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@AIRBUS

A318

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 of the 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 Services 31707 Blagnac Cedex

FRANCE

Issue: Jul 01/02 Rev: May 01/14

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@A318 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING

HIGHLIGHTS

Revision No. 10 - May 01/14

LOCATIONS CHGCODE

DESCRIPTIONS OF CHANGE

CHAPTER 1 RSection 1-1 RSubject 1-1-0 R

Purpose RSection 1-2 NSubject 1-2-0 N

Glossary N

CHAPTER 2 RSection 2-1 RSubject 02-01-00 DSubject 2-1-1 R

General Aircraft Characteristics Data R DESCRIPTION TITLE UPDATEDPART EFFECTIVITYADDED/REVISED/DELETED

Section 2-2 R

Subject 2-2-0 RGeneral Aircraft Dimensions RFIGURE General Aircraft Dimensions -Wing Tip Fence

R REVISED ILLUSTRATIONS TO SHOW THEDIMENSIONS ON WING AND HTP.ILLUSTRATION REVISED

Section 2-3 RSubject 2-3-0 R

Ground Clearances R NOTE AMENDEDFIGURE Ground Clearances R DELETED THE GROUND CLEARANCE

DIMENSIONS OF MRW (59T) IN THETABLE. IMPROVED LAYOUT.ILLUSTRATION REVISED

FIGURE Ground Clearances - GroundClearances with Sharklets

R DELETED THE GROUND CLEARANCEDIMENSIONS OF MRW (59T) IN THETABLE. IMPROVED LAYOUT.ILLUSTRATION REVISED

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LOCATIONS CHGCODE


FIGURE Ground Clearances - Flaps andFlap Track Fairings When Flaps FullyExtended

R ILLUSTRATION REVISED

FIGURE Ground Clearances - Flap TrackFairings Up


FIGURE Ground Clearances - AileronDown


FIGURE Ground Clearances - Aileron Upand Spoilers 1 to 5 Extended


FIGURE Ground Clearances - SlatsExtended


Section 2-4 RSubject 02-04-00 DSubject 2-4-1 R

Interior Arrangements - Plan View R DESCRIPTION TITLE UPDATEDFIGURE Interior Arrangements - PlanView - Typical Configuration - Single-Class, High Density

R ADDED INTERIOR ARRANGEMENTS -PLAN VIEW TO THE TITLE.ILLUSTRATION REVISED

FIGURE Interior Arrangements - PlanView - Typical Configuration - Two-Class

R ADDED INTERIOR ARRANGEMENTS -PLAN VIEW TO THE TITLE.

ILLUSTRATION REVISEDSection 2-5 RSubject 2-5-0 R

Interior Arrangements - Cross Section R DESCRIPTION TITLE UPDATEDFIGURE Interior Arrangements - CrossSection - Typical Configuration

R REVISED TITLE TO INTERIORARRANGEMENTS - CROSS SECTION.ILLUSTRATION REVISED

FIGURE Interior Arrangements - CrossSection - Economy Class, 6 Abreast -Wider Aisle


FIGURE Interior Arrangements - CrossSection - First-Class



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LOCATIONS CHGCODE


Cargo Compartments R

FIGURE Cargo Compartments -Locations, Dimensions and LoadingCombinations



Door Clearances R DESCRIPTION TITLE UPDATEDNOTE AMENDED

FIGURE Door Identification and Location- Door Identification

N ADDED ILLUSTRATIONS FOR DOORIDENTIFICATION AND LOCATION.ILLUSTRATION ADDED

Subject 2-7-1 RForward Passenger / Crew Doors R

FIGURE Doors Clearances - ForwardPassenger / Crew Doors


Subject 2-7-2 REmergency Exits RFIGURE Doors Clearances - EmergencyExits


Subject 2-7-3 R

Aft Passenger / Crew Doors R

FIGURE Doors Clearances - Aft Passenger/ Crew Doors


Subject 2-7-4 RForward Cargo Compartment Door RFIGURE Door Clearances - Forward CargoCompartment Door

R IMPROVED LAYOUT.ILLUSTRATION REVISED

Subject 2-7-5 R

Aft Cargo Compartment Door RFIGURE Doors Clearances - Aft CargoCompartment Door


Subject 2-7-7 RMain Landing Gear Doors R

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LOCATIONS CHGCODE


FIGURE Doors Clearances - Main LandingGear Doors


Subject 2-7-8 RRadome RFIGURE Doors Clearances - Radome R ILLUSTRATION REVISED

Subject 2-7-9 RAPU and Nose Landing Gear Doors RFIGURE Doors Clearances - APU andNose Landing Gear Doors


Section 2-8 R

Subject 2-8-0 REscape Slides RFIGURE Escape Slides - Location R ILLUSTRATION REVISEDFIGURE Escape Slides - Dimensions R ILLUSTRATION REVISED


Landing Gear R CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

FIGURE Landing Gear - Main Landing

Gear - Twin-Wheel

R DELETED TECHNICAL SPECIFICATION

STANDARD MS28889 IN SHEET 2.ILLUSTRATION REVISED

FIGURE Landing Gear - Main LandingGear Dimensions - Twin-Wheel


FIGURE Landing Gear - Nose LandingGear

R DELETED TECHNICAL SPECIFICATIONSTANDARD MS28889 IN SHEET 2.ILLUSTRATION REVISED

FIGURE Landing Gear - Nose LandingGear Dimensions


Landing Gear Maintenance Pits RFIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes


FIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes


Section 2-10 R

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LOCATIONS CHGCODE


Subject 2-10-0 R

Exterior Lighting RFIGURE Exterior Lighting R ILLUSTRATION REVISEDFIGURE Exterior Lighting R ILLUSTRATION REVISEDFIGURE Exterior Lighting R ILLUSTRATION REVISEDFIGURE Exterior Lighting R ILLUSTRATION REVISED


Antennas and Probes Location RFIGURE Antennas and Probes - Location R ILLUSTRATION REVISED


Auxiliary Power Unit RFIGURE Auxiliary Power Unit - AccessDoors


FIGURE Auxiliary Power Unit - GeneralLayout


Engine and Nacelle RFIGURE Power Plant Handling - MajorDimensions - CFM56 Series Engine


FIGURE Power Plant Handling - MajorDimensions - CFM56 Series Engine


FIGURE Power Plant Handling - FanCowls - CFM56 Series Engine


FIGURE Power Plant Handling - ThrustReverser Cowls - CFM56 Series Engine


FIGURE Power Plant Handling - MajorDimensions - PW 6000 Series Engine


FIGURE Power Plant Handling - NacelleDimensions - PW 6000 Series Engine


FIGURE Power Plant Handling - FanCowls - PW 6000 Series Engine


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LOCATIONS CHGCODE


FIGURE Power Plant Handling - ThrustReverser Halves - PW 6000 Series Engine



Leveling, Symmetry and Alignment RFIGURE Location of the Leveling Points R ILLUSTRATION REVISED


Jacking for Maintenance RFIGURE Jacking for Maintenance -

Jacking Point Locations

R ADDED TABLE FOR THE LOCATION OF

JACKING POINTS AND THE MAXIMUMELIGIBLE LOAD ON EACH JACKINGPOINT.ILLUSTRATION REVISED

FIGURE Jacking for Maintenance -Forward Jacking Point


FIGURE Jacking for Maintenance - WingJacking Points


FIGURE Jacking for Maintenance - SafetyStay


FIGURE Jacking for Maintenance -Jacking Design

R UPDATED JACKING CONFIGURATIONAND CORRECTED THE POSITION OFJACKS.ILLUSTRATION REVISED

Jacking of the Landing Gear R DESCRIPTION TITLE UPDATEDNOTE AMENDED

FIGURE Jacking of the Landing Gear -MLG Jacking Point Location - TwinWheels

R REVISED TITLE TO JACKING OF THELANDING GEAR.ILLUSTRATION REVISED

FIGURE Jacking of the Landing Gear -MLG Jacking with Cantilever Jack - TwinWheels


FIGURE Jacking of the Landing Gear -Loads at MLG Jacking Points - TwinWheels


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LOCATIONS CHGCODE


FIGURE Jacking of the Landing Gear -NLG Jacking - Point Location


FIGURE Jacking of the Landing Gear -Loads at NLG Jacking Points



General Information RSection 3-2 RSubject 03-02-00 DSubject 3-2-1 R

ISA Conditions RFIGURE Payload/Range N ADDED ILLUSTRATION TO SHOW

PAYLOAD/RANGE AT ISA CONDITIONS.ILLUSTRATION ADDED


Take-Off Weight Limitation - ISAConditions

R DESCRIPTION TITLE UPDATED

FIGURE Take-Off Weight Limitation -ISA Conditions - CFM56 Series Engine

R DELETED FAR/JAR FROM THE TITLE.ILLUSTRATION REVISED

FIGURE Take-Off Weight Limitation -ISA Conditions - PW 6000 Series Engine


Subject 3-3-2 RTake-Off Weight Limitation - ISA +15C(+59F) Conditions


FIGURE Take-Off Weight Limitation -ISA +15C (+59F) Conditions - CFM56Series Engine


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LOCATIONS CHGCODE


FIGURE Take-Off Weight Limitation -ISA +15C (+59F) Conditions - PW6000 Series Engine



Landing Field Length - ISA Conditions R DESCRIPTION TITLE UPDATEDFIGURE Landing Field Length - ISAConditions - CFM56-5B Series Engine

