Post on 13-Jul-2018
@AIRBUSA318
AIRCRAFT CHARACTERISTICSAIRPORT AND MAINTENANCE PLANNING
AC
The content of this document is the property of Airbus.It is supplied in confidence and commercial security on its contents must be maintained.It must not be used for any purpose other than that for which it is supplied, nor mayinformation contained in it be disclosed to unauthorized persons.It must not be reproduced in whole or in part without permission in writing from the owners ofthe copyright. Requests for reproduction of any data in this document and the media authorizedfor it must be addressed to Airbus.
© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.Customer Services
Technical Data Support and Services31707 Blagnac Cedex
FRANCE
Issue: Jul 01/02 Rev: Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 9 - Jun 01/12
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 1 R
Section 1-1
Subject 1-1-0
Purpose R PURPOSE CHANGED DUE TO MERGE OFTHE MFP AND AC MANUALS.
Section 01-02 D
CHAPTER 2 R
Section 2-1 R
Subject 2-1-0 R
General Airplane Characteristics R WEIGHT DEFINITIONS UPDATED.
Subject 2-1-1 R
General Airplane Characteristics Data R OEW AND PAYLOAD DELETED.
Section 2-2 R
Subject 2-2-0 R
General Aircraft Dimensions R REPLACED ”AIRPLANE” BY ”AIRCRAFT”AND COMPLETED TITLE OFILLUSTRATIONS.DESCRIPTION TITLE UPDATED
FIGURE General Aircraft Dimensions -Wing Tip Fence
R ILLUSTRATION REVISED
Section 2-3
Subject 2-3-0
Ground Clearances R REVISED GROUND CLEARANCES TOSHOW THE DIMENSIONS FOR A LIGHTAND HEAVY WEIGHT VARIANT.DELETED THE TERM ”OWE”.
FIGURE Ground Clearances R
FIGURE Ground Clearances - GroundClearances with Sharklets
N ILLUSTRATION ADDED
HIGHLIGHTSPage 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Clearances - Flaps andFlap Track Fairings When Flaps FullyExtended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Flap TrackFairings Up
N ILLUSTRATION ADDED
FIGURE Ground Clearances - AileronDown
N ILLUSTRATION ADDED
FIGURE Ground Clearances - Aileron Upand Spoilers 1 to 5 Extended
N ILLUSTRATION ADDED
FIGURE Ground Clearances - SlatsExtended
N ILLUSTRATION ADDED
Section 2-6 R
Subject 2-6-0
Cargo Compartments R
FIGURE Cargo Compartments -Locations, Dimensions and LoadingCombinations
N ILLUSTRATION ADDED
Subject 02-06-01 D
Section 2-8 N
Subject 2-8-0 N
Escape Slides N
FIGURE Escape Slides - Location N ILLUSTRATION ADDED
FIGURE Escape Slides - Dimensions N ILLUSTRATION ADDED
Section 2-9 N
Subject 2-9-0 N
Landing Gear N
FIGURE Landing Gear - Main LandingGear - Twin Wheel
N ILLUSTRATION ADDED
FIGURE Landing Gear - Main LandingGear Dimensions - Twin Wheel
N ILLUSTRATION ADDED
FIGURE Landing Gear - Nose LandingGear
N ILLUSTRATION ADDED
FIGURE Landing Gear - Nose LandingGear Dimensions
N ILLUSTRATION ADDED
HIGHLIGHTSPage 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Landing Gear Maintenance Pits N
FIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes
N ILLUSTRATION ADDED
FIGURE Landing Gear Maintenance Pits -Maintenance Pit Envelopes
N ILLUSTRATION ADDED
Section 2-10 N
Subject 2-10-0 N
Exterior Lighting N
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
FIGURE Exterior Lighting N ILLUSTRATION ADDED
Section 2-11 N
Subject 2-11-0 N
Antennas and Probes Location N
FIGURE Antennas and Probes - Location N ILLUSTRATION ADDED
Section 2-12 N
Subject 2-12-0 N
Auxiliary Power Unit N
FIGURE Auxiliary Power Unit - AccessDoors
N ILLUSTRATION ADDED
FIGURE Auxiliary Power Unit - GeneralLayout
N ILLUSTRATION ADDED
Engine and Nacelle N
FIGURE Power Plant Handling - MajorDimensions - CFM56 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - MajorDimensions - CFM56 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - FanCowls - CFM56 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - ThrustReverser Cowls - CFM56 Series Engine
N ILLUSTRATION ADDED
HIGHLIGHTSPage 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Power Plant Handling - MajorDimensions - PW 6000 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - NacelleDimensions - PW 6000 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - FanCowls - PW 6000 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - ThrustReverser Halves - PW 6000 Series Engine
N ILLUSTRATION ADDED
Section 2-13 N
Subject 2-13-0 N
Leveling, Symmetry and Alignment N
FIGURE Location of the Leveling Points N ILLUSTRATION ADDED
Section 2-14 N
Subject 2-14-0 N
Jacking for Maintenance N
FIGURE Jacking for Maintenance -Jacking Point Location
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Forward Jacking Point
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - WingJacking Points
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance - SafetyStay
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Jacking Design
N ILLUSTRATION ADDED
Jacking for Wheel Change N
FIGURE Landing Gear Jacking for WheelChange - MLG Jacking Point Location -Twin Wheels
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - MLG Jacking with CantileverJack - Twin Wheels
N ILLUSTRATION ADDED
HIGHLIGHTSPage 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Landing Gear Jacking for WheelChange - Loads at MLG Jacking Points -Twin Wheels
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - NLG Jacking - Point Location
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at NLG Jacking Points
N ILLUSTRATION ADDED
CHAPTER 3 R
CHAPTER 4
Section 4-2
Subject 4-2-0
FIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISED
FIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISED
Section 4-3
Subject 4-3-0
FIGURE Minimum Turning Radii R
Section 4-4
Subject 4-4-0
Visibility from Cockpit in Static Position R
FIGURE Visibility from Cockpit in StaticPosition
R
FIGURE Binocular Visibility ThroughWindows from Captain Eye Position
N ILLUSTRATION ADDED
Section 4-5 R
Subject 4-5-1
135˚ Turn - Runway to Taxiway R
FIGURE 135˚ Turn - Runway to Taxiway- Cockpit Over Centerline Method
R
FIGURE 135˚ Turn - Runway to Taxiway- Judgemental Oversteering Method
N ILLUSTRATION ADDED
Subject 4-5-2
90˚ Turn - Runway to Taxiway R
HIGHLIGHTSPage 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE 90˚ Turn - Runway to Taxiway -Cockpit Over Centerline Method
R
FIGURE 90˚ Turn - Runway to Taxiway -Judgemental Oversteering Method
N ILLUSTRATION ADDED
Subject 4-5-3 N
180˚ Turn on a Runway N
FIGURE 180˚ turn on a Runway - Edgeof Runway Method
N ILLUSTRATION ADDED
Subject 4-5-4
FIGURE 135˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
R ILLUSTRATION REVISED
Subject 4-5-5
FIGURE 90˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
R ILLUSTRATION REVISED
Subject 04-05-06 D
Section 4-6
Subject 4-6-0
FIGURE Runway Holding Bay (Apron) R
Section 4-7 R
Subject 4-7-0 R
CHAPTER 5 R
Section 5-1 R
Subject 5-1-0 R
Subject 5-1-2 R
Typical Ramp Layout - Open Apron R TITLE CHANGED FROM ”AIRCRAFT ATTHE GATE” TO ”TYPICAL RAMPLAYOUT - OPEN APRON”. ADDED”STAND SAFETY LINE” DEFINITION.DESCRIPTION TITLE UPDATED
FIGURE Typical Ramp Layout - OpenApron - Bulk Loading
R ILLUSTRATION REVISED
Subject 5-1-3 R
HIGHLIGHTSPage 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Typical Ramp Layout - Gate R TITLE CHANGED FROM ”AIRCRAFT ATAN OPEN APRON” TO ”TYPICAL RAMPLAYOUT - GATE”. ADDED ”STANDSAFETY LINE” DEFINITION.DESCRIPTION TITLE UPDATED
FIGURE Typical Ramp Layout - Gate R ILLUSTRATION REVISED
Section 5-2 R
Subject 5-2-0 R
Terminal Operations - Full Servicing TurnRound Time
R DESCRIPTION TITLE UPDATED
FIGURE Turn Round Stations - FullServicing (34 Min.)
N ILLUSTRATION ADDED
Subject 05-02-01 D
Section 5-3 R
Subject 5-3-0 R
Terminal Operation - Minimum ServicingTurn Round Time
R DESCRIPTION TITLE UPDATED
FIGURE Turn Round Stations - MinimumServicing (20 Min.)
N ILLUSTRATION ADDED
Subject 05-03-01 D
Section 5-4
Subject 5-4-1
Ground Service Connections Layout R DELETED GROUND SERVICECONNECTIONS LAYOUT TABLE.
FIGURE Ground Service Connections -Ground Service Connections Layout
R
Subject 5-4-3
Hydraulic System R
Subject 5-4-4
Electrical System R
Subject 5-4-6
Fuel System R NOTE AMENDED
HIGHLIGHTSPage 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Service Connections -Overpressure Protector and NACA FlameArrestor
N ADDED OVERPRESSURE PROTECTORAND NACA FLAME ARRESTORILLUSTRATION.ILLUSTRATION ADDED
Section 5-5
Subject 5-5-0
Engine Starting Pneumatic Requirements R CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements - Engine StartingPneumatic Requirements
N ILLUSTRATION ADDED
Subject 5-5-1 R
Low Ambient Temperatures R DESCRIPTION TITLE UPDATED
FIGURE Engine Starting PneumaticRequirements - Low AmbientTemperature -40˚C (-40˚F) -- CFM56series engine
R
FIGURE Engine Starting PneumaticRequirements - Low AmbientTemperature -40˚C (-40˚F) -- PW 6000series engine
R
Subject 5-5-2 R
Medium Ambient Temperatures R DESCRIPTION TITLE UPDATED
FIGURE Engine Starting PneumaticRequirements - Medium AmbientTemperature +15˚C (+59˚F) -- CFM56series engine
R
FIGURE Engine Starting PneumaticRequirements - Medium AmbientTemperature +15˚C (+59˚F) -- PW6000 series engine
R
Subject 5-5-3 R
High Ambient Temperatures R DESCRIPTION TITLE UPDATED
HIGHLIGHTSPage 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Engine Starting PneumaticRequirements - High AmbientTemperature +50˚C (+122˚F) -- CFM56series engine
R
FIGURE Engine Starting PneumaticRequirements - High AmbientTemperature +38˚C (+100˚F) -- PW6000 series engine
R
Section 5-6
Subject 5-6-0
Ground Pneumatic Power Requirements R ADDED NOTE FOR GROUND PNEUMATICPOWER REQUIREMENTS.
