340-maintainence

@AIRBUSA340-200/-300

MAINTENANCE FACILITY PLANNING

MFP

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: Feb 29/92 Rev: Jan 01/12

@A340-200/-300MAINTENANCE FACILITY PLANNING

HIGHLIGHTS

Revision No. 20 - Jan 01/12

LOCATIONS CHGCODE

DESCRIPTIONS OF CHANGE

CHAPTER 1

Section 1-3

General Airplane Characteristics Data R GENERAL AIRPLANE CHARACTERISTICSPARAGRAPH UPDATEDOEW AND PAYLOAD DELETEDUSABLE VOLUME BASED ON LD3UPDATEDOEW AND PAYLOAD DELETEDUSABLE VOLUME BASED ON LD3UPDATED

Section 1-4

Zoning and Access R NOTE AMENDED

FIGURE Zoning and Access - Major Zones R

FIGURE Zoning and Access - Major Sub-Zones - Zones 100, 200, 300 and 800

R

FIGURE Zoning and Access - Major Sub-Zones - Zones 400, 500 and 600 (CFM56Series Engine)

R

Specific Areas Location N

FIGURE Specific Areas Location -Pressurized Areas

N ILLUSTRATION ADDED

FIGURE Specific Areas Location - SkydrolAreas


FIGURE Specific Areas Location -Vibration Areas


FIGURE Specific Areas Location - HotAreas


FIGURE Specific Areas Location - SwampAreas


FIGURE Specific Areas Location - Fueland Fuel Vapor Areas


FIGURE Specific Areas Location - FireAreas


HIGHLIGHTSPage 1

Jan 01/12


LOCATIONS CHGCODE

DESCRIPTIONS OF CHANGE

Section 1-10

Ground Clearances R NOTE AMENDED

FIGURE Ground Clearances R ILLUSTRATION REVISED




Section 1-17

Tail Contours R

FIGURE Tail Contours R

FIGURE Tail Contours R

FIGURE Tail Contours R ILLUSTRATION REVISED

FIGURE Tail Contours R ILLUSTRATION REVISED

CHAPTER 2

Section 2-5

Cargo Compartments Loading andUnloading

R CONTAINERIZED VOLUME UPDATEDCONTAINERIZED VOLUME UPDATED

CHAPTER 3

Section 3-6

Fuel System R

Section 3-9

De-Icing and Washing R

Section 3-10

Landing Gear R CROSS REFERENCED MANUAL(S)ADDED/REVISED/DELETED

HIGHLIGHTSPage 2

Jan 01/12


LIST OF EFFECTIVE CONTENT

Revision No. 20 - Jan 01/12

CONTENT CHGCODE

LAST REVISIONDATE

CHAPTER 0

Section 0-1

Introduction May 01/07

Section 0-2

Alphabetical Index May 01/07

Section 0-3

Section Index May 01/07

CHAPTER 1

Section 1-1

Airplane Overall Dimensions and Outline Basic Reference May 01/07

FIGURE Airplane Overall Dimensions and Outline Basic ReferenceDrawing - Model 300

May 01/07

FIGURE Airplane Overall Dimensions and Outline Basic ReferenceDrawing - Model 200

May 01/07

Section 1-2

Airplane Dimensions May 01/07

FIGURE Airplane Dimensions - Model 300 May 01/07




FIGURE Airplane Dimensions - CFM56-5-C2 Inboard Engine May 01/07

FIGURE Airplane Dimensions - CFM56-5-C2 Outboard Engine May 01/07

Section 1-3

General Airplane Characteristics Data R Jan 01/12

Section 1-4

Zoning and Access R Jan 01/12

FIGURE Zoning and Access - Major Zones R Jan 01/12

L.E.C.Page 1

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Zoning and Access - Major Sub-Zones - Zones 100, 200, 300and 800

R Jan 01/12

FIGURE Zoning and Access - Major Sub-Zones - Zones 400, 500 and600 (CFM56 Series Engine)

R Jan 01/12

Specific Areas Location N Jan 01/12

FIGURE Specific Areas Location - Pressurized Areas N Jan 01/12

FIGURE Specific Areas Location - Skydrol Areas N Jan 01/12

FIGURE Specific Areas Location - Vibration Areas N Jan 01/12

FIGURE Specific Areas Location - Hot Areas N Jan 01/12

FIGURE Specific Areas Location - Swamp Areas N Jan 01/12

FIGURE Specific Areas Location - Fuel and Fuel Vapor Areas N Jan 01/12

FIGURE Specific Areas Location - Fire Areas N Jan 01/12

Section 1-5

Fuselage Frames / Stations May 01/07

FIGURE Fuselage Frames / Stations - Nose Section (FR 1 to FR 37) May 01/07

FIGURE Fuselage Frames / Stations - Center Section (FR 37.1 to FR58)

May 01/07

FIGURE Fuselage Frames / Stations - Rear Section (FR 58 to FR106A)

May 01/07

FIGURE Fuselage Frames / Stations - Center Section (FR 38 to FR58)

May 01/07

FIGURE Fuselage Frames / Stations - Rear Section (FR 58 to FR106A)

May 01/07

Section 1-6

Wing Ribs / Stations May 01/07

FIGURE Wing Ribs / Stations May 01/07

Section 1-7

Fuselage Cross-sections May 01/07

FIGURE Fuselage Cross-section - FRAME 1 - STA7662.5 May 01/07



L.E.C.Page 2

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE










FIGURE Fuselage Cross-section - FRAME 13B - STA11612.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 14 SUP - STA11837.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 14B SUP - STA12079.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 15 INF - STA12115.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 15A INF - STA12359.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 15B SUP - STA12563.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 15C SUP - STA12805.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 16A SUP - STA13047.15 May 01/07

FIGURE Fuselage Cross-section - FRAME 16 INF - STA12603.5 May 01/07

FIGURE Fuselage Cross-section - FRAME 16A INF - STA12849.5 May 01/07











L.E.C.Page 3

Jan 01/12


CONTENT CHGCODE

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L.E.C.Page 4

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE








Section 1-8

Center of Gravity Limits May 01/07

FIGURE Center of Gravity Limits - Model 253 T May 01/07







Section 1-9

Airplane Attitude Jan 01/11

FIGURE Airplane Attitude - NLG Shock Absorber Deflections Jan 01/11

FIGURE Airplane Attitude - NLG Tire Deflections Jan 01/11

FIGURE Airplane Attitude - NLG Shock Absorber Deflections Jan 01/11

FIGURE Airplane Attitude - NLG Tire Deflections Jan 01/11

FIGURE Airplane Attitude - NLG (2 Stage) Shock AbsorberDeflections

Jan 01/11

FIGURE Airplane Attitude - NLG (2 Stage) Tire Deflections Jan 01/11

FIGURE Airplane Attitude - MLG Shock Absorber Deflections Jan 01/11

FIGURE Airplane Attitude - MLG Tire Deflections Jan 01/11



L.E.C.Page 5

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE



FIGURE Airplane Attitude - Correction Factors for a Combination ofDeflated shock Absorbers and Tires

Jan 01/11

FIGURE Airplane Attitude - Wing Deflections Jan 01/11

FIGURE Airplane Attitude - Wing Deflections Jan 01/11

Section 1-10

Ground Clearances R Jan 01/12

FIGURE Ground Clearances R Jan 01/12




FIGURE Ground Clearances - Main and Center Landing Gear Doors May 01/07

FIGURE Ground Clearances - Door Clearances - APU and NoseLanding Gear Doors

May 01/07

FIGURE Ground Clearances - Door Clearances - APU and NoseLanding Gear Doors

May 01/07

FIGURE Ground Clearances - Ailerons UP May 01/07

FIGURE Ground Clearances - Ailerons UP May 01/07

FIGURE Ground Clearances - Ailerons Down May 01/07

FIGURE Ground Clearances - Ailerons Down May 01/07

FIGURE Ground Clearances - Spoilers 1 to 6 Extended May 01/07



FIGURE Ground Clearances - Leading Edge Slats Extended May 01/07

FIGURE Ground Clearances - Leading Edge Slats Extended May 01/07

FIGURE Ground Clearances - Inner and Outer Flaps Extended May 01/07



FIGURE Ground Clearances - Flap Tracks Retracted May 01/07

L.E.C.Page 6

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Ground Clearances - Flap Tracks Retracted May 01/07

FIGURE Ground Clearances - Flap Tracks Extended May 01/07

FIGURE Ground Clearances - Flap Tracks Extended May 01/07

FIGURE Ground Clearances - Wing Tip and Winglet May 01/07

FIGURE Ground Clearances - Wing Tip and Winglet May 01/07

Section 1-11

Door Clearances May 01/07

FIGURE Door Clearances - Forward Passenger/Crew Doors May 01/07

FIGURE Door Clearances - Mid Passenger/Crew Doors May 01/07

FIGURE Door Clearances - Emergency Exits May 01/07

FIGURE Door Clearances - Aft Passenger/Crew Doors May 01/07

FIGURE Door Clearances - Forward Cargo Compartment Doors May 01/07

FIGURE Door Clearances - Aft Cargo Compartment Doors May 01/07

FIGURE Door Clearances - Bulk Cargo Compartment Doors May 01/07

Section 1-12

Interior Arrangement May 01/07

FIGURE Interior Arrangements - Interior Arrangement Passengers May 01/07



FIGURE Passenger Compartment Cross-Section - Typical 6 -- AbreastSeat Configuration First Class

