearancesFIGURE-2-3-0-991-005-B01

2-3-0Page 3

Aug 01/19


**ON A/C A340-200 A340-300

20.616.28 5.99 19.65 5.95 19.52

21.206.46 6.15 20.18 6.10 20.02

21.976.70 6.36 20.86 6.30 20.68

m ft m ft m ft

A

B

AILERONS UP

MRWAFT CG

MRWFWD CG

A/C IN MAINTENANCECONFIGURATION

MID CGDESCRIPTION

AILERON 1/2

AILERON 1 INBD

CAILERON 2 OUTBD

ABC

F_AC_020300_1_0080101_01_03

Ground ClearancesAilerons -- Up

FIGURE-2-3-0-991-008-A01

2-3-0Page 4

Aug 01/19


**ON A/C A340-200 A340-300

17.615.37 5.08 16.65 5.04 16.52

18.725.71 5.40 17.70 5.35 17.55

20.166.15 5.80 19.04 5.75 18.86

m ft m ft m ft

A

B

AILERONS DOWN

MRWAFT CG

MRWFWD CG


MID CGDESCRIPTION

AILERON 1/2

AILERON 1 INBD

CAILERON 2 OUTBD

AC B

F_AC_020300_1_0100101_01_03

Ground ClearancesAilerons -- Down

FIGURE-2-3-0-991-010-A01

2-3-0Page 5

Aug 01/19


**ON A/C A340-200 A340-300

19.956.08 5.85 19.19 5.82 19.11

20.456.23 5.98 19.64 5.96 19.55

20.896.37 6.10 20.02 6.07 19.92

21.346.50 6.22 20.42 6.19 20.32

15.604.75 4.56 14.97 4.55 14.91

17.385.30 5.09 16.69 5.07 16.63

18.705.70 5.49 18.01 5.47 17.95

19.365.90 5.68 18.64 5.66 18.58

m ft m ft m ft

B

C

SPOILERS EXTENDED

D

E

F

G

A

MRWAFT CG

MRWFWD CG


MID CG

SPOILER 1 OUTBD

SPOILER 2 INBD

SPOILER 2/3

SPOILER 3/4

SPOILER 4/5

SPOILER 6 OUTBD

SPOILER 1 INBD

DESCRIPTION

H

SPOILER 5/6

ABCDEFGH

F_AC_020300_1_0110101_01_03

Ground ClearancesSpoilers -- Extended

FIGURE-2-3-0-991-011-A01

2-3-0Page 6

Aug 01/19


**ON A/C A340-200 A340-300

m ft m ft m ft

A

B

C

MRWAFT CG

MRWFWD CG


MID CGDESCRIPTION

SLAT 1 INBD

SLAT 1 OUTBD

SLAT 2 INBD

11.32

13.98

14.01

3.45

4.26

4.27

3.26

4.05

4.08

10.70

13.29

13.39

3.28

4.06

4.09

10.76

13.32

13.42

LEADING EDGE SLATS EXTENDED

DSLAT 2/3 15.194.63 4.43 14.53 4.43 14.53

ESLAT 3/4 16.244.95 4.73 15.52 4.72 15.49

FSLAT 4 OUTBD 17.195.24 5.00 16.40 4.98 16.34

GSLAT 5 INBD 17.395.30 5.06 16.60 5.03 16.50

HSLAT 5/6 18.275.57 5.30 17.39 5.27 17.29

JSLAT 6/7 19.135.83 5.53 18.14 5.49 18.01

KSLAT 7 OUTBD 19.886.06 5.73 18.80 5.68 18.64

D E F G H J KCA B

F_AC_020300_1_0210101_01_01

Ground ClearancesLeading Edge Slats -- Extended

FIGURE-2-3-0-991-021-A01

2-3-0Page 7

Aug 01/19


**ON A/C A340-200 A340-300

m ft m ft m ft

MRWAFT CG

MRWFWD CG


MID CGDESCRIPTION

AFLAP 1 INBD 8.862.70 2.50 8.22 2.48 8.14

BFLAP 1 OUTBD 13.083.99 3.77 12.38 3.75 12.30

CFLAP 2 INBD 13.053.98 3.76 12.34 3.74 12.26

DFLAP 2 OUTBD 16.765.11 4.82 15.81 4.78 15.67

FLAPS EXTENDED

AD BC

F_AC_020300_1_0220101_01_01

Ground ClearancesTrailing Edge Flaps -- Extended

FIGURE-2-3-0-991-022-A01

2-3-0Page 8

Aug 01/19


**ON A/C A340-200 A340-300

m ft m ft m ft

MRWAFT CG

MRWFWD CG


MID CGDESCRIPTION

FLAP TRACKS EXTENDED

AFLAP TRACK 2 9.582.92 2.73 8.95 2.70 8.86

BFLAP TRACK 3 11.293.44 3.25 10.66 3.22 10.55

CFLAP TRACK 4 12.013.66 3.47 11.38 3.43 11.26

DFLAP TRACK 5 13.073.98 3.79 12.44 3.75 12.30

AD BC

F_AC_020300_1_0230101_01_01

Ground ClearancesFlap Tracks -- Extended

FIGURE-2-3-0-991-023-A01

2-3-0Page 9

Aug 01/19


**ON A/C A340-200 A340-300

AIRCRAFTTYPE

A340−300

A340−200

m ft m ft m ft

A

B

C

MRWAFT CG

MRWFWD CG


MID CGDESCRIPTION

FLAP TRACK 2

FLAP TRACK 3

FLAP TRACK 4

12.63

14.14

15.05

3.85

4.31

4.59

3.66

4.12

4.37

12.01

13.51

14.33

3.64

4.10

4.33

11.94

13.45

14.20

FLAP TRACKS RETRACTED

DFLAP TRACK 5 16.074.90 4.66 15.28 4.61 15.12

12.663.86 3.66 12.01 3.64 11.94

14.204.33 4.11 13.48 4.10 13.45

15.094.60 4.37 14.33 4.34 14.23

16.174.93 4.66 15.28 4.62 15.15

FLAP TRACK 2

FLAP TRACK 3

FLAP TRACK 4

FLAP TRACK 5

A

B

C

D

ABCD

F_AC_020300_1_0300101_01_00

Ground ClearancesFlap Tracks -- Retracted

FIGURE-2-3-0-991-030-A01

2-3-0Page 10

Aug 01/19


**ON A/C A340-200 A340-300

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

11.42

12.93

13.84

3.48

3.94

4.22

3.29

3.75

4.00

10.79

12.30

13.12

FLAP TRACKS 1+F

MRWAFT CG

D 14.864.53 4.29 14.07

AIRCRAFTTYPE

A340−300

A

B

C

11.48

13.06

13.29

3.50

3.98

4.05

3.30

3.76

3.82

10.83

12.34

12.53

3.27

3.73

3.97

10.73

12.24

13.02

D 14.834.52 4.25 13.94 4.25 13.94

A340−200

3.27

3.73

3.96

10.73

12.24

12.99

4.24 13.91

AD BC

F_AC_020300_1_0330101_01_00

Ground ClearancesFlap Tracks -- 1 + F

FIGURE-2-3-0-991-033-A01

2-3-0Page 11

Aug 01/19


2-4-1 Interior Arrangements - Plan View

**ON A/C A340-200 A340-300

Interior Arrangements - Plan View

1. This section provides the typical interior configuration.

2-4-1Page 1

Aug 01/19


**ON A/C A340-300

305 ECONOMY CLASS SEATS

ATTENDANT SEATS 9

GALLEYS 6

LAVATORIES 8

STOWAGES 3

PASSENGER SEATS (335 TOTAL)

30 FIRST CLASS SEATS

ATTENDANT SEATSTOWAGEGALLEYSTOWAGE

GALLEYSTOWAGE

AFT PASSENGER/AFT PASSENGER/CREW DOOR 4 RH CREW DOOR 4 LH

LAVATORYLAVATORY

ATTENDANT SEAT ATTENDANT SEAT

ATTENDANT SEATATTENDANT SEAT

LAVATORYLAVATORY

GALLEY

GALLEY

ATTENDANT SEAT

GALLEY

LAVATORYGALLEY

LAVATORY

ATTENDANT SEAT

ECONOMYCLASS SEATS

ECONOMYCLASS SEATS

ECONOMYCLASS SEATS

FIRST CLASS SEATS

EMERGENCY EXITDOOR 3 RH

EMERGENCY EXITDOOR 3 LH

FWD PASSENGER/CREW DOOR 1 RH

FWD PASSENGER/CREW DOOR 1 LH

MID PASSENGER/CREW DOOR 2 LHMID PASSENGER/

CREW DOOR 2 RH

F_AC_020401_1_0030101_01_01

Interior Arrangements - Plan ViewTypical Configuration

FIGURE-2-4-1-991-003-A01

2-4-1Page 2

Aug 01/19


**ON A/C A340-200




ATTENDANT SEATS 9

GALLEYS 5

LAVATORIES 7

STOWAGES 3


GALLEY

LAVATORY

LAVATORY

FWD PASSENGER/CREW DOOR 1 LHATTENDANT SEAT

ATTENDANT SEAT

FIRST CLASS SEATS

ECONOMYCLASS SEATS

GALLEY

MID PASSENGER/CREW DOOR 2 RH

LAVATORY

ECONOMYCLASS SEATS

MID PASSENGER/CREW DOOR 2 LHATTENDANT SEATLAVATORY

ATTENDANT SEAT

GALLEY

ATTENDANT SEAT


EMERGENCY EXITDOOR 3 RH

ATTENDANT SEAT

ECONOMYCLASS SEATS

LAVATORY

AFT PASSENGER/CREW DOOR 4 LH

AFT PASSENGER/CREW DOOR 4 RH

ATTENDANT SEAT

GALLEYSTOWAGE

ATTENDANT SEAT

GALLEYSTOWAGE

STOWAGE

F_AC_020401_1_0040101_01_01


FIGURE-2-4-1-991-004-A01

2-4-1Page 3

Aug 01/19


**ON A/C A340-200

48 BUSINESS CLASS SEATS


ATTENDANT SEATS 14

CREW REST COMPARTMENTS 2

GALLEYS 10



LAVATORIES 8

STOWAGES 4

FWD PASSENGER/CREW DOOR 1 LH


LAVATORYGALLEY

ATTENDANT SEAT

STOWAGE

ATTENDANT SEAT

GALLEYLAVATORY

FIRST CLASS SEATS

BUSINESSCLASS SEATS

MID PASSENGER/CREW DOOR 2 RH

GALLEY

STOWAGE

ATTENDANT SEAT

GALLEY

MID PASSENGER/CREW DOOR 2 LH

LAVATORY

ATTENDANT SEAT

BUSINESSCLASS SEATS

LAVATORYATTENDANT SEAT

ECONOMYCLASS SEATS

EMERGENCY EXITDOOR 3 RHLAVATORY

ATTENDANT SEAT

LAVATORY


ECONOMYCLASS SEATS

AFT PASSENGER/CREW DOOR 4 LH

ATTENDANT SEAT

AFT PASSENGER/CREW DOOR 4 RH

ATTENDANT SEATSTOWAGE

GALLEY

ATTENDANT SEATSTOWAGE

GALLEY

ATTENDANT SEAT

ATTENDANT SEAT

CREW RESTCOMPARTMENT

CREW RESTCOMPARTMENT

GALLEY

F_AC_020401_1_0050101_01_01


FIGURE-2-4-1-991-005-A01

2-4-1Page 4

Aug 01/19


2-5-0 Interior Arrangements - Cross Section

**ON A/C A340-200 A340-300

Interior Arrangements - Cross Section

1. This section gives the typical configuration of A340-200/-300 models.

2-5-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

C D C

F N M

H

K K

222 in5.640 m

208 in5.290 m

FIRST CLASS, 6 ABREAST BUSINESS CLASS, 7 ABREAST

TOURIST CLASS, 8 ABREAST CHARTER CLASS, 9 ABREAST

A − 54.0 in (1371.6 mm)B − 21.0 in (533 mm)C − 39.6 in (1006 mm)D − 17.7 in (450 mm)E − 72.0 in (1829 mm)F − 19.0 in (483 mm)

G − 48.0 in (1219 mm)H − 19.8 in (503 mm)K − 41.5 in (1054.1 mm)M − 57.1 in (1450 mm)N − 16.5 in (419 mm)

C

ABA

D

F G

C D

DCH

C C

E

M

91.7 in2.330 mA

F_AC_020500_1_0020101_01_00

Interior Arrangements - Cross SectionTypical Configuration

FIGURE-2-5-0-991-002-A01

2-5-0Page 2

Aug 01/19


2-6-1 Lower Deck Cargo Compartments

**ON A/C A340-200 A340-300

Lower Deck Cargo Compartments

1. This section provides the following data about lower deck cargo compartments:- Location and dimensions- Loading combinations.

2-6-1Page 1

Aug 01/19


**ON A/C A340-200 A340-300

0.95 m(3.12 ft)

2.75 m(9.02 ft)

2.78 m(9.12 ft)

15.02 m(49.28 ft)

A340−300

12.88 m(42.26 ft)

A340−200

12.32 m(40.42 ft)

10.19 m(33.43 ft)

4.04 m(13.25 ft)

4.04 m(13.25 ft)

LOWER DECKFWD CARGO

COMPARTMENT

LOWER DECKAFT CARGO

COMPARTMENT

LOWER DECKBULK CARGO

COMPARTMENT

FR39.1 FR53.2 FR65 FR73FR20

NOTE:APPROXIMATE DIMENSIONS DEPENDING ON AIRCRAFT CONFIGURATION.

F_AC_020601_1_0050101_01_02

Lower Deck Cargo CompartmentsLocation and Dimensions

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

2-6-1Page 2

Aug 01/19


**ON A/C A340-200

14 LD3 60.4 in X 61.5 in

5 PALLETS 96 in X 125 in


12 LD3 60.4 in X 61.5 in



F_AC_020601_1_0060101_01_04

Lower Deck Cargo CompartmentsLoading Combinations

FIGURE-2-6-1-991-006-A01

2-6-1Page 3

Aug 01/19


**ON A/C A340-300

18 LD3 60.4 in X 61.5 in



14 LD3 60.4 in X 61.5 in



F_AC_020601_1_0060201_01_02

Lower Deck Cargo CompartmentsLoading Combinations

FIGURE-2-6-1-991-006-B01

2-6-1Page 4

Aug 01/19


2-7-0 Door Clearances

**ON A/C A340-200 A340-300

Door Clearances

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

2-7-0Page 1

Aug 01/19


**ON A/C A340-200

DOOR 1L

DOOR 2L

DOOR 3L

DOOR 4L

BULK CARGOCOMPARTMENT

DOOR AFT CARGO

COMPARTMENTDOOR

DOOR 4R

DOOR 3R DOOR 1R

DOOR 2R

FWD CARGOCOMPARTMENT

DOOR

F_AC_020700_1_0080101_01_01

Door ClearancesDoor Identification (Sheet 1 of 2)

FIGURE-2-7-0-991-008-A01

2-7-0Page 2

Aug 01/19


**ON A/C A340-200

46.69 m(153.18 ft)

33.83 m(110.99 ft)

17.74 m(58.2 ft)

5.85 m(19.19 ft)

43.07 m(141.31 ft)

9.53 m(31.27 ft)

40.09 m(131.53 ft)

F_AC_020700_1_0080102_01_00

Door ClearancesDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-008-A01

2-7-0Page 3

Aug 01/19


**ON A/C A340-300

DOOR 1L DOOR 2L DOOR 3LDOOR 4L

BULK CARGOCOMPARTMENT

DOOR AFT CARGO

COMPARTMENTDOOR

DOOR 4RDOOR 3R DOOR 1RDOOR 2R

FWD CARGOCOMPARTMENT

DOOR

F_AC_020700_1_0080201_01_01

Door ClearancesDoor Identification (Sheet 1 of 2)

FIGURE-2-7-0-991-008-B01

2-7-0Page 4

Aug 01/19


**ON A/C A340-300

50.96 m(167.19 ft)

35.96 m(117.98 ft)

17.74 m(58.2 ft)

5.85 m(19.19 ft)

47.35 m(155.35 ft)

9.53 m(31.27 ft)

44.36 m(145.54 ft)

F_AC_020700_1_0080202_01_00

Door ClearancesDoor Location (Sheet 2 of 2)FIGURE-2-7-0-991-008-B01

2-7-0Page 5

Aug 01/19


**ON A/C A340-200 A340-300

3.30 m(10.83 ft)

CLEARANCELIMIT

CRITICAL

SEECHAPTER

2−3

1.93 m(6.33 ft)

3.00 m(9.84 ft)

5.85 m(19.19 ft)

1.07 m(3.51 ft)0.64 m

(2.10 ft)

2.43 m(7.97 ft)

0.05 m(0.16 ft)

0.75 m(2.46 ft)

F_AC_020700_1_0300101_01_00

Door ClearancesForward Passenger/Crew Doors

FIGURE-2-7-0-991-030-A01

2-7-0Page 6

Aug 01/19


**ON A/C A340-200 A340-300

0.05 m(0.16 ft)

SEECHAPTER

2−3

1.93 m(6.33 ft)

0.64 m(2.10 ft)

FWD

A A

17.74 m(58.20 ft)

(FROM NOSE)

3.41 m(11.19 ft)

0.75 m(2.46 ft)

1.07 m(3.51 ft)

2.43 m(7.97 ft)

(TOP OF FLOOR)

A

A

F_AC_020700_1_0310101_01_00

Door ClearancesMid Passenger/Crew DoorsFIGURE-2-7-0-991-031-A01

2-7-0Page 7

Aug 01/19


**ON A/C A340-200 A340-300

A

A

A A

A340−200: 33.83 m (110.99 ft)A340−300: 35.96 m (117.98 ft)

SEE

2−3CHAPTER

3.41 m(11.19 ft)

(TOP OF FLOOR)

0.59 m(1.94 ft)

1.93 m(6.33 ft)

0.04 m(0.13 ft)

(FROM NOSE)

CL

0.77 m(2.53 ft)

2.36 m(7.74 ft)

1.07 m(3.51 ft)

F_AC_020700_1_0320101_01_00

Door ClearancesEmergency Exits

FIGURE-2-7-0-991-032-A01

2-7-0Page 8

Aug 01/19


**ON A/C A340-200 A340-300

CL

A A

0.05 m(0.16 ft)

A340−200: 46.69 m (153.18 ft)A340−300: 50.96 m (167.19 ft)

3.00 m(9.84 ft)

0.64 m(2.10 ft)

1.99 m(6.53 ft)

1.07 m(3.51 ft)

0.75 m(2.46 ft)

CRITICALCLEARANCE

LIMIT

2.43 m(7.97 ft)

(FROM NOSE)

SEE

2−3CHAPTER

A

A

F_AC_020700_1_0330101_01_00

Door ClearancesAft Passenger/Crew DoorsFIGURE-2-7-0-991-033-A01

2-7-0Page 9

Aug 01/19


**ON A/C A340-200 A340-300

CL

A A

2.70 m(8.86 ft)

9.53 m(31.27 ft)

FWD

(FROM NOSE)

5.27 m(17.29 ft)

A

A

SEECHAPTER

2−3

2.04 m(6.69 ft)

1.70 m(5.58 ft)

F_AC_020700_1_0340101_01_00

Door ClearancesForward Cargo Compartment Door

FIGURE-2-7-0-991-034-A01

2-7-0Page 10

Aug 01/19


**ON A/C A340-200 A340-300

A A

A340−200: 40.09 m (131.53 ft)A340−300: 44.36 m (145.54 ft)

(FROM NOSE)

CL

5.19 m(17.03 ft)

2.03 m(6.66 ft) 1.68 m

(5.51 ft)

FWD

2.78 m(9.12 ft)

A

A

SEECHAPTER

2−3

F_AC_020700_1_0350101_01_00

Door ClearancesAft Cargo Compartment DoorFIGURE-2-7-0-991-035-A01

2-7-0Page 11

Aug 01/19


**ON A/C A340-200 A340-300

SEECHAPTER

2−3

(FROM NOSE)

FWD

A

A

A340−200: 43.08 m (141.34 ft)A340−300: 47.34 m (155.31 ft)

1.11 m(3.64 ft)

0.95 m(3.12 ft)

1.41 m(4.63 ft)

1.07 m(3.51 ft)

A A

F_AC_020700_1_0360101_01_00

Door ClearancesBulk Cargo Compartment Door

FIGURE-2-7-0-991-036-A01

2-7-0Page 12

Aug 01/19


**ON A/C A340-200 A340-300

1.32 m(4.33 ft)

1.25 m(4.10 ft)

67°

1.65 m(5.41 ft)

FR1

F_AC_020700_1_0370101_01_00

Door ClearancesRadome

FIGURE-2-7-0-991-037-A01

2-7-0Page 13

Aug 01/19


**ON A/C A340-200 A340-300

Z−2.00 m (6.56 ft)

LH SHOWNRH SYMMETRICAL

A/C

A

C L

GROUND LINE

0.06 m(0.20 ft)

2.70 m(8.86 ft)

0.23 m(0.75 ft)

1.56 m(5.12 ft)

0.85 m(2.79 ft)

A340−200: 27.31 m (89.60 ft)A340−300: 29.45 m (96.62 ft)

01

NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01

1.10 m(3.61 ft)

GROUND LINE

0.95 m(3.12 ft)

A

2.34 m(7.68 ft)

0.97 m(3.18 ft)

3.03 m(9.94 ft)

3.96 m(12.99 ft)

81°

F_AC_020700_1_0380101_01_00

Door ClearancesMain and Center Landing Gear Doors

FIGURE-2-7-0-991-038-A01

2-7-0Page 14

Aug 01/19


**ON A/C A340-200

FR101FR95

FWD

MAX. 6.85 m (22.47 ft)MIN. 6.11 m (20.05 ft)

MAX. 6.51 m (21.36 ft)MIN. 5.77 m (18.93 ft)

MAX. 1.57 m (5.15 ft)MIN. 1.39 m (4.56 ft)

MAX. 2.00 m (6.56 ft)MIN. 1.82 m (5.97 ft)

01

01

0101

NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01 F_AC_020700_1_0390101_01_00

Door ClearancesAPU and Nose Landing Gear Doors

FIGURE-2-7-0-991-039-A01

2-7-0Page 15

Aug 01/19


**ON A/C A340-300

FR101FR95

FWD

01

0101

01

MAX. 6.88 m (22.57 ft)MIN. 6.14 m (20.14 ft)

MAX. 6.53 m (21.42 ft)MIN. 5.79 m (19.00 ft)

MAX. 1.58 m (5.18 ft)MIN. 1.40 m (4.59 ft)

MAX. 2.01 m (6.59 ft)MIN. 1.83 m (6.00 ft)

NOTE:DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT.01 F_AC_020700_1_0400101_01_00

Door ClearancesAPU and Nose Landing Gear Doors

FIGURE-2-7-0-991-040-A01

2-7-0Page 16

Aug 01/19


2-8-0 Escape Slides

**ON A/C A340-200 A340-300

Escape Slides

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

2. LocationEscape facilities are provided at the following locations:

A. Door Escape Facility- One dual lane escape slide-raft at each passenger/crew door (total six)- One single lane escape slide at each emergency exit door (total two).The slides are installed in a container in the lower part of the door.

2-8-0Page 1

Aug 01/19


**ON A/C A340-200

COCKPITESCAPE ROPE

FWD CABIN DUAL−LANEESCAPE SLIDE/RAFT

MID CABIN DUAL−LANEESCAPE SLIDE/RAFT

AFT CABIN DUAL−LANEESCAPE SLIDE/RAFT

NOTE:− LH SHOWN, RH SYMMETRICAL.− *THE SINGLE−LANE ESCAPE SLIDE SHOWN IS FOR A TYPE "1" DOOR.

A DUAL−LANE ESCAPE SLIDE/RAFT IS AVAILABLE FOR AIRCRAFT FITTED WITH A TYPE "A" DOOR.

EMERGENCY EXITSINGLE−LANE

ESCAPE SLIDE*

F_AC_020800_1_0030101_01_01

Escape SlidesLocation (Sheet 1 of 2)

FIGURE-2-8-0-991-003-A01

2-8-0Page 2

Aug 01/19


**ON A/C A340-200

GR

ID E

QU

ALS

1 m

(3.

28 ft

) IN

RE

ALI

TY

0 −3

−6 −9

−12

−15 −21

−18

−24

−27

−30 −33

EM

ER

GE

NC

Y D

ES

CE

NT

TH

RO

UG

H T

HE

WIN

DO

W O

PE

NIN

G W

ITH

TH

E E

SC

AP

E R

OP

E

EM

ER

GE

NC

Y E

VA

CU

AT

ION

NO

TE

:−

LH

SH

OW

N, R

H S

YM

ME

TR

ICA

L.−

DIM

EN

SIO

NS

AR

E A

PP

RO

XIM

AT

E.

F_AC_020800_1_0030102_01_01

Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-003-A01

2-8-0Page 3

Aug 01/19


**ON A/C A340-300

COCKPITESCAPE ROPE

EMERGENCY EXITSINGLE−LANE

ESCAPE SLIDE*

NOTE:− LH SHOWN, RH SYMMETRICAL.− *THE SINGLE−LANE ESCAPE SLIDE SHOWN IS FOR A TYPE "1" DOOR.

A DUAL−LANE ESCAPE SLIDE/RAFT IS AVAILABLE FOR AIRCRAFT FITTED WITH A TYPE "A" DOOR.

FWD CABIN DUAL−LANEESCAPE SLIDE/RAFT

MID CABIN DUAL−LANEESCAPE SLIDE/RAFT

AFT CABIN DUAL−LANEESCAPE SLIDE/RAFT

F_AC_020800_1_0030201_01_01

Escape SlidesLocation (Sheet 1 of 2)

FIGURE-2-8-0-991-003-B01

2-8-0Page 4

Aug 01/19


**ON A/C A340-300

GR

ID E

QU

ALS

1 m

(3.

28 ft

) IN

RE

ALI

TY

0 −3

−6 −9

−12

−15 −21

−18

−24

−27

−30 −33

EM

ER

GE

NC

Y D

ES

CE

NT

TH

RO

UG

H T

HE

WIN

DO

W O

PE

NIN

G W

ITH

TH

E E

SC

AP

E R

OP

E

EM

ER

GE

NC

Y E

VA

CU

AT

ION

NO

TE

:−

LH

SH

OW

N, R

H S

YM

ME

TR

ICA

L.−

DIM

EN

SIO

NS

AR

E A

PP

RO

XIM

AT

E.

F_AC_020800_1_0030202_01_01

Escape SlidesDimensions (Sheet 2 of 2)FIGURE-2-8-0-991-003-B01

2-8-0Page 5

Aug 01/19


2-9-0 Landing Gear

**ON A/C A340-200 A340-300

Landing Gear Maintenance Pits

1. General

The minimum maintenance pit envelopes for the main landing gear shock absorber removal are shownin Figures 1 and 2.

All dimensions shown are minimum dimensions with zero clearances.

The dimensions for the pits have been determined for these design factors:- The length and width of the pits allow the gear to rotate as the weight is taken off the landing

gear- The depth of the pits allow the shock absorber to be removed when all the weight is taken off the

landing gear.

Dimensions for elevators and associated mechanisms must be added to those in Figures 1 and 2.

A. Elevators

These can be either mechanical or hydraulic. Elevators are used to:- permit easy movement of persons and equipment around the main landing gears- to lift and remove landing gear assemblies out of the pits.

B. Jacking

The aircraft must be in position over the pits to put the gear on the elevators. Jacks must beinstalled and engaged with all the jacking points (Ref. Section 2-14 for Jacking).Jacks must support the total aircraft weight, i.e. when the landing gears do not touch theelevators on retraction/extension tests.When tripod support jacks are used, the tripod-base circle radius must be limited because thelocations required for positioning the jacks are close to the sides of the pits.

2-9-0Page 1

Aug 01/19


**ON A/C A340-300

FR

ON

T O

F N

OS

E R

AD

OM

E

FO

RW

AR

D J

AC

KIN

G P

OIN

T

WIN

G J

AC

KIN

G P

OIN

T

AIR

CR

AF

T C

EN

TE

R L

INE

WIN

G J

AC

KIN

G P

OIN

T31

.55

m(1

03.5

1 ft)

3.58

m(1

1.75

ft)

8.51

m(2

7.92

ft)

3.89

m(1

2.76

ft)

6.31

m(2

0.7

ft)

5.34

m(1

7.52

ft)

34.3

1 m

(112

.57

ft)25.3

8 m

(83.

27 ft

)

3.65

m(1

1.98

ft)

NO

TE

:E

NV

ELO

PE

S S

HO

WN

WIT

H Z

ER

O C

LEA

RA

NC

E T

O O

UT

SID

E E

DG

E O

F T

IRE

S.

F_AC_020900_1_0030101_01_00

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

FIGURE-2-9-0-991-003-A01

2-9-0Page 2

Aug 01/19


**ON A/C A340-300

DIM

EN

SIO

NS

mm

ftft

MA

IN L

AN

DIN

G G

EA

R

6.53

m(2

1.42

ft)

FU

SE

LAG

E H

OR

IZO

NT

AL

DA

TU

M

(103

.02

ft)31

.4 m

33.1

3 m

(108

.69

ft)

FR

ON

T O

F N

OS

E R

AD

OM

EAB

C6.

67 m

(21.

88 ft

)

D

1.53

5.02

0.2

0.66

0.81

2.66

mft

BC

D

mft

A

1.56

5.12

3. ’C

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

HY

DR

AU

LIC

OR

ME

CH

AN

ICA

L E

LEV

AT

OR

WIT

H T

HE

MLG

SH

OC

K A

BS

OR

BE

R IN

TH

E D

EF

LAT

ED

AN

DC

OM

PR

ES

SE

D C

ON

DIT

ION

FO

R S

HO

CK

AB

SO

RB

ER

RE

MO

VA

L.

4. ’D

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

HY

DR

AU

LIC

OR

ME

CH

AN

ICA

L E

LEV

AT

OR

WIT

H T

HE

MLG

SH

OC

K A

BS

OR

BE

R IN

TH

E E

XT

EN

DE

D C

ON

DIT

ION

FO

R S

HO

CK

AB

SO

RB

ER

RE

MO

VA

L.

1. ’A

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

NLG

WH

EE

LA

BO

VE

ST

AT

IC G

RO

UN

D L

INE

WIT

H A

IRC

RA

FT

LEV

ELL

ED

AN

D J

AC

KE

D.

A P

IT IS

NO

T R

EQ

UIR

ED

FO

R T

HE

NLG

.

2. ’B

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

LO

WE

ST

MLG

MA

IN W

HE

EL

AB

OV

E S

TA

TIC

GR

OU

ND

LIN

EW

ITH

AIR

CR

AF

T J

AC

KE

D IN

TO

PO

SIT

ION

AB

OV

E H

YD

RA

ULI

C O

R M

EC

HA

NIC

AL

ELE

VA

TO

R,

FO

R R

ET

RA

CT

ION

/EX

TE

NS

ION

TE

ST

S.

NO

TE

:

F_AC_020900_1_0030102_01_00


FIGURE-2-9-0-991-003-A01

2-9-0Page 3

Aug 01/19


**ON A/C A340-200

3.58

m(1

1.75

ft)

8.51

m(2

7.92

ft)

3.89

m(1

2.76

ft)

6.31

m(2

0.7

ft)

5.34

m(1

7.52

ft)

32.1

8 m

(105

.58

ft)

29.4

1 m

(96.

49 ft

)

23.2

4 m

(76.

25 ft

)

3.65

m(1

1.98

ft)

FR

ON

T O

F N

OS

E R

AD

OM

E

FO

RW

AR

D J

AC

KIN

G P

OIN

T

WIN

G J

AC

KIN

G P

OIN

T

AIR

CR

AF

T C

EN

TE

R L

INE

WIN

G J

AC

KIN

G P

OIN

T

NO

TE

:E

NV

ELO

PE

S S

HO

WN

WIT

H Z

ER

O C

LEA

RA

NC

E T

O O

UT

SID

E E

DG

E O

F T

IRE

S.

F_AC_020900_1_0030201_01_00


FIGURE-2-9-0-991-003-B01

2-9-0Page 4

Aug 01/19


**ON A/C A340-200

DIM

EN

SIO

NS

mm

ftft

MA

IN L

AN

DIN

G G

EA

R

6.53

m(2

1.42

ft)

FU

SE

LAG

E H

OR

IZO

NT

AL

DA

TU

M

FR

ON

T O

F N

OS

E R

AD

OM

EAB

C6.

67 m

(21.

88 ft

)

D

1.53

5.02

0.2

0.66

0.81

2.66

mft

BC

D

mft

A

1.56

5.12

(95.

83 ft

)29

.21

m

30.4

m

(99.

74 ft

)

3. ’C

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

HY

DR

AU

LIC

OR

ME

CH

AN

ICA

L E

LEV

AT

OR

WIT

H T

HE

MLG

SH

OC

K A

BS

OR

BE

R IN

TH

E D

EF

LAT

ED

AN

DC

OM

PR

ES

SE

D C

ON

DIT

ION

FO

R S

HO

CK

AB

SO

RB

ER

RE

MO

VA

L.

4. ’D

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

HY

DR

AU

LIC

OR

ME

CH

AN

ICA

L E

LEV

AT

OR

WIT

H T

HE

MLG

SH

OC

K A

BS

OR

BE

R IN

TH

E E

XT

EN

DE

D C

ON

DIT

ION

FO

R S

HO

CK

AB

SO

RB

ER

RE

MO

VA

L.

1. ’A

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

NLG

WH

EE

LA

BO

VE

ST

AT

IC G

RO

UN

D L

INE

WIT

H A

IRC

RA

FT

LEV

ELL

ED

AN

D J

AC

KE

D.

A P

IT IS

NO

T R

EQ

UIR

ED

FO

R T

HE

NLG

.