Section 5-8
Subject 5-8-0
Ground Towing Requirements R SAE REFERENCES UPDATED ANDFIGURES CORRESPONDING TO TYPICALTOW BAR CONFIGURATION DELETEDNOTE AMENDED
Section 5-9 N
Subject 5-9-0 N
De-Icing and External Cleaning N REVISED TABLES FOR DE-ICING ANDEXTERNAL CLEANING AREAS.
CHAPTER 7
Section 7-8 R
Subject 07-08-00 D
Subject 7-8-1
FIGURE Radius of Relative Stiffness -(Reference: Portland Cement Association)
R
Subject 7-8-2
Rigid Pavement Requirements - LCNConversion
R MOVED THE TEXT FROM 7-8-0 TO 7-8-2.
CHAPTER 8 R
Section 8-0 N
Subject 8-0-0 N
HIGHLIGHTSPage 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Scaled Drawings N
FIGURE Scaled Drawing N ILLUSTRATION ADDED
Section 08-01 D
CHAPTER 10 N
Section 10-0 N
Subject 10-0-0 N
Aircraft Rescue and Fire Fighting N
FIGURE Front Page N ILLUSTRATION ADDED
FIGURE Highly Flammable and HazardousMaterials and Components
N ILLUSTRATION ADDED
FIGURE Wheel Safety Area N ILLUSTRATION ADDED
FIGURE Composite Materials N ILLUSTRATION ADDED
FIGURE LG Ground Lock Safety Devices N ILLUSTRATION ADDED
FIGURE Evacuation/Escape Slide/Raft N ILLUSTRATION ADDED
FIGURE Pax/Crew Doors N ILLUSTRATION ADDED
FIGURE Emergency Exit Hatch N ILLUSTRATION ADDED
FIGURE FWD and AFT Lower DeckCargo Doors
N ILLUSTRATION ADDED
FIGURE Control Panels N ILLUSTRATION ADDED
FIGURE APU Access Door N ILLUSTRATION ADDED
FIGURE Aircraft Ground Clearances N ILLUSTRATION ADDED
FIGURE Structural Break-in Points N ILLUSTRATION ADDED
HIGHLIGHTSPage 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 9 - Jun 01/12
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 1
Subject 1-1-0
Purpose R Jun 01/12
CHAPTER 2
Subject 2-1-0
General Airplane Characteristics R Jun 01/12
Subject 2-1-1
General Airplane Characteristics Data R Jun 01/12
Subject 2-2-0
General Aircraft Dimensions R Jun 01/12
FIGURE General Aircraft Dimensions - Wing Tip Fence R Jun 01/12
Subject 2-3-0
Ground Clearances R Jun 01/12
FIGURE Ground Clearances R Jun 01/12
FIGURE Ground Clearances - Ground Clearances with Sharklets N Jun 01/12
FIGURE Ground Clearances - Flaps and Flap Track Fairings WhenFlaps Fully Extended
N Jun 01/12
FIGURE Ground Clearances - Flap Track Fairings Up N Jun 01/12
FIGURE Ground Clearances - Aileron Down N Jun 01/12
FIGURE Ground Clearances - Aileron Up and Spoilers 1 to 5 Extended N Jun 01/12
FIGURE Ground Clearances - Slats Extended N Jun 01/12
Subject 2-4-0
Interior Arrangements Dec 01/07
Subject 2-4-1
Typical Configuration Sep 01/10
FIGURE Typical Configuration - Typical Configuration Single-Class,High Density
Sep 01/10
L.E.C.Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Typical Configuration - Typical Configuration Two-Class Sep 01/10
Subject 2-5-0
Passenger Compartment Cross-section Sep 01/10
FIGURE Passenger Compartment Cross-section Sep 01/10
FIGURE Passenger Compartment Cross-section - Economy Class, 6Abreast - Wider Aisle
Sep 01/10
FIGURE Passenger Compartment Cross-section - PassengerCompartment Cross-section, First-class
Sep 01/10
Subject 2-6-0
Cargo Compartments R Jun 01/12
FIGURE Cargo Compartments - Locations, Dimensions and LoadingCombinations
N Jun 01/12
Subject 2-7-0
Doors Clearances Dec 01/07
Subject 2-7-1
Forward Passenger / Crew Doors Dec 01/07
FIGURE Doors Clearances - Forward Passenger / Crew Doors Dec 01/07
Subject 2-7-2
Emergency Exits Dec 01/07
FIGURE Doors Clearances - Emergency Exits Dec 01/07
Subject 2-7-3
Aft Passenger / Crew Doors Dec 01/07
FIGURE Doors Clearances - Aft Passenger / Crew Doors Dec 01/07
Subject 2-7-4
Forward Cargo Compartment Door Dec 01/07
FIGURE Doors Clearances - Forward Cargo Compartment Door Dec 01/07
Subject 2-7-5
Aft Cargo Compartment Door Dec 01/07
FIGURE Doors Clearances - Aft Cargo Compartment Door Dec 01/07
Subject 2-7-7
L.E.C.Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Main Landing Gear Doors Dec 01/07
FIGURE Doors Clearances - Main Landing Gear Doors Dec 01/07
Subject 2-7-8
Radome Dec 01/07
FIGURE Doors Clearances - Radome Dec 01/07
Subject 2-7-9
APU and Nose Landing Gear Doors Dec 01/07
FIGURE Doors Clearances - APU and Nose Landing Gear Doors Dec 01/07
Subject 2-8-0
Escape Slides N Jun 01/12
FIGURE Escape Slides - Location N Jun 01/12
FIGURE Escape Slides - Dimensions N Jun 01/12
Subject 2-9-0
Landing Gear N Jun 01/12
FIGURE Landing Gear - Main Landing Gear - Twin Wheel N Jun 01/12
FIGURE Landing Gear - Main Landing Gear Dimensions - Twin Wheel N Jun 01/12
FIGURE Landing Gear - Nose Landing Gear N Jun 01/12
FIGURE Landing Gear - Nose Landing Gear Dimensions N Jun 01/12
Landing Gear Maintenance Pits N Jun 01/12
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes N Jun 01/12
FIGURE Landing Gear Maintenance Pits - Maintenance Pit Envelopes N Jun 01/12
Subject 2-10-0
Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
FIGURE Exterior Lighting N Jun 01/12
Subject 2-11-0
Antennas and Probes Location N Jun 01/12
L.E.C.Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Antennas and Probes - Location N Jun 01/12
Subject 2-12-0
Auxiliary Power Unit N Jun 01/12
FIGURE Auxiliary Power Unit - Access Doors N Jun 01/12
FIGURE Auxiliary Power Unit - General Layout N Jun 01/12
Engine and Nacelle N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - CFM56 SeriesEngine
N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - CFM56 SeriesEngine
N Jun 01/12
FIGURE Power Plant Handling - Fan Cowls - CFM56 Series Engine N Jun 01/12
FIGURE Power Plant Handling - Thrust Reverser Cowls - CFM56Series Engine
N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - PW 6000 SeriesEngine
N Jun 01/12
FIGURE Power Plant Handling - Nacelle Dimensions - PW 6000Series Engine
N Jun 01/12
FIGURE Power Plant Handling - Fan Cowls - PW 6000 Series Engine N Jun 01/12
FIGURE Power Plant Handling - Thrust Reverser Halves - PW 6000Series Engine
N Jun 01/12
Subject 2-13-0
Leveling, Symmetry and Alignment N Jun 01/12
FIGURE Location of the Leveling Points N Jun 01/12
Subject 2-14-0
Jacking for Maintenance N Jun 01/12
FIGURE Jacking for Maintenance - Jacking Point Location N Jun 01/12
FIGURE Jacking for Maintenance - Forward Jacking Point N Jun 01/12
FIGURE Jacking for Maintenance - Wing Jacking Points N Jun 01/12
FIGURE Jacking for Maintenance - Safety Stay N Jun 01/12
FIGURE Jacking for Maintenance - Jacking Design N Jun 01/12
Jacking for Wheel Change N Jun 01/12
L.E.C.Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Jacking for Wheel Change - MLG JackingPoint Location - Twin Wheels
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - MLG Jacking withCantilever Jack - Twin Wheels
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at MLGJacking Points - Twin Wheels
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - NLG Jacking -Point Location
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at NLGJacking Points
N Jun 01/12
CHAPTER 3
Subject 3-1-0
General Information Dec 01/07
Subject 3-2-0
Payload / Range Dec 01/07
Subject 3-2-1
ISA Conditions Dec 01/07
FIGURE Payload / Range - CFM56 series engine Dec 01/07
FIGURE Payload / Range - PW 6000 series engine Dec 01/07
Subject 3-3-0
FAR / JAR Take-off Weight Limitation Dec 01/07
Subject 3-3-1
ISA Conditions Dec 01/07
FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions --CFM56 series engine
Dec 01/07
FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions --PW 6000 series engine
Dec 01/07
Subject 3-3-2
ISA +15˚C (+59˚F) Conditions Dec 01/07
FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C(+59˚F) Conditions -- CFM56 series engine
Dec 01/07
L.E.C.Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C(+59˚F) Conditions -- PW 6000 series engine
Dec 01/07
Subject 3-4-0
FAR / JAR Landing Field Length Dec 01/07
Subject 3-4-1
ISA Conditions Dec 01/07
FIGURE FAR / JAR Landing Field Length - CFM56-5B series engine Dec 01/07
FIGURE FAR / JAR Landing Field Length - PW 6000 series engine Dec 01/07
Subject 3-5-0
Final Approach Speed Dec 01/07
FIGURE Final Approach Speed - CFM56-5B8 and CFM56-5B9 seriesengine
Dec 01/07
FIGURE Final Approach Speed - PW 6000 series engine Dec 01/07
CHAPTER 4
Subject 4-1-0
General Information Dec 01/07
Subject 4-2-0
Turning Radii Dec 01/07
FIGURE Turning Radii, No Slip Angle R Jun 01/12
FIGURE Turning Radii, No Slip Angle R Jun 01/12
Subject 4-3-0
Minimum Turning Radii Dec 01/07
FIGURE Minimum Turning Radii R Jun 01/12
Subject 4-4-0
Visibility from Cockpit in Static Position R Jun 01/12
FIGURE Visibility from Cockpit in Static Position R Jun 01/12
FIGURE Binocular Visibility Through Windows from Captain EyePosition
N Jun 01/12
Subject 4-5-0
Runway and Taxiway Turn Paths Dec 01/07
L.E.C.Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Subject 4-5-1
135˚ Turn - Runway to Taxiway R Jun 01/12
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
N Jun 01/12
Subject 4-5-2
90˚ Turn - Runway to Taxiway R Jun 01/12
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
N Jun 01/12
Subject 4-5-3
180˚ Turn on a Runway N Jun 01/12
FIGURE 180˚ turn on a Runway - Edge of Runway Method N Jun 01/12
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway Dec 01/07
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway Dec 01/07
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
Subject 4-6-0
Runway Holding Bay (Apron) Dec 01/07
FIGURE Runway Holding Bay (Apron) R Jun 01/12
Subject 4-7-0
Airplane Parking Dec 01/07
FIGURE Airplane Parking - Minimum Parking Space Requirements Dec 01/07