R REVISED TITLE TO LANDING FIELDLENGTH - ISA CONDITIONS. IMPROVEDLAYOUT.ILLUSTRATION REVISED

FIGURE Landing Field Length - ISAConditions - PW 6000 Series Engine

R REVISED TITLE TO LANDING FIELDLENGTH - ISA CONDITIONS. IMPROVEDLAYOUT.ILLUSTRATION REVISED


Final Approach Speed R


General Information RSection 4-2 RSubject 4-2-0 R

Turning Radii RFIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISEDFIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISED

Section 4-3 R

Subject 4-3-0 RMinimum Turning Radii RFIGURE Minimum Turning Radii R ILLUSTRATION REVISED


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LOCATIONS CHGCODE


Visibility from Cockpit in Static Position R

FIGURE Visibility from Cockpit in StaticPosition R ILLUSTRATION REVISED

FIGURE Binocular Visibility ThroughWindows from Captain Eye Position



Runway and Taxiway Turn Paths RSubject 4-5-1 R

135 Turn - Runway to Taxiway R

FIGURE 135 Turn - Runway to Taxiway- Cockpit Over Centerline Method R ILLUSTRATION REVISED

FIGURE 135 Turn - Runway to Taxiway- Judgemental Oversteering Method


Subject 4-5-2 R90 Turn - Runway to Taxiway RFIGURE 90 Turn - Runway to Taxiway -Cockpit Over Centerline Method


FIGURE 90 Turn - Runway to Taxiway -

Judgemental Oversteering Method


Subject 4-5-3 R180 Turn on a Runway RFIGURE 180 turn on a Runway - Edgeof Runway Method


Subject 4-5-4 R135 Turn - Taxiway to Taxiway RFIGURE 135 Turn - Taxiway to Taxiway- Cockpit Over Centerline Method


Subject 4-5-5 R90 Turn - Taxiway to Taxiway RFIGURE 90 Turn - Taxiway to Taxiway- Cockpit Over Centerline Method


Section 4-6 R

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LOCATIONS CHGCODE



Terminal Operations - Full Servicing TurnRound Time

R

FIGURE Full Servicing Turn Round TimeChart

R REVISED TRT TO 35 MIN. UPDATED TRTCHART AND ILLUSTRATION TITLE.ILLUSTRATION REVISED


Terminal Operations - Outstation TurnRound Time


FIGURE Outstation Turn Round TimeChart

R REVISED TRT TO 21 MIN. UPDATED TRTCHART AND ILLUSTRATION TITLE.ILLUSTRATION REVISED


Ground Service Connections Layout RFIGURE Ground Service ConnectionsLayout

R ADDED NOTE ABOUT THE LOCATION OFENGINE OIL SERVICING POINTS (8).

IMPROVED LAYOUT AND ADDED THELOCATIONS OF NACA VENT INTAKE (12)AND OVERPRESSURE PROTECTORS (9).ILLUSTRATION REVISED

Subject 5-4-2 R

Grounding (Earthing) Points R DESCRIPTION TITLE UPDATEDNOTE AMENDED

FIGURE Ground Service Connections -Grounding (Earthing) Points - LandingGear

R REVISED THE ILLUSTRATION TO ADDTHE WORD EARTHING TO THE TERMGROUNDING. IMPROVED LAYOUT.

ILLUSTRATION REVISEDFIGURE Ground Service Connections -Grounding (Earthing) Points - Wing (If Installed)


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LOCATIONS CHGCODE


FIGURE Ground Service Connections -Grounding (Earthing) Point - AvionicsCompartment Door-Frame

N ADDED ILLUSTRATION FOR GROUNDING(EARTHING) POINT ON THE AVIONICSCOMPARTMENT DOOR-FRAME.ILLUSTRATION ADDED

FIGURE Ground Service Connections -Grounding (Earthing) Point - Engine AirIntake (If Installed)

N ADDED ILLUSTRATION FOR GROUNDING(EARTHING) POINT ON THE ENGINE AIRINTAKE.ILLUSTRATION ADDED

Subject 5-4-3 RHydraulic System R NOTE AMENDEDFIGURE Hydraulic System - Green System

Ground Service Panel

R REVISED ILLUSTRATION TO LOCATE

RESERVOIR DEPRESSURIZATIONCONNECTION AND SELECTOR VALVE.ILLUSTRATION REVISED

FIGURE Hydraulic System - Blue SystemGround Service Panel

R REVISED ILLUSTRATION TO LOCATERESERVOIR DEPRESSURIZATION VALVEAND DRAIN VALVE.ILLUSTRATION REVISED

FIGURE Hydraulic System - YellowSystem Ground Service Panel

R REVISED ILLUSTRATION TO LOCATERESERVOIR DEPRESSURIZATION VALVEAND HAND PUMP LEVER.ILLUSTRATION REVISED

Subject 5-4-4 RElectrical System R NOTE AMENDEDFIGURE Ground Service Connections -External Power Receptacles


Subject 5-4-5 ROxygen System NFIGURE Ground Service Connections -Oxygen System

N ADDED ILLUSTRATION FOR OXYGENSYSTEM SERVICING.ILLUSTRATION ADDED

Subject 5-4-6 RFuel System R PART EFFECTIVITY

ADDED/REVISED/DELETED

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LOCATIONS CHGCODE


FIGURE Ground Service Connections -Refuel/Defuel Control Panel

R REVISED ILLUSTRATION TITLE TOREFUEL/DEFUEL CONTROL PANEL.ILLUSTRATION REVISED

FIGURE Ground Service Connections -Refuel/Defuel Couplings


FIGURE Ground Service Connections -Overwing Gravity-Refuel Cap (If Installed)

R REVISED ILLUSTRATION TITLE TOOVERWING GRAVITY-REFUEL CAP.ADDED (IF INSTALLED) IN THE

ILLUSTRATION TITLE.ILLUSTRATION REVISED

FIGURE Ground Service Connections -Overpressure Protectors and NACA VentIntake

R REVISED ILLUSTRATION TO SHOW THEWING TANK OVERPRESSURE-PROTECTOR.ILLUSTRATION REVISED

Subject 5-4-7 RPneumatic System R NOTE AMENDEDFIGURE Ground Service Connections - LPand HP Ground Connectors

N ADDED ILLUSTRATION ABOUT GROUNDSERVICE CONNECTIONS FORPNEUMATIC SYSTEM.ILLUSTRATION ADDED

Subject 5-4-8 R

Oil System R DESCRIPTION TITLE UPDATEDFIGURE Ground Service Connections -Engine Oil Tank -- CFM56 Series Engine

N MIGRATED OIL SYSTEM FROMSECTION 05-04-09 TO 05-04-08.ILLUSTRATION ADDED

FIGURE Ground Service Connections -IDG Oil Tank -- CFM56 Series Engine


FIGURE Ground Service Connections -Starter Oil Tank -- CFM56 Series Engine


FIGURE Ground Service Connections -Engine Oil Tank -- PW6000 Series Engine


FIGURE Ground Service Connections -IDG Oil Tank -- PW6000 Series Engine


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LOCATIONS CHGCODE


FIGURE Ground Service Connections -Starter Oil Tank -- PW6000 Series Engine


FIGURE Ground Service Connections -APU Oil Tank


Subject 5-4-9 RPotable Water System R DESCRIPTION TITLE UPDATEDFIGURE Ground Service Connections -Potable Water Ground Service Panels

N MIGRATED POTABLE WATER SYSTEMFROM SECTION 05-04-08 TO 05-04-09.ILLUSTRATION ADDED

FIGURE Ground Service Connections -Potable Water Tank Location N ADDED ILLUSTRATION OF THEPOTABLE WATER TANK LOCATION.ILLUSTRATION ADDED

Subject 5-4-10 RVacuum Toilet System R NOTE AMENDEDFIGURE Ground Service Connections -Waste Water Ground Service Panel


FIGURE Ground Service Connections -Waste Tank Location

N ILLUSTRATION ADDED


Engine Starting Pneumatic Requirements R CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

FIGURE Example for Use of the Charts N ADDED ILLUSTRATION TO SHOW HOWTO USE THE CHARTS.ILLUSTRATION ADDED

FIGURE Engine Starting PneumaticRequirements - PW 6000 Series Engine

N ADDED ILLUSTRATION FOR THE PW6000 SERIES ENGINE.ILLUSTRATION ADDED

FIGURE Engine Starting PneumaticRequirements - CFM56 Series Engine N ADDED ILLUSTRATION FOR THE CFM56SERIES ENGINE.ILLUSTRATION ADDED

Subject 05-05-01 DSubject 05-05-02 D

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LOCATIONS CHGCODE


Subject 05-05-03 D

Section 5-6 RSubject 5-6-0 RGround Pneumatic Power Requirements RFIGURE Ground Pneumatic PowerRequirements - Heating

N ADDED ILLUSTRATION OF PULL UPPERFORMANCE FOR HEATING THECABIN.ILLUSTRATION ADDED

FIGURE Ground Pneumatic PowerRequirements - Cooling

N ADDED ILLUSTRATION OF PULL DOWNPERFORMANCE FOR COOLING THECABIN.

ILLUSTRATION ADDEDSubject 05-06-01 DSubject 05-06-02 DSection 5-7 RSubject 5-7-0 R

Preconditioned Airflow Requirements R UPDATED SCOPE FOR PRECONDITIONEDAIRFLOW REQUIREMENTS.