May 01/07

FIGURE Passenger Compartment Cross-Section - Typical 6 -- AbreastSeat Configuration Business Class

May 01/07

FIGURE Passenger Compartment Cross-Section - Typical 8 -- AbreastSeat Configuration Economy Class

May 01/07

Section 1-13

Radome May 01/07

FIGURE Radome May 01/07

Section 1-14

Nose Contours May 01/07

L.E.C.Page 7

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Nose Contours - Level Positions May 01/07

FIGURE Nose Contours May 01/07

FIGURE Nose Contours May 01/07

Section 1-15

Vertical Stabilizer Contours May 01/07

FIGURE Vertical Stabilizer - Level Position May 01/07

FIGURE Vertical Stabilizer - Contours May 01/07

Section 1-16

Horizontal Stabilizer Contours May 01/07

FIGURE Horizontal Stabilizer - Contours May 01/07

FIGURE Horizontal Stabilizer - Level Positions May 01/07

Section 1-17

Tail Contours R Jan 01/12

FIGURE Tail Contours R Jan 01/12




Section 1-18

Wing Profiles Jan 01/11

FIGURE Wing Profile - Locations Jan 01/11

FIGURE Wing Profile - Locations Jan 01/11

CHAPTER 2

Section 2-1

Airplane Servicing Arrangement Jan 01/10

FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(Open Apron)

Jan 01/10

FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(Open Apron)

Jan 01/10

FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(gate area)

Jan 01/10

L.E.C.Page 8

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Airplane Servicing Arrangements - Typical Ramp Layout(gate area)

Jan 01/10

Section 2-2

Terminal Operations Jan 01/10

FIGURE Full Servicing Turn Round Charts - Turn Round Time 59min.

Jan 01/10

FIGURE Full Servicing Turn Round Charts - Turn Round Time 70min.

Jan 01/10

FIGURE Transit Turn Round Charts - Turn Round Time 39 min Jan 01/10

FIGURE Transit Turn Round Charts - Turn Round Time 43 min Jan 01/10

Section 2-3

Ground Service Connections and Locations May 01/07

FIGURE Ground Service Connections - Ground Service ConnectionsLayout

May 01/07

FIGURE Ground Service Connections - Ground Service ConnectionsLayout

May 01/07

Grounding Points May 01/07

FIGURE Ground Service Connections - Grounding Points May 01/07

FIGURE Ground Service Connections - Grounding Points May 01/07

Hydraulic System May 01/07

Electrical System May 01/07

Oxygen System May 01/07

Fuel System Jan 01/11

Pneumatic System May 01/07

Potable Water System May 01/07

Oil System May 01/07

FIGURE Ground Service Connections - Engine Oil Tank - CFM56-5C2series engine

May 01/07

FIGURE Ground Service Connections - IDG Oil Tank - CFM56-5C2series engine

May 01/07

APU Oil System Jan 01/10

L.E.C.Page 9

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Ground Service Connections - APU Oil Tank Jan 01/10

Vacuum Toilet System May 01/07

Cabin and Service Interphone Jan 01/11

FIGURE Cabin and Service Interphone - Location of ServiceInterphone Jacks

Jan 01/11

FIGURE Cabin and Service Interphone - Service InterphoneComponent Location

Jan 01/11

Section 2-4

Ground Service Connections - Capacities and Flow May 01/07

FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature -40C (-40F) -- CFM56-5C2 (C3-C4) series engine

May 01/07

FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature +15C (59F) -- CFM56-5C2 (C3-C4) series engine

May 01/07

FIGURE Engine Starting Pneumatic Requirements - AmbientTemperature +55C (+131F) -- CFM56-5C2 (C3-C4) series engine

May 01/07

FIGURE Ground Pneumatic Power Requirements - Heating May 01/07

FIGURE Ground Pneumatic Power Requirements - Cooling May 01/07

FIGURE Preconditioned Airflow Requirements May 01/07

Section 2-5

Cargo Compartments Loading and Unloading R Jan 01/12

FIGURE Lower Deck Compartments - Cargo Flexibility May 01/07

FIGURE Lower Deck Compartments - Cargo Flexibility -- LoadingCombinations

May 01/07

Section 2-6

Galleys - General Information May 01/07

FIGURE Galleys - General Location of the Galleys May 01/07

FIGURE Galleys - General Layout - Galley N 1 May 01/07

FIGURE Galleys - General Layout - Galleys N 2/3 May 01/07

FIGURE Galleys - General Layout - Galleys N 4 and 5 (Fixed) May 01/07

Section 2-7

Galleys - Loading and Unloading May 01/07

L.E.C.Page 10

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

Section 2-8

Ground Maneuvering Jan 01/11

FIGURE Ground Maneuvering - Turning Radii Jan 01/11



FIGURE Ground Maneuvering - Minimum Turning Radii Jan 01/11

FIGURE Ground Maneuvering - Minimum Turning Radii Jan 01/11

FIGURE 135 Turn - Runway to Taxiway - Judgemental OversteerMethod

Jan 01/11

FIGURE 135 Turn - Runway to Taxiway - Cockpit Over CenterlineMethod

Jan 01/11


Jan 01/11


Jan 01/11


Jan 01/11


Jan 01/11


Jan 01/11


Jan 01/11

FIGURE Ground Maneuvering - 180 Turn on a 202 ft Wide Runway Jan 01/11




FIGURE 135 turn - Taxiway to Taxiway - Judgemental OversteerMethod

Jan 01/11

FIGURE 135 turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod

Jan 01/11

FIGURE 135 turn - Taxiway to Taxiway - Judgemental OversteerMethod

Jan 01/11

L.E.C.Page 11

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE 135 turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod

Jan 01/11

FIGURE 90 Turn - Taxiway to Taxiway - Judgemental OversteerMethod

Jan 01/11

FIGURE 90 Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod

Jan 01/11

FIGURE 90 Turn - Taxiway to Taxiway - Judgemental OversteerMethod

Jan 01/11

FIGURE 90 Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod

Jan 01/11

FIGURE Ground Maneuvering - Runway Holding Bay (Apron) Jan 01/11

Section 2-9

Airplane Parking May 01/07

FIGURE Airplane Parking - Steering Geometry May 01/07


FIGURE Airplane Parking - Minimum Parking Space Requirements May 01/07



FIGURE Airplane Parking - Minimum Parking Space Requirements May 01/07

Section 2-10

Towing Jan 01/10

FIGURE Towing - Ground Towing Requirements Jan 01/10

FIGURE Towing - Typical tow bar configuration 1 Jan 01/10

FIGURE Towing - Typical tow bar configuration 2 Jan 01/10

FIGURE Towing - Maximum Extension of the NLG Shock Absorber Jan 01/10

Section 2-11

Operating Conditions May 01/07

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

May 01/07

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

May 01/07

L.E.C.Page 12

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Engine Exhaust Velocities Contours - Breakaway Power -CFM56-5C series engine

May 01/07

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

May 01/07

FIGURE Engine Exhaust Velocities Contours - Takeoff Power -CFM56-5C series engine

May 01/07

FIGURE Engine Exhaust Temperatures Contours - Takeoff Power -CFM56-5C series engine

May 01/07

FIGURE Airport and Community Noise - Noise Data - CFM56-5Cseries engine

May 01/07

FIGURE Danger Areas of Engines - Ground Idle Power - CFM56-5Cseries engine

May 01/07

FIGURE Danger Areas of Engines - Breakaway Power - CFM56-5Cseries engine

May 01/07

FIGURE Danger Areas of Engines - Takeoff Power - CFM56-5C seriesengine

May 01/07

FIGURE APU - Exhaust Velocities and Temperatures - GARRETTGTCP 331-350

May 01/07

CHAPTER 3

Section 3-1

Air Conditioning and Pneumatic May 01/07

FIGURE Air Conditioning - Schematic May 01/07

FIGURE Air Conditioning - General Layout May 01/07

FIGURE Air Conditioning - Air Conditioning Pack May 01/07

Section 3-2

Communications, Navigation, Information Systems and Recording May 01/07

Section 3-3

Electrical Power May 01/07

FIGURE Electrical Power - General Block Diagram May 01/07

FIGURE Electrical Power - AC Electrical Load Distribution -- General May 01/07

FIGURE Electrical Power - AC Emergency Generation -- BlockDiagram

May 01/07

L.E.C.Page 13

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Electrical Power - DC Electrical Load Distribution -- General May 01/07

FIGURE Electrical Power - External Power Configuration -- BlockDiagram

May 01/07

FIGURE Electrical Power - Electrical Power -- Component Location May 01/07

Section 3-4

Fire Protection May 01/07

Section 3-5

Flight Controls May 01/07

FIGURE Flight Controls - Control Surface Travel -- Typical Sections May 01/07

FIGURE Flight Controls - Control Surface Travel -- Inner Aileron andOuter Aileron