FIGURE Airplane Parking - Steering Geometry Dec 01/07
FIGURE Airplane Parking - Steering Geometry Dec 01/07
L.E.C.Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Airplane Parking - Steering Geometry Dec 01/07
FIGURE Airplane Parking - Steering Geometry Dec 01/07
FIGURE Airplane Parking - Steering Geometry Dec 01/07
FIGURE Airplane Parking - Steering Geometry Dec 01/07
FIGURE Airplane Parking - Steering Geometry Dec 01/07
CHAPTER 5
Subject 5-0-0
Terminal Servicing Sep 01/10
Subject 5-1-0
Airplane Servicing Arrangements Sep 01/10
Subject 5-1-1
Symbols Used on Servicing Diagrams Sep 01/10
Subject 5-1-2
Typical Ramp Layout - Open Apron R Jun 01/12
FIGURE Typical Ramp Layout - Open Apron - Bulk Loading R Jun 01/12
Subject 5-1-3
Typical Ramp Layout - Gate R Jun 01/12
FIGURE Typical Ramp Layout - Gate R Jun 01/12
Subject 5-2-0
Terminal Operations - Full Servicing Turn Round Time R Jun 01/12
FIGURE Turn Round Stations - Full Servicing (34 Min.) N Jun 01/12
Subject 5-3-0
Terminal Operation - Minimum Servicing Turn Round Time R Jun 01/12
FIGURE Turn Round Stations - Minimum Servicing (20 Min.) N Jun 01/12
Subject 5-4-0
Ground Service Connections Dec 01/07
Subject 5-4-1
Ground Service Connections Layout R Jun 01/12
L.E.C.Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Ground Service Connections - Ground Service ConnectionsLayout
R Jun 01/12
Subject 5-4-2
Grounding Points Dec 01/07
FIGURE Ground Service Connections - Grounding Points Dec 01/07
FIGURE Ground Service Connections - Grounding Points Dec 01/07
Subject 5-4-3
Hydraulic System R Jun 01/12
FIGURE Hydraulic System - Green System Ground Service Panel Sep 01/10
FIGURE Hydraulic System - Blue System Ground Service Panel Sep 01/10
FIGURE Hydraulic System - Yellow System Ground Service Panel Sep 01/10
Subject 5-4-4
Electrical System R Jun 01/12
FIGURE Ground Service Connections - External Power Receptacles Sep 01/10
Subject 5-4-5
Oxygen System Dec 01/07
Subject 5-4-6
Fuel System R Jun 01/12
FIGURE Ground Service Connections - Refuel/Defuel Panel Sep 01/10
FIGURE Ground Service Connections - Refuel/Defuel Couplings Sep 01/10
FIGURE Ground Service Connections - Gravity Refuel Couplings Sep 01/10
FIGURE Ground Service Connections - Overpressure Protector andNACA Flame Arrestor
N Jun 01/12
Subject 5-4-7
Pneumatic System Sep 01/10
Subject 5-4-8
Potable Water System Sep 01/10
FIGURE Ground Service Connections - Potable Water Ground ServicePanel
Sep 01/10
Subject 5-4-9
L.E.C.Page 9
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Oil System Sep 01/10
FIGURE Ground Service Connections - Engine Oil Tank -- CFM56Series Engine
Sep 01/10
FIGURE Ground Service Connections - IDG Oil Tank -- CFM56 SeriesEngine
Sep 01/10
FIGURE Ground Service Connections - Starter Oil Tank -- CFM56Series Engine
Sep 01/10
FIGURE Ground Service Connections - Engine Oil Tank -- PW 6000Series Engine
Sep 01/10
FIGURE Ground Service Connections - IDG Oil Tank -- PW 6000Series Engine
Sep 01/10
FIGURE Ground Service Connections - Starter Oil Tank -- PW 6000Series Engine
Sep 01/10
FIGURE Ground Service Connections - APU Oil Tank Dec 01/07
Subject 5-4-10
Vacuum Toilet System Sep 01/10
FIGURE Ground Service Connections - Waste Water Ground ServicePanel
Sep 01/10
Subject 5-5-0
Engine Starting Pneumatic Requirements R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Engine StartingPneumatic Requirements
N Jun 01/12
Subject 5-5-1
Low Ambient Temperatures R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Low AmbientTemperature -40˚C (-40˚F) -- CFM56 series engine
R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Low AmbientTemperature -40˚C (-40˚F) -- PW 6000 series engine
R Jun 01/12
Subject 5-5-2
Medium Ambient Temperatures R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - Medium AmbientTemperature +15˚C (+59˚F) -- CFM56 series engine
R Jun 01/12
L.E.C.Page 10
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Starting Pneumatic Requirements - Medium AmbientTemperature +15˚C (+59˚F) -- PW 6000 series engine
R Jun 01/12
Subject 5-5-3
High Ambient Temperatures R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - High AmbientTemperature +50˚C (+122˚F) -- CFM56 series engine
R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - High AmbientTemperature +38˚C (+100˚F) -- PW 6000 series engine
R Jun 01/12
Subject 5-6-0
Ground Pneumatic Power Requirements R Jun 01/12
Subject 5-6-1
Heating Dec 01/07
FIGURE Ground Pneumatic Power Requirements - Heating Dec 01/07
Subject 5-6-2
Cooling Dec 01/07
FIGURE Ground Pneumatic Power Requirements - Cooling Dec 01/07
Subject 5-7-0
Preconditioned Airflow Requirements Dec 01/07
FIGURE Preconditioned Airflow Requirements Dec 01/07
Subject 5-8-0
Ground Towing Requirements R Jun 01/12
FIGURE Ground Towing Requirements Sep 01/10
Subject 5-9-0
De-Icing and External Cleaning N Jun 01/12
CHAPTER 6
Subject 6-1-0
Engine Exhaust Velocities and Temperatures Dec 01/07
Subject 6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power Dec 01/07
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Exhaust Velocities - Ground Idle Power -- CFM56series engine
Dec 01/07
FIGURE Engine Exhaust Velocities - Ground Idle Power -- PW 6000series engine
Dec 01/07
Subject 6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power Dec 01/07
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- CFM56series engine
Dec 01/07
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- PW6000 series engine
Dec 01/07
Subject 6-1-3
Engine Exhaust Velocities Contours - Breakaway Power Dec 01/07
FIGURE Engine Exhaust Velocities - Breakaway Power -- CFM56series engine
Dec 01/07
FIGURE Engine Exhaust Velocities - Breakaway Power -- PW 6000series engine
Dec 01/07
Subject 6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power Dec 01/07
FIGURE Engine Exhaust Temperatures - Breakaway Power -- CFM56series engine
Dec 01/07
FIGURE Engine Exhaust Temperatures - Breakaway Power -- PW6000 series engine
Dec 01/07
Subject 6-1-5
Engine Exhaust Velocities Contours - Takeoff Power Dec 01/07
FIGURE Engine Exhaust Velocities - Takeoff Power -- CFM56 seriesengine
Dec 01/07
FIGURE Engine Exhaust Velocities - Takeoff Power -- PW 6000 seriesengine
Dec 01/07
Subject 6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power Dec 01/07
FIGURE Engine Exhaust Temperatures - Takeoff Power -- CFM56series engine
Dec 01/07
L.E.C.Page 12
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Exhaust Temperatures - Takeoff Power -- PW 6000series engine
Dec 01/07
Subject 6-2-0
Airport and Community Noise Dec 01/07
Subject 6-2-1
Noise Data Dec 01/07
FIGURE Airport and Community Noise - CFM56-5A series engine Dec 01/07
FIGURE Airport and Community Noise - CFM56-5B series engine Dec 01/07
FIGURE Airport and Community Noise - PW 6000 series engine Dec 01/07
Subject 6-3-0
Danger Areas of Engines Dec 01/07
Subject 6-3-1
Ground Idle Power Dec 01/07
FIGURE Danger Areas of Engines - CFM56 series engine Dec 01/07
FIGURE Danger Areas of Engines - PW 6000 series engine Dec 01/07
Subject 6-3-2
Takeoff Power Dec 01/07
FIGURE Danger Areas of Engines - CFM56 series engine Dec 01/07
FIGURE Danger Areas of Engines - PW 6000 series engine Dec 01/07
Subject 6-4-0
APU Exhaust Velocities and Temperatures Dec 01/07
Subject 6-4-1
APU - APIC & GARRETT Dec 01/07
FIGURE Exhaust Velocities and Temperatures - APU -- APIC &GARRETT
Dec 01/07
CHAPTER 7
Subject 7-1-0
General Information May 01/11
FIGURE Aircraft Codes May 01/11
Subject 7-2-0
L.E.C.Page 13
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint - Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint - Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint - Landing Gear Footprint May 01/11
Subject 7-3-0
Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/11
Subject 7-4-0
Landing Gear Loading on Pavement May 01/11
Subject 7-4-1
Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
Subject 7-5-0
Flexible Pavement Requirements - U.S. Army Corps of EngineersDesign Method
May 01/11
Subject 7-5-1
Flexible Pavement Requirements - U.S. Army Corps of EngineersDesign Method
May 01/11
FIGURE Flexible Pavement Requirements May 01/11
L.E.C.Page 14
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
Subject 7-6-0
Flexible Pavement Requirements - LCN Conversion May 01/11
Subject 7-6-1
Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
Subject 7-7-0
Rigid Pavement Requirements - Portland Cement Association DesignMethod
May 01/11
Subject 7-7-1
Rigid Pavement Requirements - Portland Cement Association DesignMethod
May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
L.E.C.Page 15
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
Subject 7-8-1
Radius of Relative Stiffness Dec 01/07
FIGURE Radius of Relative Stiffness - (Reference: Portland CementAssociation)
R Jun 01/12
Subject 7-8-2
Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
Subject 7-8-3
Radius of Relative Stiffness (Other values of ”E” and ”L”) May 01/11
Subject 7-8-4
Radius of Relative Stiffness Dec 01/07
FIGURE Radius of Relative Stiffness - (Effect E and µ on ”L” values) May 01/11
Subject 7-9-0
ACN/PCN Reporting System May 01/11
L.E.C.Page 16
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
Subject 7-9-1
Aircraft Classification Number - Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
Subject 7-9-2
Aircraft Classification Number - Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
CHAPTER 8
Subject 8-0-0
Scaled Drawings N Jun 01/12