FIGURE Preconditioned AirflowRequirements

R REVISED THE COOLING/HEATINGPERFORMANCE GRAPH AS PER THE

NEW CONDITIONS.ILLUSTRATION REVISEDSection 5-8 RSubject 5-8-0 R

Ground Towing Requirements R CROSS REFERENCED MANUAL(S)ADDED/REVISED/DELETEDNOTE AMENDED

FIGURE Ground Towing Requirements R IMPROVED LAYOUT AND REVISEDBREAKAWAY RESISTANCE TO 4%.ILLUSTRATION REVISED


De-Icing and External Cleaning R NOTE AMENDED

CHAPTER 6 R

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LOCATIONS CHGCODE



Engine Exhaust Velocities andTemperatures

R

Subject 6-1-1 REngine Exhaust Velocities Contours -Ground Idle Power

R

FIGURE Engine Exhaust Velocities -Ground Idle Power -- CFM56 series engine


FIGURE Engine Exhaust Velocities -Ground Idle Power -- PW 6000 seriesengine


Subject 6-1-2 REngine Exhaust Temperatures Contours -Ground Idle Power

R

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


FIGURE Engine Exhaust Temperatures -Ground Idle Power -- PW 6000 seriesengine


Subject 6-1-3 REngine Exhaust Velocities Contours -Breakaway Power

R

FIGURE Engine Exhaust Velocities -Breakaway Power -- CFM56 series engine


FIGURE Engine Exhaust Velocities -Breakaway Power -- PW 6000 seriesengine


Subject 6-1-4 R

Engine Exhaust Temperatures Contours -Breakaway Power

R

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


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LOCATIONS CHGCODE


FIGURE Engine Exhaust Temperatures -Breakaway Power -- PW 6000 seriesengine


Subject 6-1-5 REngine Exhaust Velocities Contours -Takeoff Power

R

FIGURE Engine Exhaust Velocities -Takeoff Power -- CFM56 series engine


FIGURE Engine Exhaust Velocities -Takeoff Power -- PW 6000 series engine


Subject 6-1-6 REngine Exhaust Temperatures Contours -Takeoff Power

R

FIGURE Engine Exhaust Temperatures -Takeoff Power -- CFM56 series engine


FIGURE Engine Exhaust Temperatures -Takeoff Power -- PW 6000 series engine



Airport and Community Noise RSubject 6-2-1 R

Noise Data RFIGURE Airport and Community Noise -CFM56-5A Series Engine

R ADDED UNIT dB (A) IN THE TABLE.ILLUSTRATION REVISED

FIGURE Airport and Community Noise -CFM56-5B Series Engine


FIGURE Airport and Community Noise -PW 6000 Series Engine



Danger Areas of Engines RSubject 6-3-1 R

Ground Idle Power R

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LOCATIONS CHGCODE


FIGURE Danger Areas of the Engines -CFM56 series engine


FIGURE Danger Areas of the Engines -PW 6000 series engine


Subject 6-3-2 RTakeoff Power RFIGURE Danger Areas of the Engines -CFM56 series engine


FIGURE Danger Areas of the Engines -PW 6000 series engine



APU - APIC & GARRETT RFIGURE Exhaust Velocities andTemperatures - APU -- APIC &GARRETT


CHAPTER 7 RSection 7-1 R

Subject 7-1-0 RGeneral Information R CROSS REFERENCED DOCUMENTARY

UNIT ADDED/REVISED/DELETED


Landing Gear Footprint R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

FIGURE Landing Gear Footprint R REVISED ILLUSTRATION TO SHOW THE

LANDING GEAR FOOTPRINT DATA FORALL THE WEIGHT VARIANTS.ILLUSTRATION REVISED


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LOCATIONS CHGCODE


Maximum Pavement Loads R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

FIGURE Maximum Pavement Loads R REVISED ILLUSTRATION TO SHOW THEMAXIMUM PAVEMENT LOADS FOR ALLTHE WEIGHT VARIANTS.ILLUSTRATION REVISED


Landing Gear Loading on Pavement R NOTE AMENDEDFIGURE Landing Gear Loading on

Pavement - WV006, MRW 56 400 kg, CG35%

N ADDED ILLUSTRATION FOR LANDING

GEAR LOADING ON PAVEMENT FORWV006.ILLUSTRATION ADDED

FIGURE Landing Gear Loading onPavement - WV005, MRW 68 400 kg, CG32%

N ADDED ILLUSTRATION FOR LANDINGGEAR LOADING ON PAVEMENT FORWV005.ILLUSTRATION ADDED

Subject 07-04-01 DSection 7-5 RSubject 7-5-0 R

Flexible Pavement Requirements - USArmy Corps of Engineers Design Method

R DESCRIPTION TITLE UPDATEDNOTE AMENDED

FIGURE Flexible Pavement Requirements- WV006, MRW 56 400 kg, CG 35 %

N ADDED ILLUSTRATION OF FLEXIBLEPAVEMENT REQUIREMENTS FOR WV006.ILLUSTRATION ADDED

FIGURE Flexible Pavement Requirements- WV005, MRW 68 400 kg, CG 32 %


Subject 07-05-01 D


Flexible Pavement Requirements - LCNConversion

R

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LOCATIONS CHGCODE


FIGURE Flexible Pavement Requirements- LCN Table

N ADDED ILLUSTRATION OF FLEXIBLEPAVEMENT REQUIREMENTS - LCNDATA.ILLUSTRATION ADDED

FIGURE Flexible Pavement Requirements- LCN - WV006, MRW 56 400 kg, CG 35%


FIGURE Flexible Pavement Requirements- LCN - WV005, MRW 68 400 kg, CG 32%


Subject 07-06-01 DSection 7-7 RSubject 7-7-0 R

Rigid Pavement Requirements - PortlandCement Association Design Method

R NOTE AMENDED

FIGURE Rigid Pavement Requirements -WV006, MRW 56 400 kg, CG 35 %

N ADDED ILLUSTRATION OF RIGIDPAVEMENT REQUIREMENTS FOR WV006.ILLUSTRATION ADDED

FIGURE Rigid Pavement Requirements -WV005, MRW 68 400 kg, CG 32 %

N ADDED ILLUSTRATION OF RIGIDPAVEMENT REQUIREMENTS FOR WV005.ILLUSTRATION ADDED

Subject 07-07-01 DSection 7-8 RSubject 7-8-0 N

Rigid Pavement Requirements - LCNConversion

N

FIGURE Rigid Pavement Requirements -LCN Table


FIGURE Radius of Relative Stiffness (L) N ILLUSTRATION ADDED

FIGURE Rigid Pavement Requirements -

LCN - WV006, MRW 56 400 kg, CG 35%


FIGURE Rigid Pavement Requirements -LCN - WV005, MRW 68 400 kg, CG 32%


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LOCATIONS CHGCODE


FIGURE Radius of Relative Stiffness(Effect of E and on L Values)


Subject 07-08-01 DSubject 07-08-02 DSubject 07-08-03 DSubject 07-08-04 DSection 7-9 RSubject 7-9-0 R

Aircraft Classification Number - Flexibleand Rigid Pavements

R DESCRIPTION TITLE UPDATEDNOTE AMENDED

FIGURE Aircraft Classification Number -ACN Table

N ADDED ILLUSTRATION FOR ACN TABLEILLUSTRATION ADDED

FIGURE Aircraft Classification Number -Flexible Pavement - WV006, MRW 56400 kg, CG 35 %

N ADDED ILLUSTRATIONS OF FLEXIBLEAND RIGID PAVEMENT GRAPHS FORWV006.ILLUSTRATION ADDED

FIGURE Aircraft Classification Number -Flexible Pavement - WV005, MRW 68400 kg, CG 32 %

N ADDED ILLUSTRATIONS OF FLEXIBLEAND RIGID PAVEMENT GRAPHS FORWV005.ILLUSTRATION ADDED

Subject 07-09-01 DSubject 07-09-02 D


Scaled Drawings RFIGURE Scaled Drawing R ILLUSTRATION REVISED

CHAPTER 10Section 10-0 RSubject 10-0-0 R

Aircraft Rescue and Fire Fighting RFIGURE Front Page R UPDATED THE REVISION DATE.