2. ’B

’ RE

PR

ES

EN

TS

PO

SIT

ION

OF

LO

WE

ST

MLG

MA

IN W

HE

EL

AB

OV

E S

TA

TIC

GR

OU

ND

LIN

EW

ITH

AIR

CR

AF

T J

AC

KE

D IN

TO

PO

SIT

ION

AB

OV

E H

YD

RA

ULI

C O

R M

EC

HA

NIC

AL

ELE

VA

TO

R,

FO

R R

ET

RA

CT

ION

/EX

TE

NS

ION

TE

ST

S.

NO

TE

:

F_AC_020900_1_0030202_01_00


FIGURE-2-9-0-991-003-B01

2-9-0Page 5

Aug 01/19


**ON A/C A340-200 A340-300

Landing Gear

1. General

The aircraft has:- Two Main Landing Gears (MLG) with four wheel bogie assembly and related doors,- A Centerline Landing Gear (CLG) with twin wheel assembly and related doors,- A Nose Landing Gear (NLG) retracts forward into a fuselage compartment below the cockpit.

The main landing gears are located under each wing and retract sideways towards the fuselagecenterline.The centerline landing gear is located on the belly and retract forward into a bay in the fuselage.The nose landing gear retracts forward into a fuselage compartment below the cockpit.The retraction and extension of the landing gears and landing gear doors are operated hydraulicallyand mechanically. The control, sequence and indication are electrical.In abnormal operation, the landing gears can be extended by gravity.

For the dimensions of the landing gear footprint and tire size, refer to 07-02-00.

2. Main Landing Gear and Doors

Each MLG has a leg assembly and a four-wheel bogie beam. The MLG leg includes a shorteningmechanism, a bogie pitch trimmer and an oleo-pneumatic shock absorber. In-flight, with the MLGextended, the bogie is held in a trailing condition (rear wheels low) by an articulation linkage and apitch trimmer. The folding sidestay is locked mechanically by a lockstay (which is operated by thedownlock actuator) when the MLG is fully extended.

Each MLG bay has the following doors:- A hydraulically-operated main door,- A mechanically-operated hinged door,- A fairing door on the MLG leg.

All the doors close when the MLG retracts. When the MLG is extended the main door closes and thehinged door stays open. A manually operated mechanism (for maintenance personnel) lets the maindoors be opened for access to the MLG bay when the aircraft is on the ground.

3. Centerline Landing Gear and Doors

The CLG includes a twin-wheel axle assembly and a leg assembly that includes an oleo-pneumaticshock absorber. The CLG is supported longitudinally by a two-piece folding dragstay. The dragstay islocked mechanically by the lock links when the CLG is fully extended.

Each CLG bay has the following doors:

2-9-0Page 6

Aug 01/19


- Two hydraulically-operated FWD doors,- Two mechanically-operated AFT doors,- A fixed fairing door on the CLG leg.

All the doors close when the CLG retracts. When the CLG is extended the FWD doors close and theAFT doors stay open. A door opening mechanism lets the FWD doors be opened on the ground foraccess to the CLG bay.

4. Nose Landing Gear and Doors

The NLG includes a twin-wheel axle assembly and an oleo-pneumatic shock absorber. The NLG issupported longitudinally by a two-piece dragstay. The dragstay is locked mechanically by the locklinks when the NLG is fully extended.

Each NLG bay has the following doors:- Two hydraulically-operated FWD doors,- Two mechanically-operated AFT doors,- A fixed fairing door on the NLG leg.

All the doors close when the NLG retracts. When the NLG is extended the FWD doors close and theAFT doors stay open. A door opening mechanism lets the FWD doors be opened on the ground foraccess to the NLG bay.

5. Nose Wheel Steering (NWS)

Nose wheel steering system is a computer controlled electro-hydraulic system. The system uses thegreen main hydraulic power system to operate the hydraulic components.The steering is controlled by two hand wheel transmitters in the cockpit, which supply the primarysteering inputs to the BSCU (Brake and Steering Control Unit).A steering disconnection box is installed on the NLG to disconnect the steering for towing.

For the operation and control of nose wheel steering, refer to AMM 32-51-00.For the steering angle limits, refer to AMM 09-10-00.

6. Tow Truck Power

Electric power to the navigation lights can be provided through the tow truck power connector on the5GC or 8GH service panel, see FIGURE 2-9-0-991-016-A and for connector definition, see 05-04-04.

7. Landing Gear Servicing Points

A. GeneralFluid filling and gas charging of the MLG, CLG and NLG shock absorbers are accomplishedthrough MS28889 standard valves.

B. Charging PressuresFor charging of the landing gear shock absorbers, refer to AMM 12-14-32.

2-9-0Page 7

Aug 01/19


8. Landing Gear Control

The landing gear and door operation is controlled electrically by one of the two Landing Gear Controland Interface Units (LGCIU). Control changes from one LGCIU to the other after each extensioncycle.In normal operation, the landing gears and doors are operated by the green hydraulic system.In abnormal operation, the landing gears can be extended by the operation of electro-mechanical free-fall system. The related electrical switches in the cockpit disengages the doors and the landing gearuplocks. The landing gears then extend by free-fall and the downlock links of each landing gear (L/G)are locked in position by springs.

9. Braking

A. GeneralCarbon multi-disc brakes are installed on each wheel of the MLG. Each brake assembly has twowear indicators installed.

The braking system has four braking modes with autobrake and anti-skid systems:- Normal braking with anti-skid,- Alternate braking with anti-skid,- Alternate braking without anti-skid,- Parking brake with full brake pressure.

B. In-Flight Wheel BrakingBraking occurs automatically during the retraction of the landing gears. This stops the rotationof the MLG wheels before the landing gears go into their related bays.The wheels of the NLG are braked by spring loaded pads.

10. Tire Pressure Indicating System (TPIS)

The TPIS automatically monitors the tire pressures and shows these values on Test Equipment(BITE) and also supplies other data and warnings on the WHEEL page of the System Display (SD).

11. Built In Test Equipment (BITE)

The BITE has hardware and software for these functions:- to automatically do a self test at power-up,- to continuously monitor the related systems for failures,- to continuously monitor the interface with other specified systems in the aircraft,- to keep a record of each failure and defect and send this data to other systems in the aircraft,- to automatically do a functional test of some related systems before a landing,- to do specified system tests during ground maintenance.

The BITE for the following systems is described in these chapters:- The Brakes and Steering AMM 32-46-00,- The TPIS AMM 32-49-00,

2-9-0Page 8

Aug 01/19


- The Landing GearAMM 32-69-00.

2-9-0Page 9

Aug 01/19


**ON A/C A340-200 A340-300

MAIN DOOR

HINGED DOOR

FIXED FAIRING DOOR

A

B

C

D

F

E

DOWNLOCKACTUATOR

SHORTENINGMECHANISM

SIDE STAYASSEMBLY MLG LEG

ASSEMBLY

TORQUE LINKS

BOGIE PITCHTRIMMER

BOGIE BEAMASSEMBLY

SHOCK ABSORBER

ARTICULATING LINKS

RADIAL OR BIASPLY TIRES

A

(HYDRAULICALLYOPERATED)

FWD AXLE

AFT AXLE

BRAKE RODASSEMBLY

F_AC_020900_1_0090101_01_00

Main Landing GearGeneral (Sheet 1 of 3)

FIGURE-2-9-0-991-009-A01

2-9-0Page 10

Aug 01/19


**ON A/C A340-200 A340-300

C

WARNING FLAG

GROUND LOCK PIN

LOCK STAY

BLH SHOWN

RH SYMMETRICAL

QUICK RELEASE PIN

SAFETYCOLLAR

WARNING FLAG

WARNING FLAG

QUICK RELEASE PIN

DOOR ACTUATOR

F_AC_020900_1_0090102_01_00

Main Landing GearSafety Devices (Sheet 2 of 3)FIGURE-2-9-0-991-009-A01

2-9-0Page 11

Aug 01/19


**ON A/C A340-200 A340-300

SEAL CHANGEOVERVALVE

BLEED/INFLATIONVALVE

D

E

F

FWD

FILL VALVE

GROUND POINT

F_AC_020900_1_0090103_01_00

Main Landing GearServicing (Sheet 3 of 3)

FIGURE-2-9-0-991-009-A01

2-9-0Page 12

Aug 01/19


**ON A/C A340-200 A340-300

E

F

RETRACTIONACTUATOR

SIDE MEMBER

MAIN FITTING

BARREL

UPLOCK PIN

WEIGHT AND BALANCE SENSORATTACHMENT POINTS

SHOCKABSORBER

AXLE

TORQUE LINKS

SERVICING PLATE

HINGED DOOR DRIVE MECHANISM

ATTACHEMENT POINT

A

AFT DOOROPERATING ROD

AFT DOOR

FIXED FAIRING

FWD DOOR

A

D

(MECHANICALLYOPERATED)

(HYDRAULICALLYOPERATED)

C

B

B


F_AC_020900_1_0100101_01_00

Centerline Landing GearGeneral (Sheet 1 of 3)

FIGURE-2-9-0-991-010-A01

2-9-0Page 13

Aug 01/19


**ON A/C A340-200 A340-300

BRH SHOWN

LH SYMMETRICAL

GROUNDLOCK PIN

DRAG STAY

DOWNLOCK SPRINGS

C

ASSEMBLY

SAFETYCOLLAR

QUICK RELEASE PIN

WARNING FLAG

WARNING FLAG

QUICK RELEASE PIN

WARNINGFLAG

DOOR ACTUATOR

F_AC_020900_1_0100102_01_00

Centerline Landing GearSafety Devices (Sheet 2 of 3)FIGURE-2-9-0-991-010-A01

2-9-0Page 14

Aug 01/19


**ON A/C A340-200 A340-300

D

G

OIL FILLERVALVE

INFLATION VALVE(FIRST STAGE)

E

INFLATION VALVE(SECOND STAGE)

F

FWD


G

FWD

F_AC_020900_1_0100103_01_00

Centerline Landing GearServicing (Sheet 3 of 3)

FIGURE-2-9-0-991-010-A01

2-9-0Page 15

Aug 01/19


**ON A/C A340-200 A340-300

RETRACTION ACTUATOR

DOWNLOCKACTUATOR

MAIN FITTING

DOWNLOCK SPRINGS

TORQUE LINKS


TOWING BRACKET

SHOCK ABSORBER

AXLE

NWS ACTUATORS

LOWER DRAGSTAY(FOLDING STRUT)

UPPER DRAGSTAY(FOLDING STRUT)

EH

D

AFT DOOR(MECHANICALLY OPERATED)

FWD DOORS

A

(HYDRAULICALLY

AFT DOOR(MECHANICALLY OPERATED)

FIXED FAIRING

A

C

F

G

OPERATED)

B

B

F_AC_020900_1_0110101_01_00

Nose Landing GearGeneral (Sheet 1 of 4)

FIGURE-2-9-0-991-011-A01

2-9-0Page 16

Aug 01/19


**ON A/C A340-200 A340-300

B

DRAG STAYATTACHMENT

GROUNDLOCK PIN

LOCK SPRINGATTACHMENT

LOWERLOCK−LINK

UPPERLOCK−LINK

DOWN LOCKACTUATOR

ATTACHMENT

WARNING FLAG

C

RH SHOWNLH SYMMETRICAL

SAFETYCOLLAR

QUICK RELEASE PIN

WARNING FLAG

WARNING FLAG

QUICK RELEASE PIN

DOOR ACTUATOR

F_AC_020900_1_0110102_01_00

Nose Landing GearSafety Devices (Sheet 2 of 4)FIGURE-2-9-0-991-011-A01

2-9-0Page 17

Aug 01/19


**ON A/C A340-200 A340-300


CHARGE VALVE

BLEED VALVE

E

D

INFLATION VALVE(FIRST STAGE)

FWD

F_AC_020900_1_0110103_01_00

Nose Landing GearServicing (Sheet 3 of 4)

FIGURE-2-9-0-991-011-A01

2-9-0Page 18

Aug 01/19


**ON A/C A340-200 A340-300

INFLATION VALVE(SECOND STAGE)

LANDING GEAR

GROUND POINT

FWD

F

TOWING LEVER

SAFETY PIN(TOWING POSITION)

WARNING FLAG

NORMAL POSITION(NOSE WHEEL STEERING

OPERATIONAL)

TOWING POSITION(NOSE WHEEL STEERING

DEACTIVATED)

G

H

F_AC_020900_1_0110104_01_00

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

FIGURE-2-9-0-991-011-A01

2-9-0Page 19

Aug 01/19


**ON A/C A340-200 A340-300

5GC

5GCB

TOW−TRUCK POWER CABLE 03

TOW−TRUCK POWER CABLE 02

8GH 01

B

8GH

SAFETY PIN

ELECTRIC BOX(NLG OVERSTEER WARNING)

ELECTRICALDEACTIVATION BOX

WARNING FLAG

IF ELECTRICAL BOX03

CONNECT THE TOW−TRUCK POWER CABLE TO CONNECTOR02IF INSTALLED01

IS INSTALLED ON THE AIRCRAFT.

TO CONNECTOR

NOTE:

8GH IS NOT INSTALLED, CONNECT THE TOW−TRUCK POWER CABLE

8GH

5GC.

8GHB

8GHB IF ELECTRICAL BOX

5GCB ON ELECTRICAL DEACTIVATION BOX

AB

CONNECTOR

CONNECTOR

FOR PIN ALLOCATIONSEE 05−04−04

FOR PIN ALLOCATION

ASEE 05−04−04

F_AC_020900_1_0160101_01_00

Tow Truck PowerFIGURE-2-9-0-991-016-A01

2-9-0Page 20

Aug 01/19


2-10-0 Exterior Lighting

**ON A/C A340-200 A340-300

Exterior Lighting

1. GeneralThis section provides the location of the aircraft exterior lighting.

EXTERIOR LIGHTINGITEM DESCRIPTION

1 RIGHT NAVIGATION LIGHT (GREEN)

2 LEFT NAVIGATION LIGHT (RED)

3 TAIL NAVIGATION LIGHT (WHITE)

4 UPPER ANTI-COLLISION LIGHT/BEACON(RED)

5 LOWER ANTI-COLLISION LIGHT/BEACON(RED)

6 LOGO LIGHTS7 ENGINE SCAN LIGHTS8 WING SCAN LIGHTS9 WING STROBE LIGHT (HIGH INTENSITY,

WHITE)

10 TAIL STROBE LIGHT (HIGH INTENSITY,WHITE)

11 LANDING LIGHTS12 RUNWAY TURN-OFF LIGHTS13 TAXI LIGHTS14 TAKE-OFF LIGHTS15 CARGO COMPARTMENT FLOOD LIGHTS16 LANDING GEAR BAY/WELL LIGHTS (DOME)

2-10-0Page 1

Aug 01/19


**ON A/C A340-200

1 RH

2 LH

87 9

5

10

3

64

F_AC_021000_1_0040101_01_00

Exterior Lighting(Sheet 1 of 5)

FIGURE-2-10-0-991-004-A01

2-10-0Page 2

Aug 01/19


**ON A/C A340-200

13 12 11

14

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

F_AC_021000_1_0040102_01_00


FIGURE-2-10-0-991-004-A01

2-10-0Page 3

Aug 01/19


**ON A/C A340-200

7

21

3

7

12 12

13

14

F_AC_021000_1_0040103_01_00


FIGURE-2-10-0-991-004-A01

2-10-0Page 4

Aug 01/19


**ON A/C A340-200

99

4 5

8

10

8

1111

F_AC_021000_1_0040104_01_00


FIGURE-2-10-0-991-004-A01

2-10-0Page 5

Aug 01/19


**ON A/C A340-200

EXAMPLE FOR LIGHT N° 15

CEILING LIGHT

SPOT LIGHT

GROUND

6

6

15 16 15 16

F_AC_021000_1_0040105_01_00


FIGURE-2-10-0-991-004-A01

2-10-0Page 6

Aug 01/19


**ON A/C A340-300

1 RH

LH

4

78

6

2

9

3

10

5

F_AC_021000_1_0050101_01_00


FIGURE-2-10-0-991-005-A01

2-10-0Page 7

Aug 01/19


**ON A/C A340-300

12

14

1113

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

F_AC_021000_1_0050102_01_00


FIGURE-2-10-0-991-005-A01

2-10-0Page 8

Aug 01/19


**ON A/C A340-300

21

7

12

13

14

12

7

3

F_AC_021000_1_0050103_01_00


FIGURE-2-10-0-991-005-A01

2-10-0Page 9

Aug 01/19


**ON A/C A340-300

99

10

8

54

8

1111

F_AC_021000_1_0050104_01_00


FIGURE-2-10-0-991-005-A01

2-10-0Page 10

Aug 01/19


**ON A/C A340-300

EXAMPLE FOR LIGHT N° 15

CEILING LIGHT

SPOT LIGHT

GROUND

6

6

15 16 15 16

F_AC_021000_1_0050105_01_00


FIGURE-2-10-0-991-005-A01

2-10-0Page 11

Aug 01/19


2-11-0 Antennas and Probes Location

**ON A/C A340-200 A340-300

Antennas and Probes Location

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

2-11-0Page 1

Aug 01/19


**ON A/C A340-200

LOC

GP

S(1

)

GP

S(2

)

TC

AS

TO

P

VH

F(1

)

GP

S(2

)V

HF

(3)

ELT

MA

RK

ER

GP

S(1

)

ST

AT

IC P

RO

BE

(1)

EM

ER

GE

NC

Y S

TA

TIC

PR

OB

E(3

)

ST

AT

IC P

RO

BE

(2)

RA

DIO

ALT

IME

TE

R(2

)

RA

DIO

ALT

IME

TE

R(1

)

AT

C(4

)

WE

AT

HE

R R

AD

AR

VH

F(4

)

HF

TC

AS

BO

TT

OM

DM

E(2

)

PIT

OT

PR

OB

E(3

)

GLI

DE

AO

A S

EN

SO

R(1

)

TA

T P

RO

BE

ICE

DE

TE

CT

OR

PR

OB

E

PIT

OT

PR

OB

E(1

)

DM

E(1

)

AT

C(1

)

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0040101_01_00

Antennas and ProbesLocation (Sheet 1 of 2)

FIGURE-2-11-0-991-004-A01

2-11-0Page 2

Aug 01/19


**ON A/C A340-200

AD

F(2

)

AD

F(1

)

VO

R

EM

ER

GE

NC

Y S

TA

TIC

PR

OB

E(3

)

AT

C(3

)

PIT

OT

PR

OB

E(2

)

ICE

DE

TE

CT

OR

PR

OB

E

TA

T P

RO

BE

SA

TC

OM

VH

F(2

)S

TA

TIC

PR

OB

E(1

)

ST

AT

IC P

RO

BE

(2)

AT

C(2

)AO

A S

EN

SO

R(2

)

AO

A S

EN

SO

R(3

) S

TB

Y

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0040102_01_00


FIGURE-2-11-0-991-004-A01

2-11-0Page 3

Aug 01/19


**ON A/C A340-300

GP

S(1

)

GP

S(2

)

TC

AS

TO

P

VH

F(1

)

AT

C(4

)

GP

S(2

)V

HF

(3)

ELT

GP

S(1

)

WE

AT

HE

R R

AD

AR

HF

ST

AT

IC P

RO

BE

(1)

EM

ER

GE

NC

Y S

TA

TIC

PR

OB

E(3

)

ST

AT

IC P

RO

BE

(2)

TC

AS

BO

TT

OM

AO

A S

EN

SO

R(1

)

ICE

DE

TE

CT

OR

PR

OB

E

PIT

OT

PR

OB

E(1

)

LOC

MA

RK

ER

DM

E(2

)

DM

E(1

)

AT

C(1

)VH

F(4

)

PIT

OT

PR

OB

E(3

)

GLI

DE

TA

T P

RO

BE

RA

DIO

ALT

IME

TE

R(2

)

RA

DIO

ALT

IME

TE

R(1

)

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0050101_01_00


FIGURE-2-11-0-991-005-A01

2-11-0Page 4

Aug 01/19


**ON A/C A340-300

AD

F(2

)

AD

F(1

)

VO

R

AO

A S

EN

SO

R(3

) S

TB

Y

AO

A S

EN

SO

R(2

)

AT

C(2

)S

TA

TIC

PR

OB

E(2

)

EM

ER

GE

NC

Y S

TA

TIC

PR

OB

E(3

)

ST

AT

IC P

RO

BE

(1)

VH

F(2

)

AT

C(3

)T

AT

PR

OB

E

PIT

OT

PR

OB

E(2

)

ICE

DE

TE

CT

OR

PR

OB

E

SA

TC

OM

NO

TE

:D

EP

EN

DIN

G O

N A

IRC

RA

FT

CO

NF

IGU

RA

TIO

N

F_AC_021100_1_0050102_01_00


FIGURE-2-11-0-991-005-A01

2-11-0Page 5

Aug 01/19


2-12-0 Engine and Nacelle

**ON A/C A340-200 A340-300

Engine and Nacelle

1. Engine and Nacelle - CFM 56-5C Engine

A. EngineThe engine is an axial flow, dual spool, high bypass ratio, turbofan engine.The principal modules of the engine are:- The fan and booster- The high pressure compressor- The combustion chamber- The High Pressure Turbine (HPT)- The Low Pressure Turbine (LPT)- The accessory drive gearbox.

The fan and booster assembly consists of a single-stage fan rotor and a four-stage axial booster,cantilever-mounted at the rear of the fan disk. The compressor is a nine-stage axial flowassembly. Air, taken in through the fan and booster sections, passes through successive stagesof rotor blades and stator vanes, being compressed as it passes from stage to stage. Afterpassing through the 9 high pressure compressor stages, the air is fully compressed. The InletGuide Vanes (IGV) and the first 3 stages of the compressor are variable. The combustionchamber is a short, annular structure. The combustion of fuel takes place in the combustorinstalled in the combustion casing. The HPT module consists of a single-stage nozzle and rotor.The HPT is an air-cooled single-stage high-energy turbine. Rotor blades are individuallyreplaceable without the need for rotor disassembly or re-balancing. The LPT consists of 5 stagesof blades and vanes. The LPT drives the fan rotor through the inner concentric shaft and isaerodynamically coupled to the high pressure system. The engine and aircraft accessories aremounted on the accessory gearbox which is located on the lower portion of the fan casing and isdriven by a shaft from the transfer gearbox. Power for the engine and the aircraft accessories isextracted from the high pressure compressor rotor shaft through an inlet gearbox through theradial drive shaft to the transfer gearbox.

B. NacelleThe nacelle provides protection for the engine and the engine accessories, and aerodynamicairflow around the engine during operation. Each engine is housed in a nacelle suspended from apylon attached below the wing. The nacelle consists of the following major components:

(1) Air Intake Cowl AssemblyThe engine air intake cowl structure is an interchangeable aerodynamically-faired assembly.It is installed on the forward face of the engine fan case.

2-12-0Page 1

Aug 01/19


(2) Fan Cowl AssemblyThe fan cowls are interchangeable units. They enclose the engine fan case between the airintake cowl and the thrust reverser. Three hinges at the pylon support each fan cowl. Thefan cowls are latched at the bottom with three adjustable tension hook latches.

(3) Fan Thrust ReverserThe thrust reverser comprises two cowls. Each cowl is hinged at the top to the pylon andlatched to the other cowl along the bottom centerline; the forward end is secured onto theaft outer flange of the fan case and the aft end onto the forward outer barrel of theexhaust nozzle. The fan thrust reverser assembly forms the passage for fan airstream flowbetween the fan case aft frame and the exhaust nozzle/mixer inlet. When in reverse thrustmode, four pivoting doors turn the engine fan air flow forward and provide a braking effectto reduce the aircraft stopping distance. The thrust reverser is designed for groundoperation only. A hydraulically-actuated cowl-opening system allows each thrust reversercowl to be opened independently.

(4) Exhaust NozzleThe exhaust nozzle attaches to the thrust reverser when the reverser cowls are closed.When they are open the exhaust nozzle is maintained on the mixer by two support pinslocated on the upper forward part of the mixer and by a strut. The nozzle can be removedalone or together with the engine.

2-12-0Page 2

Aug 01/19


**ON A/C A340-200 A340-300

HP COMPRESSORFAN AND BOOSTER

1.01 m(3.31 ft)

2.62 m(8.6 ft)

2.99 m(9.81 ft)

COMBUSTIONSECTION

1.07 m(3.51 ft)

HP TURBINE

LP TURBINE

TURBINEREAR FRAME

ACCESSORY DRIVESECTION

A

1.98 m(6.5 ft)

1.05 m(3.44 ft)

2.09 m(6.86 ft)

1.28 m(4.2 ft)

2.25 m(7.38 ft)

A

B

B

NOTE:APPROXIMATE DIMENSIONS

FWD

F_AC_021200_1_0160101_01_00

Engine and NacelleEngine Dimensions - CFM 56-5C

FIGURE-2-12-0-991-016-A01

2-12-0Page 3

Aug 01/19


**ON A/C A340-200 A340-300

(4.63 ft)1.41 m

E E

(6.66 ft)2.03 m

(6.43 ft)1.96 m

D D

(7.22 ft)2.2 m BLOCKER

DOOREXTENDED

3.17 m(10.4 ft)

C C

(7.32 ft)2.23 m

(7.91 ft)2.41 m


A A B B

NAC STA

(27.99 ft)8.53 m

NAC STA

(22.28 ft)6.79 m

NAC STA

(19.13 ft)5.83 m

NAC STA

(12.43 ft)3.79 m

NAC STA

(9.35 ft)2.85 m

NAC STA

(17.03 ft)5.19 m

(18.67 ft)5.69 m

FANCOWL

EXHAUSTNOZZLETHRUST

REVERSERDISTANCE FROM

THE NOSE

A

A

B

B

C

C

E

E

D

D

AIR INTAKECOWL

DISTANCE FROMTHE NOSE A340−300 A340−200

(73.46 ft)22.39 m

(66.44 ft)20.25 m

(95.01 ft)28.96 m

(88.02 ft)26.83 m

INBOARDENGINE

OUTBOARDENGINE

(7.97 ft)2.43 m

F_AC_021200_1_0170101_01_00

Engine and NacelleNacelle Dimensions - CFM 56-5C

FIGURE-2-12-0-991-017-A01

2-12-0Page 4

Aug 01/19


**ON A/C A340-200 A340-300

4.43 m(14.53 ft)

2.01 m(6.59 ft)

1.99 m(6.53 ft)

55°

0.8 m(2.62 ft)

0.76 m2.49 ft

CONDITIONS: MTOW, MID C.G., STATIC, CFM ENGINES.

INBOARDENGINE

OUTBOARDENGINE

(REFER TOCHAPTER 2−3)

A


1.24 m (4.07 ft)

2.53 m (8.3 ft)

A

F_AC_021200_1_0180101_01_00

Engine and NacelleFan Cowls - CFM 56-5C

FIGURE-2-12-0-991-018-A01

2-12-0Page 5

Aug 01/19


**ON A/C A340-200 A340-300

ABSORBERS AND TIRES ARE AT NOMINAL PRESSURE.HEIGHT DATA GIVEN IS CORRECT WHEN LANDING GEAR SHOCK STRUT

1.69 m(5.54 ft)


DISTANCE FROMTHE GROUND

INBOARDENGINE

OUTBOARDENGINE

1.21 m(3.97 ft)

2.99 m(9.81 ft)

2.52 m(8.27 ft)

A B

4.05 m(13.29 ft)

* *

45°

A

*

GROUND LINE

*

* * FWD: 1.72 m (5.64 ft)AFT: 1.61 m (5.28 ft)

FWD: 1.2 m (3.94 ft)AFT: 1.33 m (4.36 ft)

B

F_AC_021200_1_0190101_01_00

Engine and NacelleThrust Reverser Cowls - CFM 56-5C

FIGURE-2-12-0-991-019-A01

2-12-0Page 6

Aug 01/19


2-12-1 Auxiliary Power Unit

**ON A/C A340-200 A340-300

Auxiliary Power Unit

1. GeneralThe Auxiliary Power Unit (APU) and its related mechanical components are installed at the rear partof the fuselage in the tailcone section. The APU compartment is a fireproof area (identified as theFire Zone).The APU is a pneumatic and shaft-power gas-turbine engine and is used for the ground and in-flightpower supply of the aircraft.

The APU supplies:- mechanical shaft-power to operate a generator- bleed-air to the Main Engine Start (MES) and the Environmental Control System (ECS).

A part of the automatic system, with the pneumatic and the electromechanical controls, operates thestart and the acceleration functions of the APU.An air intake system with a flap-type door is installed in front of the APU compartment. The exhaustgases pass overboard at the end of the fuselage cone.

2. PowerplantThe APU is the Garrett Gas-Turbine Compressor Power-unit (GTCP) 331-350C with a single shaftengine.

The engine is the primary component of the APU, which is of the modular design. The modules ofthe engine are:- The power section- The load compressor- The accessory drive gearbox with LRU(s).

The power section has a two-stage centrifugal compressor, a reverse-flow annular combustionchamber and a three-stage axial turbine. The power section directly operates the one-stagecentrifugal load-compressor which supplies the bleed-air to the pneumatic system. The inlet guidevanes as part of the load compressor, control the airflow.The power section also operates the gearbox which is attached to the load compressor. The followingLRU’s are mounted on the gearbox :- the APU generator,- the starter motor,- the oil pump,- the Fuel Control Unit (FCU),- the cooling air fan.The APU has a gearbox-driven oil-cooled AC generator.

2-12-1Page 1

Aug 01/19


The cooling air and ventilation system of the APU supplies the air for cooling of the APU and theequipment on the APU. It also supplies the air for ventilation of the APU compartment.

3. Control circuitThe Electronic Control Box (ECB), which controls the Fuel Control Unit (FCU) and the Inlet GuideVanes (IGV), keeps the APU at a constant speed. The control circuit is used to start the APU, toshut it down, to control it and to prevent internal failure.

4. Controls and IndicationThe primary APU controls and indications are installed in the overhead panel, on the center pedestalpanel and on the forward center panel. External APU panels are also installed on the nose landinggear and on the refuel/defuel panel, to initiate an APU emergency shut-down.

2-12-1Page 2

Aug 01/19


**ON A/C A340-200 A340-300

FR106A

FR103

FR101

FR95

FR94

FR92

FR91 317AL

315AL

313AL

Z310

A B

A

316AR

F_AC_021201_1_0020101_01_00

Auxiliary Power UnitAccess Doors (Sheet 1 of 2)FIGURE-2-12-1-991-002-A01

2-12-1Page 3

Aug 01/19


**ON A/C A340-200 A340-300

FIRE EXTINGUISHERBOTTLE

AIR INTAKE DUCT

APU

FIRE WALL

BLEED AIR LINE

OIL COOLER OUTLET

EXHAUST MUFFLER

FIXED DIVERTER

GUTTER

FR90

FR92

FR95

FR106A

FIRE WALL

FR101

B

AIR INTAKE

FORWARD

REAR

F_AC_021201_1_0020102_01_00

Auxiliary Power UnitGeneral Layout (Sheet 2 of 2)FIGURE-2-12-1-991-002-A01

2-12-1Page 4

Aug 01/19


2-13-0 Levelling, symmetry and Alignment

**ON A/C A340-200 A340-300

Leveling, Symmetry and Alignment

1. Quick LevelingThere are three alternative procedures to level the aircraft:- Quick leveling procedure with Air Data/Inertial Reference System (ADIRS)- Quick leveling procedure with a spirit level in the passenger compartment- Quick leveling procedure with a spirit level in the FWD cargo compartment.

2. Precision LevelingFor precise leveling, it is necessary to install sighting rods in the receptacles located under thefuselage (points 12 and 13 for longitudinal leveling) and under the wings (points 2LH and 2RH forlateral leveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until thereference marks on the sighting rods are aligned in the sighting plane (aircraft level).

3. Symmetry and Alignment CheckPossible deformation of the aircraft is measured by photogrammetry.

2-13-0Page 1

Aug 01/19


**ON A/C A340-200

FR57 FR58RIB12

RIB12

FR38 FR39

13

2 RH

2 LH

12

F_AC_021300_1_0040101_01_00

Location of Leveling PointsFIGURE-2-13-0-991-004-A01

2-13-0Page 2

Aug 01/19


**ON A/C A340-300

FR38 FR39

RIB12

FR58FR57.4RIB12

132 LH

2 RH

12

F_AC_021300_1_0050101_01_00

Location of Leveling PointsFIGURE-2-13-0-991-005-A01

2-13-0Page 3

Aug 01/19


2-14-0 Jacking for Maintenance

**ON A/C A340-200 A340-300

Jacking for Maintenance

1. Aircraft Jacking Points for Maintenance

A. General

(1) The A340-200/-300 can be jacked:- At not more than 152 000 kg (335 103 lb),- Within the limits of the permissible wind speed when the aircraft is jacked outside a

closed environment.

B. Primary Jacking Points

(1) The aircraft are provided with three primary jacking points:- One located under the forward fuselage (after FR10A),- Two located under the wings (one under each wing), at the intersection of RIB10 and

the rear of the spar-datum.

(2) Three jack adapters (ground equipment) are used as intermediary parts between theaircraft jacking points and the jacks:- One male spherical jack adapter at the forward fuselage,- Two female spherical jack pad adapters at the wings (one at each wing).

C. Auxiliary Jacking Point (Safety Stay)

(1) When the aircraft is on jacks, a safety stay is placed under the fuselage at FR85 to preventtail tipping caused by accidental displacement of the aircraft center of gravity.

(2) The safety point must not be used for lifting the aircraft.

(3) One male spherical stay adapter (ground equipment) is used as an intermediary partbetween the aircraft safety point and the stay.

2. Jacks and Safety Stay

A. Jack Design

(1) The maximum eligible loads given in the table (Ref. FIGURE 2-14-0-991-008-AFIGURE2-14-0-991-008-B) are the maximum loads applicable on jack fittings.