FIGURE Scaled Drawing N Jun 01/12
CHAPTER 10
Subject 10-0-0
L.E.C.Page 17
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CONTENT CHGCODE
LAST REVISIONDATE
Aircraft Rescue and Fire Fighting N Jun 01/12
FIGURE Front Page N Jun 01/12
FIGURE Highly Flammable and Hazardous Materials and Components N Jun 01/12
FIGURE Wheel Safety Area N Jun 01/12
FIGURE Composite Materials N Jun 01/12
FIGURE LG Ground Lock Safety Devices N Jun 01/12
FIGURE Evacuation/Escape Slide/Raft N Jun 01/12
FIGURE Pax/Crew Doors N Jun 01/12
FIGURE Emergency Exit Hatch N Jun 01/12
FIGURE FWD and AFT Lower Deck Cargo Doors N Jun 01/12
FIGURE Control Panels N Jun 01/12
FIGURE APU Access Door N Jun 01/12
FIGURE Aircraft Ground Clearances N Jun 01/12
FIGURE Structural Break-in Points N Jun 01/12
L.E.C.Page 18
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TABLE OF CONTENTS
1 SCOPE
1-1-0 Purpose
2 AIRCRAFT DESCRIPTION
2-1-0 General Aircraft Characteristics
2-1-1 General Aircraft Characteristics Data
2-2-0 General Aircraft Dimensions
2-3-0 Ground Clearances
2-4-0 Interior Arrangements
2-4-1 Passenger Compartment Layout
2-5-0 Passenger Compartment Cross Section
2-6-0 Cargo Compartments
2-7-0 Door Clearances
2-7-1 Forward Passenger / Crew Doors
2-7-2 Emergency Exits
2-7-3 Aft Passenger / Crew Doors
2-7-4 Forward Cargo Compartment Doors
2-7-5 Aft Cargo Compartment Doors
2-7-7 Main Landing Gear Doors
2-7-8 Radome
2-7-9 APU and Nose Landing Gear Doors
2-8-0 Escape Slides
2-9-0 Landing Gear
2-10-0 Exterior Lighting
2-11-0 Antennas and Probes Location
2-12-0 Power Plant
2-13-0 Leveling, Symmetry and Alignment
2-14-0 Jacking
3 AIRCRAFT PERFORMANCE
3-1-0 General Information
3-2-0 Payload / Range
3-2-1 ISA Conditions
3-3-0 FAR / JAR Takeoff Weight Limitation
3-3-1 ISA Conditions
T.O.C.Page 1
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2 ISA +15˚C (+59˚F) Conditions
3-4-0 FAR / JAR Landing Field Length
3-4-1 ISA Conditions
3-5-0 Final Approach Speed
4 GROUND MANEUVERING
4-1-0 General Information
4-2-0 Turning Radii
4-3-0 Minimum Turning Radii
4-4-0 Visibility from Cockpit in Static Position
4-5-0 Runway and Taxiway Turn Paths
4-5-1 135˚ Turn - Runway to Taxiway
4-5-2 90˚ Turn - Runway to Taxiway
4-5-3 180˚ Turn on a Runway
4-5-4 135˚ Turn - Taxiway to Taxiway
4-5-5 90˚ Turn - Taxiway to Taxiway
4-6-0 Runway Holding Bay (Apron)
4-7-0 Parking
5 TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
5-1-0 Servicing Arrangements
5-1-1 Symbols Used on Servicing Diagrams
5-1-2 Typical Ramp Layout - Open Apron
5-1-3 Typical Ramp Layout - Gate
5-2-0 Terminal Operations - Full Servicing
5-3-0 Terminal Operation - Transit
5-4-0 Ground Service Connections
5-4-1 Ground Service Connections Layout
5-4-2 Grounding Points
5-4-3 Hydraulic System
5-4-4 Electrical System
5-4-5 Oxygen System
5-4-6 Fuel System
5-4-7 Pneumatic System
5-4-8 Potable Water System
5-4-9 Oil System
5-4-10 Vacuum Toilet System
T.O.C.Page 2
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
5-5-1 Low Ambient Temperatures
5-5-2 Medium Ambient Temperatures
5-5-3 High Ambient Temperatures
5-6-0 Ground Pneumatic Power Requirements
5-6-1 Heating
5-6-2 Cooling
5-7-0 Preconditioned Airflow Requirements
5-8-0 Ground Towing Requirements
5-9-0 De-Icing and External Cleaning
6 OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
6-2-0 Airport and Community Noise
6-2-1 Noise Data
6-3-0 Danger Areas of Engines
6-3-1 Ground Idle Power
6-3-2 Takeoff Power
6-4-0 APU Exhaust Velocities and Temperatures
6-4-1 APU
7 PAVEMENT DATA
7-1-0 General Information
7-2-0 Landing Gear Footprint
7-3-0 Maximum Pavement Loads
7-4-0 Landing Gear Loading on Pavement
7-4-1 Landing Gear Loading on Pavement
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-6-0 Flexible Pavement Requirements - LCN Conversion
7-6-1 Flexible Pavement Requirements - LCN Conversion
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
T.O.C.Page 3
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-1 Radius of Relative Stiffness
7-8-2 Rigid Pavement Requirements - LCN Conversion
7-8-3 Radius of Relative Stiffness (Other values of E and L)
7-8-4 Radius of Relative Stiffness
7-9-0 ACN/PCN Reporting System
7-9-1 Aircraft Classification Number - Flexible Pavement
7-9-2 Aircraft Classification Number - Rigid Pavement
8 SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
10 AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
T.O.C.Page 4
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0 Purpose
**ON A/C A318-100
Purpose
1. GeneralThe 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 revision is now a merge of the Maintenance Facility planning (MFP) document and the AirplaneCharacteristics for Airport Planning (AC). This document has been renamed Aircraft Characteristics --Airport and Maintenance Planning (AC) to reflect this change.Additionally, a chapter 10 ”Aircraft Rescue and Fire Fighting” has been added to the AC. Thischapter contains the illustrations of the Aircraft Rescue and Fire fighting Charts poster and replacesthe PDF document that was available for download.
The data given in this issue of the A318-100 AC equipped with Sharklets can be subject to changepending completion of the flight test phase. It is given for guidance only and does not constitute acontractual commitment.
This non-customized document conforms to NAS 3601 specification.This document must not be used for training purposes.
The single aisle A320 Family is a short to medium range aircraft delivering superior fuel efficiency,passenger comfort, environmental characteristics and economics, with a global market coverage.With record number of operators and wide market approval, the A320 Family benefits fromcontinuous improvements such as:- SharkletsThe A320 Family wider fuselage, advanced troubleshooting and Cargo Loading System enable easyand cost effective ground handling, whilst minimizing aircraft turn round time.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services1, Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0Page 1
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-0 General Aircraft Characteristics
**ON A/C A318-100
General Airplane Characteristics
1. General Airplane CharacteristicsThe 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.
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-1-1 General Aircraft Characteristics Data
**ON A/C A318-100
General Airplane 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
Kilograms 59 400 61 900 63 400 64 900 66 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds130 955 136 466 139 773 143 080 146 387
Kilograms 59 000 61 500 63 000 64 500 66 000Maximum TakeoffWeight (MTOW) Pounds 130 073 135 584 138 891 142 198 145 505
Kilograms 56 000 56 000 57 500 57 500 57 500Maximum LandingWeight (MLW) Pounds 123 459 123 459 126 766 126 766 126 766
Kilograms 53 000 53 000 54 500 54 500 54 500Maximum Zero FuelWeight (MZFW) Pounds 116 845 116 845 120 152 120 152 120 152
Aircraft CharacteristicsWV005 WV006 WV007 WV008
Kilograms 68 400 56 400 61 400 64 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds150 796 124 341 135 364 141 978
Kilograms 68 000 56 000 61 000 64 000Maximum Takeoff Weight(MTOW) Pounds 149 914 123 459 134 482 141 096
Kilograms 57 500 56 000 56 000 56 000Maximum Landing Weight(MLW) Pounds 126 766 123 459 123 459 123 459
Kilograms 54 500 53 000 53 000 53 000Maximum Zero Fuel Weight(MZFW) Pounds 120 152 116 845 116 845 116 845
2. The following table provides characteristics of A318 Models, these data are common to each WeightVariant:
Aircraft CharacteristicsStandard SeatingCapacity
Single-class132
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsLiters 23 859US gallons 6 303
Kilograms(density =0.785 kg/l)
18 729
Usable Fuel Capacity
Pounds 41 290Cubic meters 257Pressurized Fuselage
Volume (A/C nonequipped)
Cubic feet9 076
Cubic meters 107Passenger CompartmentVolume Cubic feet 3 779
Cubic meters 9Cockpit VolumeCubic feet 318Cubic meters 6.72Usable Volume, FWD
CC Cubic feet 237.3Cubic meters 8.87Usable Volume, AFT CCCubic feet 313.3Cubic meters 5.71Usable Volume, Bulk CCCubic feet 201.6Cubic meters 8.34Water Volume, FWD CCCubic feet 294.5Cubic meters 10.38Water Volume, AFT CCCubic feet 366.6Cubic meters 5.97Water Volume, Bulk CCCubic feet 210.8
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
12.45 m(40.85 ft)
34.10 m(111.88 ft)
4.14
m(1
3.58
ft)
10.25 m(33.63 ft)
5.07 m(16.63 ft)
6.62
m(2
1.72
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)
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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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
31.45 m(103.18 ft)
8.8 m(28.87 ft)
9.1 m(29.86 ft)
CFM56
PW6000
5.75
m(1
8.86
ft)
3.95
m(1
2.96
ft)
8.32
m(2
7.30
ft)
11.9
3 m
(39.
14 ft
)
4.91
m(1
6.11
ft)
N_AC_020200_1_0010107_01_00
General Aircraft DimensionsWing Tip Fence (Sheet 2 of 4)
FIGURE-2-2-0-991-001-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
4.14
m(1
3.58
ft)
10.25 m(33.63 ft)
5.07 m(16.63 ft)
6.62
m(2
1.72
ft)
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
2-2-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
31.45 m
(103.18 ft)
8.8 m
(28.87 ft)
9.1 m
(29.86 ft)
CFM56
PW6000
5.75
m
(18.
86 ft
)
3.95
m
(12.
96 ft
)
8.32
m
(27.
30 ft
)
11.9
3 m
(39.
14 ft
)
4.91
m
(16.
11 ft
)
21.06 m
(69.09 ft)
3.22 m
(10.56 ft)
1.64 m
(5.38 ft)
1.61 m
(5.28 ft)
16.2
9 m
(53.