May 01/07

FIGURE Flight Controls - Control Surface Travel -- Spoilers 1--6 May 01/07

FIGURE Flight Controls - Control Surface Travel -- Sections 10--18 May 01/07

FIGURE Flight Controls - Control Surface Travel -- Slat/Section 1--8 May 01/07

FIGURE Flight Controls - Control Surface Travel -- Slats 1--7 May 01/07

FIGURE Flight Controls - Control Surface Travel - Inner Flap andOuter Flap

May 01/07

FIGURE Flight Controls - Control Surface Travel TrimmableHorizontal Stabilizer and Elevator

May 01/07

FIGURE Flight Controls - Control Surface Travel TrimmableHorizontal Stabilizer and Elevator

May 01/07

FIGURE Flight Controls - Control Surface Travel -- Rudder May 01/07

FIGURE Flight Controls - Control Surface Travel -- Rudder May 01/07

Section 3-6

Fuel System R Jan 01/12

FIGURE Fuel System - Fuel and Vent Surge Tanks May 01/07

FIGURE Fuel System - Wing and Trim Tank Venting System May 01/07

FIGURE Fuel System - Fuel Feed, Transfer and Crossfeed System --Models with no ACT

May 01/07

FIGURE Fuel System - Fuel Feed, Transfer and Crossfeed System --Models with ACT Option

Jan 01/11

L.E.C.Page 14

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Fuel System - Fuel Feed, Transfer and Crossfeed System --Models with ACT Option

Jan 01/11

FIGURE Fuel System - Fuel Feed, Transfer and Crossfeed System May 01/07

FIGURE Fuel System - Refuel/Defuel Control Panel (990VU) --Models with no ACTs

May 01/07

FIGURE Fuel System - Refuel/Defuel Control Panel (990VU) -- Modelwith ACT Option

May 01/07

FIGURE Fuel System - Refuel/Defuel Coupling May 01/07

Section 3-7

Hydraulic Power May 01/07

FIGURE Hydraulic Power - Symbols May 01/07

FIGURE Hydraulic Power - General May 01/07

FIGURE Hydraulic Power - Green System May 01/07

FIGURE Hydraulic Power - Blue System May 01/07

FIGURE Hydraulic Power - Yellow System May 01/07

FIGURE Hydraulic Power - Distribution May 01/07

Section 3-8

Ice and Rain Protection May 01/07

FIGURE Ice and Rain Protection - Wing Ice and Rain Protection May 01/07

Section 3-9

De-Icing and Washing R Jan 01/12

FIGURE De-Icing and Washing - Mobile Equipment for Airplane May 01/07

Section 3-10

Landing Gear R Jan 01/12

FIGURE Landing Gear - Footprint May 01/07

FIGURE Landing Gear - Footprint May 01/07

FIGURE Landing Gear - Main Landing Gear May 01/07

FIGURE Landing Gear - Nose Landing Gear May 01/07

FIGURE Landing Gear - Center Landing Gear May 01/07

FIGURE Landing Gear - Nose Wheel Gear Steering Disconnection Box May 01/07

L.E.C.Page 15

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Landing Gear - Main Landing Gear Dimensions and Locationof Servicing Points

May 01/07

FIGURE Landing Gear - Nose Landing Gear Dimensions and Locationof Servicing Points

May 01/07

FIGURE Landing Gear - Center Landing Gear Dimensions andLocation of Servicing Points

May 01/07

FIGURE Landing Gear - Wheel Brake Pressure System Schematic May 01/07

Section 3-11

Auto flight May 01/07

Section 3-12

Auxiliary Power Unit May 01/07

FIGURE Auxiliary Power Unit - Access Doors May 01/07

FIGURE Auxiliary Power Unit - Access Doors May 01/07

FIGURE Auxiliary Power Unit - General Layout May 01/07

FIGURE Auxiliary Power Unit - General Layout May 01/07

Section 3-13

Leveling, Symmetry and Alignment May 01/07

FIGURE Leveling, Symmetry and Alignment - Quick Leveling --Location of Attitude Monitor

May 01/07

FIGURE Leveling, Symmetry and Alignment - Precision Leveling --Location of references Points

May 01/07

FIGURE Leveling, Symmetry and Alignment - Lateral andLongitudinal Leveling

May 01/07

Section 3-14

Airplane Maintenance Jacking Jan 01/10

FIGURE Airplane Maintenance Jacking - Location of auxiliary JackingPoints

May 01/07

FIGURE Airplane Maintenance Jacking - Location of auxiliary JackingPoints

May 01/07

FIGURE Airplane Maintenance Jacking - Landing Gear and JackingPoint Location

Jan 01/10

FIGURE Airplane Maintenance Jacking - Landing Gear and JackingPoint Location

Jan 01/10

L.E.C.Page 16

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Airplane Maintenance Jacking - Jacking Design Jan 01/10

FIGURE Airplane Maintenance Jacking - Jacking Design Jan 01/10

FIGURE Airplane Maintenance Jacking - Forward Jacking Point A,Underwing Jacking Points B, Safety Stay Point C

Jan 01/10

FIGURE Airplane Maintenance Jacking - Load at the Aircraft JackingPoints

Jan 01/10

FIGURE Airplane Maintenance Jacking - Load at the Aircraft JackingPoints

Jan 01/10

Section 3-15

Landing Gear Jacking for wheel change Jan 01/11

FIGURE Landing Gear Jacking for wheel change - MLG Jacking PointHeights

Jan 01/11


Jan 01/11


Jan 01/11

FIGURE Landing Gear Jacking for wheel change - NLG Jacking PointHeights

Jan 01/11

FIGURE Landing Gear Jacking for wheel change - CLG Jacking PointHeights

Jan 01/11

FIGURE Landing Gear Jacking for wheel change - MLG Jacking PointLoads

Jan 01/11

FIGURE Landing Gear Jacking for wheel change - MLG Jacking PointLoads

Jan 01/11

FIGURE Landing Gear Jacking for wheel change - NLG Jacking PointLoads

Jan 01/11

FIGURE Landing Gear Jacking for wheel change - NLG Jacking PointLoads

Jan 01/11

FIGURE Landing Gear Jacking for wheel change - CLG Jacking PointLoads

Jan 01/11

FIGURE Landing Gear Jacking for wheel change - CLG Jacking PointLoads

Jan 01/11

Section 3-16

Exterior Lighting Jan 01/11

L.E.C.Page 17

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Exterior Lighting - Exterior Lighting Available in Flight Jan 01/11

FIGURE Exterior Lighting - Exterior Lighting Available in Flight Jan 01/11

FIGURE Exterior Lighting - Exterior Lighting for Ground Use Jan 01/11

Section 3-17

Power Plant Handling May 01/07

FIGURE Power Plant Handling - Major dimensions -- CFM 56-5Cseries engine

May 01/07

FIGURE Power Plant Handling - Major dimensions -- CFM 56-5Cseries engine

May 01/07

FIGURE Power Plant Handling - Fan Cowl -- CFM 56-5C seriesengine

May 01/07

FIGURE Power Plant Handling - Fan Cowl -- CFM 56-5C seriesengine

May 01/07

FIGURE Thrust Reverser Cowls -- Inboard Engine - AFT LookingFWD -- CFM 56-5C series engine

May 01/07

FIGURE Thrust Reverser Cowls -- Outboard Engine - AFT LookingFWD -- CFM 56-5C series engine

May 01/07

Section 3-18

Component Weights May 01/07

Section 3-19

Component Handling May 01/07

FIGURE Component Handling - Identification of the Various WingControl Surfaces

May 01/07

FIGURE Component Handling - Inboard Flap -- C.G. Location May 01/07

FIGURE Component Handling - Outboard Flap -- C.G. Location May 01/07

FIGURE Component Handling - Spoilers 1, 3, 4 and 5 -- C.G. Location May 01/07

FIGURE Component Handling - Spoiler 2 -- C.G. Location May 01/07

FIGURE Component Handling - Spoiler 6 -- C.G. Location May 01/07

FIGURE Component Handling - Slat 1 -- C.G. Location May 01/07



L.E.C.Page 18

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE





FIGURE Component Handling - Horizontal Stabilizer -- C.G. Location May 01/07

FIGURE Component Handling - Vertical Stabilizer and Rudder -- C.G.Location

May 01/07

FIGURE Component Handling - Tail Cone -- C.G. Location May 01/07

FIGURE Component Handling - Tail Cone -- C.G. Location May 01/07

Section 3-20

Suggested Hangar Arrangement May 01/07

FIGURE Suggested Hangar Arrangement - Nose--in Position May 01/07

FIGURE Suggested Hangar Arrangement - Nose--in Position May 01/07

FIGURE Suggested Hangar Arrangement - Tail--in Position May 01/07

FIGURE Suggested Hangar Arrangement - Tail--in Position May 01/07

Section 3-21

Landing Gear Maintenance Pits May 01/07

FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes May 01/07




Section 3-22

Recommended Workstands May 01/07

FIGURE Recommended Workstands - General Arrangement May 01/07

FIGURE Recommended Workstands - Cargo Compartment Platform May 01/07

FIGURE Recommended Workstands - Engine Platform May 01/07

FIGURE Recommended Workstands - MLG Compartment Platform May 01/07

FIGURE Recommended Workstands - Rear Fuselage Platform May 01/07

FIGURE Recommended Workstands - Hydraulic Platform-Giraffe May 01/07

L.E.C.Page 19

Jan 01/12


CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Recommended Workstands - Pax Door PlatformFWD/MID/AFT