ILLUSTRATION REVISED

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LIST OF EFFECTIVE CONTENT

Revision No. 10 - May 01/14

CONTENT CHGCODE

LAST REVISIONDATE

CHAPTER 1Subject 1-1-0

Purpose R May 01/14

Subject 1-2-0

Glossary N May 01/14

CHAPTER 2

Subject 2-1-1General Aircraft Characteristics Data R May 01/14

Subject 2-2-0

General Aircraft Dimensions R May 01/14

FIGURE General Aircraft Dimensions - Wing Tip Fence R May 01/14

Subject 2-3-0

Ground Clearances R May 01/14

FIGURE Ground Clearances R May 01/14

FIGURE Ground Clearances - Ground Clearances with Sharklets R May 01/14FIGURE Ground Clearances - Flaps and Flap Track Fairings WhenFlaps Fully Extended

R May 01/14

FIGURE Ground Clearances - Flap Track Fairings Up R May 01/14

FIGURE Ground Clearances - Aileron Down R May 01/14

FIGURE Ground Clearances - Aileron Up and Spoilers 1 to 5 Extended R May 01/14

FIGURE Ground Clearances - Slats Extended R May 01/14

Subject 2-4-1

Interior Arrangements - Plan View R May 01/14FIGURE Interior Arrangements - Plan View - Typical Configuration -Single-Class, High Density

R May 01/14

FIGURE Interior Arrangements - Plan View - Typical Configuration -Two-Class

R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

Subject 2-5-0

Interior Arrangements - Cross Section R May 01/14FIGURE Interior Arrangements - Cross Section - TypicalConfiguration

R May 01/14

FIGURE Interior Arrangements - Cross Section - Economy Class, 6Abreast - Wider Aisle

R May 01/14

FIGURE Interior Arrangements - Cross Section - First-Class R May 01/14

Subject 2-6-0

Cargo Compartments R May 01/14

FIGURE Cargo Compartments - Locations, Dimensions and Loading

Combinations

R May 01/14

Subject 2-7-0

Door Clearances R May 01/14

FIGURE Door Identification and Location - Door Identification N May 01/14

Subject 2-7-1

Forward Passenger / Crew Doors R May 01/14

FIGURE Doors Clearances - Forward Passenger / Crew Doors R May 01/14

Subject 2-7-2

Emergency Exits R May 01/14FIGURE Doors Clearances - Emergency Exits R May 01/14

Subject 2-7-3

Aft Passenger / Crew Doors R May 01/14

FIGURE Doors Clearances - Aft Passenger / Crew Doors R May 01/14

Subject 2-7-4

Forward Cargo Compartment Door R May 01/14

FIGURE Door Clearances - Forward Cargo Compartment Door R May 01/14

Subject 2-7-5

Aft Cargo Compartment Door R May 01/14

FIGURE Doors Clearances - Aft Cargo Compartment Door R May 01/14

Subject 2-7-7

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CONTENT CHGCODE

LAST REVISIONDATE

Main Landing Gear Doors R May 01/14

FIGURE Doors Clearances - Main Landing Gear Doors R May 01/14Subject 2-7-8

Radome R May 01/14

FIGURE Doors Clearances - Radome R May 01/14

Subject 2-7-9

APU and Nose Landing Gear Doors R May 01/14

FIGURE Doors Clearances - APU and Nose Landing Gear Doors R May 01/14

Subject 2-8-0

Escape Slides R May 01/14FIGURE Escape Slides - Location R May 01/14

FIGURE Escape Slides - Dimensions R May 01/14

Subject 2-9-0

Landing Gear R May 01/14

FIGURE Landing Gear - Main Landing Gear - Twin-Wheel R May 01/14

FIGURE Landing Gear - Main Landing Gear Dimensions - Twin-Wheel R May 01/14

FIGURE Landing Gear - Nose Landing Gear R May 01/14

FIGURE Landing Gear - Nose Landing Gear Dimensions R May 01/14

Landing Gear Maintenance Pits R May 01/14

FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes R May 01/14

FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes R May 01/14

Subject 2-10-0

Exterior Lighting R May 01/14

FIGURE Exterior Lighting R May 01/14




Subject 2-11-0

Antennas and Probes Location R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Antennas and Probes - Location R May 01/14

Subject 2-12-0Auxiliary Power Unit R May 01/14

FIGURE Auxiliary Power Unit - Access Doors R May 01/14

FIGURE Auxiliary Power Unit - General Layout R May 01/14

Engine and Nacelle R May 01/14

FIGURE Power Plant Handling - Major Dimensions - CFM56 SeriesEngine

R May 01/14

FIGURE Power Plant Handling - Major Dimensions - CFM56 SeriesEngine

R May 01/14

FIGURE Power Plant Handling - Fan Cowls - CFM56 Series Engine R May 01/14

FIGURE Power Plant Handling - Thrust Reverser Cowls - CFM56Series Engine

R May 01/14

FIGURE Power Plant Handling - Major Dimensions - PW 6000 SeriesEngine

R May 01/14

FIGURE Power Plant Handling - Nacelle Dimensions - PW 6000Series Engine

R May 01/14

FIGURE Power Plant Handling - Fan Cowls - PW 6000 Series Engine R May 01/14

FIGURE Power Plant Handling - Thrust Reverser Halves - PW 6000Series Engine R May 01/14

Subject 2-13-0

Leveling, Symmetry and Alignment R May 01/14

FIGURE Location of the Leveling Points R May 01/14

Subject 2-14-0

Jacking for Maintenance R May 01/14

FIGURE Jacking for Maintenance - Jacking Point Locations R May 01/14

FIGURE Jacking for Maintenance - Forward Jacking Point R May 01/14FIGURE Jacking for Maintenance - Wing Jacking Points R May 01/14

FIGURE Jacking for Maintenance - Safety Stay R May 01/14

FIGURE Jacking for Maintenance - Jacking Design R May 01/14

Jacking of the Landing Gear R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Jacking of the Landing Gear - MLG Jacking Point Location -Twin Wheels

R May 01/14

FIGURE Jacking of the Landing Gear - MLG Jacking with CantileverJack - Twin Wheels

R May 01/14

FIGURE Jacking of the Landing Gear - Loads at MLG Jacking Points- Twin Wheels

R May 01/14

FIGURE Jacking of the Landing Gear - NLG Jacking - Point Location R May 01/14

FIGURE Jacking of the Landing Gear - Loads at NLG Jacking Points R May 01/14


General Information R May 01/14Subject 3-2-1

ISA Conditions R May 01/14

FIGURE Payload/Range N May 01/14

Subject 3-3-1

Take-Off Weight Limitation - ISA Conditions R May 01/14

FIGURE Take-Off Weight Limitation - ISA Conditions - CFM56Series Engine

R May 01/14

FIGURE Take-Off Weight Limitation - ISA Conditions - PW 6000Series Engine

R May 01/14

Subject 3-3-2

Take-Off Weight Limitation - ISA +15C (+59F) Conditions R May 01/14

FIGURE Take-Off Weight Limitation - ISA +15C (+59F)Conditions - CFM56 Series Engine

R May 01/14

FIGURE Take-Off Weight Limitation - ISA +15C (+59F)Conditions - PW 6000 Series Engine

R May 01/14

Subject 3-4-1

Landing Field Length - ISA Conditions R May 01/14

FIGURE Landing Field Length - ISA Conditions - CFM56-5B SeriesEngine

R May 01/14

FIGURE Landing Field Length - ISA Conditions - PW 6000 SeriesEngine

R May 01/14

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LAST REVISIONDATE

Subject 3-5-0

Final Approach Speed R May 01/14CHAPTER 4Subject 4-1-0

General Information R May 01/14

Subject 4-2-0

Turning Radii R May 01/14

FIGURE Turning Radii, No Slip Angle R May 01/14

FIGURE Turning Radii, No Slip Angle R May 01/14

Subject 4-3-0Minimum Turning Radii R May 01/14

FIGURE Minimum Turning Radii R May 01/14

Subject 4-4-0

Visibility from Cockpit in Static Position R May 01/14

FIGURE Visibility from Cockpit in Static Position R May 01/14

FIGURE Binocular Visibility Through Windows from Captain EyePosition

R May 01/14

Subject 4-5-0Runway and Taxiway Turn Paths R May 01/14

Subject 4-5-1

135 Turn - Runway to Taxiway R May 01/14

FIGURE 135 Turn - Runway to Taxiway - Cockpit Over CenterlineMethod

R May 01/14

FIGURE 135 Turn - Runway to Taxiway - Judgemental OversteeringMethod

R May 01/14

Subject 4-5-2

90 Turn - Runway to Taxiway R May 01/14

FIGURE 90 Turn - Runway to Taxiway - Cockpit Over CenterlineMethod

R May 01/14

FIGURE 90 Turn - Runway to Taxiway - Judgemental OversteeringMethod

R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

Subject 4-5-3

180 Turn on a Runway R May 01/14FIGURE 180 turn on a Runway - Edge of Runway Method R May 01/14

Subject 4-5-4

135 Turn - Taxiway to Taxiway R May 01/14

FIGURE 135 Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod

R May 01/14

Subject 4-5-5

90 Turn - Taxiway to Taxiway R May 01/14

FIGURE 90 Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod

R May 01/14

Subject 4-6-0

Runway Holding Bay (Apron) R May 01/14

FIGURE Runway Holding Bay (Apron) R May 01/14

Subject 4-7-0

Minimum Line-Up Distance Corrections R May 01/14

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

N May 01/14

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

N May 01/14

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

N May 01/14

Subject 4-8-0

Aircraft Mooring N May 01/14

FIGURE Aircraft Mooring N May 01/14

CHAPTER 5

Subject 5-1-1Aircraft Servicing Arrangements R May 01/14

Subject 5-1-2

Typical Ramp Layout - Open Apron R May 01/14

FIGURE Typical Ramp Layout - Open Apron - Bulk Loading R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

Subject 5-1-3

Typical Ramp Layout - Gate R May 01/14FIGURE Typical Ramp Layout - Gate R May 01/14

Subject 5-2-0

Terminal Operations - Full Servicing Turn Round Time R May 01/14

FIGURE Full Servicing Turn Round Time Chart R May 01/14

Subject 5-3-0

Terminal Operations - Outstation Turn Round Time R May 01/14

FIGURE Outstation Turn Round Time Chart R May 01/14

Subject 5-4-1Ground Service Connections Layout R May 01/14

FIGURE Ground Service Connections Layout R May 01/14

Subject 5-4-2

Grounding (Earthing) Points R May 01/14

FIGURE Ground Service Connections - Grounding (Earthing) Points -Landing Gear

R May 01/14

FIGURE Ground Service Connections - Grounding (Earthing) Points -Wing (If Installed)