44 ft
)
N_AC_020200_1_0010108_01_00
General Aircraft DimensionsSharklet (Sheet 4 of 4)
FIGURE-2-2-0-991-001-A01
2-2-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0 Ground Clearances
**ON A/C A318-100
Ground Clearances
1. This section gives the height of various points of the aircraft, above the ground, for different aircraftconfigurations.Dimensions in the tables are approximate and will vary with tire type, weight and balance and otherspecial conditions.
The dimensions are given for:- a light weight, for an A/C in maintenance configuration with a mid CG,- the MRW for a light weight variant with a FWD CG and a AFT CG,- the MRW for a heavy weight variant with a FWD CG and a AFT CG,- aircraft on jacks, FDL at 4.6 m (15.09 ft).
NOTE : Passenger and cargo door clearances are measured from the center of the door sill and fromfloor level.
2-3-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
CG 25% FWD CG 15% FWD CG 15.8%
A/C JACKED FDL
AFT CG 32%
3.452.081.791.935.936.080.660.781.742.733.173.512.20
BC1C2D1D2
E (CFM)E (PW)
FF1F2F3G
3.372.011.711.895.866.040.600.721.692.683.123.472.16
3.442.051.761.855.916.000.610.731.672.663.093.432.13
3.372.001.711.875.866.020.590.711.672.673.113.452.14
3.422.031.741.845.895.990.600.721.652.653.08
4.132.712.432.436.586.581.241.362.263.253.68
3.72H 3.70 3.61 3.67
3.42 4.012.11 2.713.60 4.13
NOTE:
12.89J 12.88 12.74 12.85 12.74 13.203.92K1 3.88 3.83 3.86 3.82 4.384.89K2 4.86 4.80 4.83 4.79 5.355.62L 5.60 5.47 5.57 5.46 5.933.97N 3.91 3.92 3.90 3.90 4.544.22P 4.14 4.23 4.13 4.21 4.964.91Q 4.91 4.76 4.87 4.75 5.20
AFT CG 33.9%
P C1 BD1 E
N
C2G HD2 Q J
L F F1 F2 F3 K1 K2
13.558.897.977.9721.5921.594.074.467.41
10.6612.0713.168.8913.5543.3114.3717.5519.4614.8916.2717.06
11.226.665.716.0419.3219.651.972.365.418.6910.1011.226.9211.8141.8012.5315.7217.9112.8013.8115.58
11.066.565.616.1419.2319.751.942.335.488.7610.2011.327.02
12.0442.1612.6615.8518.2712.8013.5515.98
11.296.735.776.07
19.3919.682.002.405.488.73
10.1411.256.99
11.8441.8012.5715.7517.9512.8613.8815.62
11.066.595.616.2019.2319.821.972.365.548.79
10.2411.387.09
12.1442.2612.7315.9418.3712.8313.5816.11
11.326.825.876.33
19.4619.952.172.565.718.9610.4011.527.22
12.2042.2912.8616.0418.4413.0213.8516.11
m ft m ft m ft m ft m ft m ft
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
A/CCONFIG−URATION
39 t 59 tMRW
64 tMRW
= 4.60 m(15.09 ft)
A
N_AC_020300_1_0010101_01_05
Ground ClearancesFIGURE-2-3-0-991-001-A01
2-3-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
CG 25% FWD CG 15% FWD CG 15.8%
A/C JACKED FDL
AFT CG 32%
3.452.081.791.935.936.080.660.781.742.733.173.512.20
BC1C2D1D2
E (CFM)E (PW)
FF1F2F3G
3.372.011.711.895.866.040.600.721.692.683.123.472.16
3.442.051.761.855.916.000.610.731.672.663.093.432.13
3.372.001.711.875.866.020.590.711.672.673.113.452.14
3.422.031.741.845.895.990.600.721.652.653.08
4.132.712.432.436.586.581.241.362.263.253.68
3.72H 3.70 3.61 3.67
3.42 4.012.11 2.713.60 4.13
NOTE:
12.89J 12.88 12.74 12.85 12.74 13.204.19K1 4.15 4.10 4.13 4.09 4.656.83K2 6.80 6.74 6.77 6.73 7.295.62L 5.60 5.47 5.57 5.46 5.933.97N 3.91 3.92 3.90 3.90 4.544.22P 4.14 4.23 4.13 4.21 4.964.91Q 4.91 4.76 4.87 4.75 5.20
AFT CG 33.9%
13.558.897.977.9721.5921.594.074.467.41
10.6612.0713.168.8913.5543.3115.2623.9219.4614.8916.2717.06
11.226.665.716.0419.3219.651.972.365.418.6910.1011.226.9211.8141.8013.4222.0817.9112.8013.8115.58
11.066.565.616.1419.2319.751.942.335.488.7610.2011.327.02
12.0442.1613.5522.2118.2712.8013.5515.98
11.296.735.776.07
19.3919.682.002.405.488.73
10.1411.256.99
11.8441.8013.4522.1117.9512.8613.8815.62
11.066.595.616.2019.2319.821.972.365.548.79
10.2411.387.09
12.1442.2613.6222.3118.3712.8313.5816.11
11.326.825.876.33
19.4619.952.172.565.718.9610.4011.527.22
12.2042.2913.7522.4118.4413.0213.8516.11
m ft m ft m ft m ft m ft m ft
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
A/CCONFIG−URATION
39 t 59 tMRW
64 tMRW
= 4.60 m(15.09 ft)
L F F1 F2 F3 K1 K2
P A C1 B E C2 G D2 H Q JD1
N_AC_020300_1_0270101_01_00
N
Ground ClearancesGround Clearances with Sharklets
FIGURE-2-3-0-991-027-A01
2-3-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
m ft m ft m ft
A
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
EF G
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
2-3-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
m ft m ft m ft
H
J
K
2.68
3.09
3.48
2.62
3.02
3.42
2.59
3.0
3.39
8.79 8.60 8.50
10.14
11.42
9.91
11.22
9.84
11.12
HEIGHT FROM GROUND
JHK
N_AC_020300_1_0070101_01_00
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
Ground ClearancesFlap Track Fairings Up
FIGURE-2-3-0-991-007-A01
2-3-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**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
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
Ground ClearancesAileron Down
FIGURE-2-3-0-991-008-A01
2-3-0Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**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 4.57
4.37
4.51
4.31
4.26
4.45
14.99 14.80 13.98
14.34 14.14 14.60
N_AC_020300_1_0090101_01_00
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
V
W
Ground ClearancesAileron Up and Spoilers 1 to 5 Extended
FIGURE-2-3-0-991-009-A01
2-3-0Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
m ft m ft m ft
X 2.54
2.96
3.05
2.48
2.90
2.99
2.5
2.91
2.99
8.33 8.14 8.20
9.71
10.01
9.51
9.81
9.55
9.81
HEIGHT FROM GROUND
C’Y
F’
X ZE’ G’
A’
B’
C’
D’
E’
3.35
3.35
3.61
3.29
3.29
3.55
3.28
3.28
3.53
10.99 10.79 10.76
10.99
11.84
10.79
11.65
10.76
11.58
3.61
3.86
3.86
3.55
3.80
3.80
3.53
3.77
3.77
11.84 11.65 11.58
12.66
12.66
12.47
12.47
12.37
12.37
4.10 4.04 4.013.45 13.25 13.12
D’A’ B’
Y
Z
N_AC_020300_1_0100101_01_00
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
F’
G’
Ground ClearancesSlats Extended
FIGURE-2-3-0-991-010-A01
2-3-0Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-0 Interior Arrangements
**ON A/C A318-100
Interior Arrangements
1. This section gives the standard interior arrangements configuration.
2-4-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1 Passenger Compartment Layout
**ON A/C A318-100
Typical Configuration
1. This section gives the typical interior configuration.
2-4-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A AA
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(2)
AA
TT
EN
DA
NT
SE
AT
(4)
LL
AG
G
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
132
SE
AT
S A
LL T
OU
RIS
T C
LAS
S29
/30
in P
ITC
H. 6
AB
RE
AS
T. 3
.3
N_AC_020401_1_0010101_01_01
Typical ConfigurationTypical Configuration Single-Class, High Density
FIGURE-2-4-1-991-001-A01
2-4-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ITE
MD
ES
IGN
AT
ION
8 S
UP
ER
FIR
ST
CLA
SS
PA
SS
EN
GE
R S
EA
TS
(10
7 T
OT
AL)
LLA
VA
TO
RY
(2)
GG
ALL
EY
(3)
AA
TT
EN
DA
NT
SE
AT
(3)
SE
AT
PIT
CH
ES
:
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
99 E
CO
NO
MY
CLA
SS
FIR
ST
38
inE
CO
NO
MY
32
in
AF
T P
AS
SE
NG
ER
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
G
A AL
ALG
L
N_AC_020401_1_0070101_01_00
Typical ConfigurationTypical Configuration Two-Class
FIGURE-2-4-1-991-007-A01
2-4-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0 Passenger Compartment Cross Section
**ON A/C A318-100
Passenger Compartment Cross-section
1. This section gives the typical passenger compartment cross-section configuration.
2-5-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
3.95(155.51)
Cargo CompartmentFloor
CABINFLOOR
Top of cargoCompartment
AircraftDatum
Windows
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)
Passenger Compartment Cross-sectionFIGURE-2-5-0-991-001-A01
2-5-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: DIMENSIONS m (in)
1.24
(48.
9)2.
21(8
7)
6 ABREAST−WIDER AISLE
4.14
(163
)
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
Passenger Compartment Cross-sectionEconomy Class, 6 Abreast - Wider Aisle (Sheet 1 of 2)
FIGURE-2-5-0-991-005-A01
2-5-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: DIMENSIONS m (in)
6 ABREAST−WIDER SEAT
3.95(155.5)
3.64(143)
1.58(62)
0.48(19)
1.58(62)
1.24
(48.
9)2.
21(8
7)
4.14
(163
)
0.457(18)
N_AC_020500_1_0050102_01_02
Passenger Compartment Cross-sectionEconomy Class, 6 Abreast - Wider Seat (Sheet 2 of 2)
FIGURE-2-5-0-991-005-A01
2-5-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: DIMENSIONS m (in)
4 ABREAST−FIRST CLASS
3.95(155.5)
1.24
(48.
9)2.
21(8
7)
4.14
(163
)
3.59(141)
0.69(27)
1.45(57)
1.45(57)
(22.6)0.57
N_AC_020500_1_0060101_01_00
Passenger Compartment Cross-sectionPassenger Compartment Cross-section, First-class
FIGURE-2-5-0-991-006-A01
2-5-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-0 Cargo Compartments
**ON A/C A318-100
Cargo Compartments
1. This section gives the cargo compartments locations, dimensions and loading combinations.
2-6-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FW
D C
AR
GO
CO
MP
AR
TM
EN
T
6.07
m
(238
.98
in)
2.68
m
(105
.51
in)
1.28
m
(50.