(2) In fully retracted position (jack stroke at minimum), the height of the jack is such that thejack may be placed beneath the aircraft under the most adverse conditions, namely, tiresdeflated and shock absorbers depressurized, with sufficient clearance between the aircraftjacking point and the jack upper end.

(3) The lifting jack stroke enables the aircraft to be jacked up so that the Fuselage Datum line(FDL) may be positioned up to 7.2 m (23.62 ft) from the ground to allow all requiredmaintenance procedures and in particular, the removal/installation of the landing-gearshock absorbers.

2-14-0Page 1

Aug 01/19


B. Safety StayThe stay stroke enables the aircraft tail to be supported up to the Fuselage Datum Line (FDL)positioned 7.2 m (23.62 ft) from the ground.

2-14-0Page 2

Aug 01/19


**ON A/C A340-200

SAFETY STAY

WING JACKINGPOINT

C

B’

B

FORWARD FUSELAGEJACKING POINT A

3.58 11.75 0

8.51

−8.51

0

0

27.92

−27.92

0

MAXIMUMLOAD ELIGIBLE

m ft daN

YX

m ft

29.41

29.41

51.54

96.49

96.49

169.09

12 300

80 982

80 982

4 500

FWD JACKINGPOINT

SAFETYSTAY

Y

B’

B

WING JACKINGPOINT

X

NOTE:SAFETY STAY IS NOT USED FOR JACKING.

CA

WING JACKINGPOINT

F_AC_021400_1_0080101_01_00

Jacking for MaintenanceJacking Points Location

FIGURE-2-14-0-991-008-A01

2-14-0Page 3

Aug 01/19


**ON A/C A340-300

SAFETY STAY

WING JACKINGPOINT

C

B’

B

FORWARD FUSELAGEJACKING POINT A

3.58

31.55

31.55

55.81

11.75

103.51

103.51

183.1

0

8.51

−8.51

0

0

27.92

−27.92

0

MAXIMUMLOAD ELIGIBLE

m ft

12 300

daN

YX

81 084

81 084

4 500

m ft

FWD JACKINGPOINT B’

B

NOTE:SAFETY STAY IS NOT USED FOR JACKING.

Y

X

A C

SAFETYSTAY

WING JACKINGPOINT

WING JACKINGPOINT

F_AC_021400_1_0080201_01_00

Jacking for MaintenanceJacking Points Location

FIGURE-2-14-0-991-008-B01

2-14-0Page 4

Aug 01/19


**ON A/C A340-200 A340-300

Z−2157.8

Z−2136

SPHERICALRADIUS 19 mm (0.75 in)

A

FR10A

FR10AA

FWD

B

ADAPTOR −JACK NOSE

B

F_AC_021400_1_0090101_01_00

Jacking for MaintenanceForward Jacking Point

FIGURE-2-14-0-991-009-A01

2-14-0Page 5

Aug 01/19


**ON A/C A340-200 A340-300

LOWER SURFACE

EXAMPLE

Z −790.3

Z −700.6


JACKING PADSET−WING

OUTER SKIN

RIB10OUTER SKIN

B

B

A

DATUM INTERSECTIONAT MID REAR SPAR DATUM

RIB10

RIB10

A

A

F_AC_021400_1_0100101_01_00

Jacking for MaintenanceWing Jacking Points

FIGURE-2-14-0-991-010-A01

2-14-0Page 6

Aug 01/19


**ON A/C A340-200 A340-300

ADAPT−SUPP, AFT JACK


Z −474.0

Z −440.7

A

FR85

B

B

FWD

FR85

A

F_AC_021400_1_0110101_01_00

Jacking for MaintenanceAuxiliary Jacking Point - Safety Stay

FIGURE-2-14-0-991-011-A01

2-14-0Page 7

Aug 01/19


**ON A/C A340-200

L

AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 152 000 kg (335 103 lb)

2.61 m(8.56 ft)

4.46 m(14.63 ft)

5.36 m(17.59 ft)

AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES

2.2 m(7.22 ft)

4.11 m(13.48 ft)

4.77 m(15.65 ft)

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

4.37 m(14.34 ft)

5.8 m(19.03 ft)

6.06 m(19.88 ft)

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

5.07 m(16.63 ft)

6.5 m(21.33 ft)

6.76 m(22.18 ft)

L M N

AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 127 000 kg (279 987 lb)

2.62 m(8.6 ft)

4.51 m(14.8 ft)

5.43 m(17.81 ft)

FUSELAGE

N

DATUM LINE

M

F_AC_021400_1_0120101_01_00

Jacking for MaintenanceJacking Dimensions

FIGURE-2-14-0-991-012-A01

2-14-0Page 8

Aug 01/19


**ON A/C A340-300

L

AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX. JACKWEIGHT 152 000 kg (335 103 lb)

2.52 m(8.27 ft)

4.46 m(14.63 ft)

5.38 m(17.65 ft)

AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDFLAT TIRES

2.2 m(7.22 ft)

4.1 m(13.45 ft)

4.77 m(15.65 ft)

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

4.37 m(14.34 ft)

5.8 m(19.03 ft)

6.06 m(19.88 ft)

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

5.07 m(16.63 ft)

6.5 m(21.33 ft)

6.76 m(22.18 ft)

L M N

AIRCRAFT ON WHEELS WITH STANDARD TIRES,OEW 131 215 kg (279 279 lb)

2.58 m(8.47 ft)

4.51 m(14.8 ft)

5.39 m(17.68 ft)

FUSELAGE

N

DATUM LINE

M

F_AC_021400_1_0120201_01_00

Jacking for MaintenanceJacking Dimensions

FIGURE-2-14-0-991-012-B01

2-14-0Page 9

Aug 01/19


**ON A/C A340-200

80

90

100

110

120

130

140

150

0 6 8 10 12 14 16 18 20

80

90

100

110

120

130

140

150

160

170 40

2520

1510

45 20 30 40 50 60 70

5

2 4

160

170

LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1 000)

LOA

D O

N W

ING

JA

CK

ING

PO

INT

S (

kg x

1 0

00)

AIR

CR

AF

T G

RO

SS

WE

IGH

T (

kg x

1 0

00)

PERMISSIBLE WIND SPEED (km/h)

AIRCRAFT CG (%RC)

EXAMPLE:

AT 22.8% RC . THE REACTION AT THE WING JACKING POINTS IS 137 000 kg(68 500 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINT

IS 8 000 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT

ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 145 000 kg AND CENTER OF GRAVITYAB

CD

BE IN EXCESS OF 50 km/h.

A

D

C

TIP UPSECURITYMARGIN

B

3035

F_AC_021400_1_0130101_01_00

Jacking for MaintenanceLoad at the Aircraft Jacking Points

FIGURE-2-14-0-991-013-A01

2-14-0Page 10

Aug 01/19


**ON A/C A340-300

0 6 8 10 12 14 16 18 20

80

90

100

110

120

130

140

150

160

170 4035

2520

1510

45 20 30 40 50 60 70

50

2 4

80

90

100

110

120

130

140

150

160

170

EXAMPLE:

AT 22.8% RC . THE REACTION AT THE WING JACKING POINTS IS 136 000 kg(68 000 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGE JACKING POINT

IS 9 000 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE, THE WIND SPEED MUST NOT

ASSUME AIRCRAFT WITH A GROSS WEIGHT OF 145 000 kg AND CENTER OF GRAVITYAB

CD

BE IN EXCESS OF 60 km/h.

TIP UPSECURITYMARGIN

LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1 000)

LOA

D O

N W

ING

JA

CK

ING

PO

INT

S (

kg x

1 0

00)

AIR

CR

AF

T G

RO

SS

WE

IGH

T (

kg x

1 0

00)

PERMISSIBLE WIND SPEED (km/h)

30

A

B

D

C

AIRCRAFT CG (%RC)

F_AC_021400_1_0130201_01_00

Jacking for MaintenanceLoad at the Aircraft Jacking Points

FIGURE-2-14-0-991-013-B01

2-14-0Page 11

Aug 01/19


2-14-1 Jacking of the Landing Gear

**ON A/C A340-200 A340-300

Jacking of the Landing Gear

1. GeneralLanding gear jacking will be required to lift the landing gear wheels off the ground.

NOTE : You can lift the aircraft at Maximum Ramp Weight (MRW).

NOTE : The load at each jacking position is the load required to give 25.4 mm (1 in) clearancebetween the ground and the tire.

2. Main Gear JackingThe main gears are normally jacked up by placing a jack directly under the ball pad.The ball spherical radius is 19 mm (0.75 in).It is also possible to jack the main gear using a cantilever jack.

3. Nose Gear JackingFor nose gear jacking, a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shock-absorber sliding tube. Jacking can be accomplished either by placing a jack directly under the ballpad, or using an adapter fitting provided with an identical ball pad.

4. Center Gear JackingFor center gear jacking, a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shock-absorber sliding tube. Jacking can be accomplished either by placing a jack directly under the ballpad, or using an adapter fitting provided with an identical ball pad.

2-14-1Page 1

Aug 01/19


**ON A/C A340-200 A340-300

AFT WHEELS JACKED UPFWD WHEELS INSTALLED AND INFLATED

FWD WHEELS JACKED UPAFT WHEELS INSTALLED AND INFLATED

JACKING POINT570 mm

(22.44 in)

MAX DIAMETER1 443.7 mm(56.84 in)

25.4 mm(1 in)

NORMAL ATTITUDE

JACKING POINT376 mm(14.8 in)

25.4 mm(1 in)

FWD

FWD

FWD


JACKING POINT570 mm

(22.44 in)

F_AC_021401_1_0050102_01_00

Jacking of the Landing GearMLG Jacking Point Heights (Sheet 1 of 3)

FIGURE-2-14-1-991-005-A01

2-14-1Page 2

Aug 01/19


**ON A/C A340-200 A340-300

FWD AXLEBOTH TIRES SHREDDED OR DEFLATED

AFT AXLEBOTH TIRES SHREDDED OR DEFLATED

FWD AND AFT AXLEBOTH TIRES SHREDDED OR DEFLATED

JACKING POINT376 mm(14.8 in)JACKING POINT

145.9 mm(5.74 in)

JACKING POINT376 mm(14.8 in) JACKING POINT

145.5 mm(5.73 in)



FWD

FWD

FWD

F_AC_021401_1_0050103_01_00


FIGURE-2-14-1-991-005-A01

2-14-1Page 3

Aug 01/19


**ON A/C A340-200 A340-300

AFT AXLEBOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN

JACKING POINT376 mm(14.8 in) JACKING POINT

118.8 mm(4.68 in)

FWD

FWD AND AFT AXLESTIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN



FWD

JACKING POINT376 mm(14.8 in)JACKING POINT

118.8 mm(4.68 in)

FWD

FWD AXLEBOTH TIRES SHREDDED OR DEFLATED AND WHEEL RIMS WORN

F_AC_021401_1_0050104_01_00


FIGURE-2-14-1-991-005-A01

2-14-1Page 4

Aug 01/19


**ON A/C A340-200 A340-300

1 FLAT TIRE110 mm(4.33 in)180 mm MAX

(7.09 in)

(1 in)25.4 mm

400 mm

(15.75 in)

170 mm(6.69 in) FWD

F_AC_021401_1_0060101_01_00

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

FIGURE-2-14-1-991-006-A01

2-14-1Page 5

Aug 01/19


**ON A/C A340-200 A340-300

1 083 mm(42.64 in)

270 mm(10.63 in)

NORMAL ATTITUDE

TWO TIRES DEFLATED OR SHREDDED

HEIGHT OF JACKING POINT TO GROUNDTO CHANGE/REPLACE THE WHEEL ASSEMBLY

297.5 mm(11.71 in)

JACKING POINT290 mm

(11.42 in)

JACKING POINT148.5 mm(5.85 in)

JACKING POINT400 mm

(15.75 in)

25.4 mm(1 in)

FWD

FWD

FWD

F_AC_021401_1_0060102_01_00

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

FIGURE-2-14-1-991-006-A01

2-14-1Page 6

Aug 01/19


**ON A/C A340-200 A340-300

640 mm(25.19 in)

235 mm(9.25 in) FWD

300 mm(11.81 in)

94° 15’

F_AC_021401_1_0070101_01_00

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

FIGURE-2-14-1-991-007-A01

2-14-1Page 7

Aug 01/19


**ON A/C A340-200 A340-300

TWO TIRES DEFLATED OR SHREDDED

HEIGHT OF JACKING POINT TO GROUNDTO CHANGE/REPLACE THE WHEEL ASSEMBLY

NORMAL ATTITUDE

343 mm(13.5 in)


363 mm(14.29 in)

FWD

JACKING POINT236.4 mm(9.31 in)FWD

FWD

1 443.7 mm(56.84 in)


25.4 mm(1 in)

F_AC_021401_1_0070102_01_00

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

FIGURE-2-14-1-991-007-A01

2-14-1Page 8

Aug 01/19


**ON A/C A340-300

AIRCRAFT GROSS WEIGHT

280 320 360 400 440 480 520

120 140 160 180 200 220 24020

50

70

90

120

260

560

(x 1 000 kg)

(x 1 000 lb)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

kg)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

lb)

280

600

30

40

60

80

100

110

260

250

240

230

220

210

200

190

180

170

160

150

140

130

120

110

100

90

80

70

60

50

100

240

35% MAC25% MAC18% MAC

42% MACCG POSITION

F_AC_021401_1_0080101_01_00

Jacking of the Landing GearMLG Jacking Point Loads

FIGURE-2-14-1-991-008-A01

2-14-1Page 9

Aug 01/19


**ON A/C A340-200


41% MACCG POSITION


280 320 360 400 440 480 520

120 140 160 180 200 220 24040

50

60

70

80

90

100

110

120

260

560

(x 1 000 kg)

(x 1 000 lb)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

kg)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

lb)

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

280

600

100

90

F_AC_021401_1_0080201_01_00

Jacking of the Landing GearMLG Jacking Point Loads

FIGURE-2-14-1-991-008-B01

2-14-1Page 10

Aug 01/19


**ON A/C A340-300

120 140 160 180 200 220 240 260


280 320 360 400 440 480 520

2

22

30

560

(x 1 000 kg)

(x 1 000 lb)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

kg)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

lb)

280

600

6

26

100

240

55

45

35

25

15

65

4

8

20

24

18

16

14

12

10

28

10

5

20

30

40

50

60


18% MACCG POSITION

F_AC_021401_1_0090101_01_00

Jacking of the Landing GearNLG Jacking Point Loads

FIGURE-2-14-1-991-009-A01

2-14-1Page 11

Aug 01/19


**ON A/C A340-200


280 320 360 400 440 480 520

120 140 160 180 200 220 2400

5

10

15

20

25

30

35

40

260

560

(x 1 000 kg)

(x 1 000 lb)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

kg)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

lb)

10

20

30

40

50

60

70

80

280

600

0


20% MACCG POSITION

F_AC_021401_1_0090201_01_00

Jacking of the Landing GearNLG Jacking Point Loads

FIGURE-2-14-1-991-009-B01

2-14-1Page 12

Aug 01/19


**ON A/C A340-300

280 320 360 400 440 480 520 560 600240


120 140 160 180 200 220 2400

6

10

14

260(x 1 000 kg)

(x 1 000 lb)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

kg)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

lb)

280

2

4

8

12

1000

25

20

15

10

5

30


42% MACCG POSITION

F_AC_021401_1_0100101_01_00

Jacking of the Landing GearCLG Jacking Point Loads

FIGURE-2-14-1-991-010-A01

2-14-1Page 13

Aug 01/19


**ON A/C A340-200


120 140 160 180 200 220 2400

5

15

20

25

30

260(x 1 000 kg)

(x 1 000 lb)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

kg)

LOA

D A

T J

AC

KIN

G P

OIN

T (

x 1

000

lb)

280

10

35

40

45

10

20

30

40

50

60

70

80

90

0


41% MACCG POSITION

280 320 360 400 440 480 520 560 600

F_AC_021401_1_0100201_01_00

Jacking of the Landing GearCLG Jacking Point Loads

FIGURE-2-14-1-991-010-B01

2-14-1Page 14

Aug 01/19


2-14-2 Support of Aircraft

**ON A/C A340-200 A340-300

Support of Aircraft

1. Support of AircraftWhen it is necessary to support the aircraft in order to relieve the loads on the structure for theaccomplishment of modifications or major work, it is advisable to provide adapters under the wingsand the fuselage for an alternative means of lifting.

The aircraft must not be lifted or supported by the wings or fuselage alone. It is important to supportthe aircraft fuselage and wings at the same time to prevent structural damage.

A. Shoring CradlesShoring cradles are used when it is necessary to stress-jack the aircraft to carry out maintenanceand repair work. These are used to oppose the deflections of the wings and reduce the stressesto an acceptable level at the area of maintenance and repair.

The shoring cradles, each with two adjustable pads, 152.4 mm (6 in) square, are positioned atfour locations under each wing.

The adjustable pads are faced with thin rubber and are in contact with the wing profile at thedatum intersections of the ribs and the front and rear spars (F/S and R/S).

2-14-2Page 1

Aug 01/19


**ON A/C A340-200

(SAFETY STAY)FR85FR80

FR72

FR26

FR17

FR11

RIB6 RIB6

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

FR58

RIB16RIB21

RIB31

FR53.2

RIB31

RIB21RIB16

F_AC_021402_1_0020101_01_00

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

FIGURE-2-14-2-991-002-A01

2-14-2Page 2

Aug 01/19


**ON A/C A340-200

FR7

FR17

FR20

FR26.1

FR32

FR39.1 FR53.8 FR59 FR76

A

LH SHOWN

(9.02 ft)2.75 m

(15.09 ft)4.6 m

(6.89 ft)2.1 m

EXAMPLE

A

B

RH SYMMETRICAL

B B

F_AC_021402_1_0020102_01_00

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

FIGURE-2-14-2-991-002-A01

2-14-2Page 3

Aug 01/19


**ON A/C A340-300

FR80

FR72

FR26

FR17

FR11

(SAFETY STAY)FR85

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

RIB6 RIB6

RIB31

RIB21RIB16

FR58

FR53.2

RIB16RIB21

RIB31

F_AC_021402_1_0020201_01_00

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

FIGURE-2-14-2-991-002-B01

2-14-2Page 4

Aug 01/19


**ON A/C A340-300

FR7

FR17 FR20

FR26.1

FR59 FR76FR39.1FR36 FR53.8

A

LH SHOWN

(9.02 ft)2.75 m

(15.09 ft)4.6 m

(6.89 ft)2.1 m

EXAMPLE

A

B

RH SYMMETRICAL

B B

F_AC_021402_1_0020202_01_00

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

FIGURE-2-14-2-991-002-B01

2-14-2Page 5

Aug 01/19


AIRCRAFT PERFORMANCE


**ON A/C A340-200 A340-300

General Information

1. Standard day temperatures for the altitude shown are tabulated below:

Standard day temperatures for the altitude

Altitude Standard Day Temperature

FEET METERS ˚F ˚C0 0 59.0 15.02000 610 51.9 11.14000 1220 44.7 7.16000 1830 37.6 3.18000 2440 30.5 -0.8

3-1-0Page 1

Aug 01/19


3-2-1 Payload / Range - ISA Conditions

**ON A/C A340-200 A340-300

Payload / Range - ISA Conditions

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

3-2-1Page 1

Aug 01/19


**ON A/C A340-300

0

10

20

30

40

50

60

70

80

90

100

110

120

3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500

160007000 8000 9000 10000 11000 12000 13000 14000 15000

270

280

290

300

310

320

330

340

350

360

370

380

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

NOTE: MAX TAKE−OFF WEIGHTZFW

(x 1000 lb)PAYLOAD(x 1000 lb)

RANGE(nm)

RANGE(km)

MAX STRUCTURAL PAYLOAD

MAX PASSENGER PAYLOAD

CRUISE CONDITIONSISA 39000 ft M = 0.82

F_AC_030201_1_0110101_01_01

Payload / Range - ISA ConditionsCFM56-5C2 engine

FIGURE-3-2-1-991-011-A01

3-2-1Page 2

Aug 01/19


**ON A/C A340-200

0

10

20

30

40

50

60

70

80

90

100

110

120

3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500

160007000 8000 9000 10000 11000 12000 13000 14000 15000

270

280

290

300

310

320

330

340

350

360

370

380




RANGE(nm)

RANGE(km)




F_AC_030201_1_0120101_01_01


FIGURE-3-2-1-991-012-A01

3-2-1Page 3

Aug 01/19


**ON A/C A340-300

0

10

20

30

40

50

60

70

80

90

100

110

120

3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500

160007000 8000 9000 10000 11000 12000 13000 14000 15000

270

280

290

300

310

320

330

340

350

360

370

380




RANGE(nm)

RANGE(km)




F_AC_030201_1_0130101_01_01


FIGURE-3-2-1-991-013-A01

3-2-1Page 4

Aug 01/19


**ON A/C A340-200

0

10

20

30

40

50

60

70

80

90

100

110

120

3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500

160007000 8000 9000 10000 11000 12000 13000 14000 15000

270

280

290

300

310

320

330

340

350

360

370

380




RANGE(nm)

RANGE(km)




F_AC_030201_1_0140101_01_01


FIGURE-3-2-1-991-014-A01

3-2-1Page 5

Aug 01/19


**ON A/C A340-300

0

10

20

30

40

50

60

70

80

90

100

110

120

3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500

160007000 8000 9000 10000 11000 12000 13000 14000 15000

270

280

290

300

310

320

330

340

350

360

370

380




RANGE(nm)

RANGE(km)

BASIC AIRCRAFT257 000 kg MTOW

NOMINAL PERFORMANCE LEVEL




F_AC_030201_1_0150101_01_01


FIGURE-3-2-1-991-015-A01

3-2-1Page 6

Aug 01/19


**ON A/C A340-200

0

10

20

30

40

50

60

70

80

90

100

110

120

3500 4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500

160007000 8000 9000 10000 11000 12000 13000 14000 15000

270

280

290

300

310

320

330

340

350

360

370

380




RANGE(nm)

RANGE(km)




F_AC_030201_1_0160101_01_01


FIGURE-3-2-1-991-016-A01

3-2-1Page 7

Aug 01/19


**ON A/C A340-300

0

10

20

30

40

50

60

70

80

90

100

110

120

4000 4500 5000 5500 6000 6500 7000 7500 8000 90008500

160007000 8000 9000 10000 11000 12000 13000 14000 15000

270

280

290

300

310

320

330

340

350

360

370

380




RANGE(nm)

RANGE(km)

BASIC AIRCRAFT271 000 kg AND 275 000 kg MTOWNOMINAL PERFORMANCE LEVEL

275 000 kg

271 000 kg




F_AC_030201_1_0170101_01_01


FIGURE-3-2-1-991-017-A01

3-2-1Page 8

Aug 01/19


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

**ON A/C A340-200 A340-300

Take-Off Weight Limitation - ISA Conditions

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

3-3-1Page 1

Aug 01/19


**ON A/C A340-300

TAKE−OFF WEIGHT1000 lb1000 kg

RUNWAY LENGHT(1000 ft)

RUNWAY LENGHT(1000 m)

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

THES CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

640

145

165

185

205

225

245

265

285

FLAPS 3 FLAPS 1

0

F_AC_030301_1_0040101_01_00

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

2

4

6

8

BRAKE ENERGY

V.M.C

LIMITATION

Take-Off Weight LimitationISA Conditions -- CFM56-5C2 engine

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

3-3-1Page 2

Aug 01/19


**ON A/C A340-200


320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

0

FLAPS 2

580

600

620

640

145

165

185

205

225

245

265

285

FLAPS 3 FLAPS 1

NOTE: THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT

RUNWAY LENGTH(1000 ft)

RUNWAY LENGTH(1000 m)

2

F_AC_030301_1_0050101_01_00

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

4

6

8

BRAKE ENERGY

V.M.C

LIMITATION


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

3-3-1Page 3

Aug 01/19


**ON A/C A340-300


NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305



THESE CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT

8

0

4

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

6

2

BRAKE ENERGY

V.M.C

LIMITATION

F_AC_030301_1_0060101_01_00


FIGURE-3-3-1-991-006-A01

3-3-1Page 4

Aug 01/19


**ON A/C A340-200

1000 lb1000 kg

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305




F_AC_030301_1_0070101_01_00

TAKE−OFF WEIGHT

0

2

4

6

8 AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-1-991-007-A01

3-3-1Page 5

Aug 01/19


**ON A/C A340-300

1000 lb1000 kg

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305




F_AC_030301_1_0080101_01_00

TAKE−OFF WEIGHT

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)0

2

4

6

8

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-1-991-008-A01

3-3-1Page 6

Aug 01/19


**ON A/C A340-200

1000 lb1000 kg

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305




F_AC_030301_1_0090101_01_00

TAKE−OFF WEIGHT

8

6

4

2

0

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-1-991-009-A01

3-3-1Page 7

Aug 01/19


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

**ON A/C A340-200 A340-300

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

1. This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions.

3-3-2Page 1

Aug 01/19


**ON A/C A340-300

1000 lb1000 kg

RUNWAY LENGHT(1000 ft)

RUNWAY LENGHT(1000 m)

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

THES CURVES ARE GIVEN FOR INFORMATIONONLY THE APPROVED VALUES ARE STATEDIN THE "OPERATING MANUALS" SPECIFIC TOTHE AIRLINE OPERATING THE AIRCRAFT

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

640

145

165

185

205

225

245

265

285

FLAPS 3 FLAPS 1

F_AC_030302_1_0040101_01_00

TAKE−OFF WEIGHT

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)0

2

4

6

8

BRAKE ENERGY

V.M.C

LIMITATION

Take-Off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56-5C2 engine

FIGURE-3-3-2-991-004-A01

3-3-2Page 2

Aug 01/19


**ON A/C A340-200

1000 lb1000 kg

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

640

145

165

185

205

225

245

265

285

FLAPS 3 FLAPS 1




F_AC_030302_1_0050101_01_00

TAKE−OFF WEIGHT

0

2

4

6

8

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-2-991-005-A01

3-3-2Page 3

Aug 01/19


**ON A/C A340-300

1000 lb1000 kg

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305




F_AC_030302_1_0060101_01_00

TAKE−OFF WEIGHT

0

2

4

6

8 AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-2-991-006-A01

3-3-2Page 4

Aug 01/19


**ON A/C A340-200

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305




F_AC_030302_1_0070101_01_00

1000 lb1000 kgTAKE−OFF WEIGHT

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

0

2

4

6

8

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-2-991-007-A01

3-3-2Page 5

Aug 01/19


**ON A/C A340-300

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305




F_AC_030302_1_0080101_01_00


0

2

4

6

8

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-2-991-008-A01

3-3-2Page 6

Aug 01/19


**ON A/C A340-200

NOTE:

320

340

360

380

400

420

440

460

480

500

520

540

560

4 6 8 10 12 14 16

1 1.5 2 2.5 3 3.5 4 4.5 5

FLAPS 2

580

600

620

145

165

185

205

225

245

265

FLAPS 3 FLAPS 1

640

660

285

680305




F_AC_030302_1_0090101_01_00


AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)0

2

4

6

8

BRAKE ENERGY

V.M.C

LIMITATION


FIGURE-3-3-2-991-009-A01

3-3-2Page 7

Aug 01/19


3-4-1 Landing Field Length - ISA Conditions

**ON A/C A340-200 A340-300

Landing Field Length - ISA Conditions

1. This section gives the landing field length.

3-4-1Page 1

Aug 01/19


**ON A/C A340-300

345678

1

1.52

2.5

NO

TE

: TH

ES

E C

UR

VE

S A

RE

GIV

EN

FO

R IN

FO

RM

AT

ION

ON

LYT

HE

AP

PR

OV

ED

VA

LUE

S A

RE

ST

AT

ED

IN T

HE

"O

PE

RA

TIN

GM

AN

UA

LS"

SP

EC

IFIC

TO

TH

E A

IRLI

NE

OP

ER

AT

ING

TH

E A

IRC

RA

FT

.

GR

OS

S W

EIG

HT

(x 1

000

kg)

GR

OS

S W

EIG

HT

(x 1

000

lb)

(x 1

000

m)

(x 1

000

ft)

24

68

10S

EA

LE

VE

L

150

200

250

300

350

400

450

500

7510

012

515

017

520

025

050

225

ISA

CO

ND

ITIO

NS

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

LAN

DIN

G F

IELD

LE

NG

HT

F_AC_030401_1_0040101_01_01

Landing Field LengthISA Conditions -- CFM56-5C2 engine

FIGURE-3-4-1-991-004-A01

3-4-1Page 2

Aug 01/19


**ON A/C A340-200

345678

1

1.52

2.5

NO

TE

:T

HE

SE

CU

RV

ES

AR

E G

IVE

N F

OR

INF

OR

MA

TIO

N O

NLY

TH

E A

PP

RO

VE

D V

ALU

ES

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

GT

HE

AIR

CR

AF

T.

GR

OS

S W

EIG

HT

(x 1

000

kg)

GR

OS

S W

EIG

HT

(x 1

000

lb)

24

68

10S

EA

LE

VE

L

150

200

250

300

350

400

450

500

7510

012

515

017

520

025

050

225

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

LAN

DIN

G F

IELD

LE

NG

HT

(x 1

000

m)

(x 1

000

ft)

ISA

CO

ND

ITIO

NS

F_AC_030401_1_0050101_01_01


FIGURE-3-4-1-991-005-A01

3-4-1Page 3

Aug 01/19


**ON A/C A340-300

345678

1

1.52

2.5

NO

TE

:T

HE

SE

CU

RV

ES

AR

E G

IVE

N F

OR

INF

OR

MA

TIO

N O

NLY

TH

E A

PP

RO

VE

D V

ALU

ES

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

GT

HE

AIR

CR

AF

T.

GR

OS

S W

EIG

HT

(x 1

000

kg)

GR

OS

S W

EIG

HT

(x 1

000

lb)

24

68

10S

EA

LE

VE

L

150

200

250

300

350

400

450

500

7510

012

515

017

520

025

050

225

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

LAN

DIN

G F

IELD

LE

NG

HT

ISA

CO

ND

ITIO

NS

(x 1

000

m)

(x10

00 ft

)

F_AC_030401_1_0060101_01_01


FIGURE-3-4-1-991-006-A01

3-4-1Page 4

Aug 01/19


**ON A/C A340-200

345678

1

1.52

2.5

NO

TE

:T

HE

SE

CU

RV

ES

AR

E G

IVE

N F

OR

INF

OR

MA

TIO

N O

NLY

TH

E A

PP

RO

VE

D V

ALU

ES

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

GT

HE

AIR

CR

AF

T.

GR

OS

S W

EIG

HT

(x 1

000

kg)

GR

OS

S W

EIG

HT

(x 1

000

lb)

24

68

10S

EA

LE

VE

L

150

200

250

300

350

400

450

500

7510

012

515

017

520

025

050

225

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

LAN

DIN

G F

IELD

LE

NG

HT

(x 1

000

m)

(x 1

000

ft)

ISA

CO

ND

ITIO

NS

F_AC_030401_1_0070101_01_01


FIGURE-3-4-1-991-007-A01

3-4-1Page 5

Aug 01/19


**ON A/C A340-300

345678

1

1.52

2.5

NO

TE

:T

HE

SE

CU

RV

ES

AR

E G

IVE

N F

OR

INF

OR

MA

TIO

N O

NLY

TH

E A

PP

RO

VE

D V

ALU

ES

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

GT

HE

AIR

CR

AF

T.

GR

OS

S W

EIG

HT

(x 1

000

kg)

GR

OS

S W

EIG

HT

(x 1

000

lb)

24

68

10S

EA

LE

VE

L

150

200

250

300

350

400

450

500

7510

012

515

017

520

025

050

225

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

LAN

DIN

G F

IELD

LE

NG

HT

ISA

CO

ND

ITIO

NS

(x 1

000

m)

(x 1

000

ft)

F_AC_030401_1_0080101_01_01


FIGURE-3-4-1-991-008-A01

3-4-1Page 6

Aug 01/19


**ON A/C A340-200

345678

1

1.52

2.5

NO

TE

:T

HE

SE

CU

RV

ES

AR

E G

IVE

N F

OR

INF

OR

MA

TIO

N O

NLY

TH

E A

PP

RO

VE

D V

ALU

ES

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

GT

HE

AIR

CR

AF

T.

GR

OS

S W

EIG

HT

(x 1

000

kg)

GR

OS

S W

EIG

HT

(x 1

000

lb)

24

68

10S

EA

LE

VE

L

150

200

250

300

350

400

450

500

7510

012

515

017

520

025

050

225

AIR

FIE

LD E

LEV

AT

ION

(x 1

000

ft)

LAN

DIN

G F

IELD

LE

NG

HT

(x 1

000

m)

(x 1

000

ft)

ISA

CO

ND

ITIO

NS

F_AC_030401_1_0090101_01_01


FIGURE-3-4-1-991-009-A01

3-4-1Page 7

Aug 01/19


3-5-0 Final Approach Speed

**ON A/C A340-200 A340-300

Final Approach Speed

**ON A/C A340-200

1. Final Approach Speed

A. This section gives the final approach speed. This is the indicated airspeed at threshold in thelanding configuration, at the certificated maximum flap setting and maximum landing weight, instandard atmospheric conditions. The approach speed is used to classify the aircraft into anAircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.

B. The final approach speed is 136 kt at a Maximum Landing Weight (MLW) of 185 000 kg (407855 lb) and classifies the aircraft into the Aircraft Approach Category C.

NOTE : This value is given for information only.

**ON A/C A340-300

2. Final Approach Speed

A. This section gives the final approach speed. This is the indicated airspeed at threshold in thelanding configuration, at the certificated maximum flap setting and maximum landing weight, instandard atmospheric conditions. The approach speed is used to classify the aircraft into anAircraft Approach Category, a grouping of aircraft based on the indicated airspeed at threshold.

B. The final approach speed is 138 kt at a Maximum Landing Weight (MLW) of 192 000 kg (423287 lb) and classifies the aircraft into the Aircraft Approach Category C.

NOTE : This value is given for information only.