May 01/07

FIGURE Recommended Workstands - Fuselage Platform May 01/07

FIGURE Recommended Workstands - Inner Wing Platform May 01/07

FIGURE Recommended Workstands - Outer Wing Platform May 01/07

CHAPTER 4

Section 4-1

Air Conditioning and Pneumatic May 01/07

Section 4-2

Electrical Power May 01/07

Section 4-3

Fuel System Components May 01/07

Section 4-4

Hydraulic Power May 01/07

Section 4-5

Flight Controls May 01/07

CHAPTER 5

Section 5-1

Ground Support Vendors Information May 01/07

L.E.C.Page 20

Jan 01/12


TABLE OF CONTENTS

0 Introduction

0-1 Introduction

0-2 Alphabetical Index

0-3 Section Index

1 General Information

1-1 Airplane Overall Dimensions and Outline Basic Reference Drawing

1-2 Airplane Dimensions

1-3 General Airplane Characteristics

1-4 Zoning and Access

1-5 Fuselage Frames / Stations

1-6 Wing Ribs / Stations

1-7 Fuselage Cross-sections

1-8 Center of Gravity Limits

1-9 Airplane Attitude

1-10 Ground Clearances

1-11 Door Clearances

1-12 Interior Arrangement

1-13 Radome Travel

1-14 Nose Contours

1-15 Vertical Stabilizer Contours

1-16 Horizontal Stabilizer Contours

1-17 Tail Contours

1-18 Wing Profiles

2 Terminal and Ramp

2-1 Airplane Servicing Arrangements

2-2 Terminal Operations

2-3 Ground Service Connections and Locations

2-4 Ground Service Connections - Capacities and Flow

2-5 Cargo Compartments Loading and Unloading

2-6 Galleys - General Information

2-7 Galleys - Loading and Unloading

2-8 Ground Maneuvering

2-9 Airplane Parking

T.O.C.Page 1

Jan 01/12


2-10 Towing

2-11 Operating Conditions

3 Line Maintenance and Hangar

3-1 Air Conditioning and Pneumatic

3-2 Communications, Navigation, Information Systems and Recording

3-3 Electrical Power

3-4 Fire Protection

3-5 Flight Controls

3-6 Fuel System

3-7 Hydraulic Power

3-8 Ice and Rain Protection

3-9 De-Icing and Washing

3-10 Landing Gear

3-11 Auto flight

3-12 Auxiliary Power Unit

3-13 Leveling, Symmetry and Alignment

3-14 Airplane Maintenance Jacking

3-15 Landing Gear Jacking for wheel change

3-16 Exterior Lighting

3-17 Power Plant Handling

3-18 Component Weights

3-19 Component Handling

3-20 Suggested Hangar Arrangement

3-21 Landing Gear Maintenance Pits

3-22 Recommended Workstands

4 Component Repair/Overhaul and Functional Test


4-2 Electrical Power

4-3 Fuel System Components

4-4 Hydraulic Power

4-5 Flight Controls

5 Appendix

5-1 Ground Support Vendors Information

T.O.C.Page 2

Jan 01/12


Introduction

0-1 Introduction

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

Introduction

1. PURPOSE

The A340-200/-300 MAINTENANCE FACILITY PLANNING (MFP) manual is issued for theA340-200/-300 basic versions to provide the necessary data needed by airport operators and airlinesfor the planning of airport facilities.

2. CORRESPONDENCE

Correspondence concerning this publication should be directed to :

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

3. CONTENTS

The manual comprises 5 sections, with a List of Effective Pages (LEP) and a Table Of Contents(TOC) at the beginning of each section.

Section 0 : INTRODUCTION

Section 1 : GENERAL INFORMATION

This section contains general dimensional and other basic data concerning the A340-200/-300 aircraftto help operators to assess their needs for terminal and hangar facilities and maintenance docks.

It covers :- aircraft dimensions,- zoning and access; fuselage frame and wing stations,- cross-sections and profile for fuselage, wings and tail,- ground clearances and travel limits of movable parts,- aircraft center of gravity limits and aircraft attitude.

0-1Page 1

Jan 01/12


Section 2 : TERMINAL AND RAMP

This section contains the ground equipment required for the aircraft servicing at turnaround stations.

It covers :- suggested servicing arrangement around the aircraft,- estimated servicing times for turnaround,- ground service connections and locations with their characteristics,- cargo compartment loading and unloading,- ground maneuvering capabilities and characteristics.

Section 3 : LINE MAINTENANCE AND HANGAR

This section outlines the technical data and requirements related to maintenance functions, regardlessof whether these would be performed inside or outside the hangar or on the ramp.

The data contained in this part of the manual is supplied only to enable airlines to proceed with theirpreliminary design and planning. Maintenance procedures are contained in the Aircraft MaintenanceManual (AMM).

It includes :- description of the main aircraft systems, shows their general layout or schematic and gives their

functional testing,- the aircraft jacking, levelling and the landing gear lifting,- the main removable components weight and handling,- the suggested hangar arrangement with the corresponding workstands.

Section 4 : COMPONENT REPAIR/OVERHAUL AND FUNCTIONAL TEST

This section contains the minimum technical data and requirements relative to aircraft componentsrepair/overhaul and functional testing for each of the main aircraft systems.

The data contained in this part of the manual is supplied only to enable airlines to proceed with theirpreliminary design and planning. Overhaul procedures are contained in the OverhaulManual/Component Maintenance Manual (CMM)

Section 5 : APPENDIX

The Vendor information.

0-1Page 2

Jan 01/12


0-2 Alphabetical Index

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

Alphabetical Index

1. Alphabetical index

Subject Section

Air Conditioning and Pneumatic 3-1

Air Conditioning and Pneumatic 4-1

Airplane Attitude 1-9

Airplane Dimensions 1-2

Airplane Maintenance Jacking 3-14

Airplane Overall Dimensions and Outline Basic Reference Drawing 1-1

Airplane Parking 2-9

Airplane Servicing Arrangement 2-1

Auto flight 3-11

Auxiliary Power Unit 3-12

Cargo Compartments - Loading and Unloading 2-5

Center of Gravity Limits 1-8

Communications, Navigation, Information Systems and Recording 3-2

Component Handling 3-19

Component Weights 3-18

De-Icing and Washing 3-9

Door Clearances 1-11Electrical Power 3-3Electrical Power 4-2Exterior Lighting 3-16

Fire Protection 3-4Flight Controls 3-5

Flight Controls 4-5

Fuel System 3-6

Fuel System Components 4-3

Fuselage Cross-sections 1-7

Fuselage Frames/Stations 1-5

Galleys - General Information 2-6

Galleys - Loading and Unloading 2-7

General Airplane Characteristics 1-3

0-2Page 1

Jan 01/12


Subject Section

Ground Clearances 1-10Ground Maneuvering 2-8

Ground Service Connections and Locations 2-3Ground Service Connections - Capacities and Flow 2-4

Ground Support Vendors Information 5-1

Horizontal Stabilizer Contours 1-16Hydraulic Power 4-4

Hydraulic Power 3-7

Ice and Rain Protection 3-8Interior Arrangement 1-12

Introduction 0-1Landing Gear 3-10

Landing Gear Jacking 3-15

Landing Gear Maintenance Pits 3-21

Leveling, Symmetry and Alignment 3-13

Nose Contours 1-14Operating Conditions 2-11

Power Plant Handling 3-17

Radome 1-13Recommended Workstands 3-22Section Index 0-3Suggested Hangar Arrangement 3-20

Tail Contours 1-17Towing 2-10

Turn around Stations 2-2Vertical Stabilizer Contours 1-15Wing Profiles 1-18

Wing Ribs/Stations 1-6

Zoning and Access 1-4

0-2Page 2

Jan 01/12


0-3 Section Index

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

Section Index

1. Section index

0-0 Table Of Contents0-1 Introduction0-2 Alphabetical Index

0-3 Section Index

1-0 Table Of Contents1-1 Airplane Overall Dimensions and Outline Basic Reference Drawing




1-5 Fuselage Frames/Stations

1-6 Wing Ribs/Stations


1-8 Center of Gravity Limits

1-9 Airplane Attitude

1-10 Ground Clearances1-11 Door Clearances1-12 Interior Arrangement

1-13 Radome1-14 Nose Contours1-15 Vertical Stabilizer Contours1-16 Horizontal Stabilizer Contours1-17 Tail Contours1-18 Wing Profiles