R May 01/14

FIGURE Ground Service Connections - Grounding (Earthing) Point -Avionics Compartment Door-Frame

N May 01/14

FIGURE Ground Service Connections - Grounding (Earthing) Point -Engine Air Intake (If Installed)

N May 01/14

Subject 5-4-3

Hydraulic System R May 01/14

FIGURE Hydraulic System - Green System Ground Service Panel R May 01/14

FIGURE Hydraulic System - Blue System Ground Service Panel R May 01/14

FIGURE Hydraulic System - Yellow System Ground Service Panel R May 01/14

Subject 5-4-4

Electrical System R May 01/14

FIGURE Ground Service Connections - External Power Receptacles R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Ground Service Connections - Potable Water Ground ServicePanels

N May 01/14

FIGURE Ground Service Connections - Potable Water Tank Location N May 01/14

Subject 5-4-10

Vacuum Toilet System R May 01/14

FIGURE Ground Service Connections - Waste Water Ground ServicePanel

R May 01/14

FIGURE Ground Service Connections - Waste Tank Location N May 01/14

Subject 5-5-0

Engine Starting Pneumatic Requirements R May 01/14

FIGURE Example for Use of the Charts N May 01/14FIGURE Engine Starting Pneumatic Requirements - PW 6000 SeriesEngine

N May 01/14

FIGURE Engine Starting Pneumatic Requirements - CFM56 SeriesEngine

N May 01/14

Subject 5-6-0

Ground Pneumatic Power Requirements R May 01/14

FIGURE Ground Pneumatic Power Requirements - Heating N May 01/14

FIGURE Ground Pneumatic Power Requirements - Cooling N May 01/14Subject 5-7-0

Preconditioned Airflow Requirements R May 01/14

FIGURE Preconditioned Airflow Requirements R May 01/14

Subject 5-8-0

Ground Towing Requirements R May 01/14

FIGURE Ground Towing Requirements R May 01/14

Subject 5-9-0

De-Icing and External Cleaning R May 01/14


Engine Exhaust Velocities and Temperatures R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

Subject 6-1-1

Engine Exhaust Velocities Contours - Ground Idle Power R May 01/14FIGURE Engine Exhaust Velocities - Ground Idle Power -- CFM56series engine

R May 01/14

FIGURE Engine Exhaust Velocities - Ground Idle Power -- PW 6000series engine

R May 01/14

Subject 6-1-2

Engine Exhaust Temperatures Contours - Ground Idle Power R May 01/14

FIGURE Engine Exhaust Temperatures - Ground Idle Power -- CFM56series engine

R May 01/14

FIGURE Engine Exhaust Temperatures - Ground Idle Power -- PW6000 series engine

R May 01/14

Subject 6-1-3

Engine Exhaust Velocities Contours - Breakaway Power R May 01/14

FIGURE Engine Exhaust Velocities - Breakaway Power -- CFM56series engine

R May 01/14

FIGURE Engine Exhaust Velocities - Breakaway Power -- PW 6000series engine

R May 01/14

Subject 6-1-4

Engine Exhaust Temperatures Contours - Breakaway Power R May 01/14

FIGURE Engine Exhaust Temperatures - Breakaway Power -- CFM56series engine

R May 01/14

FIGURE Engine Exhaust Temperatures - Breakaway Power -- PW6000 series engine

R May 01/14

Subject 6-1-5

Engine Exhaust Velocities Contours - Takeoff Power R May 01/14

FIGURE Engine Exhaust Velocities - Takeoff Power -- CFM56 series

engine

R May 01/14

FIGURE Engine Exhaust Velocities - Takeoff Power -- PW 6000 seriesengine

R May 01/14

Subject 6-1-6

Engine Exhaust Temperatures Contours - Takeoff Power R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Engine Exhaust Temperatures - Takeoff Power -- CFM56series engine

R May 01/14

FIGURE Engine Exhaust Temperatures - Takeoff Power -- PW 6000series engine

R May 01/14

Subject 6-2-0

Airport and Community Noise R May 01/14

Subject 6-2-1

Noise Data R May 01/14

FIGURE Airport and Community Noise - CFM56-5A Series Engine R May 01/14

FIGURE Airport and Community Noise - CFM56-5B Series Engine R May 01/14

FIGURE Airport and Community Noise - PW 6000 Series Engine R May 01/14

Subject 6-3-0

Danger Areas of Engines R May 01/14

Subject 6-3-1

Ground Idle Power R May 01/14

FIGURE Danger Areas of the Engines - CFM56 series engine R May 01/14

FIGURE Danger Areas of the Engines - PW 6000 series engine R May 01/14

Subject 6-3-2

Takeoff Power R May 01/14

FIGURE Danger Areas of the Engines - CFM56 series engine R May 01/14

FIGURE Danger Areas of the Engines - PW 6000 series engine R May 01/14

Subject 6-4-1

APU - APIC & GARRETT R May 01/14

FIGURE Exhaust Velocities and Temperatures - APU -- APIC &GARRETT

R May 01/14


General Information R May 01/14

Subject 7-2-0

Landing Gear Footprint R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Landing Gear Footprint R May 01/14

Subject 7-3-0Maximum Pavement Loads R May 01/14

FIGURE Maximum Pavement Loads R May 01/14

Subject 7-4-0

Landing Gear Loading on Pavement R May 01/14

FIGURE Landing Gear Loading on Pavement - WV006, MRW 56 400kg, CG 35%

N May 01/14

FIGURE Landing Gear Loading on Pavement - WV005, MRW 68 400kg, CG 32%

N May 01/14

Subject 7-5-0

Flexible Pavement Requirements - US Army Corps of EngineersDesign Method

R May 01/14

FIGURE Flexible Pavement Requirements - WV006, MRW 56 400 kg,CG 35 %

N May 01/14

FIGURE Flexible Pavement Requirements - WV005, MRW 68 400 kg,CG 32 %

N May 01/14

Subject 7-6-0

Flexible Pavement Requirements - LCN Conversion R May 01/14

FIGURE Flexible Pavement Requirements - LCN Table N May 01/14

FIGURE Flexible Pavement Requirements - LCN - WV006, MRW 56400 kg, CG 35 %

N May 01/14

FIGURE Flexible Pavement Requirements - LCN - WV005, MRW 68400 kg, CG 32 %

N May 01/14

Subject 7-7-0

Rigid Pavement Requirements - Portland Cement Association DesignMethod

R May 01/14

FIGURE Rigid Pavement Requirements - WV006, MRW 56 400 kg,CG 35 % N May 01/14

FIGURE Rigid Pavement Requirements - WV005, MRW 68 400 kg,CG 32 %

N May 01/14

Subject 7-8-0

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LAST REVISIONDATE

Rigid Pavement Requirements - LCN Conversion N May 01/14

FIGURE Rigid Pavement Requirements - LCN Table N May 01/14FIGURE Radius of Relative Stiffness (L) N May 01/14

FIGURE Rigid Pavement Requirements - LCN - WV006, MRW 56400 kg, CG 35 %

N May 01/14

FIGURE Rigid Pavement Requirements - LCN - WV005, MRW 68400 kg, CG 32 %

N May 01/14

FIGURE Radius of Relative Stiffness (Effect of E and on LValues)

N May 01/14

Subject 7-9-0

Aircraft Classification Number - Flexible and Rigid Pavements R May 01/14FIGURE Aircraft Classification Number - ACN Table N May 01/14

FIGURE Aircraft Classification Number - Flexible Pavement - WV006,MRW 56 400 kg, CG 35 %

N May 01/14

FIGURE Aircraft Classification Number - Flexible Pavement - WV005,MRW 68 400 kg, CG 32 %

N May 01/14


Scaled Drawings R May 01/14FIGURE Scaled Drawing R May 01/14


Aircraft Rescue and Fire Fighting R May 01/14

FIGURE Front Page R May 01/14

FIGURE Highly Flammable and Hazardous Materials and Components R May 01/14

FIGURE Batteries Location and Access N May 01/14

FIGURE Wheel/Brake Overheat - Wheel Safety Area R May 01/14

FIGURE Composite Materials R May 01/14

FIGURE L/G Ground Lock Safety Devices R May 01/14

FIGURE Emergency Evacuation Devices R May 01/14

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CONTENT CHGCODE

LAST REVISIONDATE

FIGURE Pax/Crew Doors R May 01/14

FIGURE Emergency Exit Hatch R May 01/14FIGURE FWD and AFT Lower Deck Cargo Doors R May 01/14

FIGURE Control Panels R May 01/14

FIGURE APU Access Door R May 01/14

FIGURE Aircraft Ground Clearances R May 01/14

FIGURE Structural Break-in Points R May 01/14

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TABLE OF CONTENTS

1 SCOPE1-1-0 Introduction1-2-0 Glossary

2 AIRCRAFT DESCRIPTION2-1-1 General Aircraft Characteristics Data2-2-0 General Aircraft Dimensions2-3-0 Ground Clearances2-4-1 Interior Arrangements - Plan View2-5-0 Interior Arrangements - Cross Section