3-5-0Page 1

Aug 01/19


GROUND MANEUVERING


**ON A/C A340-200 A340-300

General Information

1. This section provides aircraft turning capability and maneuvering characteristics.

For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.

In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the airlines in question prior to layout planning

4-1-0Page 1

Aug 01/19


4-2-0 Turning Radii

**ON A/C A340-200 A340-300

Turning Radii

1. This section provides the turning radii.

4-2-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

62°60°

55°

R6

R4

R5

R3

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

R2

R1

F_AC_040200_1_0050101_01_02

Turning Radii(Sheet 1)

FIGURE-4-2-0-991-005-A01

4-2-0Page 2

Aug 01/19


**ON A/C A340-300

19.320

TYPE OFTURN

267.9223

A340−300 TURNING RADII

m

ft78.6258

77.2253

R4WING

102.9338

R5NOSE

79.1260

R6TAIL

87.9288

R1RMLG

R2LMLG

R3NLG

24.125252.3172

62.9206

62.6205

87.3286

65.1214

73.5241

28.930241.5136

52.2171

52.9174

76.7252

56.0184

64.0210

33.735233.7111

44.4146

46.2152

68.9226

49.8163

57.3188

38.440227.791

38.3126

41.3135

62.9206

45.3149

52.4172

43.045222.875

33.5110

37.6123

58.1191

42.0138

48.6159

47.550218.862

29.597

34.8114

54.2178

39.6130

45.7150

51.955215.5

5126.286

32.6107

51.0167

37.7124

43.3142

56.060212.842

23.477

30.9101

48.2158

36.3119

41.5136

59.665210.534

21.270

29.797

46.0151

35.3116

40.1132

62.47028.929

19.564

28.995

44.4146

34.7114

39.1128

51.750115.752

26.487

32.7107

51.1168

37.8124

43.4142

56.555112.4

4123.176

30.7101

47.9157

36.2119

41.3135

61.26019.531

20.266

29.296

45.1148

34.9115

39.5130

65.96517.023

17.758

28.092

42.6140

34.0112

38.0125

70.47014.715

15.350

27.189

40.3132

33.3109

36.8121

m

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ft

m

ftm

ftm

ftm

ftm

ft

STEERING ANGLE (deg)EFFECTIVESTEERING

ANGLE (deg)

NOTE:ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION.TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; AND NO DIFFERENTIAL BRAKING AT ALL.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYINGDIFFERENTIAL BRAKING DURING THE WHOLE TURN.

63.27228.428

19.163

28.794

44.0144

34.5113

38.8127

m

ft

72.27213.812

14.548

26.888

39.5130

33.1109

36.3119

m

ft

F_AC_040200_1_0100101_01_01


FIGURE-4-2-0-991-010-A01

4-2-0Page 3

Aug 01/19


**ON A/C A340-200

19.120

TYPE OFTURN

262.6205

A340−200 TURNING RADII

m

ft73.3240

71.4234

R4WING

97.6320

R5NOSE

73.4241

R6TAIL

82.2270

R1RMLG

R2LMLG

R3NLG

23.925248.1158

58.8193

57.9190

83.2273

60.4198

68.8226

28.630238.2125

48.9160

49.0161

73.4241

52.1171

60.1197

33.335231.0102

41.7137

42.8140

66.3218

46.4152

53.9177

37.940225.584

36.2119

38.3126

60.8199

42.3139

49.4162

42.445221.169

31.7104

34.9115

56.4185

39.3129

45.9151

46.850217.557

28.192

32.3106

52.9174

37.0121

43.2142

50.955214.548

25.283

30.399

49.9164

35.4116

41.1135

54.860212.039

22.775

28.894

47.5156

34.1112

39.4129

58.065210.133

20.868

27.791

45.7150

33.2109

38.2125

60.37028.929

19.664

27.089

44.4146

32.7107

37.4123

51.350114.247

24.982

30.199

49.7163

35.2115

40.9134

56.155111.337

22.072

28.393

46.8154

33.8111

38.9128

60.76018.729

19.363

26.988

44.2145

32.6107

37.3122

65.36516.321

17.056

25.885

42.0138

31.8104

35.9118

69.77014.214

14.949

25.082

39.9131

31.1102

34.7114

m

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ftm

ft

m

ftm

ftm

ftm

ftm

ft


ANGLE (deg)

NOTE:ABOVE 50°, AIRLINES MAY USE TYPE 1 OR TYPE 2 TURNS DEPENDING ON THE SITUATION.TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLE TURN; ANDDIFFERENTIAL BRAKING TO INITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLE TURN; AND NO DIFFERENTIAL BRAKING AT ALL.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1 BY APPLYINGDIFFERENTIAL BRAKING DURING THE WHOLE TURN.

60.87228.628

19.363

26.988

44.2145

32.6107

37.2122

m

ft

71.67213.411

14.146

24.781

39.1128

30.9101

34.3113

m

ft

F_AC_040200_1_0110101_01_01


FIGURE-4-2-0-991-011-A01

4-2-0Page 4

Aug 01/19


4-3-0 Minimum Turning Radii

**ON A/C A340-200 A340-300

Minimum Turning Radii

1. This section provides the minimum turning radii.

4-3-0Page 1

Aug 01/19


**ON A/C A340-300

NOTE:TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLETURN; AND NO DIFFERENTIAL BRAKING AT ALL.

A(MINIMUM TURNING WIDTH)

65.965 (MAX)

TYPE OFTURN

111.437

A340−300 MINIMUM TURNING RADII

m

ft46.0151

28.092

R4WING

42.6140

R5NOSE

34.0112

R6TAIL

38.0125

R3NLG

59.665 (MAX)214.949

51.2168

29.797

46.0151

35.3116

40.1132

m

ft


ANGLE (deg)

NOTE:IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.

25.483

25.483

AX Y

Y

R6

R4

OUTSIDE FACEOF TIRE

72 (MAX)

72 (MAX)

2

1

63.2

72.2m

ftm

ft

8.227

41.7137

26.888

39.5130

33.1109

36.3119

12.842

48.1158

28.794

44.0144

34.5113

38.8127

25.483

25.483

R5

R3

X

F_AC_040300_1_0030101_01_02

Minimum Turning RadiiFIGURE-4-3-0-991-003-A01

4-3-0Page 2

Aug 01/19


**ON A/C A340-200

NOTE:TYPE 1 TURNS USE:ASYMMETRIC THRUST DURING THE WHOLETURN; AND DIFFERENTIAL BRAKING TOINITIATE THE TURN ONLY.TYPE 2 TURNS USE:SYMMETRIC THRUST DURING THE WHOLETURN; AND NO DIFFERENTIAL BRAKING AT ALL.

A(MINIMUM TURNING WIDTH)

65.365 (MAX)

TYPE OFTURN

110.735

A340−200 MINIMUM TURNING RADII

m

ft43.2142

25.885

R4WING

42.0138

R5NOSE

31.8104

R6TAIL

35.9118

R3NLG

58.065 (MAX)214.548

48.8160

27.791

45.7150

33.2109

38.2125

m

ft


ANGLE (deg)

NOTE:IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.

23.276

23.276

AX Y

72 (MAX)

72 (MAX)

2

1

60.8

71.6m

ftm

ft

7.725

39.1128

24.781

39.1128

30.9101

34.3113

13.043

46.5153

26.988

44.2145

32.6107

37.2122

23.276

23.276

R6

R4

R5

R3

Y

OUTSIDE FACEOF TIRE

X

F_AC_040300_1_0040101_01_02

Minimum Turning RadiiFIGURE-4-3-0-991-004-A01

4-3-0Page 3

Aug 01/19


4-4-0 Visibility from Cockpit in Static Position

**ON A/C A340-200 A340-300

Visibility from Cockpit in Static Position

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

4-4-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

NOT TO BE USED FORLANDING APPROACH VISIBILITY

CAPTAIN FIELD OF VIEW

VISUAL ANGLES IN HORIZONTALPLANE THROUGH PILOTEYE POSITION.

FIRST OFFICERFIELD OF VIEW

25°

20°

13.75 m(45.11 ft)

6.67 m(21.88 ft)

VISUAL ANGLES IN VERTICALPLANE THROUGH PILOTEYE POSITION.

DIMENSIONS ARE APPROXIMATE

2.4 m(7.87 ft)

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

ZONE THAT CANNOT BE SEEN

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

0.53 m(1.74 ft)

62°

42°

30°36°

30°

VISUAL ANGLES IN PLANEPERPENDICULAR TOLONGITUDINAL AXIS.

62°

42°

WITH HEAD MOVED125 mm (5 in) OUTBOARD

36°

115°

135°

115°

135°

F_AC_040400_1_0040101_01_02

Visibility from Cockpit in Static PositionFIGURE-4-4-0-991-004-A01

4-4-0Page 2

Aug 01/19


**ON A/C A340-200 A340-300

CA

PT

AIN

WIN

DS

HIE

LDC

AP

TA

IN S

LID

ING

WIN

DO

WC

AP

TA

INF

IXE

D W

IND

OW

WIN

G T

IPV

ISIB

LE

CA

PT

AIN

’S F

IELD

OF

VIE

W S

HO

WN

, TH

RO

UG

H C

AP

TA

IN W

IND

OW

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40°

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°40

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°70

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0°12

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F_AC_040400_1_0080101_01_00

Binocular Visibility Through Windows from Captain Eye PositionFIGURE-4-4-0-991-008-A01

4-4-0Page 3

Aug 01/19


4-5-0 Runway and Taxiway Turn Paths

**ON A/C A340-200 A340-300

Runway and Taxiway Turn Paths

1. Runway and Taxiway Turn Paths.

4-5-0Page 1

Aug 01/19



**ON A/C A340-200 A340-300

135˚ Turn - Runway to Taxiway

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

4-5-1Page 1

Aug 01/19


**ON A/C A340-300

FAA LEAD−IN FILLET

L = 75 m (250 ft)

(15 ft)APPROX 4.5 m

APPROX 11.7 m(39 ft)

FILLET R = 25.5 m(85 ft)

TURN R = 45 m(150 ft)

45 m(150 ft)

23 m(75 ft)

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

NLG PATH

MLG PATH

F_AC_040501_1_0030101_01_01

135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method

FIGURE-4-5-1-991-003-A01

4-5-1Page 2

Aug 01/19


**ON A/C A340-300

APPROX 2 m(7 ft)

ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE


TURN R = 45 m(150 ft)

45 m(150 ft)


L = 75 m (250 ft)

23 m(75 ft)

F_AC_040501_1_0080101_01_00

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

NLG PATH

MLG PATH

135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method

FIGURE-4-5-1-991-008-A01

4-5-1Page 3

Aug 01/19


**ON A/C A340-200

45 m(150 ft)



TURN R = 45 m(150 ft)

APPROX 6.4 m(21 ft)

23 m(75 ft)


L = 75 m (250 ft)

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

NLG PATH

MLG PATH

F_AC_040501_1_0090101_01_00

135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method

FIGURE-4-5-1-991-009-A01

4-5-1Page 4

Aug 01/19


**ON A/C A340-200

APPROX 3.4 m(11 ft)

ADDITIONAL FILLET TO MEET

4.5 m (15 ft) EDGE CLEARANCE


TURN R = 45 m(150 ft)


L = 75 m (250 ft)

45 m150 ft

23 m(75 ft)

F_AC_040501_1_0100101_01_00

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

NLG PATH

MLG PATH


FIGURE-4-5-1-991-010-A01

4-5-1Page 5

Aug 01/19



**ON A/C A340-200 A340-300

90˚ Turn - Runway to Taxiway

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

4-5-2Page 1

Aug 01/19


**ON A/C A340-300

FAA LEAD−IN FILLETL = 75 m (250 ft)

(41 ft)APPROX 12.3 m



TURN R = 45 m(150 ft)

45 m(150 ft)

F_AC_040502_1_0030101_01_01

23 m(75 ft)

NLG PATH

MLG PATH

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

F_AC_040502_1_0030101_01_01

90˚ Turn - Runway to TaxiwayJudgement Oversteering Method

FIGURE-4-5-2-991-003-A01

4-5-2Page 2

Aug 01/19


**ON A/C A340-300

(18 ft)APPROX 5.4 m



45 m(150 ft)

TURN R = 45 m(150 ft)

23 m(75 ft)

NLG PATH

MLG PATH

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

F_AC_040502_1_0100101_01_00


FIGURE-4-5-2-991-010-A01

4-5-2Page 3

Aug 01/19


**ON A/C A340-200

45 m(150 ft)





TURN R = 45 m(150 ft)

23 m(75 ft)

NLG PATH

MLG PATH

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

F_AC_040502_1_0110101_01_00

90˚ Turn - Runway to TaxiwayJudgement Oversteering Method

FIGURE-4-5-2-991-011-A01

4-5-2Page 4

Aug 01/19


**ON A/C A340-200


(27 ft)APPROX 8 m


45 m(150 ft)

TURN R = 45 m(150 ft)

23 m(75 ft)

NLG PATH

MLG PATH

RUNWAYCENTERLINE

TAXIWAYCENTERLINE

F_AC_040502_1_0120101_01_00


FIGURE-4-5-2-991-012-A01

4-5-2Page 5

Aug 01/19


4-5-3 180˚ Turn on a Runway

**ON A/C A340-200 A340-300

180˚ Turn on a Runway

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

4-5-3Page 1

Aug 01/19


**ON A/C A340-300

NLG PATH

MLG PATH

NOSE TIP PATH

WING TIP PATH

TAIL TIP PATHNOTE:

TYPE 1 VALUES FOR MAX STEERING ANGLE = 72°.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.

50.7 m(166 ft)

41.7 m(137 ft)

4.5 m

20.2 m(66 ft)

14.6 m(48 ft)

0.9 m(3 ft)

4.5 m(15 ft)

R4 = 39.5 m(130 ft)

R6 = 36.3 m(119 ft) R3 = 26.8 m

(88 ft)

R5 = 33.1 m(109 ft)

RUNWAY CENTERLINE

(15 ft)

F_AC_040503_1_0060101_01_03

180˚ Turn on a RunwayFIGURE-4-5-3-991-006-A01

4-5-3Page 2

Aug 01/19


**ON A/C A340-200

NLG PATH

MLG PATH

NOSE TIP PATH

WING TIP PATH

TAIL TIP PATH

NLG PATH

MLG PATH

NOSE TIP PATH

WING TIP PATH

TAIL TIP PATHNOTE:

TYPE 1 VALUES FOR MAX STEERING ANGLE = 72°.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.

R5 = 30.9 m(101 ft)

4.5 m(15 ft)

20.4 m(67 ft)

13.4 m(44 ft)

0.9 m(3 ft)

4.5 m(15 ft)

R3 = 24.7 m(81 ft)

R6 = 34.3 m(113 ft)

R4 = 39.1 m(128 ft)

48.1 m(158 ft)

39.1 m(128 ft)

RUNWAY CENTERLINE

F_AC_040503_1_0070101_01_03

180˚ Turn on a RunwayFIGURE-4-5-3-991-007-A01

4-5-3Page 3

Aug 01/19



**ON A/C A340-200 A340-300

135˚ Turn - Taxiway to Taxiway

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

4-5-4Page 1

Aug 01/19


**ON A/C A340-300

TURN R = 45 m(150 ft)



APPROX 4.5 m(15 ft)


L = 75 m (250 ft)

TAXIWAY CENTERLINE

TAXIWAY CENTERLINE

NLG PATH

MLG PATH

(75 ft)23 m

23 m(75 ft)

F_AC_040504_1_0090101_01_00

135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method

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

4-5-4Page 2

Aug 01/19


**ON A/C A340-300



L = 75 m (250 ft)

APPROX 3.5 m(12 ft)

ADDITIONAL FILLET TO MEET4.5 m (15 ft) EDGE CLEARANCE

TAXIWAY CENTERLINE

TAXIWAY CENTERLINE

23 m(75 ft)

(75 ft)23 m

TURN R = 45 m(150 ft)

NLG PATH

MLG PATH

F_AC_040504_1_0100101_01_00

135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method

FIGURE-4-5-4-991-010-A01

4-5-4Page 3

Aug 01/19


**ON A/C A340-200

APPROX 13 m(43 ft)


TURN R = 45 m(150 ft)

TAXIWAY CENTERLINE

APPROX 5.1 m(17 ft)


L = 75 m (250 ft)

(75 ft)23 m

TAXIWAY CENTERLINE

NLG PATH

MLG PATH

23 m(75 ft)

F_AC_040504_1_0110101_01_00

135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method

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

4-5-4Page 4

Aug 01/19


**ON A/C A340-200


APPROX 5.2 m(17 ft)

TAXIWAY CENTERLINE


L = 75 m (250 ft)

23 m(75 ft)

TAXIWAY CENTERLINE

(75 ft)23 m

NLG PATH

MLG PATH

TURN R = 45 m(150 ft)

F_AC_040504_1_0120101_01_00


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

4-5-4Page 5

Aug 01/19



**ON A/C A340-200 A340-300

90˚ Turn - Taxiway to Taxiway

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

4-5-5Page 1

Aug 01/19


**ON A/C A340-300

(40 ft)APPROX 12 m


TAXIWAY CENTERLINE(43 ft)APPROX 12.9 m


TURN R = 45 m(150 ft)

TAXIWAY CENTERLINE

23 m(75 ft)

(75 ft)23 m NLG PATH

MLG PATH

F_AC_040505_1_0050101_01_01

90˚ Turn - Taxiway to TaxiwayJudgement Oversteering Method

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

4-5-5Page 2

Aug 01/19


**ON A/C A340-300


(14 ft)APPROX 4.1 m


TURN R = 45 m(150 ft)

4.5 m (15 ft) EDGE CLEARANCEADDITIONAL FILLET TO MEET

TAXIWAY CENTERLINE

23 m(75 ft)

TAXIWAY CENTERLINE

(75 ft)23 m

NLG PATH

MLG PATHF_AC_040505_1_0130101_01_00


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

4-5-5Page 3

Aug 01/19


**ON A/C A340-200



TURN R = 45 m(150 ft)



TAXIWAY CENTERLINE

(75 ft)23 m NLG PATH

MLG PATH

23 m(75 ft)

TAXIWAY CENTERLINE

F_AC_040505_1_0060101_01_02

90˚ Turn - Taxiway to TaxiwayJudgement Oversteering Method

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

4-5-5Page 4

Aug 01/19


**ON A/C A340-200


(24 ft)APPROX 7.1 m


TURN R = 45 m(150 ft)

TAXIWAY CENTERLINE

(75 ft)23 m

NLG PATH

MLG PATH

TAXIWAY CENTERLINE

23 m(75 ft)

F_AC_040505_1_0140101_01_00


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

4-5-5Page 5

Aug 01/19


4-6-0 Runway Holding Bay (Apron)

**ON A/C A340-200 A340-300

Runway Holding Bay (Apron)

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

4-6-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

TAXIWAYCENTERLINE

23 m(75 ft)

45 m(150 ft)

RUNWAYCENTERLINE

HOLDINGPOINT6.1 m

(20 ft)

90 m(300 ft)

97.3 m(319 ft)

6.1 m(20 ft)

12.2 m(40 ft)

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

190 m(625 ft)

NOTE:

F_AC_040600_1_0030101_01_03

Runway Holding Bay (Apron)FIGURE-4-6-0-991-003-A01

4-6-0Page 2

Aug 01/19


4-7-0 Minimum Line-Up Distance Corrections

**ON A/C A340-200 A340-300

Minimum Line-Up Distance Corrections

1. The ground maneuvers were performed using asymmetric thrust and differential-only braking toinitiate the turn.TODA: Take-Off Distance AvailableASDA: Acceleration-Stop Distance Available

2. 90˚ Turn on Runway Entry

This section gives the minimum line-up distance correction for a 90˚ turn on runway entry.This maneuver consists in a 90˚ turn at minimum turn radius. It starts with the edge of the MLG ata distance of 4.5 m (15 ft) from the taxiway edge, and finishes with the aircraft aligned on thecenterline of the runway, see FIGURE 4-7-0-991-022-A.During the turn, all the clearances must meet the minimum value of 4.5 m (15 ft) for this category ofaircraft as recommended in ICAO Annex 14.

3. 180˚ Turn on Runway Turn Pad

This section gives the minimum line-up distance correction for a 180˚ turn on the runway turn pad.This maneuver consists in a 180˚ turn at minimum turn radius on a runway turn pad with standardICAO geometry.It starts with the edge of the MLG at a distance of 4.5 m (15 ft) from the pavement edge, and itfinishes with the aircraft aligned on the centerline of the runway, see FIGURE 4-7-0-991-023-A.During the turn, all the clearances must meet the minimum value of 4.5 m (15 ft) for this category ofaircraft as recommended in ICAO Annex 14.

4. 180˚ Turn on Runway Width

This section gives the minimum line-up distance correction for a 180˚ turn on the runway width.For this maneuver, the pavement width is considered to be the runway width, which is a frozenparameter (45 m (150 ft) and 60 m (200 ft)).As per the standard operating procedures for the ”180˚ turn on runway” (described in the FlightCrew Operating Manual), the aircraft is initially angled with respect to the runway centerline whenstarting the 180˚ turn, see FIGURE 4-7-0-991-024-A.The value of this angle depends on the aircraft type and is mentioned in the FCOM.During the turn, all the clearances must meet the minimum value of 4.5 m (15 ft) for this category ofaircraft as recommended in ICAO Annex 14.

4-7-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

TAXIWAYCENTERLINE

RUNWAY

> 4.5 m(15 ft)

TODA

4.5 m(15 ft)

ASDA

CENTERLINE

90° TURN ON RUNWAY ENTRY

AIRCRAFTTYPE

STEERINGANGLE

MAX

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

MINIMUM LINE−UP DISTANCE CORRECTION

65°A340−200 21.5 m 70 ft 44.7 m 147 ftON TODA ON ASDA

72°A340−200 18.6 m 61 ft 41.8 m 137 ft

NOTE:

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

65°A340−300 22.2 m 73 ft 47.6 m 156 ft72°A340−300 20.5 m 67 ft 45.9 m 151 ft

F_AC_040700_1_0220101_01_00

Minimum Line-Up Distance Corrections90˚ Turn on Runway EntryFIGURE-4-7-0-991-022-A01

4-7-0Page 2

Aug 01/19


**ON A/C A340-200 A340-300

NOTE:


TODA

ASDA

MINIMUM PAVEMENT WIDTH

RUNWAY CENTERLINE

180° TURN ON RUNWAY TURNPAD

AIRCRAFTTYPE

STEERINGANGLE

MAX(STANDARD WIDTH)

DISTANCE CORRECTIONMINIMUM LINE−UP

DISTANCE CORRECTIONMINIMUM LINE−UP MINIMUM

REQUIRED

PAVEMENTWIDTH

65°A340−200 100 ft30.5 m 176 ft53.7 m 179 ft54.6 mON TODA ON ASDA

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

72°A340−200 97 ft29.5 m 173 ft52.7 m 160 ft48.8 m

ON TODA ON ASDA

65°A340−300 108 ft32.8 m 191 ft58.2 m 184 ft56.0 m72°A340−300 106 ft32.2 m 189 ft57.6 m 173 ft52.7 m104 ft31.7 m 187 ft57.1 m

SAME AS 45 m WIDE RWY

4.5 m(15 ft)

> 4.5 m(15 ft)

4.5 m(15 ft)

F_AC_040700_1_0230101_01_00

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

FIGURE-4-7-0-991-023-A01

4-7-0Page 3

Aug 01/19


**ON A/C A340-200 A340-300

180° TURN ON RUNWAY WIDTH

AIRCRAFTTYPE

STEERINGANGLE

MAX(STANDARD WIDTH)



65°A340−200 138 ft42.0 m 214 ft65.2 mON TODA ON ASDA ON TODA ON ASDA

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

72°A340−200NOT POSSIBLE

ASDA

TODA

> 4.5 m(15 ft)

20° RUNWAY CENTERLINE

(15 ft)

4.5 m(15 ft)

A340−300A340−300

65°72°

97 ft29.5 m 173 ft52.7 m156 ft47.6 m 239 ft73.0 m104 ft31.7 m 187 ft57.1 m

NOTE:


4.5 m

F_AC_040700_1_0240101_01_00

Minimum Line-Up Distance Corrections180˚ Turn on Runway WidthFIGURE-4-7-0-991-024-A01

4-7-0Page 4

Aug 01/19


4-8-0 Aircraft Mooring

**ON A/C A340-200 A340-300

Aircraft Mooring

1. This section provides information on aircraft mooring.

4-8-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

TOWING FITTING

GROUND ANCHOR

A

TOWING FITTING

B

WARNING FLAG

B

A

F_AC_040800_1_0010101_01_00

Aircraft MooringFIGURE-4-8-0-991-001-A01

4-8-0Page 2

Aug 01/19


TERMINAL SERVICING

5-1-0 Aircraft Servicing Arrangements

**ON A/C A340-200 A340-300

Aircraft Servicing Arrangements

1. This section provides typical ramp layouts, showing the various GSE items in position during typicalturn-round scenarios for passenger aircraft.

These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for positioning and operation on the ramp.

5-1-0Page 1

Aug 01/19


5-1-1 Symbols Used on Servicing Diagrams

**ON A/C A340-200 A340-300

Symbols Used on Servicing Diagrams

1. This table gives the symbols used on servicing diagrams.

Ground Support Equipment

AC AIR CONDITIONING UNITAS AIR START UNIT

BULK BULK TRAINCAT CATERING TRUCK

CB CONVEYOR BELTCLEAN CLEANING TRUCK

FUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNIT

LD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLE

PBB PASSENGER BOARDING BRIDGEPS PASSENGER STAIRS

TOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE

5-1-1Page 1

Aug 01/19


5-1-2 Typical Ramp Layout - Open Apron

**ON A/C A340-200 A340-300

Typical Ramp Layout - Open Apron

1. This section provides the typical servicing arrangements on the open apron, for the passenger versionof the aircraft.The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (24.61 ft) fromthe aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheelchocks in position on landing gears).

5-1-2Page 1

Aug 01/19


**ON A/C A340-300

PS CAT

PS

PS CAT

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

AS

GPU

LD CL

LD CL

AC

ULD

FUELFUEL

LV

CB

ULD

BULKWV

TOW

STAND SAFETY LINE

CAT

F_AC_050102_1_0030101_01_02

Typical Ramp LayoutOpen Apron

FIGURE-5-1-2-991-003-A01

5-1-2Page 2

Aug 01/19


**ON A/C A340-200

PS

PS

CAT

CAT

PS CAT

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

TOW

AS

GPU

LD CL

LD CL

AC

ULD

ULD

BULKCBWV

LV

FUELFUEL

STAND SAFETY LINE

F_AC_050102_1_0040101_01_02

Typical Ramp LayoutOpen Apron

FIGURE-5-1-2-991-004-A01

5-1-2Page 3

Aug 01/19


5-1-3 Typical Ramp Layout - Gate

**ON A/C A340-200 A340-300

Typical Ramp Layout - Gate

1. This section provides the typical servicing arrangements in the gate area for the passenger version ofthe aircraft, with two Passenger Boarding Bridges.The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m (24.61 ft) fromthe aircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheelchocks in position on landing gears).

5-1-3Page 1

Aug 01/19


**ON A/C A340-300

CLEAN

CAT

CAT

CAT

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

TOW

AS

GPU

LD CL

LD CL

AC

ULD

ULD

BULKCB

LV

FUELFUEL

PBB

PBB

WV

STAND SAFETY LINE

F_AC_050103_1_0020101_01_02

Typical Ramp LayoutGate

FIGURE-5-1-3-991-002-A01

5-1-3Page 2

Aug 01/19


**ON A/C A340-200

CLEAN

WV

CAT

CAT

CAT

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

AS

GPU

LD CL

LD CL

AC

ULD

FUELFUEL

LV

CB

ULD

BULK

TOW

PBB

PBB

STAND SAFETY LINE

F_AC_050103_1_0030101_01_02

Typical Ramp LayoutGate

FIGURE-5-1-3-991-003-A01

5-1-3Page 3

Aug 01/19


5-2-0 Terminal Operations - Full Servicing

**ON A/C A340-300

Terminal Operations - Full Servicing Turn Round Time

1. This section provides a typical turn round time charts showing the typical time for ramp activitiesduring aircraft turn round.Actual times may vary due to each operator’s specific practices, resources, equipment and operatingconditions.

2. Assumptions used for full servicing turn round time chart

A. PASSENGER HANDLING270 pax: 10 F/C + 28 B/C + 232 Y/C.All passengers deplane and board the aircraft.2 Passenger Boarding Bridges (PBB) used at doors L1 and L2.Equipment positioning + opening door = +3 min.Closing door + equipment removal = +3 min.No Passenger with Reduced Mobility (PRM) on board.

Deplaning:- 135 pax at door L1 (10 F/C + 28 B/C + 97 Y/C)- 135 pax at door L2 (135 Y/C)- Deplaning rate = 25 pax/min per door- Priority deplaning for premium passengers.

Boarding:- 135 pax at door L1 (10 F/C + 28 B/C + 97 Y/C)- 135 pax at door L2 (135 Y/C)- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min.

B. CARGO2 cargo loaders + 1 belt loader.Opening door + equipment positioning = +2.5 minEquipment removal + closing door = +2.5 min.

Cargo exchange:- FWD cargo compartment: 12 LD3 + 2 pallets- AFT cargo compartment: 8 LD3 + 2 pallets- Bulk cargo compartment: 1 000 kg (2 205 lb).

LD3 unloading/loading times:- Unloading = 1.2 min/LD3- Loading = 1.4 min/LD3.

5-2-0Page 1

Aug 01/19


Pallet unloading/loading times:- Unloading = 2.4 min/pallet- Loading = 2.8 min/pallet.

Bulk unloading/loading times:- Unloading = 9.2 min/t- Loading = 10.5 min/t.

C. REFUELINGBlock-fuel quantity for nominal range through 2 nozzles.127 000 l (33 550 US gal) at 50 psi (3.45 bar).Dispenser positioning + connection = +3 min.Disconnection + dispenser removal = +3 min.

D. CLEANINGCleaning is performed in available time.

E. CATERING3 catering trucks for servicing galleys at doors R1, R2 and R4.Equipment positioning + opening door = +5 min.Closing door + equipment removal = +3 min.

Full Size Trolley Equivalent (FSTE) to unload and load: 48 FSTE- 10 FSTE at door R1- 13 FSTE at door R2- 25 FSTE at door R4.Time for trolley exchange = 1.5 min per FSTE.

F. GROUND HANDLING/GENERAL SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min.

Vehicle positioning/removal = +2 min (except for fuel and catering trucks).Ground Power Unit (GPU): up to 2 × 90 kVA.Air conditioning: two hoses.Potable water servicing: 100% uplift, 700 l (185 US gal) at 60 l/min (15.85 US gal/min).Waste water servicing: draining + rinsing.

5-2-0Page 2

Aug 01/19


**ON A/C A340-300

GSE POSITIONING/REMOVAL

ACTIVITY

CRITICAL PATH

TRT: 62 min

100 20 30 40 50 60 70

DEPLANING/BOARDING AT L1

HEADCOUNTING

CATERING AT R2

CLEANING

CARGO FWD CC

BULK

REFUELING

POTABLE WATER SERVICING

WASTE WATER SERVICING


CATERING AT R4

CARGO AFT CC

CATERING AT R1

AVAILABLE TIME

F_AC_050200_1_0040101_01_01

Full Servicing Turn Round Time ChartFIGURE-5-2-0-991-004-A01

5-2-0Page 3

Aug 01/19


**ON A/C A340-200

Terminal Operations - Full Servicing Turn Round Time

1. This section provides a typical turn round time charts showing the typical time for ramp activitiesduring aircraft turn round.Actual times may vary due to each operator’s specific practices, resources, equipment and operatingconditions.

2. Assumptions used for full servicing turn round time chart

A. PASSENGER HANDLING231 pax: 10 F/C + 42 B/C + 179 Y/C.All passengers deplane and board the aircraft.2 Passenger Boarding Bridges (PBB) used at doors L1 and L2.Equipment positioning + opening door = +3 min.Closing door + equipment removal = +3 min.No Passenger with Reduced Mobility (PRM) on board.

Deplaning:- 116 pax at door L1 (10 F/C + 42 B/C + 64 Y/C)- 115 pax at door L2 (115 Y/C)- Deplaning rate = 25 pax/min per door- Priority deplaning for premium passengers.

Boarding:- 116 pax at door L1 (10 F/C + 42 B/C + 64 Y/C)- 115 pax at door L2 (115 Y/C)- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min.

B. CARGO2 cargo loaders + 1 belt loader.Opening door + equipment positioning = +2.5 min.Equipment removal + closing door = +2.5 min.

Cargo exchange:- FWD cargo compartment: 8 LD3 + 2 pallets- AFT cargo compartment: 6 LD3 + 2 pallets- Bulk cargo compartment: 1 000 kg (2 205 lb).

LD3 unloading/loading times:- Unloading = 1.2 min/LD3- Loading = 1.4 min/LD3.

Pallet unloading/loading times:

5-2-0Page 4

Aug 01/19


- Unloading = 2.4 min/pallet- Loading = 2.8 min/pallet.

Bulk unloading/loading times:- Unloading = 9.2 min/t- Loading = 10.5 min/t.

C. REFUELINGBlock-fuel quantity for nominal range through 4 nozzles.127 000 l (33 550 US gal) at 50 psi (3.45 bar).Dispenser positioning + connection = +3 min.Disconnection + dispenser removal = +3 min.

D. CLEANINGCleaning is performed in available time.

E. CATERING3 catering trucks for servicing galleys at doors R1, R2 and R4.Equipment positioning + opening door = +5 min.Closing door + equipment removal = +3 min.

Full Size Trolley Equivalent (FSTE) to unload and load: 36 FSTE- 7 FSTE at door R1- 9 FSTE at door R2- 20 FSTE at door R4.Time for trolley exchange = 1.5 min per FSTE.