2-0 Table Of Contents2-1 Airplane Servicing Arrangement

2-2 Turnaround Stations2-3 Ground Service Connections and Locations

0-3Page 1

Jan 01/12


2-4 Ground Service Connections - Capacities and Flow

2-5 Cargo Compartments -- Loading and Unloading

2-6 Galleys -- General Information

2-7 Galleys -- Loading and Unloading

2-8 Ground Maneuvering

2-9 Airplane Parking

2-10 Towing

2-11 Operating Conditions

3-0 Table Of Contents3-1 Air Conditioning and Pneumatic

3-2 Communications, Navigation, Information Systems and Recording

3-3 Electrical Power3-4 Fire Protection3-5 Flight Controls

3-6 Fuel System

3-7 Hydraulic Power

3-8 Ice and Rain Protection3-9 De-Icing and Washing

3-10 Landing Gear

3-11 Auto Flight

3-12 Auxiliary Power Unit

3-13 Leveling, Symmetry and Alignment

3-14 Airplane Maintenance Jacking

3-15 Landing Gear Jacking

3-16 Exterior Lighting

3-17 Power Plant Handling

3-18 Component Weights

3-19 Component Handling

3-20 Suggested Hangar Arrangement

3-21 Landing Gear Maintenance Pits

3-22 Recommended Workstands

4-0 Table Of Contents

0-3Page 2

Jan 01/12



4-2 Electrical Power4-3 Fuel System Components

4-4 Hydraulic Power

4-5 Flight Controls

5-0 Table Of Contents5-1 Ground Support Vendors Information

0-3Page 3

Jan 01/12


General Information

1-1 Airplane Overall Dimensions and Outline Basic Reference Drawing

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

Airplane Overall Dimensions and Outline Basic Reference

1. This section shows the airplane overall dimensions and outline basic reference drawing.

1-1Page 1

Jan 01/12


**ON A/C A340-300

0 5 10 15SCALE METER

0SCALE FEET10 20 30 40 50

F_MF_010100_1_0040101_01_01

Airplane Overall Dimensions and Outline Basic Reference DrawingModel 300

FIGURE-1-1-0-991-004-A01

1-1Page 2

Jan 01/12


**ON A/C A340-200

0 5 10 15SCALE METER

0SCALE FEET10 20 30 40 50

F_MF_010100_1_0050101_01_01

Airplane Overall Dimensions and Outline Basic Reference DrawingModel 200

FIGURE-1-1-0-991-005-A01

1-1Page 3

Jan 01/12



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

Airplane Dimensions

1. This section gives the airplane dimensions.

1-2Page 1

Jan 01/12


**ON A/C A340-300

25%

AM

CAM

C A B C D E F G KH

19.4

04 m

63 ft

6 in

R=2

.820

m11

1 in

60.3

04 m

198

ft

10.6

84 m

35 ft

18.7

4 m

61 ft

5.8

in39

.20

m12

8 ft

7.4

in

62.8

83 m

206

ft 38

in

25.3

7 m

83 ft

24

in

27.3

83 m

89 ft

8 in

63.6

58 m

208

ft 10

in

29.9

66 m

98 ft

3 in

8.14

m26

ft 8

.5 in

3.10

m10

ft 2

in

5.78

8 m

18 ft

11.

9 in

7.80

m25

ft 7

in3.

554

m11

ft 7

.9 in

8.3

m27

ft 2

.8 in

0.71

m27

.9 in

1.39

7 m

55 in

0.96

5 m

38 in

6.67

1 m

21 ft

10.

7 in

53.6

% A

MC

EBA

G KH

F

SECT

ION

110

SEE

D

C

F_MF_010200_1_0120101_01_01

Airplane DimensionsModel 300

FIGURE-1-2-0-991-012-A01

1-2Page 2

Jan 01/12


**ON A/C A340-200

A B C D E F G KH

8.14

m26

ft 8

.5 in

3.10

m10

ft 2

in

5.78

8 m

18 ft

11.

9 in

7.80

m25

ft 7

in3.

554

m11

ft 7

.9 in

8.3

m27

ft 2

.8 in

0.71

m27

.9 in

1.39

7 m

55 in

0.96

5 m

38 in

SEE

SECT

ION

110

25%

AM

CAM

C

C

58.6

16 m

192

ft 31

in

23.2

4 m

76 ft

27

in

27.8

33 m

91 ft

35

in

59.3

90 m

194

ft 96

in

25.2

49 m

82 ft

98

in

53.6

% A

MC

F

BA D

6.67

1 m

21 ft

10.7

in

E

39.2

0 m

128

ft 7.

4 in

60.3

04 m

198

ft

R=2

.820

m11

1 in

19.4

04 m

63 ft

6 in 1

0.68

4 m

35 ft

18.7

4 m

61 ft

5.8

in

GH

K

F_MF_010200_1_0130101_01_01


FIGURE-1-2-0-991-013-A01

1-2Page 3

Jan 01/12


**ON A/C A340-300

28.9

62 m

94 ft

11

in

A B2.

404

m7

ft 10

in

5.64

0 m

18 ft

5 in

C8.

453

m27

ft 8

in

2.01

9 m

6 ft

6 in

D E5.

345

m17

ft 5

in

F4.

120

m13

ft 5

in

G3.

932

m12

ft 9

in

H19

.404

m63

ft 7

in

D

G

H

60.3

04 m

197

ft 9

in

E

C

19.6

00 m

64 ft

3 in

29.0

00 m

95 ft

1 in

9.37

0 m

30 ft

8 in

11.1

80 m

36 ft

6 in

AF

B

F_MF_010200_1_0140101_01_00

39.1

00 m

128

ft 5

in41

.600

m13

6 ft

5 in 5

8.95

0 m

193

ft 4

in63

.688

m20

8 ft

9 in

28.9

84 m

95 ft

22.8

00 m

74 ft

8 in

7.16

6 m

23 ft

6 in

22.3

88 m

73 ft

5 in


FIGURE-1-2-0-991-014-A01

1-2Page 4

Jan 01/12


**ON A/C A340-200

A B C D E F G H

26.8

51 m

88 ft

20.2

54 m

66 ft

5 in

67 ft

94

in 36.

967

m12

1 ft

3 in

39.4

67 m

129

ft 5

in54

.692

m17

9 ft

4 in

59.1

22 m

194

ft 11

in

5.64

0 m

18 ft

5 in

2.40

4 m

7 ft

10 in

8.45

3 m

27 ft

8 in

2.01

9 m

6 ft

6 in

5.34

5 m

17 ft

5 in

4.12

0 m

13 ft

5 in

3.93

2 m

12 ft

9 in

19.4

04 m

63 ft

7 in

26.8

29 m

88 ft

29.0

00 m

95 ft

1 in

20.6

67 m9.

370

m30

ft 8

in11

.180

m36

ft 6

in

H

7.16

6 m

6 in

19.6

0064

ft 3

in

60.3

04 m

197

ft 9

in

CD

E

F

G

23 ft

A

B

F_MF_010200_1_0150101_01_01


FIGURE-1-2-0-991-015-A01

1-2Page 5

Jan 01/12


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

FUSELAGE DATUM LINE

REFER TO CHAPTER 110

GROUND LINE

CL

6.50

0 m

21 ft

3 in

1.6

ORIGIN OF NOSEUP MOUVEMENT

C/L ENGINE

// VRZ 0

5

A

B

2.38

7 m

7 ft

8 in

1

VRX 6576.8

VRY

5176

.8 m

m

A BVR

Y =

0

FROM NOSE

3.74 m12 ft 3.36 in

2.48 m8 ft 1.8 in

B

A

C

ENGINE SUSPENSION

// CL A/C

MODEL 300 MODEL 200FROM NOSE22.3877 m73 ft 4 inA

B

C

20.2541 m66 ft 5 in

20.4241 m66 ft 1 in

20.6671 m67 ft 9 in

22.8007 m74 ft 8 in

22.5577 m73 ft 9 in

PYLON ENGINE C/L

* AIRCRAFT ON GROUND FUSELAGEDATUM LINE PARALLEL TO THE GROUND

F_MF_010200_1_0160101_01_00

Airplane DimensionsCFM56-5-C2 Inboard EngineFIGURE-1-2-0-991-016-A01

1-2Page 6

Jan 01/12


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

FUSELAGE DATUM LINE

REFER TO CHAPTER 110

GROUND LINE

CL

ORIGIN OF NOSEUP MOUVEMENT

C/L ENGINE

// VRZ 0

5

A

B

A

FROM NOSE1

VRY

1135

8.3

mm

2.6

ENGINE SUSPENSION

PYLON ENGINE C/L

// CL A/C

MODEL 300 MODEL 200FROM NOSE

A

B

* AIRCRAFT ON GROUND FUSELAGEDATUM LINE PARALLEL TO THE GROUND

A

B

VRX 16806.8

1.19

6 m

3 ft

11 in

3.74 m12 ft 3.36 in

2.48 m8 ft 1.8 in

6.50

0 m

21 ft

3 in

VRY

= 0

28.9625 m95 ft

29.1325 m95 ft 5 in

26.9989 m88 ft 66 in

26.8289 m87 ft 12 in

B

F_MF_010200_1_0170101_01_00

Airplane DimensionsCFM56-5-C2 Outboard EngineFIGURE-1-2-0-991-017-A01

1-2Page 7

Jan 01/12



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

General Airplane Characteristics Data

1. General Airplane Characteristics

The weight terms used throughout this manual are given below together with their respectivedefinitions.