39 in
)
AF
T C
AR
GO
CO
MP
AR
TM
EN
T BU
LK C
AR
GO
CO
MP
AR
TM
EN
T
1.28
m
(50.
39 in
)
FR
24A
FR
34F
R47
FR
54/
FR
60F
R65
N_AC_020600_1_0010101_01_00
Cargo CompartmentsLocations, Dimensions and Loading Combinations
FIGURE-2-6-0-991-001-A01
2-6-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0 Door Clearances
**ON A/C A318-100
Doors Clearances
1. This section gives doors clearances.
2-7-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-1 Forward Passenger / Crew Doors
**ON A/C A318-100
Forward Passenger / Crew Doors
1. This section gives forward passenger / crew doors clearances.
2-7-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
CRITICAL
CLEARANCE LIMIT
0.61 m(2 ft)
0.48 m(1 ft 6.88 in)
2.54 m(8 ft 3.99 in)
5.02 m(16 ft 5.62 in)
1.8 m(5 ft 10.8 in) 0.81 m
(2 ft 7.8 in)
1.85 m(6 ft 0.82 in)
SEECHAPTER
2.375 m(7 ft 9.48 in)
2−3
CL
CLCL
0.03 m(1.18 in)
N_AC_020701_1_0010101_01_00
Doors ClearancesForward Passenger / Crew Doors
FIGURE-2-7-1-991-001-A01
2-7-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-2 Emergency Exits
**ON A/C A318-100
Emergency Exits
1. This section gives emergency exits doors clearances.
2-7-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
(FRAME 47)
NOTE: ESCAPE SLIDE COMPARTMENT DOOROPENS ON WING UPPER SURFACE.
(FROM NOSE)
CL
12.89 m(42 ft 3.46 in)
0.56 m
0.47 m(1ft 6.49 in)
1.23 m(4 ft 0.42 in)
0.2 m(7.87 in)
FWD
0.9 m(2 ft 11.4 in)
0.495 m(1ft 7.48 in)
(TOP OF FLOOR)
0.12 m(4.72 in)
SEESECTION
2−3
B B
A
A
B
B
CL
(1ft 10 in)
A A
N_AC_020702_1_0020101_01_00
Doors ClearancesEmergency Exits
FIGURE-2-7-2-991-002-A01
2-7-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-3 Aft Passenger / Crew Doors
**ON A/C A318-100
Aft Passenger / Crew Doors
1. This section gives Aft passenger / crew doors clearances.
2-7-3Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
1.79 m(5 ft 10.46 in)
0.81 m(2 ft 7.88 in)
0.58 m(1 ft 10.8 in)
CRITICALCLEARANCE
LIMIT
23.52 m(77 ft 1.98 in)
(FROM NOSE)
2.44 m(8 ft)
1.85 m(6 ft 0.82 in)
0.6 m(1 ft 11.6 in)
(1.18 in)0.03 m
FWD
SEE
2−3CHAPTER
A A
A
A
N_AC_020703_1_0010101_01_00
Doors ClearancesAft Passenger / Crew DoorsFIGURE-2-7-3-991-001-A01
2-7-3Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-4 Forward Cargo Compartment Doors
**ON A/C A318-100
Forward Cargo Compartment Door
1. This section gives forward cargo compartment door clearances.
2-7-4Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
7.89
(25 ft 10.6 in)
1.33 m(4 ft 4.35 in)
1.24 m(4 ft 0.81 in)
3.945 m(12 ft 11.3 in)
1.495 m(4 ft 10.84 in)
0.26 m(10.23 in)
(FROM NOSE)
2−3
SEECHAPTER
A
A
FWD
A A
2.9 m(9 ft 6.16 in)
N_AC_020704_1_0010101_01_00
Doors ClearancesForward Cargo Compartment Door
FIGURE-2-7-4-991-001-A01
2-7-4Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-5 Aft Cargo Compartment Doors
**ON A/C A318-100
Aft Cargo Compartment Door
1. This section gives Aft cargo compartment door clearances.
2-7-5Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
1.23 m(4 ft 0.42 in)
3.945 m(12 ft 11.3 in)
1.43 m(4 ft 8.29 in)
2−3
SEECHAPTER
A A
FWD
1 m
(3 ft 3.36 in)
19.96 m
(62 ft 2.44 in)
1.33 m(4 ft 4.35 in)
(FROM NOSE)
FWD
A
A
N_AC_020705_1_0010101_01_01
Doors ClearancesAft Cargo Compartment DoorFIGURE-2-7-5-991-001-A01
2-7-5Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-7 Main Landing Gear Doors
**ON A/C A318-100
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances.
2-7-7Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
13.97 m(45 ft 10 in)
GROUND LINE
0.207 m(8.14 in)
0.485 m
(1 ft 7.09 in)
NOTE: VALUE OF CG: 25% RC.AIRCRAFT
1.23 m(4 ft 0.42 in)
0.14 m(5.51 in)
84°
1.942 m
(6 ft 4.45 in)
1.826 m(5 ft 11.88 in)
A
1.761 m(5 ft 9.32 in)
A
N_AC_020707_1_0010101_01_02
Doors ClearancesMain Landing Gear Doors
FIGURE-2-7-7-991-001-A01
2-7-7Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-8 Radome
**ON A/C A318-100
Radome
1. This section gives the radome clearances.
2-7-8Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
0.63 m(2 ft 0.79 in)
1.54 m(5 ft 0.62 in)
STA 3500FR1
65°
N_AC_020708_1_0010101_01_00
Doors ClearancesRadome
FIGURE-2-7-8-991-001-A01
2-7-8Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-9 APU and Nose Landing Gear Doors
**ON A/C A318-100
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances.
2-7-9Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
1.5
m(4
ft 1
1 in
)
FR80
FR84
3.23
m(1
0 ft
7.16
in)
3.86
m(1
2 ft
7.96
in)
1.4
m(4
ft 7
.11
in)
NOTE: VALUE OF CG: 25% RC.
N_AC_020709_1_0010101_01_00
Doors ClearancesAPU and Nose Landing Gear Doors
FIGURE-2-7-9-991-001-A01
2-7-9Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0 Escape Slides
**ON A/C A318-100
Escape Slides
1. GeneralThis section gives location of cabin escape facilities and related clearances.
2. LocationEscape facilities are provided at the following locations:- one slide-raft at each passenger/crew door (total four)- one slide for each emergency exit door (total two). Dual lane offwing escape slides are installed
above the wings in the left and right wing-to-fuselage fairings for off-the-wing evacuation.
2-8-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FWD CABIN ESCAPE SLIDE
OFF WING ESCAPE SLIDE
N_AC_020800_1_0010101_01_00
AFT CABINESCAPE SLIDE
Escape SlidesLocation
FIGURE-2-8-0-991-001-A01
2-8-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
EMERGENCY DESCENT DEVICETHROUGH WINDOW OPENING
GRID EQUALS 1 m (3.28 ft) IN REALITY
N_AC_020800_1_0020101_01_00
Escape SlidesDimensions
FIGURE-2-8-0-991-002-A01
2-8-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0 Landing Gear
**ON A/C A318-100
Landing Gear
1. General
The landing gear is of the conventional retractable tricycle type comprising:- Two main gears with twin wheel- A twin wheel nose gear.
The main landing gears are located under the wing and retract sideways towards the fuselagecenterline.
The nose landing gear retracts forward into a fuselage compartment located between STA 5394/FR 9and 8077/FR 20.
The landing gear and landing gear doors operation is controlled electrically and hydraulicallyoperated.In abnormal operation, the landing gear can be extended by gravity.
For landing gear footprint and tire size, refer to 7-2-0.
2. Main Landing Gear
A. Twin wheel
Each of the two main landing gear assemblies consists of a conventional two wheel direct typewith an integral shock absorber supported in the fore and aft direction by a fixed drag strut andlaterally by a folding strut mechanically locked when in the DOWN position.
3. Nose Landing Gear
The nose landing gear comprises of a leg with a built-in shock absorber strut, carrying twin wheelwith adequate shimmy damping and a folding strut mechanically locked when in the DOWN position.
4. Nose Wheel Steering
Steering is controlled by two hand wheels in the cockpit. For steering angle controlled by the handwheels, refer to AMM 32-51-00.For steering angle limitation, refer to AMM 09-10-00.
A steering disconnection box installed on the nose landing gear to allow steering deactivation fortowing purpose.
2-9-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5. Landing Gear Servicing Points
A. General
Filling of the landing gear shock absorbers is through MS28889 standard valves.
Charging of the landing gear shock absorbers is accomplished with nitrogen through MS28889standard valves.
B. Charging Pressure
For charging of the landing gear shock absorbers, refer to AMM 12-14-32.
6. Braking
A. General
The four main wheels are equipped with carbon multidisc brakes.
The braking system is electrically controlled and hydraulically operated.
The braking system has four braking modes plus autobrake and anti-skid systems:- Normal braking with anti-skid capability- Alternative braking with anti-skid capability- Alternative braking without anti-skid capability- Parking brake with full pressure application capability only.
B. In-Flight Wheel Braking
The main gear wheels are braked automatically before the wheels enter the wheel bay.
The nose gear wheels are stopped by the wheels contacting a rubbing strip (the brake band)when the gear is in the retracted position.