F. GROUND HANDLING/GENERAL SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min

Vehicle positioning/removal = +2 min (except for fuel and catering trucks).Ground Power Unit (GPU): up to 2 × 90 kVA.Air conditioning: two hoses.Potable water servicing: 100% uplift, 700 l (185 US gal) at 60 l/min (15.85 US gal/min).Waste water servicing: draining + rinsing.

5-2-0Page 5

Aug 01/19


**ON A/C A340-200


ACTIVITY

CRITICAL PATH

TRT: 52 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_0050101_01_01

Full Servicing Turn Round Time ChartFIGURE-5-2-0-991-005-A01

5-2-0Page 6

Aug 01/19


5-3-0 Terminal Operations - Transit

**ON A/C A340-300

Terminal Operations - Minimum Servicing Turn-Round Time

1. This section provides typical turn-round time chart showing the typical times for ramp activitiesduring aircraft turn-round.Actual times may vary due to each operator’s specific practice and operating conditions.

2. Assumptions for minimum servicing turn-round time chart

A. PASSENGER HANDLING270 pax (10 F/C + 38 B/C + 222 Y/C)50% of passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board

Deboarding:- 135 pax at door L1- Deboarding rate = 25 pax/min per door

Boarding:- 135 pax at door L1- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min

B. CARGO1 cargo loader + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min

Cargo exchange:- 4 LD3 in AFT cargo compartment- 500 kg (1 102 lb) in bulk cargo compartment

LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3

Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t

C. REFUELLINGRefuelling through 2 nozzles30% of max capacity at 50 psi (3.45 bar)

5-3-0Page 1

Aug 01/19


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

Aug 01/19


**ON A/C A340-300

TRT: 33 min

50 10 15 20 25 30 35

AT L1DEBOARDING/BOARDING

HEADCOUNTING

CLEANING

CARGO FWD CC

BULK

REFUELLING


TOILET SERVICING

CATERING

CARGO AFT CC

40

AVAILABLE TIME


ACTIVITY

CRITICAL PATH

F_AC_050300_1_0050101_01_00

Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-005-A01

5-3-0Page 3

Aug 01/19


**ON A/C A340-200

Terminal Operations - Minimum Servicing Turn-Round Time

1. This section provides typical turn-round time chart showing the typical times for ramp activitiesduring aircraft turn-round.Actual times may vary due to each operator’s specific practice and operating conditions.

2. Assumptions for minimum servicing turn-round time chart

A. PASSENGER HANDLING231 pax (10 F/C + 42 B/C + 179 Y/C)50% of passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 3 minNo Passenger with Reduced Mobility (PRM) on board

Deboarding:- 116 pax at door L1- Deboarding rate = 25 pax/min per door

Boarding:- 116 pax at door L1- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +4 min

B. CARGO1 cargo loader + 1 belt loaderEquipment positioning/removal + opening/closing door = 2.5 min

Cargo exchange:- 4 LD3 in AFT cargo compartment- 500 kg (1 102 lb) in bulk cargo compartment

LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3

Bulk off-loading/loading times:- Off-loading = 9.2 min/t- Loading = 10.5 min/t

C. REFUELLINGRefuelling through 2 nozzles30% of max capacity at 50 psi (3.45 bar)Dispenser positioning/removal = 3 min

5-3-0Page 4

Aug 01/19


D. CLEANINGPerformed in available time

E. CATERING1 catering truck for servicing galleys as requiredEquipment positioning + door opening = 5 minEquipment removal + door closing = 3 minPerformed in available timeTime for trolley exchange = 1.5 min per FSTE

F. GROUND HANDLING/SERVICINGStart of operations:- Bridges: t0 = 0- Others: t0 + 1 min

Vehicle positioning/removal = 2 min (except for fuel and catering trucks)Ground Power Unit (GPU): up to 2 × 90 kVAAir conditioning: two hosesNo potable water servicingNo toilet servicing

5-3-0Page 5

Aug 01/19


**ON A/C A340-200

TRT: 31 min

50 10 15 20 25 30 35

AT L1DEBOARDING/BOARDING

HEADCOUNTING

CLEANING

CARGO FWD CC

BULK

REFUELLING


TOILET SERVICING

CATERING

CARGO AFT CC

40

AVAILABLE TIME


ACTIVITY

CRITICAL PATH

F_AC_050300_1_0060101_01_00

Minimum Servicing Turn-Round TimeFIGURE-5-3-0-991-006-A01

5-3-0Page 6

Aug 01/19


5-4-1 Ground Service Connections Layout

**ON A/C A340-200 A340-300

Ground Service Connections Layout

1. This section provides the ground service connections layout.

5-4-1Page 1

Aug 01/19


**ON A/C A340-200 A340-300

1 − OXYGEN SERVICING2 − GROUND ELECTRICAL POWER CONNECTORS3 − POTABLE WATER DRAIN4 − LOW PRESSURE AIR PRE−CONDITIONING

AND ENGINE STARTING6 − ENGINE OIL FILLING7 − IDG OIL FILLING8 − PRESSURE REFUEL/DEFUEL COUPLINGS9 − OVERWING REFUEL (IF INSTALLED)

10 − HYDRAULIC GROUND POWER SUPPLY

5 − HIGH PRESSURE AIR PRE−CONDITIONING

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

14 − POTABLE WATER SERVICE PANEL15 − WASTE WATER SERVICE PANEL16 − APU OIL FILLING17 − GROUNDING (EARTHING) POINT

13 − REFUEL/DEFUEL PANEL

11 − HYDRAULIC RESERVOIR FILLING AND GROUNDPOWER SUPPLY (GREEN)

18 − NACA FLAME ARRESTOR19 − OVERPRESSURE PROTECTOR

(YELLOW)

1

217

3

45106 7

12 6

78 6

7

1918

9

17

11

133

1415

16

18 19

179

8

6 719 18

F_AC_050401_1_0030101_01_03

Ground Service Connections LayoutFIGURE-5-4-1-991-003-A01

5-4-1Page 2

Aug 01/19


5-4-2 Grounding Points

**ON A/C A340-200 A340-300

Grounding (Earthing) Points

**ON A/C A340-300

1. Grounding (Earthing) Points

DISTANCEFROM AIRCRAFT CENTERLINEACCESS

AFT OF NOSELH SIDE RH SIDE

MEAN HEIGHTFROM GROUND

On Nose Landing Gearleg:

6.57 m(21.56 ft) On centerline

1.40 m(4.59 ft)

On left Main LandingGear leg:

31.58 m(103.61 ft)

5.34 m(17.52 ft)

1.50 m(4.92 ft)

On right MainLanding Gear leg:

31.58 m(103.61 ft)

5.34 m(17.52 ft)

1.50 m(4.92 ft)

A. The grounding (earthing) stud on each landing gear leg is designed for use with a clip-onconnector (such as Appleton TGR).

B. The grounding (earthing) studs are used to connect the aircraft to an approved ground (earth)connection on the ramp or in the hangar for:- Refuel/defuel operations- Maintenance operations- Bad weather conditions.

NOTE : In all other conditions, the electrostatic discharge through the tire is sufficient.

**ON A/C A340-200

2. Grounding (Earthing) Points




On Nose Landing Gearleg:


1.40 m(4.59 ft)

On left Main LandingGear leg:

29.40 m(96.46 ft)

5.34 m(17.52 ft)

1.50 m(4.92 ft)

5-4-2Page 1

Aug 01/19





On right Main LandingGear leg:

29.40 m(96.46 ft)

5.34 m(17.52 ft)

1.50 m(4.92 ft)

A. The grounding (earthing) stud on each landing gear leg is designed for use with a clip-onconnector (such as Appleton TGR).

B. The grounding (earthing) studs are used to connect the aircraft to an approved ground (earth)connection on the ramp or in the hangar for:- Refuel/defuel operations- Maintenance operations- Bad weather conditions.

NOTE : In all other conditions, the electrostatic discharge through the tire is sufficient.

5-4-2Page 2

Aug 01/19


**ON A/C A340-200 A340-300

NOSE LANDING GEAR MAIN LANDING GEAR

A

A

LANDINGGEAR

A

GROUNDING (EARTHING) POINTGROUNDING (EARTHING) CABLE

TYPICALF_AC_050402_1_0030101_01_01

Ground Service ConnectionsGrounding (Earthing) PointsFIGURE-5-4-2-991-003-A01

5-4-2Page 3

Aug 01/19


**ON A/C A340-200 A340-300

BFWD

A

A

ALH SHOWN

RH SYMMETRICAL

RIB22

RIB23

B

F_AC_050402_1_0040101_01_01

Ground Service ConnectionsGrounding (Earthing) PointsFIGURE-5-4-2-991-004-A01

5-4-2Page 4

Aug 01/19


5-4-3 Hydraulic System

**ON A/C A340-200 A340-300

Hydraulic Servicing

**ON A/C A340-300

1. Ground Service Panels

DISTANCEFROM AIRCRAFT CENTERLINE

ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Green System:Access Door 197CB

34.90 m(114.50 ft)

1.34 m(4.40 ft)

2.23 m(7.32 ft)

Yellow System:Access Door 196BB

29.00 m(95.14 ft)

1.30 m(4.27 ft)

1.95 m(6.40 ft)

Blue System:Access Door 195BB

28.00 m(91.86 ft)

1.28 m(4.20 ft)

1.94 m(6.36 ft)

**ON A/C A340-200

2. Ground Service Panels


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Green System:Access Door 197CB

32.79 m(107.58 ft)

1.34 m(4.40 ft)

2.23 m(7.32 ft)

Yellow System:Access Door 196BB

26.89 m(88.22 ft)

1.30 m(4.27 ft)

1.95 m(6.40 ft)

Blue System:Access Door 195BB

25.90 m(84.97 ft)

1.28 m(4.20 ft)

1.94 m(6.36 ft)

**ON A/C A340-300

3. Reservoir PressurizationOne 1/4 in. self-sealing connection common to the 3 reservoirs.

5-4-3Page 1

Aug 01/19



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHT FROM

GROUNDBlue System GroundService Panel:Access Door 195BB

34.47 m(113.09 ft)

1.41 m(4.63 ft)

1.89 m(6.20 ft)

**ON A/C A340-200

4. Reservoir PressurizationOne 1/4 in. self-sealing connection common to the 3 reservoirs.


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDBlue System GroundService Panel:Access Door 195BB

32.34 m(106.10 ft)

1.41 m(4.63 ft)

1.89 m(6.20 ft)

**ON A/C A340-300

5. Accumulator ChargingFive connections (one for each accumulator):


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDGreen SystemAccumulator:Access Door 197CB

41.52 m(136.22 ft)

1.33 m(4.36 ft)

2.19 m(7.19 ft)

Yellow SystemAccumulator:Access Door 196BB

35.55 m(116.63 ft)

1.43 m(4.69 ft)

1.91 m(6.27 ft)

Blue System Accumulator:Access Door 195BB

34.54 m(113.32 ft)

1.38 m(4.53 ft)

1.90 m(6.23 ft)

5-4-3Page 2

Aug 01/19



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDBlue System BrakeAccumulator:Access Door 195BB

34.54 m(113.32 ft)

1.24 m(4.07 ft)

1.90 m(6.23 ft)

**ON A/C A340-200

6. Accumulator ChargingFive connections (one for each accumulator):


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDGreen SystemAccumulator:Access Door 197CB

39.39 m(129.23 ft)

1.33 m(4.36 ft)

2.19 m(7.19 ft)

Yellow SystemAccumulator:Access Door 196BB

33.42 m(109.65 ft)

1.43 m(4.69 ft)

1.91 m(6.27 ft)

Blue System Accumulator:Access Door 195BB

32.41 m(106.33 ft)

1.38 m(4.53 ft)

1.90 m(6.23 ft)

Blue System BrakeAccumulator:Access Door 195BB

32.41 m(106.33 ft)

1.18 m(3.87 ft)

1.90 m(6.23 ft)

**ON A/C A340-300

7. Reservoir FillingTwo connections (one self-sealing connection for pressurized supply on the Green system groundservice panel).

5-4-3Page 3

Aug 01/19



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDOne handpump fillingconnection:Access Door 197CB

41.31 m(135.53 ft)

1.30 m(4.27 ft)

2.11 m(6.92 ft)

**ON A/C A340-200

8. Reservoir FillingTwo connections (one self-sealing connection for pressurized supply on the Green system groundservice panel).


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDOne handpump fillingconnection:Access Door 197CB

39.18 m(128.54 ft)

1.30 m(4.27 ft)

2.11 m(6.92 ft)

**ON A/C A340-300

9. Reservoir DrainOne 3/8 in. self-sealing connection on the reservoir for:


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Green System33.17 m(108.83 ft)

0.70 m(2.30 ft)

3.80 m(12.47 ft)

Yellow System29.03 m(95.24 ft)

2.12 m(6.96 ft)

2.40 m(7.87 ft)

Blue System29.03 m(95.24 ft)

2.12 m(6.96 ft)

2.40 m(7.87 ft)

5-4-3Page 4

Aug 01/19


**ON A/C A340-200

10. Reservoir DrainOne 3/8 in. self-sealing connection on the reservoir for:


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND

Green System31.04 m(101.84 ft)

0.70 m(2.30 ft)

3.80 m(12.47 ft)

Yellow System26.90 m(88.25 ft)

2.12 m(6.96 ft)

2.40 m(7.87 ft)

Blue System26.90 m(88.25 ft)

2.12 m(6.96 ft)

2.40 m(7.87 ft)

**ON A/C A340-300

11. Ground TestThree 1 in. self-sealing connections and three 1-1/2 in. self-sealing connections (one pair per system).


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDGreen System GroundService Panel:Access Door 197CB

34.92 m(114.57 ft)

1.35 m(4.43 ft)

2.20 m(7.22 ft)

Yellow System GroundService Panel:Access Door 196BB

29.03 m(95.24 ft)

1.30 m(4.27 ft)

2.00 m(6.56 ft)

Blue System GroundService Panel:Access Door 195BB

28.03 m(91.96 ft)

1.28 m(4.20 ft)

2.00 m(6.56 ft)

**ON A/C A340-200

12. Ground TestThree 1 in. self-sealing connections and three 1-1/2 in. self-sealing connections (one pair per system).

5-4-3Page 5

Aug 01/19



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDGreen System GroundService Panel:Access Door 197CB

32.79 m(107.58 ft)

1.35 m(4.43 ft)

2.20 m(7.22 ft)

Yellow System GroundService Panel:Access Door 196BB

26.90 m(88.25 ft)

1.30 m(4.27 ft)

2.00 m(6.56 ft)

Blue System GroundService Panel:Access Door 195BB

25.90 m(84.97 ft)

1.28 m(4.20 ft)

2.00 m(6.56 ft)

**ON A/C A340-300

13. A/C Emergency Generation


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDRAT Safety-PinInstallation:Access Panel 633SL

34.60 m(113.52 ft)

14.20 m(46.59 ft)

4.30 m(14.11 ft)

**ON A/C A340-200

14. A/C Emergency Generation


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDRAT Safety-PinInstallation:Access Panel 633SL

32.40 m(106.30 ft)

14.20 m(46.59 ft)

4.30 m(14.11 ft)

5-4-3Page 6

Aug 01/19


**ON A/C A340-200 A340-300

MAN SELECTORVALVE−RSVR

FILLING

LEVER HANDPUMP

GND CNCTR−SELFSEALING RSVR

FILLING

HAND PUMPRSVR FILLING

FILTER−RSVRFILLING

RSVRFILLING VALVE

GND CNCTR−SELFSEALING, G SUCTION

GND CNCTR−SELFSEALING, G DELIVERY

VALVE−MANDEPRESS, G−RSVR

HYDRSVR FILLINGADJUSTMENT

INDICATOR

PRESS GAGEG POWER ACCU

GND CNCTRNITROGEN CHARGING

G POWER ACCU

FWD

A

FR53.4 FR53.5197CB

A

F_AC_050403_1_0040101_01_00

Ground Service ConnectionsGreen System Ground Service Panel

FIGURE-5-4-3-991-004-A01

5-4-3Page 7

Aug 01/19


**ON A/C A340-200 A340-300

PRESS GAGEB POWER ACCU

GND CNCTRNITROGENCHARGING

B POWER ACCU

GND CNCTRSELF−SEALING,

B SUCTION

VALVE−MANDEPRESS, B RSVR

GND CNCTR−SELFSEALING,

B DELIVERY

GND CNCTRSELF−SEALING,

B/Y RSVR PRESS

GND CNCTRSELF−SEALING,G RSVR PRESS

PRESS GAGESPARK BRK ACCU

PARK BRK ACCU

FWD

A

FR44 FR45

A

195BB

F_AC_050403_1_0050101_01_00

Ground Service ConnectionsBlue System Ground Service Panel

FIGURE-5-4-3-991-005-A01

5-4-3Page 8

Aug 01/19


**ON A/C A340-200 A340-300

SIGHTGLASSCARGO DOOR

SELECTOR MANIFOLD

HAND PUMPCARGO DOORS, Y RAT STOW PANEL

GND CNCTR−SELFSEALING, Y SUCTION

VALVE−MANDEPRESS, Y RSVR

GND CNCTR−SELFSEALING, Y DELIVERY

PRESS GAGEY POWER ACCU

GND CNCTRNITROGEN CHARGING

Y POWER ACCU

FWD

A

FR46FR47

A

196BB

F_AC_050403_1_0060101_01_00

Ground Service ConnectionsYellow System Ground Service Panel

FIGURE-5-4-3-991-006-A01

5-4-3Page 9

Aug 01/19


**ON A/C A340-200 A340-300

A

633SL

A

Z633

RAT UPLOCK SAFETY−PIN

633GB

RAM AIR TURBINE (RAT)

B

C

RAT RETRACTED

RAT EXTENDED

C

B

F_AC_050403_1_0110101_01_00

Ground Service ConnectionsRAT

FIGURE-5-4-3-991-011-A01

5-4-3Page 10

Aug 01/19


5-4-4 Electrical System

**ON A/C A340-200 A340-300

Electrical Servicing

1. A/C External Power


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

A/C External Power:Access Door 121EL


1.98 m(6.50 ft)

NOTE : Distances are approximate.

2. Technical Specifications

A. External Power Receptacles:- Two receptacles according to MS 90362-3 - 90 kVA.

B. Power Supply:- Three-phase, 115 V, 400 Hz.

C. Electrical Connectors for Servicing:- AC outlets: HUBBELL 5258- DC outlets: HUBBELL 7472.

3. Tow Truck Power


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

NLG Service Panel: 5GC6.67 m(21.88 ft)

0.50 m(1.64 ft) TBD

NLG Service Panel: 8GH6.67 m(21.88 ft) On centerline TBD


A. Power Supply:- Two-phase, 115 V, 400 Hz- 28V DC.

B. Electrical Connector for Servicing:- Bernier, 22-11-10-13 Connector.

5-4-4Page 1

Aug 01/19


C. Pin Allocation:

Pin IdentificationA 28V DCB 0V DCD 115V ACE 0V ACGH

PWR SPLYINT LOCK

NOTE : The power cable should be extendable in order to guarantee fit and non-interferencewith nose gear nor tow vehicle during the pick-up and the towing process. Theconnector shall be secured against pull-out by means of straps against the nose gear.

5-4-4Page 2

Aug 01/19


**ON A/C A340-200 A340-300

FR19 FR18

A

A

121EL

B925VU

EXTERNAL POWER RECEPTACLESB

FR18

FR19

TYPICAL

F_AC_050404_1_0020101_01_01

Ground Service ConnectionsElectrical Service Panel

FIGURE-5-4-4-991-002-A01

5-4-4Page 3

Aug 01/19


5-4-5 Oxygen System

**ON A/C A340-200 A340-300

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: External charging in the avionic compartment- 1 -- Option- 2 -- Option.Zero, one or two MIL-DTL 7891 standard service connections (external charging in the avionicscompartment).

NOTE : Internal charging connection provided.

5-4-5Page 1

Aug 01/19


**ON A/C A340-200 A340-300

A

B

OXYGENFILLING PORT

TESTPORT

FWD

FR4

FR7

NOTE:THE NUMBER OF OXYGEN CYLINDERS DEPENDS ON THE SYSTEM CONFIGURATION.

B

FR20

FR1

AVIONICS COMPARTMENT DOOR

FR7

FR10

Z120

A

811

F_AC_050405_1_0030101_01_01

Ground Service ConnectionsOxygen Servicing

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

5-4-5Page 2

Aug 01/19


5-4-6 Fuel System

**ON A/C A340-200 A340-300

Fuel System

**ON A/C A340-200

1. Refuel/Defuel Control Panel


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel ControlPanel:Access Door 198DB

32.2 m(105.64 ft)

-0.8 m(2.62 ft)

1.9 m(6.23 ft)

A. Flow rate: 1250 l/min (330 US gal/min) per connection.

B. Maximum pressure: 50 psi (3.45 bar).

2. Refuel/Defuel Connectors


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel Coupling,Left:Access Door 522HB

27.8 m(91.21 ft)

12.6 m(41.34 ft)

-5 m(16.4 ft)

Refuel/Defuel Coupling,Right:Access Door 622HB

27.8 m(91.21 ft)

-12.6 m(41.34 ft)

5 m(16.4 ft)

Overwing GravityRefuel Cap

31.2 m(102.36 ft)

17.2 m(56.43 ft)

17.2 m(56.43 ft)

5.8 m(19.03 ft)

A. Four standard 2.5 in. ISO 45 connections.

B. Two service connections (gravity refuel).

5-4-6Page 1

Aug 01/19


3. Overpressure Protector and NACA Flame Arrestor


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

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

37.36 m(122.57 ft)

27.17 m(89.14 ft)

27.17 m(89.14 ft)

5.75 m(18.86 ft)

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

37 m(121.39 ft)

26.53 m(87.04 ft)

26.53 m(87.04 ft)

5.7 m(18.7 ft)

Overpressure Protector(Trim Tank)Access Panel 346AB

57.4 m(188.32 ft)

8 m(26.25 ft)

8 m(26.25 ft)

5.7 m(18.7 ft)

NACA Flame Arrestor(Trim Tank)Access Panel 346AB

57.4 m(188.32 ft)

8 m(26.25 ft)

8 m(26.25 ft)

5.7 m(18.7 ft)

**ON A/C A340-300

4. Refuel/Defuel Control Panel


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel ControlPanel:Access Door 198DB

34.3 m(112.53 ft)

-0.8 m(2.62 ft)

1.9 m(6.23 ft)

A. Flow rate: 1250 l/min (330 US gal/min) per connection.

B. Maximum pressure: 50 psi (3.45 bar).

5-4-6Page 2

Aug 01/19


5. Refuel/Defuel Connectors


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUND

Refuel/Defuel Coupling,Left:Access Door 522HB

30 m(98.43 ft)

12.6 m(41.34 ft)

-5 m(16.4 ft)

Refuel/Defuel Coupling,Right:Access Door 622HB

30 m(98.43 ft)

-12.6 m(41.34 ft)

5 m(16.4 ft)

Overwing GravityRefuel Cap

34.5 m(113.19 ft)

17.2 m(56.43 ft)

17.2 m(56.43 ft)

5.8 m(19.03 ft)

A. Four standard 2.5 in. ISO 45 connections.

B. Two service connections (gravity refuel).

6. Overpressure Protector and NACA Flame Arrestor


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

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

39.48 m(129.53 ft)

27.17 m(89.14 ft)

27.17 m(89.14 ft)

5.75 m(18.86 ft)

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

39.12 m(128.35 ft)

26.53 m(87.04 ft)

26.53 m(87.04 ft)

5.7 m(18.7 ft)

Overpressure Protector(Trim Tank)Access Panel 346AB

61.67 m(202.33 ft)

8 m(26.25 ft)

8 m(26.25 ft)

5.7 m(18.7 ft)

NACA Flame Arrestor(Trim Tank)Access Panel 346AB

61.67 m(202.33 ft)

8 m(26.25 ft)

8 m(26.25 ft)

5.7 m(18.7 ft)

5-4-6Page 3

Aug 01/19


**ON A/C A340-200 A340-300

A

R OUTER TK

R OUTER TKOVERFLOW

INC

LOAD

HI LEVELTEST

TRANSF. VALVE

OPEN

CLOSED

APU EMERG.

SHUTDOWN

PWRSUPPLY

NORM

BAT

L TT R

DEC

REFUEL/DEFUEL VALVESMODE SELECTL OUTER TK L INNER TK CTR TK

L OUTER TK L INNER TK CTR TK TRIM TKHIGH LEVEL

REFUEL

OFFDEFUEL

R INNER TK

R INNER TK

OPENNORMSHUT

L INR. CENTER R INR.

L OUTER R OUTERTRIM ACTUAL

CKPTEND

x 1000

kg1b

PRESELECTED

TRIM TK

198DB FR53.2FR53.4

A

F_AC_050406_1_0140101_01_00

Ground Service ConnectionsRefuel/Defuel Control PanelFIGURE-5-4-6-991-014-A01

5-4-6Page 4

Aug 01/19


**ON A/C A340-200 A340-300

A

522HB(622HB)

TYPICAL

A

REFUEL/DEFUELCOUPLINGS

REFUEL/DEFUELCOUPLING CAP

REFUEL/DEFUELCOUPLING CAP

F_AC_050406_1_0150101_01_01

Ground Service ConnectionsRefuel/Defuel Coupling

FIGURE-5-4-6-991-015-A01

5-4-6Page 5

Aug 01/19


**ON A/C A340-200 A340-300

C

OVERPRESSURE PROTECTOR

A

NACA FLAME ARRESTOR

B

A

A

FWD

LH SIDE SHOWNRH SIDE SYMMETRICAL

B

C

RIB36

RIB37

RIB38

550EB(650EB)

550DB(650DB)

F_AC_050406_1_0030101_01_00

Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor - Wing

FIGURE-5-4-6-991-003-A01

5-4-6Page 6

Aug 01/19


**ON A/C A340-200 A340-300

B

TRIM−TANK NACA VENT

TRIM−TANK OVERPRESSURE

BOTTOM SKIN

A

Z343

346AB

FWD

A

B

RIB19RIB18

F_AC_050406_1_0160101_01_00

Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor - Trim Tank

FIGURE-5-4-6-991-016-A01

5-4-6Page 7

Aug 01/19


5-4-7 Pneumatic System

**ON A/C A340-200 A340-300

Pneumatic Servicing

**ON A/C A340-300

1. High Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND23.9 m(78.41 ft)

0.84 m(2.76 ft)

1.79 m(5.87 ft)HP Connectors:

Access Door 193CB 24.25 m(79.56 ft)

0.84 m(2.76 ft)

1.79 m(5.87 ft)

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

2. Low Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND22.48 m(73.75 ft)

0.31 m(1.02 ft)

1.86 m(6.1 ft)LP Connectors:

Access Door 191EB 22.48 m(73.75 ft)

0.76 m(2.49 ft)

1.89 m(6.2 ft)

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

5-4-7Page 1

Aug 01/19


**ON A/C A340-200

3. High Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND21.77 m(71.42 ft)

0.84 m(2.76 ft)

1.79 m(5.87 ft)HP Connectors:

Access Door 193CB 22.12 m(72.57 ft)

0.84 m(2.76 ft)

1.79 m(5.87 ft)

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

4. Low Pressure Air Connection


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUND20.35 m(66.77 ft)

0.31 m(1.02 ft)

1.86 m(6.1 ft)LP Connectors:

Access Door 191EB 20.35 m(66.77 ft)

0.76 m(2.49 ft)

1.89 m(6.2 ft)

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

5-4-7Page 2

Aug 01/19


**ON A/C A340-200 A340-300

193CB

191EB

B

A

FR40

HP CONNECTOR

B

LP CONNECTOR

A

F_AC_050407_1_0020101_01_00

Ground Service ConnectionsLP and HP Ground Connectors

FIGURE-5-4-7-991-002-A01

5-4-7Page 3

Aug 01/19


5-4-8 Oil System

**ON A/C A340-200 A340-300

Oil Servicing

**ON A/C A340-300

1. CFM56-5C2 Series Engine

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

(1) Engine Oil Gravity Filling


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

GROUNDEngine 1:Access Door: 415BL

31.03 m(101.80 ft)

20.56 m(67.45 ft)

3.47 m(11.38 ft)

Engine 2:Access Door: 425BL

24.46 m(80.25 ft)

10.33 m(33.89 ft)

2.20 m(7.22 ft)


24.46 m(80.25 ft)

8.41 m(27.59 ft)

2.20 m(7.22 ft)


31.03 m(101.80 ft)

18.64 m(61.15 ft)

3.47 m(11.38 ft)

(2) Engine Oil Pressure Filling


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM


30.90 m(101.38 ft)

20.64 m(67.72 ft)

3.47 m(11.38 ft)


24.32 m(79.79 ft)

10.41 m(34.15 ft)

2.20 m(7.22 ft)


24.32 m(79.79 ft)

8.32 m(27.30 ft)

2.20 m(7.22 ft)

5-4-8Page 1

Aug 01/19



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM


30.90 m(101.38 ft)

18.56 m(60.89 ft)

3.47 m(11.38 ft)

- Max delivery pressure required: 1.72 bar (25 psi).- Max delivery flow required: 249.84 l/hour (66.00 US gal/hour).

(3) Tank capacity:- Full level: 19.00 l (5.02 US gal).- Usable: 10.68 l (2.82 US gal).

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


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM

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

30.12 m(98.82 ft)

19.40 m(63.65 ft)

2.55 m(8.37 ft)

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

23.54 m(77.23 ft)

9.17 m(30.09 ft)

1.35 m(4.43 ft)


23.54 m(77.23 ft)

9.57 m(31.40 ft)

1.35 m(4.43 ft)


30.12 m(98.82 ft)

19.80 m(64.96 ft)

2.55 m(8.37 ft)

- Max delivery pressure required: 2.76 bar (40 psi).- Max oil capacity of the IDG: 4.00 l (1.06 US gal).

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

5-4-8Page 2

Aug 01/19



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM


30.12 m(98.82 ft)

19.40 m(63.65 ft)

2.55 m(8.37 ft)


23.54 m(77.23 ft)

9.17 m(30.09 ft)

1.35 m(4.43 ft)


23.54 m(77.23 ft)

9.57 m(31.40 ft)

1.35 m(4.43 ft)


30.12 m(98.82 ft)

19.80 m(64.96 ft)

2.55 m(8.37 ft)

- Max oil capacity of the Starter: 0.80 l (0.21 US gal).

**ON A/C A340-200

2. CFM56-5C2 Series Engine

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

(1) Engine Oil Gravity Filling


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM


28.90 m(94.82 ft)

20.56 m(67.45 ft)

3.47 m(11.38 ft)


22.33 m(73.26 ft)

10.33 m(33.89 ft)

2.20 m(7.22 ft)


22.33 m(73.26 ft)

8.41 m(27.59 ft)

2.20 m(7.22 ft)


28.90 m(94.82 ft)

18.64 m(61.15 ft)

3.47 m(11.38 ft)

(2) Engine Oil Pressure Filling

5-4-8Page 3

Aug 01/19



ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM


28.77 m(94.39 ft)

20.64 m(67.72 ft)

3.47 m(11.38 ft)


22.19 m(72.80 ft)

10.41 m(34.15 ft)

2.20 m(7.22 ft)


22.19 m(72.80 ft)

8.32 m(27.30 ft)

2.20 m(7.22 ft)


28.77 m(94.39 ft)

18.56 m(60.89 ft)

3.47 m(11.38 ft)

- Max delivery pressure required: 1.72 bar (25 psi).- Max delivery flow required: 249.84 l/hour (66.00 US gal/hour).

(3) Tank capacity:- Full level: 19.00 l (5.02 US gal).- Usable: 10.68 l (2.82 US gal).

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


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM


27.99 m(91.83 ft)

19.40 m(63.65 ft)

2.55 m(8.37 ft)


21.41 m(70.24 ft)

9.17 m(30.09 ft)

1.35 m(4.43 ft)


21.41 m(70.24 ft)

9.57 m(31.40 ft)

1.35 m(4.43 ft)


27.99 m(91.83 ft)

19.80 m(64.96 ft)

2.55 m(8.37 ft)

- Max delivery pressure required: 2.76 bar (40 psi).- Max oil capacity of the IDG: 4.00 l (1.06 US gal).

5-4-8Page 4

Aug 01/19


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


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEANHEIGHTFROM


27.99 m(91.83 ft)

19.40 m(63.65 ft)

2.55 m(8.37 ft)


21.41 m(70.24 ft)

9.17 m(30.09 ft)

1.35 m(4.43 ft)


21.41 m(70.24 ft)

9.57 m(31.40 ft)

1.35 m(4.43 ft)


27.99 m(91.83 ft)

19.80 m(64.96 ft)

2.55 m(8.37 ft)

- Max oil capacity of the Starter: 0.80 l (0.21 US gal).