2-6-0 Cargo Compartments2-7-0 Door Clearances and Location2-7-1 Forward Passenger / Crew Doors2-7-2 Emergency Exits2-7-3 Aft Passenger / Crew Doors2-7-4 Forward Cargo Compartment Door2-7-5 Aft Cargo Compartment Door2-7-7 Main Landing Gear Doors2-7-8 Radome

2-7-9 APU and Nose Landing Gear Doors2-8-0 Escape Slides2-9-0 Landing Gear2-10-0 Exterior Lighting2-11-0 Antennas and Probes Location2-12-0 Power Plant2-13-0 Leveling, Symmetry and Alignment2-14-0 Jacking

3 AIRCRAFT PERFORMANCE3-1-0 General Information3-2-1 Payload / Range - ISA Conditions3-3-1 Take-off Weight Limitation - ISA Conditions3-3-2 Take-off Weight Limitation - ISA +15C (+59F) Conditions3-4-1 Landing Field Length - ISA Conditions3-5-0 Final Approach Speed

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4 GROUND MANEUVERING4-1-0 General Information4-2-0 Turning Radii4-3-0 Minimum Turning Radii4-4-0 Visibility from Cockpit in Static Position4-5-0 Runway and Taxiway Turn Paths4-5-1 135 Turn - Runway to Taxiway4-5-2 90 Turn - Runway to Taxiway4-5-3 180 Turn on a Runway4-5-4 135 Turn - Taxiway to Taxiway4-5-5 90 Turn - Taxiway to Taxiway4-6-0 Runway Holding Bay (Apron)

4-7-0 Minimum Line-Up Distance Corrections4-8-0 Aircraft Mooring

5 TERMINAL SERVICING5-1-1 Aircraft Servicing Arrangements5-1-2 Typical Ramp Layout - Open Apron5-1-3 Typical Ramp Layout - Gate5-2-0 Terminal Operations - Full Servicing Turn Round Time Chart5-3-0 Terminal Operation - Outstation Turn Round Time Chart

5-4-1 Ground Service Connections5-4-2 Grounding Points5-4-3 Hydraulic System5-4-4 Electrical System5-4-5 Oxygen System5-4-6 Fuel System5-4-7 Pneumatic System5-4-8 Oil System5-4-9 Potable Water System5-4-10 Waste Water System5-5-0 Engine Starting Pneumatic Requirements5-6-0 Ground Pneumatic Power Requirements5-7-0 Preconditioned Airflow Requirements5-8-0 Ground Towing Requirements5-9-0 De-Icing and External Cleaning

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6 OPERATING CONDITIONS6-1-0 Engine Exhaust Velocities and Temperatures6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power6-1-3 Engine Exhaust Velocities Contours - Breakaway Power6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power6-1-5 Engine Exhaust Velocities Contours - Takeoff Power6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power6-2-0 Airport and Community Noise6-2-1 Noise Data6-3-0 Danger Areas of Engines6-3-1 Ground Idle Power6-3-2 Takeoff Power

6-4-1 APU

7 PAVEMENT DATA7-1-0 General Information7-2-0 Landing Gear Footprint7-3-0 Maximum Pavement Loads7-4-0 Landing Gear Loading on Pavement7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method7-6-0 Flexible Pavement Requirements - LCN Conversion7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method7-8-0 Rigid Pavement Requirements - LCN Conversion7-9-0 ACN/PCN Reporting System - Flexible and Rigid Pavements

8 SCALED DRAWINGS8-0-0 SCALED DRAWINGS

10 AIRCRAFT RESCUE AND FIRE FIGHTING10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING

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SCOPE

1-1-0 Introduction

**ON A/C A318-100Purpose1. General

The A318 AIRCRAFT CHARACTERISTICS -- AIRPORT AND MAINTENANCE PLANNING (AC)manual is issued for the A318-100 series aircraft equipped with wing-tip fences or sharklets, toprovide necessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO)for airport and maintenance facilities planning.

This document is not customized and must not be used for training purposes. No information withinmay constitute a contractual commitment.

The A320 Family is the worlds best-selling single-aisle aircraft. An A320 takes off or landssomewhere in the world every 2.5 seconds of every day, the family has logged more than 50 millioncycles since entry-into-service and records a best-in-class dispatch reliability of 99.7%.

To ensure this true market leadership, Airbus continues to invest in improvements in the A320Family: enhancements to aerodynamics such as the sharklet wingtip devices, upgrades to the widestpassenger cabin in its class, the A320 Family neo (New Engine Option). The latter combines top-of-class engine efficiency offered by two new engine options: the PW1100G PurePower fromPratt&Whitney and the LEAP-1A from CFM International with superior aerodynamics offered by thenew sharklet devices.

The neo will offer a minimum of 15% fuel savings and an additional flight range of about 500 nm(926 km). For the environment, the neo fuel savings will translate into some 3 600 t (7 936 639 lb)less CO2 per aircraft per year, together with a double-digit reduction in NOx emissions and reducedengine noise.

Correspondence concerning this publication should be directed to:

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

1-1-0

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1-2-0 Glossary

**ON A/C A318-100

Glossary

1. List of AbbreviationsA/C AircraftACN Aircraft Classification NumberAMM Aircraft Maintenance ManualAPU Auxiliary Power UnitB/C Business ClassCBR California Bearing RatioCC Cargo CompartmentCG Center of Gravity

CKPT CockpitE Youngs ModulusELEC Electric, Electrical, ElectricityESWL Equivalent Single Wheel LoadFAA Federal Aviation AdministrationF/C First ClassFDL Fuselage Datum LineFR FrameFSTE Full Size Trolley Equivalent

FWD ForwardGPU Ground Power UnitGSE Ground Support EquipmentHYD HydraulicICAO International Civil Aviation OrganisationIDG Integrated Drive GeneratorISA International Standard AtmosphereL LeftL Radius of relative stiffnessLCN Load Classification NumberLD Lower DeckL/G Landing GearLH Left HandLPS Last Pax SeatingMAC Mean Aerodynamic ChordMAX Maximum

1-2-0

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MIN MinimumMLG Main Landing GearNLG Nose Landing GearOAT Outside Air TemperaturePAX PassengerPBB Passenger Boarding BridgePCA Portland Cement AssociationPCN Pavement Classification NumberPRM Passenger with Reduced MobilityR RightRH Right HandULD Unit Load DeviceUS United States

WV Weight VariantY/C Tourist 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 Takeoff Weight (MTOW):Maximum weight for takeoff 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.

1-2-0

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2-1-1 General Aircraft Characteristics Data

**ON A/C A318-100

General Aircraft Characteristics Data

1. The following table provides characteristics of A318-100 Models, these data are specific to eachWeight Variant:

Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004

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

59 400 kg(130 955 lb)

61 900 kg(136 466 lb)

63 400 kg(139 773 lb)

64 900 kg(143 080 lb)

66 400 kg(146 387 lb)

Maximum Take-Off Weight(MTOW)

59 000 kg(130 073 lb)

61 500 kg(135 584 lb)

63 000 kg(138 891 lb)

64 500 kg(142 198 lb)

66 000 kg(145 505 lb)

Maximum Landing Weight(MLW)

56 000 kg(123 459 lb)

56 000 kg(123 459 lb)

57 500 kg(126 766 lb)

57 500 kg(126 766 lb)

57 500 kg(126 766 lb)

Maximum Zero Fuel Weight(MZFW)

53 000 kg(116 845 lb)

53 000 kg(116 845 lb)

54 500 kg(120 152 lb)

54 500 kg(120 152 lb)

54 500 kg(120 152 lb)

Aircraft CharacteristicsWV005 WV006 WV007 WV008

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

68 400 kg(150 796 lb)

56 400 kg(124 341 lb)

61 400 kg(135 364 lb)

64 400 kg(141 978 lb)

Maximum Take-Off Weight(MTOW) 68 000 kg(149 914 lb) 56 000 kg(123 459 lb) 61 000 kg(134 482 lb) 64 000 kg(141 096 lb)Maximum Landing Weight (MLW) 57 500 kg

(126 766 lb)56 000 kg

(123 459 lb)56 000 kg

(123 459 lb)56 000 kg

(123 459 lb)Maximum Zero Fuel Weight(MZFW)

54 500 kg(120 152 lb)

53 000 kg(116 845 lb)

53 000 kg(116 845 lb)

53 000 kg(116 845 lb)

2. The following table provides characteristics of A318-100 Models, these data are common to eachWeight Variant:

Aircraft CharacteristicsStandard Seating Capacity 132 (Single-Class)

23 859 l(6 303 US gal)

Usable Fuel Capacity(density = 0.785 kg/l)

18 729 kg(41 290 lb)

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Aircraft CharacteristicsPressurized Fuselage Volume(A/C non equipped)

257 m3

(9 076 ft3)Passenger CompartmentVolume

107 m3

(3 779 ft3)Cockpit Volume 9 m3

(318 ft3)Usable Volume, FWD CC 6.72 m3

(237 ft3)Usable Volume, AFT CC 8.87 m3

(313 ft3)Usable Volume, Bulk CC 5.71 m3

(202 ft3)

Water Volume, FWD CC 8.34 m3

(295 ft3)Water Volume, AFT CC 10.38 m3

(367 ft3)Water Volume, Bulk CC 5.97 m3

(211 ft 3)

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2-2-0 General Aircraft Dimensions