2-9-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ACTUATINGCYLINDER
UNLOCK
LOCK STAY
MAIN
SIDE STAY
TORQUELINK
SHOCK
ACTUATOR
FITTING
ABSORBER
D
E
A
MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION.NOTE:
MAIN DOOR(HYDRAULICALLY OPERATED)
FIXEDRAMPS
UPLOCKROLLER
ADJUSTABLERAMP
STEPS
FIXEDFAIRING
HINGEDFAIRING
HINGED FAIRING(MECHANICALLY OPERATED)
PROXIMITY SENSORS
DOOR ACTUATING CYLINDER
A
B
C
N_AC_020900_1_0020101_01_00
D
Landing GearMain Landing Gear - Twin Wheel (Sheet 1 of 2)
FIGURE-2-9-0-991-002-A01
2-9-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
DOORACTUATINGCYLINDER
FLAG
TOP FILLING AND CHARGING CONNECTION MS28889
BOTTOM FILLING ANDCHARGING CONNECTIONMS28889
LOCKSTAYACTUATINGCYLINDER
GROUND LOCK SLEEVE
FLAG
BC
ED
LOCKINGPIN
LOCKINGPIN
EXAMPLEN_AC_020900_1_0020102_01_00
Landing GearMain Landing Gear - Twin Wheel (Sheet 2 of 2)
FIGURE-2-9-0-991-002-A01
2-9-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
Y=COMPRESSED
EXTENDED
58.4
0 %
AM
C
3 795 mm
3 453 mm(135.94 in) 80°30
RETRACTIONANGLE
(36.50 in)927.10 mm
2 868.70 mm(112.94 in)
2 265 mm(89.17 in)
X= 20 252.50 mm(797.34 in)
469.90 mm(18.50 in)
(149.41 in)
N_AC_020900_1_0030101_01_00
Landing GearMain Landing Gear Dimensions - Twin Wheel
FIGURE-2-9-0-991-003-A01
2-9-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ACTUATINGCYLINDER
NOSE WHEELSTEERINGSERVO CONTROL
STEERINGACTUATINGCYLINDER
TORQUELINK
DOWNLOCKPROXIMITY
DETECTORS
SHOCKABSORBER
TOWINGFITTING
LEG DOOR
AFT DOORS
ASSEMBLYFITTING
FWD DOORS
CONTROL ROD
DOORACTUATINGCYLINDER
CRANK
DOOR UPLOCKASSEMBLY GEAR UPLOCK
ASSEMBLY
BELL
FR20
FR9
DRAG STRUTASSEMBLY
A
A
ROTATING ROD
BC
E
D
N_AC_020900_1_0040101_01_00
Landing GearNose Landing Gear (Sheet 1 of 2)
FIGURE-2-9-0-991-004-A01
2-9-0Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
TOWING LEVER
(NOSE WHEEL STREERINGNORMAL POSITION
(TOWING POSITION)SAFETY PIN
(NOSE WHEEL STEERING DEACTIVATED)TOWING POSITION
E
DOOR HINGE
NLG DOOR
NLG DOORSAFETY PIN
FLAG
LH SYMMETRICALRH SHOWN
FLAG
DOWNLOCKSAFETY PIN
LOCKSTAY
BC
D
OPERATIONAL)
N_AC_020900_1_0040102_01_00
CONNECTION MS28889FILLING AND CHARGING
Landing GearNose Landing Gear (Sheet 2 of 2)
FIGURE-2-9-0-991-004-A01
2-9-0Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_020900_1_0050101_01_00
92°
9°
X =
500 mm(19.69 in)
7 561 mm(297.68 in)
430 mm(16.93 in)
1 957.03 mm(77.05 in)
2 338 mm(92.05 in)
EXTENDED
COMPRESSED
Landing GearNose Landing Gear Dimensions
FIGURE-2-9-0-991-005-A01
2-9-0Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
Landing Gear Maintenance Pits
1. Description
The minimum maintenance pit envelopes for the main gear shock absorber removal are shown inFigures 1 and 2.
All dimensions shown are minimum dimensions with zero clearances.
The dimensions for the pits have been determined as follows:- The length and width of the pits allow the gear to rotate as the weight is taken off the landing
gear- The depth of the pits allows the shock absorber to be removed when all the weight is taken off
the landing gear.
Dimensions for elevators and associated mechanisms must be added to those in Figures 1 and 2.
2-9-0Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
MA
IN J
AC
KIN
G P
OIN
T
= =
==
7.61
m(2
4.97
ft)
5.28
m
1 m
(3.2
8 ft)
1.5
m(4
.92
ft)
(17.
32 ft
)
1.92
m(6
.30
ft)
17.7
2 m
(58.
14 ft
)M
AIN
JA
CK
ING
PO
INT
2.95
m(9
.68
ft)
3.76
m(1
2.34
ft)
2.5
m(8
.20
ft)7.
59 m
(24.
90 ft
)
3.79
m(1
2.43
ft)
6.49
m(2
1.29
ft)
FROM X0
17.8
7 m
(58.
63 ft
)
FW
D J
AC
KIN
G P
OIN
T
N_AC_020900_1_0200101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-020-A01
2-9-0Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:1 2
0.52
1.1
73.
84
mft
AB
mft
AB
ST
AT
IC G
RO
UN
D L
INE
1
2
1
2
7.6
1 m
(24.
97 ft
)
1.7
1
RE
PR
ES
EN
TS
TO
P O
F M
EC
HA
NIC
AL
OR
HY
DR
AU
LIC
ELE
VA
TO
R, W
ITH
AIR
CR
AF
T W
EIG
HT
SU
PP
OR
TE
DA
ND
LA
ND
ING
GE
AR
SH
OC
K A
BS
OR
BE
RS
EX
TE
ND
ED
.
RE
PR
ES
EN
TS
TO
P O
F M
EC
HA
NIC
AL
OR
HY
DR
AU
LIC
ELE
VA
TO
R, S
HO
WN
WIT
H Z
ER
O C
LEA
RA
NC
ELO
WE
RE
D F
OR
SH
OC
K A
BS
OR
BE
R R
EM
OV
AL.
1.60
m(5
.25
ft)0.
40 m
(1.3
1 ft)
17
.87
m(5
8.63
ft)
DIM
QU
OT
ED
ISW
ITH
WH
EE
LS R
EM
OV
ED
AN
D 1
53 m
m (
6.02
in)
CLE
AR
AN
CE
AT
JAC
KIN
G D
OM
E
FROM X0
N_AC_020900_1_0210101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-021-A01
2-9-0Page 11
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0 Exterior Lighting
**ON A/C A318-100
Exterior Lighting
1. General
This section gives the location of the aircraft exterior lighting.
EXTERIOR LIGHTINGITEM DESCRIPTION
1 RIGHT NAVIGATION LIGHT (GREEN)
2 TAIL NAVIGATION LIGHT (WHITE)
3 LEFT NAVIGATION LIGHT (RED)
4 RETRACTABLE LANDING LIGHT5 RUNWAY TURN OFF LIGHT6 TAXI LIGHT7 TAKE-OFF LIGHT8 LOGO LIGHT
9 UPPER ANTI-COLLISION LIGHT/BEACON (RED)
10 LOWER ANTI-COLLISION LIGHT/BEACON (RED)
11 WING STROBE LIGHT (HIGH INTENSITY, WHITE)
12 TAIL STROBE LIGHT (HIGH INTENSITY, WHITE)
13 WING/ENGINE SCAN LIGHT
14 WHEEL WELL LIGHT (DOME)
15 CARGO COMPARTMENT FLOOD LIGHT
2-10-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10
12
11
1
3
11
6 75 4
13
8
2
89
1
3
N_AC_021000_1_0010101_01_00
RH
LH
RH
LH
Exterior LightingFIGURE-2-10-0-991-001-A01
2-10-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_021000_1_0020101_01_00
2
1 3
55
7
Exterior LightingFIGURE-2-10-0-991-002-A01
2-10-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_021000_1_0030101_01_00
109
1313
11 11
12
4
6
Exterior LightingFIGURE-2-10-0-991-003-A01
2-10-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
CEILING LIGHT
SPOT LIGHT
GROUND
8 8
1514
15
N_AC_021000_1_0170101_01_00
EXAMPLE FOR LIGHT N° 15
Exterior LightingFIGURE-2-10-0-991-017-A01
2-10-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0 Antennas and Probes Location
**ON A/C A318-100
Antennas and Probes Location
1. This section gives the location of antennas and probes.
2-11-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RADIO ALTIMETER(2)
RADIO ALTIMETER(1)
VHF(2)
MARKER
DME(2)
STATIC PROBE(1)
DME(1)
STATIC PROBE(2)
PITOT PROBE(1)
PITOT PROBE(3)
TAT PROBE
GLIDE
LOC
EMERGENCY STATIC PROBE
WEATHER RADAR
VHF(1)
AOA SENSOR(1)
EMERGENCY STATIC PROBE
TAT PROBE
PITOT PROBE(2)
STATIC PROBE(2)
STATIC PROBE(1)
AOA SENSOR(2)
GPS(2)
GPS(1)
TCAS BOTTOM
ATC(1)
TCAS TOP VHF(3)
ELT
ATC(2)
VOR
HF
ATC(3)
AOA SENSOR(3) STBYATC(4)
NOTE: DEPENDING ON AIRCRAFT CONFIGURATION
ADF(1)
N_AC_021100_1_0010101_01_00
Antennas and ProbesLocation
FIGURE-2-11-0-991-001-A01
2-11-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0 Power Plant
**ON A/C A318-100
Auxiliary Power Unit
1. General
The APU is installed at the rear part of the fuselage in the tail cone. An air intake system with aflap-type door is installed in front of the APU compartment. The exhaust gases pass overboard at theend of the fuselage cone.
2. Controls and Indication
The primary APU controls and indications are installed on the overhead panel, on the center pedestaland on the center instrument panel. Additionally, an external APU panel is installed on the noselanding gear to initiate an APU emergency shutdown.
2-12-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FRONT FIREWALLREAR FIREWALL
LH FIREWALL
RH FIREWALL
AIR INTAKECUT OUT
AIR INTAKE FIXEDON ACCESS DOOR
CUT OUT SEALED WITHLABYRINTH GASKET
CUT OUT SEALEDWITH LABYRINTH GASKET
UPPERFIREWALL
VENTLOUVER
UPPERFIREWALL
A
FR84/STA32824
FR80/STA31174
Z310
315AL
316AR
N_AC_021200_1_0010101_01_00
A B
Auxiliary Power UnitAccess Doors
FIGURE-2-12-0-991-001-A01
2-12-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
BLEED AIR LINE
APU SUSPENSION(7 RODS)
GENERATOR
AFT APU MOUNT
EXHAUST MUFFLER
OIL COOLER
OIL COOLER OUTLET
AIR INTAKE DUCT
FIXED DIVERTER
AIR INTAKE HOUSING
FIREWALL
/
LH FORWARD APU MOUNT
APU−FUEL−LINE
FIRE EXINGUISINGBOTTLE
STA33992 FR87
/FR84
/FR80
/FR76
STA32824
STA31174
STA30011
316AR
315AL314AR
B
N_AC_021200_1_0020101_01_00
Auxiliary Power UnitGeneral Layout
FIGURE-2-12-0-991-002-A01
2-12-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
Engine and Nacelle
1. Engine and Nacelle - CFM Engine
A. EngineThe engine is a dual-rotor, variable stator, high bypass ratio turbo fan power plant for subsonicservices. The principal modules of the engine are:- low pressure compressor (fan stator and fan rotor)- high pressure compressor- turbine frame- combustion chamber- high pressure turbine- low pressure turbine- accessory drives (gear box).The 9 stage high pressure compressor is driven by 1 stage high pressure turbine, and theintegrated front fan and booster is driven by 4 stage low pressure turbine. An annular combustorconverts fuel and compressor discharge air into energy to provide engine thrust part throughprimary exhaust and to drive the turbines. The accessory drive system extracts energy from thehigh pressure rotor to drive the engine accessories and the engine mounted aircraft accessories.Reverse thrust for braking the aircraft after landing is supplied by an integrated system whichacts on the fan discharge airflow.