5-4-8Page 5

Aug 01/19


**ON A/C A340-200 A340-300

OIL TANKFILLER CAP

A

OIL TANK

OIL

LEVEL

SIGHT CAGE

BFWD

A

415BL425BL435BL445BL

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

FULL MARK

B

F_AC_050408_1_0170101_01_00

Ground Service ConnectionsEngine Oil Tank - CFM56-5C2 Series Engine

FIGURE-5-4-8-991-017-A01

5-4-8Page 6

Aug 01/19


**ON A/C A340-200 A340-300

CASEDRAINPLUG

DUSTCAP

PRESSUREFILL VALVE

OVERFILLDRAINVALVE

A

B

A340OVER

ADDOIL

CFM56−5C2

FULL

ADDOIL

STABLE OIL

B

FWD

A

445AL

415AL425AL435AL


446AR

416AR426AR436AR


SIGHT GLASS

F_AC_050408_1_0180101_01_00

Ground Service ConnectionsIDG Oil Tank - CFM56-5C2 Series Engine

FIGURE-5-4-8-991-018-A01

5-4-8Page 7

Aug 01/19


**ON A/C A340-200 A340-300

PNEUMATICSTARTER

OIL FILLPLUG

OIL LEVELOVERFLOW

PLUG

MAGNETIC CHIPDETECTOR

DRAINPLUG

ACCESSORYGEARBOX

A

445AL

415AL425AL435AL


446AR

416AR426AR436AR

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

F_AC_050408_1_0270101_01_00

Ground Service ConnectionsStarter Oil Tank - CFM56-5C2 Series Engine

FIGURE-5-4-8-991-027-A01

5-4-8Page 8

Aug 01/19


**ON A/C A340-200 A340-300

APU Oil Servicing

**ON A/C A340-300

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




APU OilReplenishment:Access Doors:316AR, 315AL

60.3 m(197.83 ft)

0.4 m(1.31 ft)

8 m(26.25 ft)

A. Tank capacity (usable):- APU Type: 331-350: 7.3 l (1.93 US gal)- APU Type: 331-600: 11 l (2.91 US gal).

**ON A/C A340-200

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




APU OilReplenishment:Access Doors:316AR, 315AL

56 m(183.73 ft)

0.4 m(1.31 ft)

8 m(26.25 ft)

A. Tank capacity (usable):- APU Type: 331-350: 7.3 l (1.93 US gal)- APU Type: 331-600: 11 l (2.91 US gal).

5-4-8Page 9

Aug 01/19


**ON A/C A340-200 A340-300

PRESSURE FILLOVERFLOW PORT

PRESSUREFILL PORT

OIL SIGHTGLASS

BFWD

DO NOT REMOVE OILFILLER CAP WHEN OILLEVEL IS ABOVE FULLMARK ON SIGHT GLASS

OIL SCUPPER

GRAVITY FILLPORT

LUBRIFICATION OIL FILTER

GENERATOR SCAVENGE OIL FILTER

OIL PUMPMODULE

A

OIL FILLERCAP

B

FR95

FR101

316AR

315AL

A

F_AC_050408_1_0220101_01_00

Ground Service ConnectionsAPU Oil Servicing

FIGURE-5-4-8-991-022-A01

5-4-8Page 10

Aug 01/19


5-4-9 Potable Water System

**ON A/C A340-300

Potable Water Servicing

1. Potable Water Servicing




Potable-WaterService Panel:Access Door 164AR

48.15 m(157.97 ft)

0.51 m(1.67 ft)

3.15 m(10.33 ft)

FWD Drain Panel:Access Door 133BL

14.7 m(48.23 ft)

0.6 m(1.97 ft)

1.92 m(6.30 ft)

AFT Drain Panel:Access Door 154AR

40.18 m(131.82 ft)

0.72 m(2.36 ft)

2.46 m(8.07 ft)



A. Connections

(1) On the potable-water service panel (access door 164AR):- One heated 3/4 in. (ISO 17775) quick release filling connection- One heated 3/4 in. (ISO 17775) overflow and discharge connection- One ground pressurization connection.

(2) On the FWD drain panel (access door 133BL):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control.

(3) On the AFT drain panel (access door 154AR):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control- One standard 3/4 in. (ISO 17775) overflow and discharge connection with back-up

mechanical control.

B. Capacity- 700 l (184.92 US gal) standard- 1050 l (277.38 US gal) standard option.

C. Filling Pressure and Flow Rate

FWD tank:- Filling pressure: 3.45/8.62 bar (50/125 psi)- Flow rate: 45/73 l/min (11.89/19.28 US gal/min).

AFT tank:

5-4-9Page 1

Aug 01/19


- Filling pressure: 3.45/8.62 bar (50/125 psi)- Flow rate: 56/85 l/min (14.79/22.45 US gal/min).

5-4-9Page 2

Aug 01/19


**ON A/C A340-300

164AR

154AR

133BL

DRAIN NIPPLEDRAIN NIPPLE

FWD POTABLE−WATER DRAIN PANELAFT POTABLE−WATER DRAIN PANEL

CB

OVERFLOW NIPPLE

APOTABLE−WATER SERVICE PANEL

CAPASSEMBLY

FILL/DRAINNIPPLE

FR69

FILL/DRAINCONTROL HANDLE

FR70

MAINTENANCE DOORLIMIT−SWITCH

GROUND AIRCONNECTION

DRAIN VALVECONTROL HANDLE

FR29

FR28FR57.1

FR57.2OVERFLOW

NIPPLEDRAIN CONTROL HANDLE(FILLING LINE DRAIN VALVE)

OVERFLOW CONTROL HANDLE(FILL/DRAIN VALVE)

AB

C

F_AC_050409_1_0290101_01_00

Ground Service ConnectionsPotable-Water Ground Service Panels

FIGURE-5-4-9-991-029-A01

5-4-9Page 3

Aug 01/19


**ON A/C A340-300

POTABLE WATERTANK

OVERFLOW LINE

ANOTE:

TYPICAL01

01

POTABLE WATERFILL/DRAIN LINE

FR53.8

FR57

FR73

A

A

AFT CARGO DOOR

BULK CARGO DOOR

Z152

Z172

FR53.2

FR65

FR80Z160

FR72

FR76

F_AC_050409_1_0300101_01_00

Ground Service ConnectionsPotable-Water Tanks LocationFIGURE-5-4-9-991-030-A01

5-4-9Page 4

Aug 01/19


**ON A/C A340-200

Potable Water Servicing

1. Potable Water Servicing




Potable-WaterService Panel:Access Door 164AR

43.88 m(143.96 ft)

0.51 m(1.67 ft)

3.13 m(10.27 ft)

FWD Drain Panel:Access Door 133BL

14.7 m(48.23 ft)

0.60 m(1.97 ft)

1.92 m(6.30 ft)

AFT Drain Panel:Access Door 154AR

36.51 m(119.78 ft)

0.72 m(2.36 ft)

2.44 m(8.01 ft)



A. Connections

(1) On the potable-water service panel (access door 164AR):- One heated 3/4 in. (ISO 17775) quick release filling connection- One heated 3/4 in. (ISO 17775) overflow and discharge connection- One ground pressurization connection.

(2) On the FWD drain panel (access door 133BL):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control.

(3) On the AFT drain panel (access door 154AR):- One standard 3/4 in. (ISO 17775) drain connection with back-up mechanical control- One standard 3/4 in. (ISO 17775) overflow and discharge connection with back-up

mechanical control.

B. Capacity- 700 l (184.92 US gal) standard- 1050 l (277.38 US gal) standard option.

C. Filling Pressure and Flow Rate

FWD tank:- Filling pressure: 3.45/8.62 bar (50/125 psi)- Flow rate: 45/73 l/min (11.89/19.28 US gal/min).

AFT tank:- Filling pressure: 3.45/8.62 bar (50/125 psi)

5-4-9Page 5

Aug 01/19


- Flow rate: 56/85 l/min (14.79/22.45 US gal/min).

5-4-9Page 6

Aug 01/19


**ON A/C A340-200

DRAIN NIPPLEDRAIN NIPPLE

FWD POTABLE−WATER DRAIN PANELAFT POTABLE−WATER DRAIN PANEL

CB

OVERFLOW NIPPLE

APOTABLE−WATER SERVICE PANEL

CAPASSEMBLY

FILL/DRAINNIPPLE

FR69

FILL/DRAINCONTROL HANDLE

FR70

MAINTENANCE DOORLIMIT−SWITCH

GROUND AIRCONNECTION

DRAIN VALVECONTROL HANDLE

FR29

FR28

OVERFLOWNIPPLEDRAIN CONTROL HANDLE

(FILLING LINE DRAIN VALVE)

OVERFLOW CONTROL HANDLE(FILL/DRAIN VALVE)

164AR

154AR

133BL

FR56

FR57

B A

C

F_AC_050409_1_0310101_01_00

Ground Service ConnectionsPotable-Water Ground Service Panels

FIGURE-5-4-9-991-031-A01

5-4-9Page 7

Aug 01/19


**ON A/C A340-200

POTABLE WATERTANK

OVERFLOW LINE

ANOTE:

TYPICAL01

01

POTABLE WATERFILL/DRAIN LINE

FR73

A

AFT CARGO DOOR

BULK CARGO DOOR

Z152

Z172

A

FR53.4

FR53.9

Z160

FR53.2

FR65

FR80

FR72

FR76

F_AC_050409_1_0320101_01_00

Ground Service ConnectionsPotable-Water Tanks LocationFIGURE-5-4-9-991-032-A01

5-4-9Page 8

Aug 01/19


5-4-10 Waste Water System

**ON A/C A340-200 A340-300

Waste Water Servicing

**ON A/C A340-300

1. Waste Water Servicing


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDWaste Water GroundService Panel:Access Door 171AL

50.00 m(164.04 ft)

0.09 m(0.30 ft)

3.60 m(11.81 ft)

A. Waste water ground service panel comprising:- Standard: One standard 4 in. (ISO 17775) drain connection and two 1 in. (ISO 17775)

flushing connections- Standard option: One standard 4 in. (ISO 17775) drain connection and three 1 in. (ISO

17775) flushing connections.

B. Capacity waste tanks:- Standard: 700 l (184.92 US gal)- Standard option: 1050 l (277.38 US gal).

C. Chemical fluid:- Standard: 36 l (9.51 US gal)- Standard option: 54 l (14.27 US gal).

**ON A/C A340-200

2. Waste Water Servicing


ACCESSAFT OF NOSE

LH SIDE RH SIDE

MEAN HEIGHTFROM

GROUNDWaste Water GroundService Panel:Access Door 171AL

45.72 m(150.00 ft)

0.09 m(0.30 ft)

3.60 m(11.81 ft)

A. Waste water ground service panel comprising:- Standard: One standard 4 in. (ISO 17775) drain connection and two 1 in. (ISO 17775)

flushing connections

5-4-10Page 1

Aug 01/19


- Standard option: One standard 4 in. (ISO 17775) drain connection and three 1 in. (ISO17775) flushing connections.

B. Capacity waste tanks:- Standard: 700 l (184.92 US gal)- Standard option: 1050 l (277.38 US gal).

C. Chemical fluid:- Standard: 36 l (9.51 US gal)- Standard option: 54 l (14.27 US gal).

5-4-10Page 2

Aug 01/19


**ON A/C A340-200 A340-300

LIMIT SWITCHWASTE−PANEL

RINSE CONNECTIONTANK 2 FILL AND

TANK 1 FILL ANDRINSE CONNECTION

WASTEDRAIN−LINE VALVE

DRAIN−VALVECONTROL LEVERS

FR75

FR59

FR74 FR73

A171AL

OPEN

CLOSE

LH RH

A

FWD

F_AC_050410_1_0020101_01_00

Ground Service ConnectionsWaste Water Ground Service Panel

FIGURE-5-4-10-991-002-A01

5-4-10Page 3

Aug 01/19


**ON A/C A340-200 A340-300

FR73

FR65

BULK CARGO DOOR

Z160

Z172162ZW

A

FR76

A

WASTE TANK

FR73

FR76

F_AC_050410_1_0060101_01_00

Ground Service ConnectionsWaste Tanks Location

FIGURE-5-4-10-991-006-A01

5-4-10Page 4

Aug 01/19


5-4-11 Cargo Control Panels

**ON A/C A340-200 A340-300

Cargo Control Panels

**ON A/C A340-300

1. Cargo Control Panels




FWD CLS* Panel:Access Door 122DR

14.17 m(46.49 ft)

2.60 m(8.53 ft)

3.90 m(12.80 ft)

FWD Cargo DoorPanel:Access Door 122CR

13.87 m(45.51 ft)

2.40 m(7.87 ft)

3.30 m(10.83 ft)

AFT CLS* Panel:Access Door152MR

48.95 m(160.60 ft)

2.60 m(8.53 ft)

4.60 m(15.09 ft)

AFT Cargo DoorPanel:Access Door 152NR

48.65 m(159.61 ft)

2.40 m(7.87 ft)

4.00 m(13.12 ft)

NOTE : * CLS - CARGO LOADING SYSTEMS

**ON A/C A340-200

2. Cargo Control Panels




FWD CLS* Panel:Access Door 122DR

14.17 m(46.49 ft)

2.60 m(8.53 ft)

3.90 m(12.80 ft)

FWD Cargo DoorPanel:Access Door 122CR

13.87 m(45.51 ft)

2.40 m(7.87 ft)

3.30 m(10.83 ft)

AFT CLS* Panel:Access Door152MR

44.68 m(146.59 ft)

2.60 m(8.53 ft)

4.60 m(15.09 ft)

5-4-11Page 1

Aug 01/19





AFT Cargo DoorPanel:Access Door 152NR

44.38 m(145.60 ft)

2.40 m(7.87 ft)

4.00 m(13.12 ft)

NOTE : * CLS - CARGO LOADING SYSTEMS

5-4-11Page 2

Aug 01/19


**ON A/C A340-200 A340-300

PWR ON/OFF SWITCH

JOYSTICK

DOOR SILL LATCHRELEASE LEVER

OUTSIDE CARGO LOADINGSYSTEM CONTROL PANEL

LIGHT SWITCH

INDICATOR LIGHT

DOOR OPERATION LEVER

CARGO DOOR CONTROL PANEL

122DR

122CR

A

B

FR18

FR19

FR20

A

B

FWD CARGO DOOR

F_AC_050411_1_0040101_01_00

Forward Cargo Control PanelsFIGURE-5-4-11-991-004-A01

5-4-11Page 3

Aug 01/19


**ON A/C A340-200 A340-300

PWR ON/OFF SWITCH

OUTSIDE CARGO LOADINGSYSTEM CONTROL PANEL

DOOR SILL LATCHRELEASE LEVER

JOYSTICK

CARGO DOOR CONTROL PANEL

LIGHT SWITCH

INDICATOR LIGHT

DOOR OPERATION LEVER

152MR

152NR

A

B

FR65

FR53.2

Z150

AFT CARGO DOOR

FR59FR58

A

B

F_AC_050411_1_0050101_01_00

Aft Cargo Control PanelsFIGURE-5-4-11-991-005-A01

5-4-11Page 4

Aug 01/19


5-5-0 Engine Starting Pneumatic Requirements

**ON A/C A340-200 A340-300

Engine Starting Pneumatic Requirements

1. The purpose of this section is to provide the minimum air data requirements at the aircraftconnection, needed to start the engine within no more than 70 seconds, at sea level (0 feet), for a setof Outside Air Temperatures (OAT).

ABBREVIATION DEFINITION

A/C Aircraft

ASU Air Start Unit

HPGC High Pressure Ground Connection

OAT Outside Air Temperature

A. Air data (discharge temperature, absolute discharge pressure) are given at the HPGC.

B. For the requirements below, the configuration with two HPGC is used. Using one connector only(for a given mass flow rate and discharge pressure from the ASU) will increase the pressure lossin the ducts of the bleed system and therefore lower the performances at the engine starter.

C. For a given OAT the following charts are used to determine an acceptable combination for airdischarge temperature, absolute discharge pressure and mass flow rate.

D. This section is addressing requirements for the ASU only, and is not representative of the startperformance of the aircraft using the APU or engine cross bleed procedure.

E. To protect the A/C, the charts feature, if necessary:- The maximum discharge pressure at the HPGC- The maximum discharge temperature at the HPGC.

5-5-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

AIR

FLO

W (

lb/m

in)

CFM56−5C2 SERIES/SEA LEVELSTARTING TIME: LESS THAN 70 s

AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)

OUTSIDE AIR TEMPERATURE OAT (° C)

OUTSIDE AIR TEMPERATURE OAT (° F)0 20 40 60 80 100 120 140−20−40

EXAMPLE:

NOTE:

35

40

45

50

0 10 20 30 40 50 60−10−20−30−40−50

30 35 40 45 5040

45

50

55

60

65

70

75

80

90

100

110

120

130

140

150

160

170

FOR AN OAT OF 20° C (68° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 150° C (302° F) AT HPGC:− THE REQUIRED PRESSURE AT HPGC IS 39 psia− THE REQUIRED AIRFLOW AT HPGC IS 50.5 kg/min.

IN CASE THE ACTUAL DISCHARGE TEMPERATURE OF THE ASU DIFFERS SUBSTANTIALLY FROM THE ONES GIVEN IN THE CHARTS, A SIMPLE INTERPOLATION (LINEAR) IS SUFFICIENT TO DETERMINE THE REQUIRED AIR DATA.

ABSOLUTE PRESSURE (psia)

AIR

FLO

W (

kg/m

in)

AB

SO

LUT

E P

RE

SS

UR

E (

psia

)

220° C (428° F) MAX.150° C (302° F)100° C (212° F)

ASU DISCHARGE TEMPERATURE:

F_AC_050500_1_0020101_01_02

Example for Use of the ChartsFIGURE-5-5-0-991-002-A01

5-5-0Page 2

Aug 01/19


**ON A/C A340-200 A340-300

AIR

FLO

W (

kg/m

in)

AIR

FLO

W (

lb/m

in)

AB

SO

LUT

E P

RE

SS

UR

E (

psia

)STARTING TIME: LESS THAN 70 s

AIR DATA AT AIRCRAFT CONNECTION (TWO CONNECTORS)

OUTSIDE AIR TEMPERATURE OAT (° C)

OUTSIDE AIR TEMPERATURE OAT (° F)0 20 40 60 80 100 120 140−20−40

30 35 40 45 5040

45

50

55

60

65

70

75

80

90

100

110

120

130

140

150

160

170

35

40

45

50

0 10 20 30 40 50 60−10−20−30−40−50

ABSOLUTE PRESSURE (psia)

CFM56−5C2 SERIES/SEA LEVEL

220° C (428° F) MAX.150° C (302° F)100° C (212° F)

ASU DISCHARGE TEMPERATURE:

F_AC_050500_1_0080101_01_01

Engine Starting Pneumatic RequirementsCFM56-5C2 Series

FIGURE-5-5-0-991-008-A01

5-5-0Page 3

Aug 01/19


5-6-0 Ground Pneumatic Power Requirements

**ON A/C A340-200 A340-300

Ground Pneumatic Power Requirements

1. GeneralThis section describes the required performance for the ground equipment to maintain the cabintemperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for heating cases after boarding(Section 5.7 - steady state), and provides the time needed to cool down or heat up the aircraft cabinto the required temperature (Section 5.6 - dynamic cases with aircraft empty).

ABBREVIATION DEFINITION

A/C Aircraft

AHM Aircraft Handling Manual

GC Ground ConnectionGSE Ground Service Equipment

IFE In-Flight Entertainment

LP Low PressureLPGC Low Pressure Ground ConnectionOAT Outside Air Temperature

PCA Pre-Conditioned Air

A. The air flow rates and temperature requirements for the GSE, provided in Sections 5.6 and 5.7,are given at A/C ground connection.

NOTE : The cooling capacity of the equipment (kW) is only indicative and is not sufficient byitself to ensure the performance (outlet temperature and flow rate combinations arethe requirements needed for ground power).An example of cooling capacity calculation is given in Section 5.7.

B. The air flow rates and temperature requirements for the GSE are given for the A/C in theconfiguration ”2 LP ducts connected”.

NOTE : The maximum air flow is driven by pressure limitation at LPGC.

C. For temperatures at ground connection below +2 ˚C (+35.6 ˚F) (Subfreezing), the groundequipment shall be compliant with the Airbus document ”Subfreezing PCA Carts -- ComplianceDocument for Suppliers” (contact Airbus to obtain this document) defining all the requirementswith which Subfreezing Pre-Conditioning Air equipment must comply to allow its use on Airbusaircraft. These requirements are in addition to the functional specifications included in the IATAAHM997.

5-6-0Page 1

Aug 01/19


2. Ground Pneumatic Power RequirementsThis section provides the ground pneumatic power requirements for:- Heating (pull up) the cabin, initially at OAT, up to 21 ˚C (69.8 ˚F) (see FIGURE

5-6-0-991-002-A)- Cooling (pull down) the cabin, initially at OAT, down to 27 ˚C (80.6 ˚F) (see FIGURE

5-6-0-991-004-A).

5-6-0Page 2

Aug 01/19


**ON A/C A340-200 A340-300

30 60 90 120 1500.8

1.2

1.4

1.6

1.8

2.2

2.4

2.0

2.5

3.0

3.5

4.0

4.5

5.0

AIR

FLO

W A

T G

C (

kg/s

)

AIR

FLO

W A

T G

C (

lb/s

)

PULL UP PERFORMANCE

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

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

40 50 70 80 100 110 130 140

MAXIMUM AIR FLOW

1.0

2.0

F_AC_050600_1_0020101_01_00

Ground Pneumatic Power RequirementsHeating

FIGURE-5-6-0-991-002-A01

5-6-0Page 3

Aug 01/19


**ON A/C A340-200 A340-300

30 60 90 120 1500.8

1.2

1.4

1.6

1.8

2.2

2.4

2.0

2.5

3.0

3.5

4.0

4.5

5.0

AIR

FLO

W A

T G

C (

kg/s

)

AIR

FLO

W A

T G

C (

lb/s

)

PULL DOWN PERFORMANCE

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

OAT ISA +23° C (+73.4° F); GC OUTLET +2° C (+35.6° F); EMPTY CABIN; IFE OFF; SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON

OAT ISA +23° C (+73.4° F); GC OUTLET −10° C (+14° F); EMPTY CABIN; IFE OFF; SOLAR LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON

40 50 70 80 100 110 130 140

MAXIMUM AIR FLOW

2.0

1.0

F_AC_050600_1_0040101_01_00

Ground Pneumatic Power RequirementsCooling

FIGURE-5-6-0-991-004-A01

5-6-0Page 4

Aug 01/19


5-7-0 Preconditioned Airflow Requirements

**ON A/C A340-200 A340-300

Preconditioned Airflow Requirements

1. This section provides the preconditioned airflow rate and temperature needed to maintain the cabintemperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for the heating cases.

These settings are not intended to be used for operation (they are not a substitute for the settingsgiven in the AMM). They are based on theoretical simulations and give the picture of a real steadystate.The purpose of the air conditioning (cooling) operation (described in the AMM) is to maintain thecabin temperature below 27 ˚C (80.6 ˚F) during boarding (therefore it is not a steady state).

5-7-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

AIR

FLO

W A

T G

C (

kg/s

)

−150.8

AIR

FLO

W A

T G

C (

lb/s

)

1.0

1.2

1.4

1.6

1.8

2.0

2.2

2.4

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

2.0

2.5

3.0

3.5

4.0

4.5

5.0

0 10 20 30 40 50 60 70 80

INLET TEMPERATURE AT GC (° C)

INLET TEMPERATURE AT GC (° F)

MAXIMUM AIRFLOW

COOLING/HEATING PERFORMANCE

SETTINGS NOTINTENDED TO BE USED

FOR OPERATION

OAT ISA; EMPTY CABIN; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON; GALLEYS ON

OAT ISA −38° C (−36.4° F); EMPTY CABIN; IFE OFF; LIGHTS ON; NO SOLAR LOAD; RECIRCULATIONFANS ON; GALLEYS OFF

C H

EXAMPLE:COOLING CAPACITY CALCULATION:FOR THE CONDITIONS "C", THE COOLING CAPACITY OF 1.9 kg/s x 1 kJ/(kg.° C) x (27− 5) = 41.8 kW(OR 12.5 TONS COOLING CAPACITY) IS NEEDED TO MAINTAIN THE CABIN TEMPERATURE AT 27° C (80.6° F)(1.9 kg/s AT 5° C (41° F) FOR AIR AT GC INLET).

90 100 110 120 130 140

F_AC_050700_1_0030101_01_01

Preconditioned Airflow RequirementsFIGURE-5-7-0-991-003-A01

5-7-0Page 2

Aug 01/19


5-8-0 Ground Towing Requirements

**ON A/C A340-200 A340-300

Ground Towing Requirements

1. This section provides information on aircraft towing.

The A340-200/-300 is designed with means for conventional or towbarless towing.Information/procedures can be found for both in chapter 9 of the Aircraft Maintenance Manual.Status on towbarless towing equipment qualification can be found in ISI 09.11.00001.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a towbar attached to the NLG. One towbar fitting is installed at the front of the leg(optional towing fitting for towing from the rear of the NLG available).The main landing gears have attachment points for towing or debogging (for details, refer ARM 07).

This section shows the chart to determine the drawbar pull and tow tractor mass requirements as afunction of the following physical characteristics:- Aircraft weight,- Number of engines at idle,- Slope.

The following chart is applicable to both A340-200 and -300 aircraft.

2. Towbar design guidelines

The aircraft towbar shall comply with the following standards:- ISO 8267-1, ”Aircraft - Towbar Attachment Fitting - Interface Requirements - Part 1: Main Line

Aircraft”,- ISO 9667, ”Aircraft Ground Support Equipment - Towbars”,- IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Towbar”.

A conventional type towbar is required which should be equipped with a damping system (to protectthe NLG against jerks) and with towing shear pins:- A traction shear pin calibrated at 28 620 daN (64 340 lbf),- A torsion pin calibrated at 3 130 m.daN (277 028 lbf.in).The towing head is designed according to ISO 8267-1, cat. III.

5-8-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A340−200 OR −300 AT 270 000 kg,AT 1.5% SLOPE, 2 ENGINES AT IDLE AND FOR WET TARMAC CONDITIONS:

− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (270 000 kg),− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),− FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 4,− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED No. OF ENGINES (2),− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (21 300 kg),− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (37 300 kg).

30

25

20

15

10

5

00 10 20 30 40 50 60 70 80 0 1 2 3 4 0 0.5 1.0 1.5 2.0

280255230205180155130

21.3

37.3

2 ENGINES ON1.5% SLOPE 270

ICE = 0.05

HARD SNOW = 0.2

DR

Y C

ON

CR

ETE

= 0.

8

DR

AW

BA

R P

ULL

(x

1 00

0 kg

)

A/C

WE

IGH

T (

x 1

000

kg)

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

WET

CO

NC

RET

E

= 0

.57

BREAKAWAY RESISTANCE 4%# OF ENGINES ON FOR PB: 2ENGINE THRUST 500 daN

F_AC_050800_1_0060101_01_01

Ground Towing RequirementsFIGURE-5-8-0-991-006-A01

5-8-0Page 2

Aug 01/19


5-9-0 De-Icing and External Cleaning

**ON A/C A340-200 A340-300

De-Icing and External Cleaning

1. De-Icing and External Cleaning on GroundThe mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heightsup to approximately 17 m (56 ft).

2. De-Icing

AIRCRAFT TYPEWing Top Surface

(Both Sides)

Wingtip Devices(Both Inside andOutside Surfaces)

(Both Sides)

HTP Top Surface(Both Sides)

VTP(Both Sides)

A340-200306 m2

(3 294 ft2)11 m2

(118 ft2)65 m2

(700 ft2)91 m2

(980 ft2)

A340-300306 m2

(3 294 ft2)11 m2

(118 ft2)65 m2

(700 ft2)91 m2

(980 ft2)

AIRCRAFT TYPEFuselage Top Surface

(Top Third - 120˚ Arc)

Nacelle and Pylon(Top Third - 120˚ Arc)

(All Engines)Total De-Iced Area

A340-200294 m2

(3 165 ft2)55 m2

(592 ft2)821 m2

(8 837 ft2)

A340-300319 m2

(3 434 ft2)55 m2

(592 ft2)847 m2

(9 117 ft2)

NOTE : Dimensions are approximate.

3. External Cleaning

AIRCRAFTTYPE

Wing TopSurface

(Both Sides)

Wing LowerSurface

(Including FlapTrack Fairing)(Both Sides)

Wingtip Devices(Both Insideand OutsideSurfaces)

(Both Sides)

HTP TopSurface

(Both Sides)

HTP LowerSurface

(Both Sides)

A340-200306 m2

(3 294 ft2)340 m2

(3 660 ft2)11 m2

(118 ft2)65 m2

(700 ft2)65 m2

(700 ft2)

A340-300306 m2

(3 294 ft2)340 m2

(3 660 ft2)11 m2

(118 ft2)65 m2

(700 ft2)65 m2

(700 ft2)

5-9-0Page 1

Aug 01/19


AIRCRAFT TYPEVTP

(Both Sides)Fuselage andBelly Fairing

Nacelle and Pylon(All Engines) Total Cleaned Area

A340-20091 m2

(980 ft2)896 m2

(9 644 ft2)200 m2

(2 153 ft2)1 982 m2

(21 334 ft2)

A340-30091 m2

(980 ft2)971 m2

(10 452 ft2)200 m2

(2 153 ft2)2 057 m2

(22 141 ft2)

NOTE : Dimensions are approximate.

5-9-0Page 2

Aug 01/19


OPERATING CONDITIONS

6-1-0 Engine Exhaust Velocities and Temperatures

**ON A/C A340-200 A340-300

Engine Exhaust Velocities and Temperatures

1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway and Maximum Takeoff conditions.

6-1-0Page 1

Aug 01/19


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

**ON A/C A340-200 A340-300

Engine Exhaust Velocities Contours - Ground Idle Power

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

6-1-1Page 1

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_060101_1_0040101_01_00

FE

ET

ME

TE

RS

50

GR

OU

ND

PLA

NE

AIR

PLA

NE

ELE

VA

TIO

N

100

150

200

250

300

350

400

1530

4560

7590

105

120

C L

ftm

00

V =

40

m/s

V =

20

m/s

V =

12

m/s

V =

40

m/s

V =

20

m/s

V =

12

m/s

30 121824 6

100 406080 20

030 121824 6

GR

OU

ND

IDLE

INC

LUD

ES

: (W

OR

ST

CA

SE

) G

RO

UN

D P

LAN

E P

RO

XIM

ITY

HE

AD

WIN

D (

20 K

NT

S)

PLA

N

ftm

0

100 406080 20

00

Engine Exhaust VelocitiesGround Idle Power - CFM56-5C series engine

FIGURE-6-1-1-991-004-A01

6-1-1Page 2

Aug 01/19


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

**ON A/C A340-200 A340-300

Engine Exhaust Temperatures Contours - Ground Idle Power

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

6-1-2Page 1

Aug 01/19


**ON A/C A340-200 A340-300

FEET

METERS

50

GROUND PLANE

AIRPLANE

100

15 30

CL

ftm

0

12

18

6

60

ftm

0

30

12

18

24

6

100

45

150

60

200

GROUND IDLE

INCLUDES: (WORST CASE) GROUND PLANE PROXIMITY HEADWIND (20 KNTS)

306°F152°C

207°F97°C

108°F42°C

306°F 207°F 108°F152°C 97°C 42°C

PLAN0

40

60

80

20

ELEVATION0

40

20

0

0

F_AC_060102_1_0040101_01_00

Engine Exhaust TemperaturesGround Idle Power - CFM56-5C series engine

FIGURE-6-1-2-991-004-A01

6-1-2Page 2

Aug 01/19


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

**ON A/C A340-200 A340-300

Engine Exhaust Velocities Contours - Breakaway Power

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

6-1-3Page 1

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_060103_1_0040101_01_00

FE

ET

ME

TE

RS

50

GR

OU

ND

PLA

NE

AIR

PLA

NE

ELE

VA

TIO

N 100

150

200

250

300

350

400

1530

4560

7590

105

120

C L

135

150

165

180

195

ftm

450

500

550

650

600

00

V =

40

m/s

V =

20

m/s

V =

12

m/s

4−E

NG

INE

BR

EA

KA

WA

Y

INC

LUD

ES

: (W

OR

ST

CA

SE

) G

RO

UN

D P

LAN

E P

RO

XIM

ITY

HE

AD

WIN

D (

20 K

NT

S)

V =

40

m/s

V =

20

m/s

V =

12

m/s

30 121824 6

100 406080 20

ftm

030 121824 6

PLA

N0

100 406080 20

00

Engine Exhaust VelocitiesBreakaway Power - CFM56-5C series engine

FIGURE-6-1-3-991-004-A01

6-1-3Page 2

Aug 01/19


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

**ON A/C A340-200 A340-300

Engine Exhaust Temperatures Contours - Breakaway Power

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

6-1-4Page 1

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_060104_1_0040101_01_00

GROUND PLANE

AIRPLANE

ELEVATION

PLAN CL

ftm

0 0

12

18

6

40

60

20

ftm

0 0

30

12

18

24

6

100

40

60

80

20

240°F116°C

140°F60°C

100°F38°C

240°F116°C

140°F60°C

100°F38°C

FEET

METERS

50 100

15 30 45

150

60

2000

0

Engine Exhaust TemperaturesBreakaway Power - CFM56-5C series engine

FIGURE-6-1-4-991-004-A01

6-1-4Page 2

Aug 01/19


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

**ON A/C A340-200 A340-300

Engine Exhaust Velocities Contours - Takeoff Power

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

6-1-5Page 1

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_060105_1_0040101_01_00

FE

ET

ME

TE

RS

GR

OU

ND

PLA

NE

AIR

PLA

NE

ELE

VA

TIO

N

PLA

N

100

200

300

C L

ftm 0

0

30 121824 6

100

406080 20

3060

9012

015

018

021

024

027

030

033

036

039

0

400

500

700

800

600

900

1000

1100

1200

1300

ftm 0

0

30 121824 6

100

406080 20

V =

40

m/s

V =

20

m/s

V =

12

m/s

V =

40

m/s

V =

20

m/s

V =

12

m/s

TA

KE

OF

F P

OW

ER

INC

LUD

ES

: (W

OR

ST

CA

SE

) G

RO

UN

D P

LAN

E P

RO

XIM

ITY

HE

AD

WIN

D (

20 K

NT

S)

00

Engine Exhaust VelocitiesTakeoff Power - CFM56-5C series engine

FIGURE-6-1-5-991-004-A01

6-1-5Page 2

Aug 01/19


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

**ON A/C A340-200 A340-300

Engine Exhaust Temperatures Contours - Takeoff Power

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

6-1-6Page 1

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_060106_1_0040101_01_00

FEET

METERS

50

GROUND PLANE

AIRPLANE

ELEVATION

PLAN

100

15 30

CL

ftm

0 0

30

12

18

24

6

100

40

60

80

20

45

150

306°F152°C

207°F97°C

108°F42°C

60

200 250

75 90

300

0 0

30

12

18

24

6

100

40

60

80

108°F42°C

306°F152°C

207°F97°C

TAKEOFF POWER

INCLUDES: (WORST CASE) GROUND PLANE PROXIMITY HEADWIND (20KNTS)

ftm

20

0

0

Engine Exhaust TemperaturesTakeoff Power - CFM56-5C series engine

FIGURE-6-1-6-991-004-A01

6-1-6Page 2

Aug 01/19


6-3-0 Danger Areas of Engines

**ON A/C A340-200 A340-300

Danger Areas of Engines

1. Danger Areas of the Engines.

NOTE : Areas with exhaust velocities of more than 56 km/h (35 mph, 50 ft/s or 15 m/s) aredefined as areas where injury to persons and/or damage to machinery can occur.