**ON A/C A318-100

General Aircraft Dimensions

1. This section provides general aircraft dimensions.

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**ON A/C A318-100

RELATED TO AIRCRAFT ATTITUDE AND WEIGHT

12.45 m(40.85 ft)

34.10 m(111.88 ft)

4 . 1 4 m

( 1 3 . 5 8 f t )

10.25 m

(33.63 ft)

5.07 m

(16.63 ft)

6 . 6 2 m

( 2 1 . 7 2 f t )

7.59 m(24.90 ft)

0.93 m(3.05 ft)

0.50 m(1.64 ft)

8.95 m(29.36 ft)

N_AC_020200_1_0010101_01_03

General Aircraft DimensionsWing Tip Fence (Sheet 1 of 4)

FIGURE-2-2-0-991-001-A01

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**ON A/C A318-100

RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.NOTE:

4.91 m(16.11 ft)

CFM56

PW6000

1.50 m(4.92 ft)

1.82 m(5.97 ft)

5.75 m

(18.86 ft)

6.07 m(19.91 ft)

3.95 m(12.96 ft)

1.24 m(4.07 ft)

3.31 m(10.86 ft)

31.45 m(103.18 ft)

8.80 m(28.87 ft)

9.10 m(29.86 ft)

8.32 m(27.30 ft) 11.93 m

(39.14 ft)

20.07 m(65.85 ft)

0.76 m(2.49 ft)

N_AC_020200_1_0010107_01_01

General Aircraft DimensionsWing Tip Fence (Sheet 2 of 4)

FIGURE-2-2-0-991-001-A01

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**ON A/C A318-100

RELATED TO AIRCRAFT ATTITUDE AND WEIGHT

4 . 1 4 m

( 1 3 . 5 8 f t )

10.25 m(33.63 ft)

5.07 m(16.63 ft)

6 . 6 2 m

( 2 1 . 7 2 f t )

12.45 m(40.85 ft)

35.80 m(117.45 ft)

7.59 m(24.90 ft)

0.93 m(3.05 ft)

0.50 m(1.64 ft)

8.95 m(29.36 ft)

3.79 m(12.43 ft)

2.43 m(7.97 ft)

N_AC_020200_1_0010102_01_01

General Aircraft DimensionsSharklet (Sheet 3 of 4)

FIGURE-2-2-0-991-001-A01

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**ON A/C A318-100

4.91 m(16.11 ft)

1.64 m(5.38 ft)

3.22 m(10.56 ft)

1.61 m(5.28 ft)

5.75 m

(18.86 ft)

6.07 m(19.91 ft)

3.95 m(12.96 ft)

1.24 m(4.07 ft)

3.31 m(10.86 ft)

31.45 m(103.18 ft)

8.32 m(27.30 ft) 11.93 m

(39.14 ft)

21.06 m(69.09 ft)

16.29 m(53.44 ft)

RELATED TO AIRCRAFT ATTITUDE AND WEIGHT.NOTE:

CFM56

PW6000

8.80 m(28.87 ft)

9.10 m(29.86 ft)

N_AC_020200_1_0010108_01_01

General Aircraft DimensionsSharklet (Sheet 4 of 4)

FIGURE-2-2-0-991-001-A01

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**ON A/C A318-100

F O R D I M E N S I O N S

, S E E S H E E T 2 .

P A S S E N G E R A N D C A R G O D O O R G R O U N D C L E A R A N C E S A R E M E A S U R E D

F R O M T H E C E N T E R O F T H E D O O R S I L L A N D F R O M F L O O R L E V E L .

N O T E :

J

Q

P

A

H

D 2

G C 2

N

D 1 B

C 1

E

K 2

F 3

F 2

F

F 1

L

K 1

N_AC_020300_1_0010101_01_06

Ground Clearances(Sheet 1 of 2)

FIGURE-2-3-0-991-001-A01

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**ON A/C A318-100

A

C G 2 5 %

F W D C G 1 5

. 8 %

A F T C G 3 2 %

B C 1

C 2

D 1

D 2

E ( C F M )

E ( P W )

F F 1

F 2

F 3 G H J K

1 K 2 L N P Q

m

f t

m

f t

m

f t

m

f t

A / C J A C K E D

F D L =

4 . 6 0 m

( 1 5 . 0 9 f t )

A / C

C O N F I G U R A T I O N

3 9 0 0 0 k g

( 8 5 9 8 0 l b )

M R W

3 . 4

5

2 . 0

8

1 . 7

9

1 . 9

3

5 . 9

3

6 . 0

8

0 . 6

6

0 . 7

8

1 . 7

4

2 . 7

3

3 . 1

7

3 . 5

1

2 . 2

0

3 . 7

2

1 2 . 8

9

3 . 9

2

4 . 8

9

5 . 6

2

3 . 9

7

4 . 2

2

4 . 9

1

1 1 . 3

2

6 . 8 2

5 . 8 7

6 . 3 3

1 9 . 4

6

1 9 . 9

5

2 . 1 7

2 . 5 6

5 . 7 1

8 . 9 6

1 0 . 4

0

1 1 . 5

2

7 . 2 2

1 2 . 2

0

4 2 . 2

9

1 2 . 8

6

1 6 . 0

4

1 8 . 4

4

1 3 . 0

2

1 3 . 8

5

1 6 . 1

1

3 . 3 7

2 . 0 0

1 . 7 1

1 . 8 7

5 . 8 6

6 . 0 2

0 . 5 9

0 . 7 1

1 . 6 7

2 . 6 7

3 . 1 1

3 . 4 5

2 . 1 4

3 . 6 7

1 2 . 8

5

3 . 8 6

4 . 8 3

5 . 5 7

3 . 9 0

4 . 1 3

4 . 8 7

1 1 . 0

6

6 . 5 6

5 . 6 1

6 . 1 4

1 9 . 2

3

1 9 . 7

5

1 . 9 4

2 . 3 3

5 . 4 8

8 . 7 6

1 0 . 2

0

1 1 . 3

2

7 . 0 2

1 2 . 0

4

4 2 . 1

6

1 2 . 6

6

1 5 . 8

5

1 8 . 2

7

1 2 . 8

0

1 3 . 5

5

1 5 . 9

8

3 . 4 2

2 . 0 3

1 . 7 4

1 . 8 4

5 . 8 9

5 . 9 9

0 . 6 0

0 . 7 2

1 . 6 5

2 . 6 5

3 . 0 8

3 . 4 2

2 . 1 1

3 . 6 0

1 2 . 7

4

3 . 8 2

4 . 7 9

5 . 4 6

3 . 9 0

4 . 2 1

4 . 7 5

1 1 . 2 2

6 . 6

6

5 . 7

1

6 . 0

4

1 9 . 3 2

1 9 . 6 5

1 . 9

7

2 . 3

6

5 . 4

1

8 . 6

9

1 0 . 1 0

1 1 . 2 2

6 . 9

2

1 1 . 8 1

4 1 . 8 0

1 2 . 5 3

1 5 . 7 2

1 7 . 9 1

1 2 . 8 0

1 3 . 8 1

1 5 . 5 8

4 . 1 3

2 . 7 1

2 . 4 3

2 . 4 3

6 . 5 8

6 . 5 8

1 . 2 4

1 . 3 6

2 . 2 6

3 . 2 5

3 . 6 8

4 . 0 1

2 . 7 1

4 . 1 3

1 3 . 2

0

4 . 3 8

5 . 3 5

5 . 9 3

4 . 5 4

4 . 9 6

5 . 2 0

1 3 . 5

5

8 . 8 9

7 . 9 7

7 . 9 7

2 1 . 5

9

2 1 . 5

9

4 . 0 7

4 . 4 6

7 . 4 1

1 0 . 6

6

1 2 . 0

7

1 3 . 1

6

8 . 8 9

1 3 . 5

5

4 3 . 3

1

1 4 . 3

7

1 7 . 5

5

1 9 . 4

6

1 4 . 8

9

1 6 . 2

7

1 7 . 0

6

N_AC_020300_1_0010102_01_00

Ground Clearances(Sheet 2 of 2)

FIGURE-2-3-0-991-001-A01

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**ON A/C A318-100

F O R D I M E N S I O N S

, S E E S H E E T 2 .

P A S S E N G E R A N D C A R G O D O O R G R O U N D C L E A R A N C E S A R E M E A S U R E D

F R O M T H E C E N T E R O F T H E D O O R S I L L A N D F R O M F L O O R L E V E L .