Maximum Taxi Weight (MTW):Maximum weight for ground maneuver as limited by aircraft strength and airworthiness requirements.(It includes weight of run-up and taxi fuel). It is also called Maximum Ramp Weight (MRW).

Maximum Landing Weight (MLW):Maximum weight for landing as limited by aircraft strength and airworthiness requirements.

Maximum Takeoff Weight (MTOW):Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (This isthe maximum weight at start of the takeoff run).

Maximum Zero Fuel Weight (MZFW):Maximum operational weight of the aircraft without usable fuel.

Standard Seating Capacity:Number of passengers specifically certified or anticipated for certification.

Usable Volume:Usable volume available for cargo, pressurized fuselage, passenger compartment and cockpit.

Usable Fuel Capacity:Fuel available for aircraft propulsion.Water Volume :Volume of cargo compartment.

**ON A/C A340-300

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

1-3Page 1

Jan 01/12


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 Takeoff 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)


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)


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)


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)

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)

Maximum Takeoff Weight (MTOW)275 000 kg(606 271 lb)

271 000 kg(597 453 lb)

276 500 kg(609 578 lb)

260 000 kg(573 202 lb)

Maximum Landing Weight (MLW)192 000 kg(423 287 lb)

192 000 kg(423 287 lb)

190 000 kg(418 878 lb)

188 000 kg(414 469 lb)

1-3Page 2

Jan 01/12



Maximum Zero Fuel Weight (MZFW)181 000 kg(399 037 lb)

178 000 kg(392 423 lb)

178 000 kg(392 423 lb)

178 000 kg(392 423 lb)



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)


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)


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)


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)

3. The following table provides characteristics of A340-300 Model, these data are common to eachWeight Variants:

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)

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)

1-3Page 3

Jan 01/12


Aircraft Characteristics

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)

**ON A/C A340-200

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



254 400 kg(560 856 lb)

257 900 kg(568 572 lb)

260 900 kg(575 186 lb)

275 900 kg(608 255 lb)

Maximum Takeoff Weight (MTOW)253 500 kg(558 872 lb)

257 000 kg(566 588 lb)

260 000 kg(573 202 lb)

275 000 kg(606 271 lb)

Maximum Landing Weight (MLW)181 000 kg(399 037 lb)

181 000 kg(399 037 lb)

181 000 kg(399 037 lb)

185 000 kg(407 855 lb)

Maximum Zero Fuel Weight (MZFW)169 000 kg(372 581 lb)

169 000 kg(372 581 lb)

169 000 kg(372 581 lb)

173 000 kg(381 400 lb)

5. The following table provides characteristics of A340-200 Model, these data are common to eachWeight Variants:

Aircraft CharacteristicsStandard Seating Capacity 303

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)

946 m3

(33 408 ft3)

Passenger CompartmentVolume

345 m3

(12 184 ft3)

1-3Page 4

Jan 01/12


Aircraft Characteristics

Cockpit Volume12 m3

(424 ft3)

Usable Volume, FWD CC(Based on LD3)

60.7 m3

(2 142ft3)

Usable Volume, AFT CC(Based on LD3)

52 m3

(1 836ft3)

Usable Volume, Bulk CC19.7 m3

(695 ft3)

Water Volume, FWD CC84.6 m3

(2 988ft3)

Water Volume, AFT CC71.1 m3

(2 511ft3)

Water Volume, Bulk CC22.7 m3

(802 ft3)

1-3Page 5

Jan 01/12



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

Zoning and Access

1. GeneralThis section provides the zone division/delimitation.

2. Aircraft Zoning

A. Identification Method

(1) Zones identification is based on ATA 100 Specifications

(2) The aircraft is broken down into Zones identified, each, by a three-digit (hundreds)corresponds to the Major Zones, the second digit (tens) corresponds to the Major Sub-Zones and the third digit (units) corresponds to the Zones.

B. Identification of Major Zones, Major Sub-Zones and Zones.Locations and boundaries of the Major Zones and Major Sub-Zones are illustrated on the pagesthat follows.

NOTE : Locations and boundaries of the Zones are not given in this manual.

(1) Major Zones (hundreds)

(a) Major Zones boundaries are identified by:- Frame/Stations/Stringers for fuselage.- Ribs for wing and vertical/horizontal tail.- Stations for nacelle and pylon.

(b) The Major Zones are:- 100 Lower part of fuselage (below cabin floor), including radome to forward face

of aft pressure bulkhead.- 200 Upper part of fuselage (above cabin floor), to forward face of aft pressure

bulkhead.- 300 Stabilizer and fuselage rear section from rear of aft pressure bulkhead

(including rudder and elevators).- 400 Power plants, nacelles and pylons.- 500 Left Wing.- 600 Right Wing.- 700 Landing gear and landing gear doors.- 800 Passenger/crew doors, cargo compartment doors and emergency exits.

(2) Major Sub-Zones (tens)

(a) These are divisions of the Major Zones, eg: 100 divided into 110, 120, 130, 140, etc.

(b) The sequence of Major Sub-Zones numbering for fuselage runs from the front to therear.

1-4Page 1

Jan 01/12


(3) Zones (units)

(a) These are divisions of Major Sub-Zones, eg: 120 divided into 121, 122, 123, etc.

(b) The sequence of Zones for fuselage runs from inboard to outboard, front to rear inthe wing, forward to aft and away from the floor line in the fuselage and from root totip in the vertical tail.

(c) Whenever feasible odd numbers are allocated to the zones left of fuselage or nacellecenterlines and even numbers to zones to the right.

NOTE : If no side differentiation is needed (eg: pylon, bilge area), the oldnumbering for center zones is used.

1-4Page 2

Jan 01/12


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

800 800 800 800

800 800 800

500600

400 400 700 400400700 700

300

200

100

F_MF_010400_1_0860101_01_01

Zoning and AccessMajor Zones

FIGURE-1-4-0-991-086-A01

1-4Page 3

Jan 01/12


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

C L

110

120

8202

3024

0 830

840

130

190

140

250

830

840

260

270

150

820

160

170

310

830

840

320

A

2102

20 830 840

B

190

A

340

330

B

F_MF_010400_1_0900101_01_02

Zoning and AccessMajor Sub-Zones - Zones 100, 200, 300 and 800

FIGURE-1-4-0-991-090-A01

1-4Page 4

Jan 01/12


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

ENGINE 1 AND 2 ENGINE 3 AND 4

590690

530630

580680

510610

570670

520620

540640

510610

520620

510610

550650

580680

530630

460 480440420450 470430410

F_MF_010400_1_0910101_01_01

Zoning and AccessMajor Sub-Zones - Zones 400, 500 and 600 (CFM56 Series Engine)

FIGURE-1-4-0-991-091-A01

1-4Page 5

Jan 01/12


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

Specific Areas Location

1. GeneralThis section gives the location of the specific areas on the aircraft.

2. Specific Areas Location- Pressurized Areas, see FIGURE 1---0-99--185-A- Skydrol Areas, see FIGURE 1---0-99--186-A- Vibration Areas, see FIGURE 1---0-99--187-A- Hot Areas, see FIGURE 1---0-99--188-A- Swamp Areas (Severe Weather and Moisture Prone), see FIGURE 1---0-99--189-A- Fuel and Fuel Vapor Areas, see FIGURE 1---0-99--190-A- Fire Areas, see FIGURE 1---0-99--191-A

1-4Page 6

Jan 01/12


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

Z200

Z121

(Z12

2)Z1

33(Z

134)

Z137

(Z13

8)Z1

31(Z

132)

Z145

(Z14

6)

Z153

(Z15

4)

Z171

(Z17

2)

Z151

(Z15

2)Z1

63(Z

164)

Z161

(Z16

2)

F_MF_010400_1_1850101_01_00

Specific Areas LocationPressurized Areas

FIGURE-1-4-0-991-185-A01

1-4Page 7

Jan 01/12


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

Z711

Z123

(Z12

4)Z1

47(Z

148)

Z195

(Z19

6)Z7

51Z1

49

Z322

Z323

Z325

Z311

(Z31

2)

Z731

(Z74

1)Z5

75(Z

675)

Z574

(Z67

4)

Z573

(Z67

3)

Z571

(Z67

1)

Z522

(Z62

2)

Z521

(Z62

1)

Z523

(Z62

3)

Z334

(Z34

4)

Z143

F_MF_010400_1_1860101_01_00

Specific Areas LocationSkydrol Areas

FIGURE-1-4-0-991-186-A01

1-4Page 8

Jan 01/12


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

Z123

(Z12

4)

Z711

Z195

(Z19

6)

Z751

Z731

(Z74

1)Z1

47(Z

148)

Z322

Z323

Z332

(Z34

2)

Z334

(Z34

4)Z3

31(Z

341) Z

454

(Z46

4)

Z453

(Z46

3)

Z451

(Z46

1)Z4

52(Z

462)

Z472

(Z48

2)Z4

71(Z

481)

Z473

(Z48

3)

Z474

(Z48

4)

Z143

Z315

(Z31

6)Z3

13(Z

314)

Z324

Z325

Z311

(Z31

2)Z1

49

F_MF_010400_1_1870101_01_00

Specific Areas LocationVibration Areas

FIGURE-1-4-0-991-187-A01

1-4Page 9

Jan 01/12


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

Z454

(Z46

4)