6-3-0Page 1

Aug 01/19


6-3-1 Ground Idle Power

**ON A/C A340-200 A340-300

Ground Idle Power

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

6-3-1Page 1

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_060301_1_0040101_01_00F_AC_060301_1_0040101_01_00

NOT TO SCALE

RADIUS = 9.7 ft

4.7 ft45°

CLOSE ENTRYCORRIDOR FOR

WIND DIRECTION>90 DEGREES

AB

CNO ENTRY 105 ft (32 m)AFT OF NOZZLE EXIT

GMM−1137912−00−B

AREA

A 210−145(338−233)

B 145−105(233−169)

C

D 65−20(105−32)

105−65(169−105)

E < 20 (32) BEYOND DANGER AREA.

INLET SUCTIONDANGER AREA

ENTRYCORRIDOR

EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR LESS

APPROX. WINDVELOCITYmph (km/h)

LIGHT TO MODERATE DAMAGE TO TRANSPORT − TYPE AIRCRAFT.

POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE", VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV 1951.

D

EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR GREATER

A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR;COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.

A MAN STANDING FACE − ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING; CORRUGATED STEEL STRUCTURES LESS SEVERELY.

MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AIR TRANSPORT− TYPE AIRCRAFT.

171 ft (52 m)WIDTH

TO 417 ft (127 m)E

(3.0 m)

(1.4 m)

INLET DANGER AREASINCLUDE:(WORST CASE)

GROUND PLANE PROXIMITYHEADWIND/CROSSWIND (20 kts)

EXHAUST DANGER AREASINCLUDE (WORST CASE):

GROUND PLANE PROXIMITYHEADWIND (20 kts)

INLET HAZARD DIMENSIONSBASED ON 40 ft/SEC

CRITICAL VELOCITY WITH A3 ft CONTINGENCY ADDED

Danger Areas of EnginesCFM56-5C series engine

FIGURE-6-3-1-991-004-A01

6-3-1Page 2

Aug 01/19


6-3-2 Breakaway Power

**ON A/C A340-200 A340-300

Breakaway Power

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

6-3-2Page 1

Aug 01/19


**ON A/C A340-200 A340-300

AREA

A 210−145(338−233)

B 145−105(233−169)

C

D 65−20(105−32)

105−65(169−105)







MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AIR TRANSPORT− TYPE AIRCRAFT.


ENTRYCORRIDOR

EXHAUST WAKE DANGERAREA 65 Mph (105 km/h)OR GREATER

EXHAUST WAKE DANGERAREA 65 Mph (105 km/h)OR LESS

RADIUS = 13.9 ft(4.2 m)

NOT TO SCALE

NO ENTRY 198 ft (60 m)AFT OF NOZZLE EXIT

TO 750 ft (229 m)

A

B

C

D

E







214 ft (65 m)

WIDTH

6.3 ft(1.9 m)

F_AC_060302_1_0040101_01_02


FIGURE-6-3-2-991-004-A01

6-3-2Page 2

Aug 01/19


6-3-3 Takeoff Power

**ON A/C A340-200 A340-300

Takeoff Power

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

6-3-3Page 1

Aug 01/19


**ON A/C A340-200 A340-300

RADIUS = 34 ft

NOT TO SCALE

13.4 ft

AREA

A 210−145(338−233)

B 145−105(233−169)

C

D 65−20(105−32)

105−65(169−105)



ENTRYCORRIDOR

EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR LESS




EXHAUST WAKE DANGERAREA, 65 mph (105 km/h)OR GREATER



MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AIR TRANSPORT − TYPE AIRCRAFT.

GMM−1137913−00−B

A

B

C

D

295 ft (90 m)

TO 1460 ft (445 m)

WIDTH

E

(10.4 m)

(4.1 m)

NO ENTRY 830 ft (253 m)AFT OF NOZZLE EXIT







F_AC_060303_1_0040101_01_01


FIGURE-6-3-3-991-004-A01

6-3-3Page 2

Aug 01/19


6-4-0 APU Exhaust Velocities and Temperatures

**ON A/C A340-200 A340-300

APU Exhaust Velocities and Temperatures

1. APU Exhaust Velocities and Temperatures.

6-4-0Page 1

Aug 01/19


6-4-1 APU

**ON A/C A340-200 A340-300

APU - GARRETT

1. This section gives APU exhaust velocities and temperatures.

6-4-1Page 1

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_060401_1_0020101_01_00

20

METERS

0

5 10 15

FEET

0

10 20 30 40 50

0

60

0

10

5

10

20

30

40

METERS FEET

20

METERS

FD

0

5 10 15

FEET

0

10 20 30 40 50

0

60

0

10

5

10

20

30

40

METERS FEET

121°C

93°C

204°C260°C

315.5°C427°C

15 m/s

18 m/s

24 m/s

FD

149°C177°C

61 m/s46 m/s

30.5 m/s

Exhaust Velocities and TemperaturesGARRETT GTCP 331-350FIGURE-6-4-1-991-002-A01

6-4-1Page 2

Aug 01/19


PAVEMENT DATA


**ON A/C A340-200 A340-300

General Information

1. A brief description of the pavement charts that follow will help in airport planning.

To aid in the interpolation between the discrete values shown, each aircraft configuration is shownwith a minimum range of five loads on the Main Landing Gear (MLG).

All curves on the charts represent data at a constant specified tire pressure with:- The aircraft loaded to the Maximum Ramp Weight (MRW),- The CG at its maximum permissible aft position.

Pavement requirements for commercial aircraft are derived from the static analysis of loads imposedon the MLG struts.

Landing Gear Footprint:Section 07-02-00 presents basic data on the landing gear footprint configuration, MRW and tire sizesand pressures.

Maximum Pavement Loads:Section 07-03-00 shows maximum vertical and horizontal pavement loads for certain criticalconditions at the tire-ground interfaces.

Landing Gear Loading on Pavement:Section 07-04-00 contains charts to find these loads throughout the stability limits of the aircraft atrest on the pavement.These MLG loads are used as the point of entry to the pavement design charts which follow,interpolating load values where necessary.

Flexible Pavement Requirements - US Army Corps of Engineers Design Method:Section 07-05-00 uses procedures in Instruction Report No. S-77-1 ”Procedures for Development ofCBR Design Curves”, dated June 1977 and as modified according to the methods described in ICAOAerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCNMethod), and utilizing the alpha factors approved by ICAO in October 2007.The report was prepared by the ”U.S. Army Corps Engineers Waterways Experiment Station, Soilsand Pavement Laboratory, Vicksburg, Mississippi”.The line showing 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).

Flexible Pavement Requirements - LCN Conversion Method:

7-1-0Page 1

Aug 01/19


The Load Classification Number (LCN) curves are no longer provided in section 07-06-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983. For questions regarding the LCN system, contact Airbus.

Rigid Pavement Requirements - PCA (Portland Cement Association) Design Method:Section 07-07-00 gives the rigid pavement design curves that have been prepared with the use of theWestergaard Equation.This is in general accordance with the procedures outlined in the Portland Cement Associationpublications, ”Design of Concrete Airport Pavement”, 1973 and ”Computer Program for AirportPavement Design” (Program PDILB), 1967 both by Robert G. Packard.

Rigid Pavement Requirements - LCN Conversion:The Load Classification Number (LCN) curves are no longer provided in section 07-08-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983. For questions regarding the LCN system, contact Airbus.

ACN/PCN Reporting System:Section 07-09-00 provides ACN data prepared according to the ACN/PCN system as referenced inICAO Annex 14, ”Aerodromes”, Volume 1 ”Aerodrome Design and Operations” Fourth Edition, July2004, incorporating Amendments 1 to 6.The ACN/PCN system provides a standardized international aircraft/pavement rating systemreplacing the various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world.ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.An aircraft having an ACN less than or equal to the PCN can operate without restriction on thepavement.Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.The derived single wheel load is defined as the load on a single tire inflated to 1.25 MPa (181 psi)that would have the same pavement requirements as the aircraft.Computationally the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1 forflexible pavements to calculate ACN values.

The Airport Authority must decide on the method of pavement analysis and the results of theirevaluation shown as follows:

PCNPAVEMENT

TYPESUBGRADECATEGORY

TIRE PRESSURE CATEGORY EVALUATION METHOD

R - Rigid A - High W - No pressure limit T - Technical

F - Flexible B - MediumX - High pressure limited to1.75 MPa (254 psi)

U - Using Aircraft

C - LowY - Medium pressure limited to1.25 MPa (181 psi)

7-1-0Page 2

Aug 01/19


PCNPAVEMENT

TYPESUBGRADECATEGORY

TIRE PRESSURE CATEGORY EVALUATION METHOD

D - Ultra LowZ - Low pressure limited to 0.5MPa (73 psi)

For flexible pavements, the four subgrade categories (CBR) are:

- A. High Strength CBR 15

- B. Medium Strength CBR 10

- C. Low Strength CBR 6

- D. Ultra Low Strength CBR 3

For rigid pavements, the four subgrade categories (k) are:

- A. High Strength k = 150 MN/m3 (550 pci)

- B. Medium Strength k = 80 MN/m3 (300 pci)

- C. Low Strength k = 40 MN/m3 (150 pci)

- D. Ultra Low Strength k = 20 MN/m3 (75 pci)

7-1-0Page 3

Aug 01/19


7-2-0 Landing Gear Footprint

**ON A/C A340-200 A340-300

Landing Gear Footprint

1. This section provides data about the landing gear footprint in relation to the aircraft MRW and tiresizes and pressures.The landing-gear footprint information is given for all the operational weight variants of the aircraft.

7-2-0Page 1

Aug 01/19


**ON A/C A340-300

0.71

0 m

(2.3

29 ft

)

25.3

75 m

(83.

251

ft)

10.6

84 m

(35.

052

ft)

0.96

5 m

(3.1

66 ft

)

1.39

7 m

(4.5

83 ft

)1.

981

m(6

.499

ft)

26.3

72 m

(86.

522

ft)

CE

NT

RA

L G

EA

RT

IRE

SIZ

E

1400

x530

R23

OR

54x2

1−23

(bi

as)

10.9

bar

(158

psi

)

CE

NT

RA

LG

EA

RT

IRE

PR

ES

SU

RE

WE

IGH

TV

AR

IAN

TM

AX

IMU

MR

AM

PW

EIG

HT

PE

RC

EN

TA

GE

OF

WE

IGH

TO

N M

AIN

GE

AR

GR

OU

P

NO

SE

GE

AR

TIR

EP

RE

SS

UR

EM

AIN

GE

AR

TIR

ES

IZE

MA

IN G

EA

RT

IRE

PR

ES

SU

RE

A34

0−30

0W

V00

125

7 90

0 kg

(568

575

lb)

94.7

%11

.6 b

ar(1

68 p

si)

1400

x530

R23

OR

54x2

1−23

(bi

as)

A34

0−30

0W

V00

2

A34

0−30

0W

V00

3

A34

0−30

0W

V00

4

13.2

bar

(191

psi

)10

50x3

95R

16

1050

x395

R16

1050

x395

R16

NO

SE

GE

AR

TIR

E S

IZE

1050

x395

R16

A34

0−30

0W

V02

010

50x3

95R

16

260

900

kg(5

75 1

75 lb

)93

.8%

11.6

bar

(168

psi

)13

.2 b

ar(1

91 p

si)

257

900

kg(5

68 5

75 lb

)94

.7%

11.6

bar

(168

psi

)13

.2 b

ar(1

91 p

si)

260

900

kg(5

75 1

75 lb

)93

.8%

11.6

bar

(168

psi

)13

.2 b

ar(1

91 p

si)

271

900

kg(5

99 4

25 lb

)94

.6%

12.1

bar

(175

psi

)14

.2 b

ar(2

06 p

si)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

10.4

bar

(151

psi

)A

340−

300

WV

000

254

400

kg(5

60 8

50 lb

)94

.7%

11.4

bar

(165

psi

)14

00x5

30R

23 O

R54

x21−

23 (

bias

)13

.1 b

ar(1

90 p

si)

1050

x395

R16

F_AC_070200_1_0290101_01_04

Landing Gear Footprint(Sheet 1 of 2)

FIGURE-7-2-0-991-029-A01

7-2-0Page 2

Aug 01/19


**ON A/C A340-300

CE

NT

RA

L G

EA

RT

IRE

SIZ

E

CE

NT

RA

LG

EA

RT

IRE

PR

ES

SU

RE

WE

IGH

TM

AX

IMU

MP

ER

CE

NT

AG

EN

OS

EM

AIN

GE

AR

TIR

EM

AIN

GE

AR

RA

MP

WE

IGH

T

OF

WE

IGH

TO

N M

AIN

GE

AR

GR

OU

PG

EA

R T

IRE

PR

ES

SU

RE

SIZ

ET

IRE

PR

ES

SU

RE

VA

RIA

NT

NO

SE

GE

AR

TIR

E S

IZE

1050

x395

R16

1050

x395

R16

1050

x395

R16

1050

x395

R16

1050

x395

R16

1050

x395

R16

1050

x395

R16

1050

x395

R16

1050

x395

R16

A34

0−30

0W

V02

6

A34

0−30

0W

V02

7

A34

0−30

0W

V02

8

A34

0−30

0W

V02

9

A34

0−30

0W

V05

0

275

900

kg(6

08 2

50 lb

)94

.6%

12.1

bar

(175

psi

)

A34

0−30

0W

V05

1

271

900

kg(5

99 4

25 lb

)94

.6%

12.1

bar

(175

psi

)

A34

0−30

0W

V05

2

277

400

kg(6

11 5

50 lb

)93

.8%

12.1

bar

(175

psi

)

A34

0−30

0W

V05

3

260

900

kg(5

75 1

75 lb

)94

.7%

12.1

bar

(175

psi

)

A34

0−30

0W

V05

4

275

900

kg(6

08 2

50 lb

)94

.6%

12.1

bar

(175

psi

)

275

900

kg(6

08 2

50 lb

)94

.6%

277

400

kg(6

11 5

50 lb

)93

.8%

277

400

kg(6

11 5

50 lb

)93

.8%

275

900

kg(6

08 2

50 lb

)94

.6%

12.1

bar

(175

psi

)

12.1

bar

(175

psi

)

12.1

bar

(175

psi

)

12.1

bar

(175

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1050

x395

R16

A34

0−30

0W

V02

526

0 90

0 kg

(575

175

lb)

94.7

%12

.1 b

ar(1

75 p

si)

14.2

bar

(206

psi

)10

.9 b

ar(1

58 p

si)

A34

0−30

0W

V02

1

1400

x530

R23

OR

54x2

1−23

(bi

as)

1050

x395

R16

1050

x395

R16

1050

x395

R16

1050

x395

R16

A34

0−30

0W

V02

3

A34

0−30

0W

V02

4

A34

0−30

0W

V02

5

275

900

kg(6

08 2

50 lb

)94

.6%

12.1

bar

(175

psi

)14

.2 b

ar(2

06 p

si)

262

900

kg(5

79 6

00 lb

)94

.7%

12.1

bar

(175

psi

)

275

900

kg(6

08 2

50 lb

)94

.6%

12.1

bar

(175

psi

)

260

900

kg(5

75 1

75 lb

)94

.7%

12.1

bar

(175

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

14.2

bar

(206

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)(C

G 3

8.02

%)

(CG

38%

)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

F_AC_070200_1_0300101_01_03F_AC_070200_1_0290102_01_00

Landing Gear Footprint(Sheet 2 of 2)

FIGURE-7-2-0-991-029-A01

7-2-0Page 3

Aug 01/19


**ON A/C A340-200

0.71

0 m

(2.3

29 ft

)

23.2

41 m

(76.

249

ft)

24.2

35 m

(79.

510

ft)

10.6

84 m

(35.

052

ft)

0.96

5 m

(3.1

66 ft

)

1.39

7 m

(4.5

83 ft

)1.

981

m(6

.499

ft)

CE

NT

RA

L G

EA

RT

IRE

SIZ

E

1400

x530

R23

OR

54x2

1−23

(bi

as)

10.3

bar

(149

psi

)

10.9

bar

(158

psi

)

10.9

bar

(158

psi

)

CE

NT

RA

LG

EA

RT

IRE

PR

ES

SU

RE

10.9

bar

(158

psi

)

WE

IGH

TM

AX

IMU

MP

ER

CE

NT

AG

EN

OS

E G

EA

RM

AIN

GE

AR

TIR

EM

AIN

GE

AR

RA

MP

WE

IGH

T

OF

WE

IGH

TO

N M

AIN

GE

AR

GR

OU

PT

IRE

PR

ES

SU

RE

SIZ

ET

IRE

PR

ES

SU

RE

VA

RIA

NT

A34

0−20

0W

V00

025

4 40

0 kg

(560

850

lb)

93.8

%11

.4 b

ar(1

65 p

si)

1400

x530

R23

OR

54x2

1−23

(bi

as)

A34

0−20

0W

V00

125

7 90

0 kg

(568

575

lb)

93.7

%11

.6 b

ar(1

68 p

si)

A34

0−20

0W

V00

226

0 90

0 kg

(575

175

lb)

93.7

%11

.6 b

ar(1

68 p

si)

A34

0−20

0W

V02

127

5 90

0 kg

(608

250

lb)

93.6

%13

.1 b

ar(1

90 p

si)

13 b

ar(1

89 p

si)

13.2

bar

(191

psi

)

13.2

bar

(191

psi

)

14.2

bar

(206

psi

)

1050

x395

R16

1050

x395

R16

1050

x395

R16

NO

SE

GE

AR

TIR

E S

IZE

1050

x395

R16

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

1400

x530

R23

OR

54x2

1−23

(bi

as)

F_AC_070200_1_0380101_01_02

Landing Gear FootprintFIGURE-7-2-0-991-038-A01

7-2-0Page 4

Aug 01/19


7-3-0 Maximum Pavement Loads

**ON A/C A340-200 A340-300

Maximum Pavement Loads

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

7-3-0Page 1

Aug 01/19


**ON A/C A340-300

V(M

G)

MA

XIM

UM

VE

RT

ICA

L N

OS

E G

EA

R G

RO

UN

D L

OA

D A

T M

OS

T F

WD

CG

V(N

G)

MA

XIM

UM

VE

RT

ICA

L M

AIN

GE

AR

GR

OU

ND

LO

AD

AT

MA

X A

FT

CG

V(N

G)

HM

AX

IMU

M H

OR

IZO

NT

AL

GR

OU

ND

LO

AD

FR

OM

BR

AK

ING

V(C

G)

MA

XIM

UM

VE

RT

ICA

L C

EN

TE

R G

EA

R G

RO

UN

D L

OA

D A

T M

AX

AF

T C

G

V(M

G)

H

V(C

G)

12

34

57

H (

PE

R S

TR

UT

)

MO

DE

LM

AX

IMU

MR

AM

PW

EIG

HT

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

BR

AK

ING

ST

AT

IC

AT

10

ft/s²

DE

CE

LER

AT

ION

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GB

RA

KIN

GA

T 1

0 ft/

s²D

EC

ELE

RA

TIO

N

ST

EA

DY

INS

TA

NT

AN

EO

US

BR

AK

ING

CO

EF

FIC

IEN

T =

0.8

AT

6

ST

AT

IC L

OA

D A

TM

AX

AF

T C

G

A34

0−30

0W

V00

0(5

60 8

50 lb

)25

4 40

0 kg

(56

375

lb)

25 5

70 k

g(8

3 92

5 lb

)38

070

kg

(220

975

lb)

100

230

kg(8

7 15

0 lb

)39

530

kg

(d)

(88

350

lb)

40 0

80 k

g(d

)

(89

400

lb)

40 5

50 k

g(d

)

(88

350

lb)

40 0

80 k

g(d

)

(89

400

lb)

40 5

50 k

g(d

)

(93

150

lb)

42 2

50 k

g(d

)

(94

525

lb)

42 8

80 k

g(d

)

MA

C18

% (b)

MA

C38

.18

%

(a)

(89

300

lb)

40 5

10 k

g(1

76 7

75 lb

)80

180

kg

(d)

(179

275

lb)

81 3

20 k

g(d

)

(179

875

lb)

81 5

90 k

g(d

)

(179

275

lb)

81 3

20 k

g(d

)

(179

875

lb)

81 5

90 k

g(d

)

(189

950

lb)

86 1

60 k

g(d

)

(193

050

lb)

87 5

70 k

g(d

)

MA

C38

.18

%

(a)

A34

0−30

0W

V00

1

A34

0−30

0W

V00

2

A34

0−30

0W

V00

3

A34

0−30

0W

V00

4

A34

0−30

0W

V02

0

A34

0−30

0W

V02

1

(568

575

lb)

257

900

kg(5

6 37

5 lb

)25

570

kg

(83

875

lb)

38 0

50 k

g(2

24 0

75 lb

)10

1 64

0 kg

MA

C38

.05

%

(a)

(90

200

lb)

40 9

10 k

g

(575

175

lb)

260

900

kg(5

6 37

5 lb

)25

570

kg

(83

725

lb)

37 9

80 k

g(2

24 8

25 lb

)10

1 98

0 kg

MA

C35

% (a)

(90

050

lb)

40 8

50 k

g

(568

575

lb)

257

900

kg(5

6 37

5 lb

)25

570

kg

(83

875

lb)

38 0

50 k

g(2

24 0

75 lb

)10

1 64

0 kg

MA

C38

.05

%

(a)

(90

200

lb)

40 9

10 k

g

(575

175

lb)

260

900

kg(5

6 37

5 lb

)25

570

kg

(84

025

lb)

38 1

10 k

g(2

24 8

25 lb

)10

1 98

0 kg

MA

C35

% (a)

(90

050

lb)

40 8

50 k

g

(599

425

lb)

271

900

kg(6

0 57

5 lb

)27

480

kg

(93

075

lb)

42 2

20 k

g(2

37 4

50 lb

)10

7 70

0 kg

MA

C37

.63

%

(a)

(92

150

lb)

41 8

00 k

g

(608

250

lb)

275

900

kg(6

0 72

5 lb

)27

550

kg

(93

675

lb)

42 4

90 k

g(2

41 3

25 lb

)10

9 46

0 kg

MA

C37

.5 %

(a)

(92

575

lb)

41 9

90 k

g

MA

C38

.05

%

(a)

MA

C38

.05

%

(c)

MA

C38

.05

%

(a)

MA

C(c

)

38.0

5 %

MA

C37

.63

%

(a)

MA

C37

.5 %

(a)

MA

C18

% (b)

MA

C18

% (b)

MA

C18

% (b)

MA

C18

% (b)

MA

C21

.5 %

(a)

MA

C21

.9 %

(a)

NO

TE

:(a

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T M

RW

.(b

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T 2

31 0

00 k

g (5

09 2

75 lb

).

(d)

BR

AK

ED

MA

IN G

EA

R.

LOA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T 2

57 0

00 k

g (5

66 6

00 lb

).(c

)

(PE

R S

TR

UT

)V

(MG

)V

(NG

)(P

ER

ST

RU

T)

V(C

G)

F_AC_070300_1_0070101_01_05

Maximum Pavement Loads(Sheet 1 of 2)

FIGURE-7-3-0-991-007-A01

7-3-0Page 2

Aug 01/19


**ON A/C A340-300

WV

023

A34

0−30

0(5

79 6

00 lb

)26

2 90

0 kg

(60

250

lb)

27 3

30 k

g

(58

875

lb)

26 7

10 k

g

(60

125

lb)

27 2

70 k

g

(60

725

lb)

27 5

50 k

g

(60

725

lb)

27 5

50 k

g

(60

575

lb)

27 4

80 k

g

(60

550

lb)

27 4

60 k

g

(60

125

lb)

27 2

70 k

g

(60

725

lb)

27 5

50 k

g

(60

725

lb)

27 5

50 k

g

(60

550

lb)

27 4

60 k

g

(60

550

lb)

27 4

60 k

g

(60

725

lb)

27 5

50 k

g

(91

725

lb)

41 6

10 k

g(2

28 8

50 lb

)10

3 80

0 kg

(90

075

lb)

40 8

60 k

g(d

)

(89

400

lb)

40 5

50 k

g(d

)

(89

400

lb)

40 5

50 k

g(d

)

(94

525

lb)

42 8

80 k

g(d

)

(94

525

lb)

42 8

80 k

g(d

)

(93

150

lb)

42 2

50 k

g(d

)

(95

050

lb)

43 1

10 k

g(d

)

(89

400

lb)

40 5

50 k

g(d

)

(94

525

lb)

42 8

80 k

g(d

)

(94

525

lb)

42 8

80 k

g(d

)

(95

050

lb)

43 1

10 k

g(d

)

(95

050

lb)

43 1

10 k

g(d

)

(94

525

lb)

42 8

80 k

g(d

)

MA

C20

.5 %

(a)

MA

C37

.9 %

(a)

(90

950

lb)

41 2

50 k

g(1

83 0

75 lb

)83

040

kg

(d)

(181

575

lb)

82 3

70 k

g(d

)

(181

575

lb)

82 3

70 k

g(d

)

(193

050

lb)

87 5

70 k

g(d

)

(193

050

lb)

87 5

70 k

g(d

)

(189

950

lb)

86 1

60 k

g(d

)

(192

575

lb)

87

350

kg(d

)

(181

575

lb)

82 3

60 k

g(d

)

(193

050

lb)

87 5

70 k

g(d

)

(193

050

lb)

87 5

70 k

g(d

)

(192

575

lb)

87 3

50 k

g(d

)

(192

575

lb)

87 3

50 k

g(d

)

(193

050

lb)

87 5

70 k

g(d

)

MA

C37

.9 %

(a)

WV

025

A34

0−30

0

(CG

38

%)(5

75 1

75 lb

)26

0 90

0 kg

(87

775

lb)

39 8

10 k

g(2

26 9

75 lb

)10

2 95

0 kg

(226

975

lb)

102

960

kg

(241

325

lb)

109

460

kg

(241

325

lb)

109

460

kg

107

700

kg(2

37 4

50 lb

)

(240

725

lb)

109

190

kg

(226

975

lb)

102

950

kg

(241

325

lb)

109

460

kg

(241

325

lb)

109

460

kg

(240

725

lb)

109

190

kg

(240

725

lb)

109

190

kg

(241

325

lb)

109

460

kg

MA

C18

% (e)

MA

C38

% (a)

(90

650

lb)

41 1

20 k

g

WV

025

A34

0−30

0

(CG

38.0

2 %

)(5

75 1

75 lb

)26

0 90

0 kg

(91

375

lb)

41 4

50 k

gM

AC

38.0

2 %

(a)

(90

650

lb)

41 1

20 k

g

A34

0−30

0W

V02

4

A34

0−30

0W

V02

6

A34

0−30

0W

V02

7

A34

0−30

0W

V02

8

A34

0−30

0W

V02

9

A34

0−30

0W

V05

0

A34

0−30

0W

V05

1

A34

0−30

0W

V05

2

A34

0−30

0W

V05

3

A34

0−30

0W

V05

4

(608

250

lb)

275

900

kg(9

3 67

5 lb

)42

490

kg

MA

C37

.5 %

(a)

(92

575

lb)

41 9

90 k

g

(608

250

lb)

275

900

kg(9

3 67

5 lb

)42

490

kg

MA

C37

.5 %

(a)

(92

575

lb)

41 9

90 k

g

(599

425

lb)

271

900

kg(9

3 07

5 lb

)42

220

kg

MA

C37

.63

%

(a)

(92

150

lb)

41 8

00 k

g

(611

550

lb)

277

400

kg(9

3 35

0 lb

)42

340

kg

MA

C35

% (a)

(92

475

lb)

41 9

50 k

g

(575

175

lb)

260

900

kg(9

1 37

5 lb

)41

450

kg

MA

C38

% (a)

(90

650

lb)

41 1

20 k

g

(608

250

lb)

275

900

kg(9

3 67

5 lb

)42

490

kg

MA

C37

.5 %

(a)

(92

575

lb)

41 9

90 k

g

(608

250

lb)

275

900

kg(9

3 67

5 lb

)42

490

kg

MA

C37

.5 %

(a)

(92

575

lb)

41 9

90 k

g

(611

550

lb)

277

400

kg(9

3 35

0 lb

)42

340

kg

MA

C35

% (a)

(92

475

lb)

41 9

50 k

g

(611

550

lb)

277

400

kg(9

3 35

0 lb

)42

340

kg

MA

C35

% (a)

(92

475

lb)

41 9

50 k

g

(608

250

lb)

275

900

kg(9

3 67

5 lb

)42

490

kg

MA

C37

.5 %

(a)

(92

575

lb)

41 9

90 k

g

MA

C37

.5 %

(a)

MA

C37

.5 %

(a)

MA

C37

.63

%

(a)

MA

C37

.5 %

(f)

MA

C38

% (a)

MA

C37

.5 %

(a)

MA

C37

.5 %

(a)

MA

C37

.5 %

(f)

37.5

%M

AC

(f)

MA

C37

.5 %

(a)

MA

C38

.02

%

(a)

MA

C38

% (a)

MA

C21

.9 %

(a)

MA

C20

.3 %

(a)

MA

C21

.9 %

(a)

MA

C21

.9 %

(f)

MA

C21

.9 %

(a)

MA

C21

.9 %

(a)

MA

C21

.9 %

(f)

MA

C21

.9 %

(f)

MA

C21

.9 %

(a)

MA

C21

.5 %

(a)

MA

C20

.3 %

(a)

NO

TE

:(a

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T M

RW

.(e

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T 2

41 0

00 k

g (5

31 3

25 lb

).(f

)

LOA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T 2

75 0

00 k

g (6

06 2

75 lb

).

12

34

56

(PE

R S

TR

UT

)

V(M

G)

H (

PE

R S

TR

UT

)

MO

DE

LM

AX

IMU

MR

AM

PW

EIG

HT

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC B

RA

KIN

GA

T 1

0 ft/

s²D

EC

ELE

RA

TIO

N

ST

AT

IC L

OA

D A

TM

AX

AF

T C

G

ST

EA

DY

BR

AK

ING

AT

10

ft/s²

DE

CE

LER

AT

ION

AT

INS

TA

NT

AN

EO

US

BR

AK

ING

CO

EF

FIC

IEN

T =

0.8

V(N

G)

7

(d)

BR

AK

ED

MA

IN G

EA

R.

(PE

R S

TR

UT

)

V(C

G)

ST

AT

IC L

OA

D A

TM

AX

AF

T C

G

F_AC_070300_1_0070102_01_02

Maximum Pavement Loads(Sheet 2 of 2)

FIGURE-7-3-0-991-007-A01

7-3-0Page 3

Aug 01/19


**ON A/C A340-200

V(M

G)

MA

XIM

UM

VE

RT

ICA

L N

OS

E G

EA

R G

RO

UN

D L

OA

D A

T M

OS

T F

WD

CG

V(N

G)

MA

XIM

UM

VE

RT

ICA

L M

AIN

GE

AR

GR

OU

ND

LO

AD

AT

MA

X A

FT

CG

V(N

G)

V(M

G)

H

A34

0−20

0W

V00

025

4 40

0 kg

(560

850

lb)

27 3

30 k

g(6

0 25

0 lb

)40

730

kg

(89

800

lb)

99 4

10 k

g(2

19 1

50 lb

)39

700

kg

(87

525

lb)

39 5

30 k

g(8

7 15

0 lb

)(c

)

40 0

80 k

g(8

8 35

0 lb

)(c

)

40 5

50 k

g(8

9 40

0 lb

)(c

)

42 8

80 k

g(9

4 52

5 lb

)(c

)

20 %

MA

C(b

)

37.7

%M

AC

(a)

A34

0−20

0W

V00

125

7 90

0 kg

(568

575

lb)

27 3

30 k

g(6

0 25

0 lb

)40

720

kg

(89

775

lb)

100

730

kg(2

22 0

75 lb

)40

240

kg

(88

725

lb)

20 %

MA

C(b

)

37.6

%M

AC

(a)

A34

0−20

0W

V00

226

0 90

0 kg

(575

175

lb)

27 3

30 k

g(6

0 25

0 lb

)40

700

kg

(89

725

lb)

101

950

kg(2

24 7

50 lb

)40

550

kg

(89

400

lb)

20 %

MA

C(b

)

37.5

%M

AC

(a)

37 %

MA

C(a

)A

340−

200

WV

021

275

900

kg(6

08 2

50 lb

)30

030

kg

(66

200

lb)

46 2

10 k

g(1

01 8

75 lb

)10

8 22

0 kg

(238

575

lb)

41 6

90 k

g(9

1 90

0 lb

)

23.7

%M

AC

(a)

79 5

30 k

g(1

75 3

25 lb

)(c

)

80 5

90 k

g(1

77 6

75 lb

)(c

)

81 5

60 k

g(1

79 8

00 lb

)(c

)

86 5

80 k

g(1

90 8

75 lb

)(c

)

37.7

%M

AC

(a)

37.6

%M

AC

(a)

37.5

%M

AC

(a)

37 %

MA

C(a

)

HM

AX

IMU

M H

OR

IZO

NT

AL

GR

OU

ND

LO

AD

FR

OM

BR

AK

ING

V(C

G)

MA

XIM

UM

VE

RT

ICA

L C

EN

TE

R G

EA

R G

RO

UN

D L

OA

D A

T M

AX

AF

T C

G

V(C

G)

12

34

57

MO

DE

LM

AX

IMU

MR

AM

PS

TA

TIC

LO

AD

AT

MO

ST

FW

D C

GB

RA

KIN

G

DE

CE

LER

AT

ION

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GB

RA

KIN

GA

T 1

0 ft/

s²D

EC

ELE

RA

TIO

N

INS

TA

NT

AN

EO

US

BR

AK

ING

CO

EF

FIC

IEN

T =

0.8

WE

IGH

T

6

ST

AT

IC L

OA

D A

TM

AX

AF

T C

G

AT

ST

AT

ICS

TE

AD

Y

V(N

G)

(PE

R S

TR

UT

)

V(M

G)

H (

PE

R S

TR

UT

)(P

ER

ST

RU

T)

V(C

G)

AT

10

ft/s²

NO

TE

:(a

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T M

RW

.(b

) L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

CR

AF

T A

T 2

27 0

00 k

g (5

00 4

50 lb

).B

RA

KE

D M

AIN

GE

AR

(c)

F_AC_070300_1_0090101_01_04

Maximum Pavement LoadsFIGURE-7-3-0-991-009-A01

7-3-0Page 4

Aug 01/19


7-4-0 Landing Gear Loading on Pavement

**ON A/C A340-200 A340-300

Landing Gear Loading on Pavement

1. This section provides data about the landing gear loading on pavement.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN (and LCN) and the highest ACN(and LCN) for each type of aircraft.