N O T E :

J

Q

E

P

A

H

G C 2

N

D 1 B

C 1

D 2

F 3

F 2

F

F 1

L

K 1 K 2

N_AC_020300_1_0270101_01_01

Ground ClearancesGround Clearances with Sharklets (Sheet 1 of 2)

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

2-3-0

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**ON A/C A318-100

A

C G 2 5 %

F W D C G 1 5

. 8 %

A F T C G 3 2 %

B C 1

C 2

D 1

D 2

E ( C F M )

E ( P W )

F F 1

F 2

F 3 G H J K

1 K 2 L N P Q

m

f t

m

f t

m

f t

m

f t

A / C J A C K E D

F D L =

4 . 6 0 m

( 1 5 . 0 9 f t )

A / C

C O N F I G U R A T I O N

3 9 0 0 0 k g

( 8 5 9 8 0 l b )

M R W

3 . 4

5

2 . 0

8

1 . 7

9

1 . 9

3

5 . 9

3

6 . 0

8

0 . 6

6

0 . 7

8

1 . 7

4

2 . 7

3

3 . 1

7

3 . 5

1

2 . 2

0

3 . 7

2

1 2 . 8

9

5 . 6

2

3 . 9

7

4 . 2

2

4 . 9

1

1 1 . 3

2

6 . 8 2

5 . 8 7

6 . 3 3

1 9 . 4

6

1 9 . 9

5

2 . 1 7

2 . 5 6

5 . 7 1

8 . 9 6

1 0 . 4

0

1 1 . 5

2

7 . 2 2

1 2 . 2

0

4 2 . 2

9

1 8 . 4

4

1 3 . 0

2

1 3 . 8

5

1 6 . 1

1

3 . 3 7

2 . 0 0

1 . 7 1

1 . 8 7

5 . 8 6

6 . 0 2

0 . 5 9

0 . 7 1

1 . 6 7

2 . 6 7

3 . 1 1

3 . 4 5

2 . 1 4

3 . 6 7

1 2 . 8

5

5 . 5 7

3 . 9 0

4 . 1 3

4 . 8 7

1 1 . 0

6

6 . 5 6

5 . 6 1

6 . 1 4

1 9 . 2

3

1 9 . 7

5

1 . 9 4

2 . 3 3

5 . 4 8

8 . 7 6

1 0 . 2

0

1 1 . 3

2

7 . 0 2

1 2 . 0

4

4 2 . 1

6

1 8 . 2

7

1 2 . 8

0

1 3 . 5

5

1 5 . 9

8

3 . 4 2

2 . 0 3

1 . 7 4

1 . 8 4

5 . 8 9

5 . 9 9

0 . 6 0

0 . 7 2

1 . 6 5

2 . 6 5

3 . 0 8

3 . 4 2

2 . 1 1

3 . 6 0

1 2 . 7

4

5 . 4 6

3 . 9 0

4 . 2 1

4 . 7 5

1 1 . 2 2

6 . 6

6

5 . 7

1

6 . 0

4

1 9 . 3 2

1 9 . 6 5

1 . 9

7

2 . 3

6

5 . 4

1

8 . 6

9

1 0 . 1 0

1 1 . 2 2

6 . 9

2

1 1 . 8 1

4 1 . 8 0

1 7 . 9 1

1 2 . 8 0

1 3 . 8 1

1 5 . 5 8

4 . 1 3

2 . 7 1

2 . 4 3

2 . 4 3

6 . 5 8

6 . 5 8

1 . 2 4

1 . 3 6

2 . 2 6

3 . 2 5

3 . 6 8

4 . 0 1

2 . 7 1

4 . 1 3

1 3 . 2

0

5 . 9 3

4 . 5 4

4 . 9 6

5 . 2 0

1 3 . 5

5

8 . 8 9

7 . 9 7

7 . 9 7

2 1 . 5

9

2 1 . 5

9

4 . 0 7

4 . 4 6

7 . 4 1

1 0 . 6

6

1 2 . 0

7

1 3 . 1

6

8 . 8 9

1 3 . 5

5

4 3 . 3

1

1 9 . 4

6

1 4 . 8

9

1 6 . 2

7

1 7 . 0

6

4 . 6 5

7 . 2 9

1 5 . 2

6

2 3 . 9

2

4 . 1

9

6 . 8

3

1 3 . 7

5

2 2 . 4

1

4 . 1 3

6 . 7 7

1 3 . 5

5

2 2 . 2

1

4 . 0 9

6 . 7 3

1 3 . 4 2

2 2 . 0 8

N_AC_020300_1_0270102_01_00

Ground ClearancesGround Clearances with Sharklets (Sheet 2 of 2)

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

2-3-0

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**ON A/C A318-100

m ft m ft m ftA

B

C

D

2.05

2.77

2.81

3.65

1.99

2.71

2.75

3.60

1.96

2.68

2.72

3.54

6.73 6.53 6.43

11.6111.8111.98

9.09

9.22

8.89

9.02

8.79

8.92

HEIGHT FROM GROUND

MAXIMUM RAMPWEIGHT AFT CG

AC DB

E

F

G

2.1

2.59

3.05

2.03

2.53

2.99

2.0

2.49

2.94 9.659.8110.01

6.89

8.50

6.66

8.30

6.56

8.17

E FG

N_AC_020300_1_0060101_01_00

MAXIMUM RAMPWEIGHT FWD CG

A/C IN MAINTENANCECONFIGURATION

MID CG

Ground ClearancesFlaps and Flap Track Fairings When Flaps Fully Extended

FIGURE-2-3-0-991-006-A01

2-3-0

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**ON A/C A318-100

ML

m ft m ft m ft

L

M

4.19

3.84

4.13

3.78

4.07

3.74

13.75 13.55 13.35

12.60 12.40 12.27

HEIGHT FROM GROUND

N_AC_020300_1_0080101_01_00




MID CG

Ground ClearancesAileron Down

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

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**ON A/C A318-100

m ft m ft m ft

P

Q 4.60

4.48

4.35

4.54

4.42

4.29

4.50

4.38

4.26

15.09 14.89 14.76

14.70

14.27

14.50

14.07

14.37

13.98

HEIGHT FROM GROUND

R

S

T

U

4.21

4.07

4.01

4.15

4.01

3.94

4.12

3.98

3.92

13.81 13.62 13.52

13.35

13.16

13.16

12.93

13.06

12.86

3.75 3.69 3.6612.30 12.11 12.01

T U V WQ R SPN

N 4.574.37

4.514.31

4.264.45

14.99 14.80 13.9814.34 14.14 14.60

N_AC_020300_1_0090101_01_00




MID CG

V

W

Ground ClearancesAileron Up and Spoilers 1 to 5 Extended

FIGURE-2-3-0-991-009-A01

2-3-0

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2-4-1 Interior Arrangements - Plan View

**ON A/C A318-100

Interior Arrangements - Plan View

1. This section gives the typical interior configuration.

2-4-1

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**ON A/C A318-100

A A

A

I T E M

D E S I G N A T I O N

G

G A L L E Y

( 2 )

L

L A V A T O R Y

( 2 )

A

A T T E N D A N T S E A T ( 4 )

L

L

A

G

G

F W D P A S S E N G E R

/ C R E W

D O O R

E M E R G E N C Y E X I T

A F T P A S S E N G E R

/ C R E W

D O O R


/ C R E W

D O O R



/ C R E W

D O O R

1 3 2 S E A T S A L L T O U R I S T C L A S S

2 9 / 3 0 i n

P I T C H

. 6 A B R E A S T

. 3 . 3

N_AC_020401_1_0010101_01_01

Interior Arrangements - Plan ViewTypical Configuration - Single-Class, High Density

FIGURE-2-4-1-991-001-A01

2-4-1

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**ON A/C A318-100

I T E M

D E

S I G N A T I O N

8

S U P E R F I R S T C L A S S

P A S S E N G E R S E A T S ( 1 0 7 T O T A L )

L

L A V A T O R Y

( 2 )

G

G A L L E Y

( 3 )

A

A T T E N D A N T S E A T ( 3 )

S E A T P I T C H E S :

/ C R E W D

O O R



/ C R E W

D O O R


9 9 E C O N O M Y C L A S S

F I R S T 3 8 i n

E C O N O M Y 3 2 i n



/ C R E W D

O O R


/ C R E W

D O O R

G

A A

L

A

L G

L

N_AC_020401_1_0070101_01_00

Interior Arrangements - Plan ViewTypical Configuration - Two-Class

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

2-4-1

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2-5-0 Interior Arrangements - Cross Section

**ON A/C A318-100

Interior Arrangements - Cross Section

1. This section gives the typical configuration.

2-5-0

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**ON A/C A318-100

3.95

(155.51)

Cargo CompartmentFloor

CABINFLOOR

Top of cargoCompartment

AircraftDatum

W i n d o w s

2.64(103.94)

2.13

(83.86)

1.60(62.99)

1.24(48.82)

NOTE: DIMENSIONS m (in)

0.49(19.29)

0.52(20.47)

N_AC_020500_1_0010101_01_01

3.45(135.83)

3.68(144.88)

1.42(55.91)

Interior Arrangements - Cross SectionTypical Configuration

FIGURE-2-5-0-991-001-A01

2-5-0

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**ON A/C A318-100


1 . 2 4

( 4 8 . 9 )

2 . 2 1

( 8 7 )

6 ABREASTWIDER AISLE

4 . 1 4

( 1 6 3 )

3.95(155.5)

3.64(143)

1.50(59)

0.64(25)

1.50(59)

0.432(17)

N_AC_020500_1_0050101_01_00

Interior Arrangements - Cross SectionEconomy Class, 6 Abreast - Wider Aisle (Sheet 1 of 2)

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

2-5-0

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**ON A/C A318-100


6 ABREASTWIDER SEAT

3.95(155.5)

3.64(143)

1.58(62)

0.48(19)

1.58(62)

1 . 2 4

( 4 8 . 9 )

2 . 2 1

( 8 7 )

4 . 1 4

( 1 6 3 )0.457

(18)

N_AC_020500_1_0050102_01_02

Interior Arrangements - Cross SectionEconomy Class, 6 Abreast - Wider Seat (Sheet 2 of 2)

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

2-5-0

Page 4May 01/14

Airbus-AC A318 May2014

Documents

Transcript of Airbus-AC A318 May2014