Z453

(Z46

3)

Z451

(Z46

1)

Z452

(Z46

2)Z4

72(Z

482)

Z471

(Z48

1) Z473

(Z48

3)

Z474

(Z48

4)

Z411

(Z42

1)

Z412

(Z42

2)

Z431

(Z44

1)

Z315

(Z31

6)Z3

13(Z

314)

Z432

(Z44

2)

Z191

(Z19

2)Z1

93

F_MF_010400_1_1880101_01_00

Specific Areas LocationHot Areas

FIGURE-1-4-0-991-188-A01

1-4Page 10

Jan 01/12


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

Z334

(Z34

4)

Z575

(Z67

5)

Z571

(Z67

1)

Z573

(Z67

3) Z57

4(Z

674)

Z523

(Z62

3)

Z522

(Z62

2)

Z521

(Z62

1)

Z731

(Z74

1)

Z751Z1

47(Z

148)

Z149

(Z12

4)

Z711Z1

23

F_MF_010400_1_1890101_01_00

Z325

Specific Areas LocationSwamp Areas

FIGURE-1-4-0-991-189-A01

1-4Page 11

Jan 01/12


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

Z145

(Z14

6)Z1

91(Z

192)

Z143

Z141

(Z14

2)

Z147

(Z14

8)

Z319

Z333

(Z34

3)

Z452

(Z46

2)Z4

51(Z

461)

Z472

(Z48

2)Z4

71(Z

481)

Z550

(Z65

0)

Z540

(Z64

0)

Z149

F_MF_010400_1_1900101_01_00

Specific Areas LocationFuel and Fuel Vapor AreasFIGURE-1-4-0-991-190-A01

1-4Page 12

Jan 01/12


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

F_MF_010400_1_1910101_01_00

Z315

(Z31

6)

Z313

(Z31

4)

Z451

(Z46

1)Z4

13(Z

423)

Z412

(Z42

2)Z4

17(Z

418)

Z433

(Z44

3)Z4

71(Z

481)

Z432

(Z44

2)Z4

27(Z

428)

Z437

(Z43

8)Z4

47(Z

448)

Specific Areas LocationFire Areas

FIGURE-1-4-0-991-191-A01

1-4Page 13

Jan 01/12


1-5 Fuselage Frames / Stations

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

Fuselage Frames / Stations

1. General

This section gives the fuselage frame stations measured along X datum 6382 mm from the nose.

The stations (STA) are given in millimeters without conversion.

1-5Page 1

Jan 01/12


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

X0

FR14/STA11627FR15/STA12115

FR16/STA12603

FR14A/STA11871

FR15A/STA12359

FR16A/STA12849

X = 6382

FR2/STA7942FR4/STA8355FR6/STA8809

FR10/STA9717FR11/STA10187FR12/STA10667FR13/STA11147FR13B/STA11612

FR15B/STA12563FR17/STA13153

FR8/STA9263

FR14B/STA12079

FR1/STA7662FR3/STA8149FR5/STA8582FR7/STA9036FR9/STA9490FR10A/STA9952FR11A/STA10427FR12A/STA10907FR13A/STA11387

FR14C/STA12321FR15C/STA12805FR16A/STA13047FR18/STA13398FR19/STA13928

FR25A/STA17291

FR20/STA14458FR21/STA14988FR22/STA15518FR23/STA16048FR24/STA16578FR25/STA17108FR26/STA17638FR26.1/STA18168FR26.2/STA18698FR26.3/STA19228FR26.4/STA19758FR27/STA20288FR28/STA20818FR29/STA21348FR30/STA21878FR31/STA22408FR32/STA22938FR33/STA23468FR34/STA23998FR35/STA24528

FR35A/STA24718 FR36/STA25058

FWD PAXCREW DOOR

FWD CARGOCOMPARTMENT DOOR

FR37/STA25588

CL

MID PASSENGER/CREW DOOR

FR20A/STA14541

FR14A/STA11837

F_MF_010500_1_0100101_01_00

Fuselage Frames / StationsNose Section (FR 1 to FR 37)FIGURE-1-5-0-991-010-A01

1-5Page 2

Jan 01/12


**ON A/C A340-300

FR37.3/STA27185

FR37.1/STA26118

FR38/STA28252

FR37.2/STA26652

FR37.4/STA27719

FR54/STA44171FR53.9/STA43641FR53.8/STA43111

FR53.7A/STA42771 FR53.7/STA42581FR53.6/STA42051FR53.5/STA41521FR53.4/STA40991FR53.3/STA40461FR53.2/STA39931FR53.1/STA39399FR53/STA38866FR52/STA38333FR51/STA37801FR50/STA37269FR49/STA36737FR48/STA36204FR47/STA35672FR46/STA35142FR45/STA34612FR44/STA34082FR43/STA33552FR42/STA33022FR41/STA32492FR40.3/STA31962FR40.2/STA31432FR40.1/STA30902

FR39.2/STA29842FR39.1/STA29312FR39/STA28782

EMERGENCYEXIT

CL

FR55/STA44701FR56/STA45231FR57/STA45761FR57.1/STA46291FR57.2/STA46824FR57.3/STA47358FR57.4/STA47891FR58/STA48424

FR40/STA30381

F_MF_010500_1_0110101_01_00

Fuselage Frames / StationsCenter Section (FR 37.1 to FR 58)

FIGURE-1-5-0-991-011-A01

1-5Page 3

Jan 01/12


**ON A/C A340-300

AFT CARGOCOMPARTMENT DOOR

BULK CARGOCOMPARTMENT DOOR

AFT PASSENGER/CREW DOOR

CL

FR92/STA65158FR94/STA65746FR96/STA66366FR98/STA67006

FR104A/STA68721FR106A/STA69151

FR78/STA59404FR79/STA60010FR80/82/STA60614FR83/STA61140FR84/STA61666FR85/STA62193FR86/STA62719

FR65/STA52134FR66/STA52664FR67/STA53194FR68/STA53724FR69/STA54254FR70/STA54784FR71/STA55315FR72/STA55844FR73/STA56374FR74/STA56980FR75/STA57586FR76/STA58192FR77/STA58798

FR58/STA48424FR59/STA48954FR60/STA49484FR61/STA50014FR62/STA50544FR63/STA51074FR64/STA51604

FR59A/STA49351

FR73A/STA56713

FR75A/STA57963

FR100/STA67646FR102/STA68216

FR88/STA63696FR89/STA64146FR90/STA64596FR91/STA65046FR93/STA65446

FR87/STA63246

FR95/STA66046FR97/STA66686FR99/STA67326FR101/STA67931FR103/STA68501FR105A/STA68941STA69221

F_MF_010500_1_0120101_01_01

Fuselage Frames / StationsRear Section (FR 58 to FR 106A)

FIGURE-1-5-0-991-012-A01

1-5Page 4

Jan 01/12


**ON A/C A340-200

FR38/STA26118FR39/STA26648FR39.1/STA27178FR39.2/STA27708FR40/STA28247FR40.1/STA28768FR40.2/STA29298FR40.3/STA29828FR41/STA30358FR42/STA30888FR43/STA31418

FR45/STA32478FR46/STA33008

FR49/STA34603FR50/STA35136FR51/STA35668

FR53/STA36733FR53.1/STA37265FR53.2/STA37797FR53.3/STA38327FR53.4/STA38857

FR53.6/STA39917FR53.7/STA40447FR53.8/STA40977FR53.9/STA41507FR54/STA42037

FR53.5/STA39387

FR48/STA34071

CL


FR47/STA33538

FR44/STA31948

FR52/STA36200

F_MF_010500_1_0130101_01_01

Fuselage Frames / StationsCenter Section (FR 38 to FR 58)

FIGURE-1-5-0-991-013-A01

1-5Page 5

Jan 01/12


**ON A/C A340-200

CL

FR106A/STA64884FR104A/STA64454

AFT CARGOCOMPARTMENT DOOR

BULK CARGOCOMPARTMENT DOOR

AFT PASSENGER/CREW DOOR

FR80/82/STA56347FR83/STA56873FR84/STA57399FR85/STA57926FR86/STA58452


FR100/STA63379FR102/STA63949

FR72/STA51577FR73/STA52107FR74/STA52713FR75/STA53319FR76/STA53925FR77/STA54531FR78/STA55137FR79/STA55743

FR59/STA44687FR60/STA45217FR61/STA45747FR62/STA46277FR63/STA46807FR64/STA47337FR65/STA47867FR66/STA48397FR67/STA48927FR68/STA49457FR69/STA49987FR70/STA50517FR71/STA51047

FR58/STA44157

FR59A/STA45083

FR75A/STA53696

FR73A/STA52446

FR87/STA58979

STA64954FR105A/STA64674FR103/STA64234FR101/STA63664FR99/STA63059

FR88/STA59429FR89/STA59879FR90/STA60329FR91/STA60779FR93/STA61179FR95/STA61779FR97/STA62419

F_MF_010500_1_0140101_01_01

Fuselage Frames / StationsRear Section (FR 58 to FR 106A)

FIGURE-1-5-0-991-014-A01

1-5Page 6

Jan 01/12


1-6 Wing Ribs / Stations

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

Wing Ribs / Stations

1. General

This section shows wing ribs/stations and dimensions.