2. MLG Loading on PavementExample, see FIGURE 7-4-0-991-005-A (Sheet 1), calculation of the total weight on the MLG for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- The aircraft gross weight is 200 000 kg (440 925 lb),- A percentage of weight on the MLG of 93.76% (percentage of weight on the MLG at MRW and

maximum aft CG at MRW).The total weight on the MLG group is 187 510 kg (413 400 lb).

3. Main Gear and Center Gear Loading on PavementThe MLG group consists of two main gears (4-wheel bogies) plus one center gear (twin-wheel).

Example, see FIGURE 7-4-0-991-005-A (Sheet 2), calculation of the total weight on the MLG for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- The aircraft gross weight is 200 000 kg (440 925 lb),- A percentage of weight on the MLG of 93.85% (percentage of weight on the MLG at 200 000 kg

(440 925 lb) and maximum aft CG at MRW).The load on the two main gears is 162 720 kg (358 725 lb) and the load on the center gear is 24 980kg (55 050 lb).The total weight on the MLG group is 187 690 kg (413 800 lb).

NOTE : The CG in the figure title is the CG used for ACN/LCN calculation.

7-4-0Page 1

Aug 01/19


**ON A/C A340-200

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

84 86 88 90 92 94 96 98 100

(x 1

000

kg)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

(x

1 00

0 kg

)

PERCENTAGE OF WEIGHT ON MAIN GEAR

250

300

350

400

450

500

550

600

(x 1

000

lb)

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

AIR

CR

AF

T G

RO

SS

WE

IGH

T

CG FOR ACNCALCULATION

37.7% MAC

MTOW − 253 500 kg

24.2% MAC

MLW

MZFW

LANDING

TAKE OFF

F_AC_070400_1_0050101_01_01

Landing Gear Loading on PavementWV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)

FIGURE-7-4-0-991-005-A01

7-4-0Page 2

Aug 01/19


**ON A/C A340-200

100

200

300

400

500

300

280

260

240

220

200

180

160

140

120

100

020406080100

120

140

160

180

200

220

240

300

400

500

600

LOAD ON CENTER GEAR OR LOAD ON MAIN GEARS (x 1000 Kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T (

x 10

00 K

g)

(x 1

000

lb)

MA

IN G

EA

RS

CE

NT

ER

LIN

E G

EA

R

(x 1000 lb)

F_AC_070400_1_0050102_01_00


FIGURE-7-4-0-991-005-A01

7-4-0Page 3

Aug 01/19


**ON A/C A340-200

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

84 86 88 90 92 94 96 98 100

(x 1

000

Kg)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

(x

1000

Kg)


250

300

350

400

450

500

550

600

(x 1

000

lb)

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

AIR

CR

AF

T G

RO

SS

WE

IGH

T

MTOW − 275 000 kg

TAKE OFF

MZFW


37% MAC

23.7% MAC

MLW

LANDING

F_AC_070400_1_0060101_01_00

Landing Gear Loading on PavementWV021, MRW 275 900 kg, CG 37% (Sheet 1 of 2)

FIGURE-7-4-0-991-006-A01

7-4-0Page 4

Aug 01/19


**ON A/C A340-200

100

200

300

400

500

300

280

260

240

220

200

180

160

140

120

100

020406080100

120

140

160

180

200

220

240

300

400

500

600


AIR

CR

AF

T G

RO

SS

WE

IGH

T (

x 10

00 K

g)

(x 1

000

lb)

MA

IN G

EA

RS

CE

NT

ER

LIN

E G

EA

R

(x 1000 lb)

F_AC_070400_1_0060102_01_00


FIGURE-7-4-0-991-006-A01

7-4-0Page 5

Aug 01/19


**ON A/C A340-300

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

84 86 88 90 92 94 96 98 100

(x 1

000

Kg)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

(x

1000

Kg)


250

300

350

400

450

500

550

600

(x 1

000

lb)

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

AIR

CR

AF

T G

RO

SS

WE

IGH

T

CG FOR ACNCALCULATION38.18% MAC

MTOW − 253 500 kg

22% MAC

MLW

MZFW

TAKE OFF

LANDING

F_AC_070400_1_0070101_01_00


FIGURE-7-4-0-991-007-A01

7-4-0Page 6

Aug 01/19


**ON A/C A340-300

100

200

300

400

500

300

280

260

240

220

200

180

160

140

120

100

020406080100

120

140

160

180

200

220

240

300

400

500

600


AIR

CR

AF

T G

RO

SS

WE

IGH

T (

x 10

00 K

g)

(x 1

000

lb)

MA

IN G

EA

RS

CE

NT

ER

LIN

E G

EA

R

(x 1000 lb)

F_AC_070400_1_0070102_01_00


FIGURE-7-4-0-991-007-A01

7-4-0Page 7

Aug 01/19


**ON A/C A340-300

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

84 86 88 90 92 94 96 98 100

(x 1

000

Kg)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

(x

1000

Kg)


250

300

350

400

450

500

550

600

(x 1

000

lb)

110

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

280

AIR

CR

AF

T G

RO

SS

WE

IGH

T


35% MACMTOW − 276 500 kg

24% MAC

MLW

MZFW

TAKE OFF

LANDING

F_AC_070400_1_0080101_01_00


FIGURE-7-4-0-991-008-A01

7-4-0Page 8

Aug 01/19


**ON A/C A340-300

100

200

300

400

500

300

280

260

240

220

200

180

160

140

120

100

020406080100

120

140

160

180

200

220

240

300

400

500

600


AIR

CR

AF

T G

RO

SS

WE

IGH

T (

x 10

00 K

g)

(x 1

000

lb)

MA

IN G

EA

RS

CE

NT

ER

LIN

E G

EA

R

(x 1000 lb)

F_AC_070400_1_0080102_01_00


FIGURE-7-4-0-991-008-A01

7-4-0Page 9

Aug 01/19


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

**ON A/C A340-200 A340-300

Flexible Pavement Requirements - US Army Corps of Engineers Design Method

1. This section provides data about the flexible pavement requirements.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN for each typeof aircraft.They are calculated with the US Army Corps of Engineers Design Method.To find a flexible pavement thickness, you must know the Subgrade Strength (CBR), the annualdeparture level and the weight on one MLG.The line that shows 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).The procedure that follows is used to develop flexible pavement design curves:- With the scale for pavement thickness at the bottom and the scale for CBR at the top, a random

line is made to show 10 000 coverages,- A plot is then made of the incremental values of the weight on the MLG,- Annual departure lines are made based on the load lines of the weight on the MLG that is shown

on the graph.

Example, see FIGURE 7-5-0-991-005-A (Sheet 1), calculation of the thickness of the flexiblepavement for MLG:- An aircraft with a MRW of 254 400 kg (560 850 lb),- A ”CBR” value of 10,- An annual departure level of 3 000,- The load on one MLG of 80 000 kg (176 375 lb).The required flexible pavement thickness is 59.2 cm (23 in).

NOTE : The CG in the figure title is the CG used for ACN calculation.

7-5-0Page 1

Aug 01/19


**ON A/C A340-200

SUBGRADE STRENGTH − CBR

8060403020151063

8060403020151063

FLEXIBLE PAVEMENT THICKNESS

10 15 20 30 40 60 80 100 120 150 180(cm)

(in)

10 000 COVERAGES USEDFOR ACN CALCULATIONSALPHA FACTOR = 0.8

99 410 kg (219 150 lb)WEIGHT ON ONE MAIN LANDING GEAR

80 000 kg (176 375 lb)70 000 kg (154 325 lb)

(110 225 lb)(132 275 lb)60 000 kg

50 000 kg

MAXIMUM POSSIBLEMAIN LANDING GEARLOAD AT MAXIMUMRAMP WEIGHT ANDAFT CG

1400 x 530R23 OR 54 x 21−23 (bias) TIRES

TIRE PRESSURE CONSTANT AT 13 bar (189 psi)

1 2003 0006 00015 000

ANNUAL DEPARTURES*

*20 YEAR PAVEMENT LIFE25 000

F_AC_070500_1_0050101_01_01

Flexible Pavement RequirementsWV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)

FIGURE-7-5-0-991-005-A01

7-5-0Page 2

Aug 01/19


**ON A/C A340-200


8060403020151063

80604020151063


1400 x 530R23 OR 54 x 21−23 (bias) TIRES

TIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)

10 15 20 30 40 60 80 100 120 150 180(cm)

(in)




90 000 kg (198 425 lb)80 000 kg (176 375 lb)

(132 275 lb)(154 325 lb)70 000 kg

60 000 kg

30

1 2003 0006 00015 000

ANNUAL DEPARTURES*


F_AC_070500_1_0050102_01_01

Flexible Pavement RequirementsWV021, MRW 275 900 kg, CG 37% (Sheet 2 of 2)

FIGURE-7-5-0-991-005-A01

7-5-0Page 3

Aug 01/19


**ON A/C A340-300


8060403020151063

80604020151063


1400 x 530R23 OR 54 x 21−23 (bias) TIRES


10 15 20 30 40 60 80 100 120 150 180(cm)

(in)




90 000 kg (198 425 lb)80 000 kg (176 375 lb)

(132 275 lb)(154 325 lb)70 000 kg

60 000 kg

30

1 2003 0006 00015 000

ANNUAL DEPARTURES*


F_AC_070500_1_0060101_01_01

Flexible Pavement RequirementsWV000, MRW 254 400 kg, CG 38.18% (Sheet 1 of 2)

FIGURE-7-5-0-991-006-A01

7-5-0Page 4

Aug 01/19


**ON A/C A340-300


8060403020151063

80604020151063


1400 x 530R23 OR 54 x 21−23 (bias) TIRES


10 15 20 30 40 60 80 100 120 150 180(cm)

(in)




90 000 kg (198 425 lb)80 000 kg (176 375 lb)

(132 275 lb)(154 325 lb)70 000 kg

60 000 kg

30

1 2003 0006 00015 000

ANNUAL DEPARTURES*


F_AC_070500_1_0060102_01_01

Flexible Pavement RequirementsWV028, MRW 277 400 kg, CG 35% (Sheet 2 of 2)

FIGURE-7-5-0-991-006-A01

7-5-0Page 5

Aug 01/19


7-6-0 Flexible Pavement Requirements - LCN Conversion

**ON A/C A340-200 A340-300

Flexible Pavement Requirements - LCN Conversion

1. The Load Classification Number (LCN) curves are no longer provided in section 07-06-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983.For questions regarding the LCN system, contact Airbus.

7-6-0Page 1

Aug 01/19


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

**ON A/C A340-200 A340-300

Rigid Pavement Requirements - Portland Cement Association Design Method

1. This section provides data about the rigid pavement requirements for the PCA (Portland CementAssociation) design method.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN for each typeof aircraft.To find a rigid pavement thickness, you must know the Subgrade Modulus (k), the permitted workingstress and the weight on one MLG.The procedure that follows is used to develop rigid pavement design curves:- With the scale for pavement thickness on the left and the scale for permitted working stress on

the right, a random load line is made. This represents the MLG maximum weight to be shown,- A plot is then made of all values of the subgrade modulus (k values),- More load lines for the incremental values of the weight on the MLG are made based on the

curve for k = 80 MN/m3, which is already shown on the graph.

Example, see FIGURE 7-7-0-991-004-A (sheet 1), calculation of the thickness of the rigid pavementfor the MLG:- An aircraft with a MRW of 254 400 kg (560 850 lb),- A k value of 80 MN/m3 (300 lb/in3),- A permitted working stress of 35.15 kg/cm2 (500 lb/in2),- The load on one MLG is 80 000 kg (176 375 lb).The required rigid pavement thickness is 242 mm (10 in).


7-7-0Page 1

Aug 01/19


**ON A/C A340-200

1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 13 bar (189 psi)

100

200

300

400

500

600

700

800

90015

14

38

36

34

32

13

1230

28 11

26

24

22

10

9

20

18 7

8

(kg/

cm²)

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S

(lb/in

²)

RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S(c

m)

(in)

FOR LOADS LESS THAN MAXIMUM,EXACT.LINE AND ANY VALUES FOR K ARETHE MAXIMUM LOAD REFERENCETHE VALUES OBTAINED BY USINGNOTES:

THE CURVES ARE EXACT FOR K =80 MN/m³ BUT DEVIATE SLIGHTLYFOR ANY OTHER VALUES OF K.

PDILB" PORTLAND CEMENTPAVEMENT DESIGN − PROGRAMPROGRAM FOR AIRPORTPAVEMENTS" AND "COMPUTER"DESIGN OF CONCRETE AIRPORTREFERENCE:

ASSOCIATION.

8

13

18

23

28

33

38

43

48

53

58

63

60 000 kg (132 275 lb)70 000 kg (154 325 lb)80 000 kg (176 375 lb)99 410 kg (219 150 lb)LANDING GEARWEIGHT ON ONE MAIN

50 000 kg (110 225 lb)

RAMP WEIGHT AND AFT CGGEAR LOAD AT MAXIMUMMAXIMUM POSSIBLE MAIN

K = 150 MN/m³K = 80 MN/m³K = 40 MN/m³K = 20 MN/m³

F_AC_070700_1_0040101_01_00

Rigid Pavement RequirementsWV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)

FIGURE-7-7-0-991-004-A01

7-7-0Page 2

Aug 01/19


**ON A/C A340-200

1400x530R23 OR 54x21−23 (bias) TIRESTIRE PRESSURE CONSTANT AT 14.2 bar (206 psi)

100

200

300

400

500

600

700

800

90015

14

38

36

34

32

13

1230

28 11

26

24

22

10

9

20

18 7

8

RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S(c

m)

(in)




ASSOCIATION.

(kg/

cm²)

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S

(lb/in

²)

8

13

18

23

28

33

38

43

48

53

58

63




60 000 kg (132 275 lb)

F_AC_070700_1_0040201_01_00F_AC_070700_1_0040102_01_00

Rigid Pavement RequirementsWV021, MRW 275 900 kg, CG 37% (Sheet 2 of 2)

FIGURE-7-7-0-991-004-A01

7-7-0Page 3

Aug 01/19


**ON A/C A340-300


100

200

300

400

500

600

700

800

90015

14

38

36

34

32

13

1230

28 11

26

24

22

10

9

20

18 7

8

(kg/

cm²)

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S

(lb/in

²)

RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S(c

m)

(in)




ASSOCIATION.

8

13

18

23

28

33

38

43

48

53

58

63




60 000 kg (132 275 lb)

F_AC_070700_1_0050101_01_00

Rigid Pavement RequirementsWV000, MRW 254 400 kg, CG 38.18% (Sheet 1 of 2)

FIGURE-7-7-0-991-005-A01

7-7-0Page 4

Aug 01/19


**ON A/C A340-300


100

200

300

400

500

600

700

800

90015

14

38

36

34

32

13

1230

28 11

26

24

22

10

9

20

18 7

8

RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S(c

m)

(in)




ASSOCIATION.

(kg/

cm²)

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S

(lb/in

²)

8

13

18

23

28

33

38

43

48

53

58

63




60 000 kg (132 275 lb)

F_AC_070700_1_0050201_01_00F_AC_070700_1_0050102_01_00

Rigid Pavement RequirementsWV028, MRW 277 400 kg, CG 35% (Sheet 2 of 2)

FIGURE-7-7-0-991-005-A01

7-7-0Page 5

Aug 01/19


7-8-0 Rigid Pavement Requirements - LCN Conversion

**ON A/C A340-200 A340-300

Rigid Pavement Requirements - LCN Conversion

1. The Load Classification Number (LCN) curves are no longer provided in section 07-08-00 since theLCN system for reporting pavement strength is obsolete, having been replaced by the ICAOrecommended ACN/PCN system in 1983.For questions regarding the LCN system, contact Airbus.

7-8-0Page 1

Aug 01/19


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

**ON A/C A340-200 A340-300

Aircraft Classification Number - Flexible and Rigid Pavements

1. This section provides data about the Aircraft Classification Number (ACN) for an aircraft grossweight in relation to a subgrade strength value for flexible and rigid pavement.The MLG loading on pavement graphs are given for the weight variants that produce (at the MRWand maximum aft CG and standard tire pressure) the lowest ACN and the highest ACN for each typeof aircraft.To find the ACN of an aircraft on flexible and rigid pavement, you must know the aircraft grossweight and the subgrade strength.

NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref: ICAO Aerodrome Design Manual, Part 3, Chapter 1, Second Edition 1983).

Example, see FIGURE 7-9-0-991-014-A (sheet 1), calculation of the ACN for flexible pavement for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- An aircraft gross weight of 200 000 kg (440 925 lb),- A medium subgrade strength (code B).The ACN for flexible pavement is 42.

Example, see FIGURE 7-9-0-991-014-A (sheet 2), calculation of the ACN for rigid pavement for:- An aircraft with a MRW of 254 400 kg (560 850 lb),- An aircraft gross weight of 200 000 kg (440 925 lb),- A medium subgrade strength (code B).The ACN for rigid pavement is 40.

2. Aircraft Classification Number - ACN tableThe tables in FIGURE 7-9-0-991-004-A and FIGURE 7-9-0-991-005-A provide ACN data in tabularformat similar to the one used by ICAO in the ”Aerodrome Design Manual Part 3, Pavements -Edition 1983” for all the operational weight variants of the aircraft.As an approximation, use a linear interpolation in order to get the ACN at the required operatingweight using the following equation:- ACN = ACN min + (ACN max - ACN min) x (Operating weight - 130 000 kg)/(MRW - 130 000

kg)As an approximation, also use a linear interpolation in order to get the aircraft weight at thepavement PCN using the following equation:- Operating weight = 130 000 kg + (MRW - 130 000 kg) x (PCN - ACN min) / (ACN max - ACN

min)With ACN max = ACN calculated at the MRW in the table and with ACN min = ACN calculated at130 000 kg.

7-9-0Page 1

Aug 01/19



7-9-0Page 2

Aug 01/19


**ON A/C A340-200

AIRCRAFT TYPEALL UP

MASS (kg)

LOAD ONONE MAINGEAR LEG

(%)

TIREPRESSURE

(Mpa)

4528

ACN FOR

High150

RIGID PAVEMENTSUBGRADES − MN/m³

5228

Medium80

6232

Low40

7337

Ultral−low20

5028

ACN FOR

High15

FLEXIBLE PAVEMENTSUBGRADES − CBR

5429

Medium10

6232

Low6

8439

Ultral−low3

A340−200WV000

254 400130 000

39.146.1

1.30

WV001

WV002

WV021

A340−200

A340−200

A340−200

257 900130 000

39.146.1

1.32

260 900130 000

39.146.1

1.32

275 900130 000

39.246.0

1.42

4628

5328

6332

7437

5128

5529

6332

8639

4728

5428

6432

7637

5228

5629

6532

8739

5229

6029

7133

8338

5628

6129

7032

9539

F_AC_070900_1_0040101_01_00

Aircraft Classification NumberACN Table

FIGURE-7-9-0-991-004-A01

7-9-0Page 3

Aug 01/19


**ON A/C A340-200

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

AIRCRAFT CLASSIFICATION NUMBER (ACN)(x

100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3 ba

r (1

89 p

si)

1400

x530

R23

OR

54x

21−

23 (

bias

) T

IRE

SS

EE

SE

CT

ION

7−

4−0

CH

AP

TE

R 1

. SE

CO

ND

ED

ITIO

N 1

983.

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ALP

HA

FA

CT

OR

= 0

.8

D −

CB

R

3 (

ULT

RA

LO

W)

SU

BG

RA

DE

ST

RE

NG

TH

C −

CB

R

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

F_AC_070900_1_0140101_01_00

Aircraft Classification NumberFlexible Pavement - WV000, MRW 254 400 kg, CG 37.7% (Sheet 1 of 2)

FIGURE-7-9-0-991-014-A01

7-9-0Page 4

Aug 01/19


**ON A/C A340-200

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T


100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3 ba

r (1

89 p

si)

1400

x530

R23

OR

54x

21−

23 (

bias

) T

IRE

SS

EE

SE

CT

ION

7−

4−0

CH

AP

TE

R 1

. SE

CO

ND

ED

ITIO

N 1

983.

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

F_AC_070900_1_0140102_01_00

Aircraft Classification NumberRigid Pavement - WV000, MRW 254 400 kg, CG 37.7% (Sheet 2 of 2)

FIGURE-7-9-0-991-014-A01

7-9-0Page 5

Aug 01/19


**ON A/C A340-200

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T


100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

4.2

bar

(206

psi

)14

00x5

30R

23 O

R 5

4x21

−23

(bi

as)

TIR

ES

SE

E S

EC

TIO

N 7

−4−

0C

HA

PT

ER

1. S

EC

ON

D E

DIT

ION

198

3.IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3A

CN

WA

S D

ET

ER

MIN

ED

AS

RE

FE

RE

NC

ED

IN

ALP

HA

FA

CT

OR

= 0

.8

D −

CB

R

3 (

ULT

RA

LO

W)

SU

BG

RA

DE

ST

RE

NG

TH

C −

CB

R

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

F_AC_070900_1_0150101_01_00

Aircraft Classification NumberFlexible Pavement - WV021, MRW 275 900 kg, CG 37% (Sheet 1 of 2)

FIGURE-7-9-0-991-015-A01

7-9-0Page 6

Aug 01/19


**ON A/C A340-200

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T


100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

4.2

bar

(206

psi

)14

00x5

30R

23 O

R 5

4x21

−23

(bi

as)

TIR

ES

SE

E S

EC

TIO

N 7

−4−

0C

HA

PT

ER

1. S

EC

ON

D E

DIT

ION

198

3.IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3A

CN

WA

S D

ET

ER

MIN

ED

AS

RE

FE

RE

NC

ED

IN

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

F_AC_070900_1_0150102_01_00

Aircraft Classification NumberRigid Pavement - WV021, MRW 275 900 kg, CG 37% (Sheet 2 of 2)

FIGURE-7-9-0-991-015-A01

7-9-0Page 7

Aug 01/19


**ON A/C A340-300

AIRCRAFT TYPEALL UP

MASS (kg)

LOAD ONONE MAINGEAR LEG

(%)

TIREPRESSURE

(Mpa)

4628

ACN FOR

High150

RIGID PAVEMENTSUBGRADES − MN/m³

5328

Medium80

6332

Low40

7437

Ultral−low20

5128

ACN FOR

High15

FLEXIBLE PAVEMENTSUBGRADES − CBR

55

Medium10

63

Low6

8540

Ultral−low3

A340−300 254 400130 000

39.446.2

1.31WV000

260 900

257 900

260 900

271 900

275 900

262 900

275 900

260 900

260 900

275 900

271 900

277 400

260 900

275 900

275 900

277 400

277 400

275 900

39.446.2

1.32WV001

39.146.0

1.32WV002

39.446.2

1.32WV003

39.146.0

1.32WV004

39.646.2

1.42WV020

39.746.2

1.42WV021

39.546.2

1.42WV023

39.746.2

1.42WV024

39.5

46.21.42WV025

39.5

46.21.42WV025

39.746.2WV02639.646.2WV02739.446.0WV02839.546.2WV02939.746.2WV05039.746.2WV05139.446.0WV05239.446.0WV05339.746.2WV054

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

A340−300

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

130 000

257 900

1.42

1.42

1.42

1.42

1.42

1.42

1.42

1.42

1.42

(CG 38.02%)

(CG 38%)

28

28

28

28

29

29

29

29

29

29

29

29

29

29

29

29

29

29

29

47

47

47

47

52

53

49

53

48

48

53

52

53

48

53

53

53

53

53

54 64 75 52 56 64 87

54 64 76 52 56 65 8739

54 64 75 52 56 64 8740

54 64 76 52 56 65 8739

6029

7133

8338

56 61 70 9440

61 73 85 57 62 72 9740

57 67 79 54 58 66 9040

61 73 85 57 62 72 9740

29 33 38 28 29 32 40

29 33 38 28 29 32 40

56 67 78 53 57 66 88

56 67 78 53 57 66 88

61 73 85 57 62 72 9740

60 71 83 56 61 70 9440

61 72 84 57 62 71 9639

56 67 78 53 57 66 88

61 73 85 57 62 72 97

61 73 85 57 62 72 97

61 72 84 57 62 71 9639

61 72 84 57 62 71 9639

61 73 85 57 62 72 9740

28

28

28

28

29

29

29

29

29

29

29

29

29

29

29

29

32

32

32

32

33

33

33

33

33

33

33

33

33

33

33

33

37

37

37

37

38

38

38

38

38

38

38

38

38

38

38

38

28

28

28

28

28

28

28

28

28

28

28

28

28

28

28

28

28

29

29

29

29

29

29

29

29

29

29

29

29

29

29

29

29

29

29

32

32

32

32

32

32

32

32

32

32

32

32

32

32

32

32

32

32

40

40

40

40

F_AC_070900_1_0050101_01_00

Aircraft Classification NumberACN Table

FIGURE-7-9-0-991-005-A01

7-9-0Page 8

Aug 01/19


**ON A/C A340-300

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T


100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.1

bar

(190

psi

)14

00x5

30R

23 O

R 5

4x21

−23

(bi

as)

TIR

ES

SE

E S

EC

TIO

N 7

−4−

0C

HA

PT

ER

1. S

EC

ON

D E

DIT

ION

198

3.IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3A

CN

WA

S D

ET

ER

MIN

ED

AS

RE

FE

RE

NC

ED

IN

ALP

HA

FA

CT

OR

= 0

.8

D −

CB

R

3 (

ULT

RA

LO

W)

SU

BG

RA

DE

ST

RE

NG

TH

C −

CB

R

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

F_AC_070900_1_0160101_01_00

Aircraft Classification NumberFlexible Pavement - WV000, MRW 254 400 kg, CG 38.18% (Sheet 1 of 2)

FIGURE-7-9-0-991-016-A01

7-9-0Page 9

Aug 01/19


**ON A/C A340-300

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T


100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.1

bar

(190

psi

)14

00x5

30R

23 O

R 5

4x21

−23

(bi

as)

TIR

ES

SE

E S

EC

TIO

N 7

−4−

0C

HA

PT

ER

1. S

EC

ON

D E

DIT

ION

198

3.IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3A

CN

WA

S D

ET

ER

MIN

ED

AS

RE

FE

RE

NC

ED

IN

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

F_AC_070900_1_0160102_01_00

Aircraft Classification NumberRigid Pavement - WV000, MRW 254 400 kg, CG 38.18% (Sheet 2 of 2)

FIGURE-7-9-0-991-016-A01

7-9-0Page 10

Aug 01/19


**ON A/C A340-200

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T


100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

4.2

bar

(206

psi

)14

00x5

30R

23 O

R 5

4x21

−23

(bi

as)

TIR

ES

SE

E S

EC

TIO

N 7

−4−

0C

HA

PT

ER

1. S

EC

ON

D E

DIT

ION

198

3.IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3A

CN

WA

S D

ET

ER

MIN

ED

AS

RE

FE

RE

NC

ED

IN

ALP

HA

FA

CT

OR

= 0

.8

D −

CB

R

3 (

ULT

RA

LO

W)

SU

BG

RA

DE

ST

RE

NG

TH

C −

CB

R

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

F_AC_070900_1_0170101_01_00

Aircraft Classification NumberFlexible Pavement - WV028, MRW 277 400 kg, CG 35% (Sheet 1 of 2)

FIGURE-7-9-0-991-017-A01

7-9-0Page 11

Aug 01/19


**ON A/C A340-200

300

400

500

600

0102030405060708090100

110

120

100

150

200

250

300

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T


100

0 lb

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

4.2

bar

(206

psi

)14

00x5

30R

23 O

R 5

4x21

−23

(bi

as)

TIR

ES

SE

E S

EC

TIO

N 7

−4−

0C

HA

PT

ER

1. S

EC

ON

D E

DIT

ION

198

3.IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3A

CN

WA

S D

ET

ER

MIN

ED

AS

RE

FE

RE

NC

ED

IN

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

F_AC_070900_1_0170102_01_00

Aircraft Classification NumberRigid Pavement - WV028, MRW 277 400 kg, CG 35% (Sheet 2 of 2)

FIGURE-7-9-0-991-017-A01

7-9-0Page 12

Aug 01/19


SCALED DRAWINGS

8-0-0 SCALED DRAWINGS

**ON A/C A340-200 A340-300

Scaled Drawings

1. This section provides the scaled drawings.

NOTE : When printing this drawing, make sure to adjust for proper scaling.

8-0-0Page 1

Aug 01/19


**ON A/C A340-200

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

010

2030

4050

60F

EE

T

04

812

1620

ME

TE

RS

NOTE:WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.

F_AC_080000_1_0030101_01_01

Scaled DrawingFIGURE-8-0-0-991-003-A01

8-0-0Page 2

Aug 01/19


**ON A/C A340-300

NOTE:WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.

0 10 20 30 40 50 60FEET

0 4 8 12 16 20METERS

010

2030

4050

60F

EE

T

04

812

1620

ME

TE

RS

F_AC_080000_1_0030201_01_01

Scaled DrawingFIGURE-8-0-0-991-003-B01

8-0-0Page 3

Aug 01/19


AIRCRAFT RESCUE AND FIRE FIGHTING

10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING

**ON A/C A340-200 A340-300

Aircraft Rescue and Fire Fighting

1. Aircraft Rescue and Fire Fighting ChartsThis sections provides data related to aircraft rescue and fire fighting.The figures contained in this section are the figures that are in the Aircraft Rescue and Fire FightingCharts poster available for download on AIRBUSWorld and the Airbus website.

10-0-0Page 1

Aug 01/19


**ON A/C A340-200 A340-300

JAN

UA

RY

201

7

F_AC_100000_1_0270101_01_03

Front PageFIGURE-10-0-0-991-027-A01

10-0-0Page 2

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_100000_1_0280101_01_01

Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-028-A01

10-0-0Page 3

Aug 01/19


**ON A/C A340-200 A340-300

FR

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F_AC_100000_1_0690101_01_01

Batteries Location and AccessFIGURE-10-0-0-991-069-A01

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F_AC_100000_1_0290101_01_00

Crew Rest Compartments LocationFIGURE-10-0-0-991-029-A01

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**ON A/C A340-200 A340-300

F_AC_100000_1_0300101_01_00

Wheel/Brake OverheatWheel Safety Area (Sheet 1 of 2)

FIGURE-10-0-0-991-030-A01

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**ON A/C A340-200 A340-300

F_AC_100000_1_0300102_01_00

Wheel/Brake OverheatRecommendations (Sheet 2 of 2)

FIGURE-10-0-0-991-030-A01

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Aug 01/19


**ON A/C A340-200 A340-300

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F_AC_100000_1_0310101_01_01

Composite Materials LocationFIGURE-10-0-0-991-031-A01

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**ON A/C A340-200 A340-300

BA

AB

C

C

F_AC_100000_1_0320101_01_00

Ground Lock Safety DevicesFIGURE-10-0-0-991-032-A01

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Aug 01/19


**ON A/C A340-200 A340-300

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F_AC_100000_1_0330101_01_02

Emergency Evacuation DevicesFIGURE-10-0-0-991-033-A01

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F_AC_100000_1_0340101_01_00

Pax/Crew Doors and Emergency ExitsFIGURE-10-0-0-991-034-A01

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Aug 01/19


**ON A/C A340-200 A340-300

122C

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FW

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F_AC_100000_1_0350101_01_00

FWD and AFT Lower Deck Cargo DoorsFIGURE-10-0-0-991-035-A01

10-0-0Page 12

Aug 01/19


**ON A/C A340-200 A340-300

CA

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F_AC_100000_1_0360101_01_00

Control PanelsFIGURE-10-0-0-991-036-A01

10-0-0Page 13

Aug 01/19


**ON A/C A340-200 A340-300

A

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F_AC_100000_1_0370101_01_00

APU Compartment AccessFIGURE-10-0-0-991-037-A01

10-0-0Page 14

Aug 01/19


**ON A/C A340-200 A340-300

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F_AC_100000_1_0380101_01_01

Ground ClearancesFIGURE-10-0-0-991-038-A01

10-0-0Page 15

Aug 01/19


**ON A/C A340-200 A340-300

F_AC_100000_1_0390101_01_00

Structural Break-in PointsFIGURE-10-0-0-991-039-A01

10-0-0Page 16

Aug 01/19

Documents

A340-200/-300 AIRCRAFT CHARACTERISTICS AIRPORT AND ... · FIGURE Jacking for Maintenance - Load at the Aircraft Jacking Points Jan 01/14 Subject 2-14-1 Jacking of the Landing Gear