Rib Station locations are measured from the point underneath the wing where the front of the ribmeets the front spar. These dimensions are in plan view (horizontal).

1-6Page 1

Jan 01/12


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

STA0/RIB1STA732/RIB2STA1469/RIB3

STA2205/RIB4STA2913/RIB5


STA5036/RIB8STA5676/RIB9STA6261/RIB10STA6837/RIB10A


STA8862/RIB13STA9506/RIB14STA10149/RIB15













UPPER SURFACE

2793.2 mm109.9 in

FLAP TRAK

NO

SE

1

2

3

47.

281

m23

ft 2

.3 in

10.7

75 m

35 ft

3.5

in14

.178

m46

ft 4

.6 in

17.6

04 m

57 ft

5.7

in

MODEL 20036.572 m

119 ft 11.9 in35.380 m

116 ft 11.6 in34.112 m

111 ft 11.1 in33.166 m

108 ft 10.8 in

MODEL 30038.706 m

126 ft 12.6 in37.514 m

123 ft 12.3 in36.246 m

118 ft 11.8 in35.300 m

115 ft 11.5 inCL

4

1

2

3

F_MF_010600_1_0020101_01_01

Wing Ribs / StationsFIGURE-1-6-0-991-002-A01

1-6Page 2

Jan 01/12



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

Fuselage Cross-sections

1. General

This section gives fuselage cross-sections.

The illustrations are shown viewed forward.

NOTE : For frame assembly see section 1-5.

1-7Page 1

Jan 01/12


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

FRAME 1STA7662.5

Z

Y

0 200 400 600SCALE (mm)

0

F_MF_010700_1_0920101_01_00

Z1346.876

Z718.349

Fuselage Cross-sectionFRAME 1 - STA7662.5

FIGURE-1-7-0-991-092-A01

1-7Page 2

Jan 01/12


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

FRAME 2STA7942.5SCALE (mm)

0 200 400 600

Z

Y0

F_MF_010700_1_0930101_01_00

Z973.174

Z1473.938


FIGURE-1-7-0-991-093-A01

1-7Page 3

Jan 01/12


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

Z

Y

FRAME 3STA8149.5

0 200 400 600SCALE (mm)

0

Z1561.541

F_MF_010700_1_0940101_01_00

Z1180.172


FIGURE-1-7-0-991-094-A01

1-7Page 4

Jan 01/12


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

FRAME 4STA8355.5

Z

Y

0 200 400 600SCALE (mm)

0

Z1372.020

Z1643.551

F_MF_010700_1_0950101_01_01


FIGURE-1-7-0-991-095-A01

1-7Page 5

Jan 01/12


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

Z

Y

SCALE (mm)FRAME 5

STA8582.5

0

0 200 400 600Z1539.832

Z1728.301

F_MF_010700_1_0960101_01_00


FIGURE-1-7-0-991-096-A01

1-7Page 6

Jan 01/12


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

Y

FRAME 6STA8809.5Z1670.530

0 200 400 600SCALE (mm)

0

Z

F_MF_010700_1_0970101_01_00

Z1807.527


FIGURE-1-7-0-991-097-A01

1-7Page 7

Jan 01/12


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

Z

Y

FRAME 7STA9036.5

Z1773.824

Z1881.590

0 200 400 600SCALE (mm)

0

F_MF_010700_1_0980101_01_00


FIGURE-1-7-0-991-098-A01

1-7Page 8

Jan 01/12


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

Y

FRAME 8STA9263.5

Z1859.450

Z1950.833

Z

0 200 400 600SCALE (mm)

0

F_MF_010700_1_0990101_01_00


FIGURE-1-7-0-991-099-A01

1-7Page 9

Jan 01/12


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

Z

Y

Z2015.583

FRAME 9STA9490.5

Z1936.490

0 200 400 600SCALE (mm)

0

F_MF_010700_1_1000101_01_00


FIGURE-1-7-0-991-100-A01

1-7Page 10

Jan 01/12


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

Z

Y

FRAME 10STA9717.5

Z2008.057

Z2076.147

0 200 400 600SCALE (mm)

0

F_MF_010700_1_1010101_01_00


FIGURE-1-7-0-991-101-A01

1-7Page 11

Jan 01/12


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

Z

Y

FRAME 12STA10667.5

Z2260.209

Z2294.096

SCALE (mm)0 200 400 600

0

F_MF_010700_1_1020101_01_00

Fuselage Cross-sectionFRAME 12 - STA10667.5FIGURE-1-7-0-991-102-A01

1-7Page 12

Jan 01/12


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

Z

Y

Z2364.209

FRAME 13STA11147.5

Z2386.743

200 400 600SCALE (mm)

0

0

F_MF_010700_1_1030101_01_00


1-7Page 13

Jan 01/12


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

Z

Y

FRAME 13BSTA11612.5

Z2452.230

Z2466.696

F_MF_010700_1_1040101_01_00

0 200 400 600SCALE (mm)

0

F_MF_010700_1_1040101_01_00

Fuselage Cross-sectionFRAME 13B - STA11612.5FIGURE-1-7-0-991-104-A01

1-7Page 14

Jan 01/12


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

Z

Y

Z2490.695

Z2502.149

FRAME 14 SUPSTA11837.5

0 200 400 600SCALE (mm)

0

F_MF_010700_1_1050101_01_00

Fuselage Cross-sectionFRAME 14 SUP - STA11837.5FIGURE-1-7-0-991-105-A01

1-7Page 15

Jan 01/12


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

Z

Y

FRAME 14B SUPSTA12079.5

Z2538.035

Z2529.293SCALE (mm)

0 200 400 600

0

F_MF_010700_1_1060101_01_00

Fuselage Cross-sectionFRAME 14B SUP - STA12079.5

FIGURE-1-7-0-991-106-A01

1-7Page 16

Jan 01/12


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

Z

Y

FRAME 15 INFSTA12115.5

Z2534.798

Z2543.179

SCALE (mm)0 200 400 600

0

F_MF_010700_1_1070101_01_00

Fuselage Cross-sectionFRAME 15 INF - STA12115.5FIGURE-1-7-0-991-107-A01

1-7Page 17

Jan 01/12


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

Z

Y

FRAME 15A INFSTA12359.5

Z2570.546

Z2576.749

0 200 400 600SCALE (mm)

0

F_MF_010700_1_1080101_01_00

Fuselage Cross-sectionFRAME 15A INF - STA12359.5FIGURE-1-7-0-991-108-A01

1-7Page 18

Jan 01/12


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

Z

Y

FRAME 15B SUPSTA12563.5

Z2598.379

Z2603.114

0 200 400 600SCALE (mm)

0

F_MF_010700_1_1090101_01_00

Fuselage Cross-sectionFRAME 15B SUP - STA12563.5

FIGURE-1-7-0-991-109-A01

1-7Page 19

Jan 01/12


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

Z

Y

FRAME 15C SUPSTA12805.5

Z2632.428

Z2629.075

SCALE (mm)0 200 400 600

0

F_MF_010700_1_1100101_01_00

Fuselage Cross-sectionFRAME 15C SUP - STA12805.5

FIGURE-1-7-0-991-110-A01

1-7Page 20

Jan 01/12


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

Z

Y

Z2657.349

FRAME 16A SUPSTA13047.15

Z2659.605

SCALE (mm)0 200 400 600

0

F_MF_010700_1_1110101_01_00

Fuselage Cross-sectionFRAME 16A SUP - STA13047.15

FIGURE-1-7-0-991-111-A01

1-7Page 21

Jan 01/12


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

Y

FRAME 16 INFSTA12603.5

Z2603.624

Z2608.105

6004002000

Z

0

SCALE (mm)

F_MF_010700_1_1120101_01_00

Fuselage Cross-sectionFRAME 16 INF - STA12603.5FIGURE-1-7-0-991-112-A01

1-7Page 22

Jan 01/12


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

Z

Y

Z2634.397

Z2637.530

FRAME 16A INFSTA12849.5

SCALE (mm)6004002000

0

F_MF_010700_1_1130101_01_00

Fuselage Cross-sectionFRAME 16A INF - STA12849.5FIGURE-1-7-0-991-113-A01

1-7Page 23

Jan 01/12


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

Z

Y

FRAME 17STA13153.5

Z2670.913

Z2669.0516004000 200

0

SCALE (mm)

F_MF_010700_1_1140101_01_00


1-7Page 24

Jan 01/12


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

Z

Y

0 200 400 600SCALE MM

STA13398.5/FR18

Z2694.3

Z2695.5

0

F_MF_010700_1_1150101_01_00


1-7Page 25

Jan 01/12


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

Z

Y

0 200 400 600SCALE MM

STA13928.5/FR19

Z2741.1

Z2741.3

0

F_MF_010700_1_1160101_01_00


1-7Page 26

Jan 01/12


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

Y

0 200 400 600SCALE MM

Z

FWD CARGODOOR

STA16048.5/FR23

Z180.1

Z2363.8

Z2820

Z2820

0

F_MF_01

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