B. NacelleThe cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine ishoused in a nacelle suspended from a pylon attached to the wing lower surface. The nacelleconsists of the demountable powerplant, the fan cowls and the thrust reverser cowls.The nacelle installation is designed to provide cooling and ventilation air for engine accessoriesmounted along the fan and core casing. The nacelle provides:- protection for the engine and the accessories- airflow around the engine during its operation- lighting protection- HIRF and EMI attenuation.
2. Engine and Nacelle - PW Engine
A. EngineThe engine is a two spool, axial flow, high bypass ratio turbofan powerplant for subsonic sevice.The main modules of the engine are:- compressor section- combustion section- turbine section- accessory drives (gear box) section.The four stage Low Pressure Compressor (LPC) is driven by a three stage Low Pressure Turbine(LPT) and the six stage High Pressure Compressor (HPC) by a single stage High PressureTurbine (HPT).
2-12-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The PW6000 incorporates a Full Authority Digital Engine Control (FADEC) which governs allengine functions, including power management.
B. NacelleThe cowls enclose the periphery of the engine so as to form the engine nacelle. Each engine ishoused in a nacelle suspended from a pylon attached below the wing.The nacelle installation is designed to provide cooling and ventilation air for engine accessoriesmounted along the fan and core casing. The nacelle provides:- protection for the engine and the accessories- airflow around the engine during its operation- lighting protection- HIRF and EMI attenuation.
2-12-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
POINTFWD HOISTING
POINTFWD HANDLING
B
1 125 mm(44.28 in)
TURBINE FRAME
COMBUSTOR
COMPRESSOR
2 600 mm(102.36 in)
2 943 mm(115.87 in)
986 mm(38.82 in)
DIA
1 820 mm(71.65 in)
2 145 mm(84.45 in)
1 978 mm(77.87 in)
989 mm(38.94 in)
1 130 mm(44.49 in)
B
HANDLING POINTAFT HOISTING AND
BOOSTERFAN AND
LPTURBINE
DRIVEACCESSORY
AGB
HP
TGBTURBINE
A
N_AC_021200_1_0110101_01_00
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-011-A01
2-12-0Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FAN COWL
CENTERBODY
FANREVERSER
6°
PRIMARYNOZZLE
8.8 m(28.9 in)
0.93 m
(3.1 ft)
1.3 m(4.3 ft)
1.2 m(3.9 ft)
1.2 m(3.9 ft)
DISTANCE FROMTHE NOSE
0.33 m(1.1 ft)
2.3 m(7.5 ft)
ENGINE AIRINLET COWL
A
A
B
B
C
C
D
D
0.57 m(1.9 ft)
2.07 m(6.8 ft)
B B
1.2 m(3.9 ft)
1.8 m(5.9 ft)
2.1 m(6.9 ft)
BLOCKER DOOREXTENDED
1.9 m(6.2 ft)
A A
D DC C
1.6 m(5.2 ft)
N_AC_021200_1_0120101_01_00
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-012-A01
2-12-0Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
0.55 m(1.8 ft)
C
B
A B C
VIEWCOWLING
AFT
VIEWCOWLING
FWD
m (ft)
42°27
55°15
40°40
52°56
1.8 (5.9)
2.0 (6.6)
1.8 (5.9 )
2.0 (6.6)
1.5 (4.9)
1.8 (5.9)
1.4 (4.6)
1.7 (5.6)
1.3 (4.3)
1.7 (5.6)
1.3 (4.3)
1.6 (5.2)
NOTE: APPROXIMATE DIMENSIONS
N_AC_021200_1_0130101_01_00
Power Plant HandlingFan Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-013-A01
2-12-0Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
3.7 m(12.1 ft)
3.3 m(10.8 ft)
(3 ft)0.9 m
CAUTIONDO NOT ACTUATE SLATS:
− WITH THRUST REVERSER COWLS 45° OPEN POSITION− WITH BLOCKER DOORS OPEN AND THRUST REVERSER COWLS AT 35° AND 45° OPEN POSITION
APPROXIMATE DIMENSIONSNOTE:
GROUND
0.5 m(1.6 ft)
0.7 m(2.3 ft)
1 m(3.3 ft)
N_AC_021200_1_0140101_01_00
45°35°
1 m(3.3 ft)
Power Plant HandlingThrust Reverser Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-014-A01
2-12-0Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
3 746 mm(147.50 in)
3 355 mm(132.10 in)
1 245 mm(49.02 in)
1 146 mm(45.12 in)
142 mm(5.59 in)
ACCESSORYDRIVE
FAN ANDBOOSTER
COMPRESSOR
COMBUSTOR
TURBINE SECTION
2 002 mm(78.82 in)
(82.60 in)2 098 mm
(45.31 in)1 151 mm
1 590 mm(62.60 in)
A
BN_AC_021200_1_0150101_01_00
A
Power Plant HandlingMajor Dimensions - PW 6000 Series Engine
FIGURE-2-12-0-991-015-A01
2-12-0Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
V
ALL SIZES GIVEN ON THIS ILLUSTRATION ARE APPROXIMATE
1.43 m
(4.7 ft)
W U V
2 m(6.6 ft)
0.9 m(3 ft)
1.05 m(3.4 ft)
2.08 m(6.8 ft)
0.96 m(3.1 ft)
1.07 m(3.5 ft)
1.63 m(5.3 ft)
0.76 m(2.5 ft)
0.81 m(2.7 ft)
1.12 m(3.7 ft)
0.56 m(1.8 ft)
0.56 m(1.8 ft)
W
D
D
C
C
B
B
A
A
1.66 m
(5.44 ft)
1.24 m
(4.1 ft)
8.85 m
(29 ft)
DISTANCEFROM THE
NOSE
AIR INTAKECOWL FAN COWL
THRUSTREVERSER
COMMON NOZZLEASSY
1.03 m
(3.37 ft)
NOTE:
A−A
B−B
C−C
D−D
N_AC_021200_1_0160101_01_00
U
Power Plant HandlingNacelle Dimensions - PW 6000 Series Engine
FIGURE-2-12-0-991-016-A01
2-12-0Page 11
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
27°
53°
A B C D
GROUND
3.05 m(10 ft)3.85 m
(12.63 ft)
0.90 m(2.95 ft)1.65 m(5.41 ft)
D + 0.84 m(D + 2.8 ft)
0.7 m(2.3 ft)
D + 0.2 m(D + 0.7 ft)
A
B
D
C
APPROXIMATE DIMENSIONSONLY MAIN DIMENSIONS SHOWN
NOTE:
N_AC_021200_1_0170101_01_00
°
Power Plant HandlingFan Cowls - PW 6000 Series Engine
FIGURE-2-12-0-991-017-A01
2-12-0Page 12
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
GROUND
OPEN
CLOSED
(6.82 ft)2.08 m
A
CB
45°
A B C
3.5 m(11.48 ft)
1.1 m(3.6 ft)
1.08 m(3.5 ft)
N_AC_021200_1_0180101_01_00
°
Power Plant HandlingThrust Reverser Halves - PW 6000 Series Engine
FIGURE-2-12-0-991-018-A01
2-12-0Page 13
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0 Leveling, Symmetry and Alignment
**ON A/C A318-100
Leveling, Symmetry and Alignment
1. Quick LevelingThere are three alternative procedures to level the aircraft:- Quick leveling procedure with Air Data/Inertial Reference Unit (ADIRU).- Quick leveling procedure with a spirit level in the passenger compartment.- Quick leveling procedure with a spirit level in the FWD cargo compartment.
2. Precise LevelingFor precise leveling, it is necessary to install sighting rods in the receptacles located under thefuselage (points 11 and 12 for longitudinal leveling) and under the wings (points 2LH and 2RH forlateral leveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until thereference marks on the sighting rods are aligned in the sighting plane (aircraft level).
3. Symmetry and Alignment CheckPossible deformation of the aircraft is measured by photogrammetry.
2-13-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FR28
FR34
FR54 FR57
11
12
2LH
2RH
RIB10
RIB10
N_AC_021300_1_0010101_01_00
Location of the Leveling PointsFIGURE-2-13-0-991-001-A01
2-13-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0 Jacking
**ON A/C A318-100
Jacking for Maintenance
1. Jacking for Maintenance
A. General
The A318 aircraft can be jacked:- at not more than the maximum permitted aircraft weight for jacking (53 000 kg (116 845
lb)) and,- within the limits of the permissible wind speed when the aircraft is jacked outside a closed
environment.
B. Primary Jacking Points
The aircraft is provided with three jacking points:- one located under the forward fuselage (STA5194/FR8),- two located under the wings: one under each wing, located at the intersection of
STA4862/RIB9 and the rear of spar-datum.
Three jacking adapters are used as intermediary parts between the airplane and jacks:- one male spherical jacking adapter of 19 mm (0.75 in) radius, forming part of the airplane
structure, FR8,- a wing jack pad, attached to each wing at RIB 9 by 2 bolts, provides the location for
jacking adaptor.Wing jack pads are ground equipment.
C. Auxiliary Jacking Points - Safety Stay
When the aircraft is on jacks, it is recommended that a safety stay be placed under the fuselage,between FR73 and FR74 to prevent tail tipping caused by accidental displacement of the centerof gravity.
The safety stay is not used to lift the aircraft.
A male spherical ball pad with a 19 mm (0.75 in) radius, forming part of the airplane structureis provided for using the safety stay.
2. Jack Design
In fully retracted position (jack stroke at minimum), the height of the jack may be placed beneaththe airplane under the most adverse conditions, namely, tires deflated and shock absorbersdepressurized.
2-14-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
In addition, a clearance of 50 mm (1.97 in) approximately must be provided between the airplanejacking point and the jack upper end. The lifting jack stroke enables the aircraft to be jacked up sothat the fuselage longitudinal datum line (aircraft center line) parallel to the ground, with a 100 mm(3.94 in) clearance between the main landing gear wheels and the ground.In particular, this enables the landing gear extension/retraction tests to be performed.
Jacking Point Location Z Maximum Permitted Load
Forward Fuselage Jacking Point-1.987 m(-6.52 ft)
6 800 daN(15 287 lbf)
Wing Jacking Point-0.828 m(-2.72 ft)
28 500 daN(64 071 lbf)
Safety Stay-0.748 m(-2.45 ft)
2 000 daN(4 496 lbf)
The maximum permitted aircraft weight for the jacking procedure is 53 000 kg (116 845 lb).Centerline at 4.6 mm (0.18 in) parallel to the ground.
2-14-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FWD JACKINGPOINT
SAFETYPOINT
26.44 m
15.18 m
2.74 m(8.99 ft)
6.5 m
CL
(49.80 ft)
(86.75 ft)
WING JACKINGPOINT
(21.33 ft)
WING JACKINGPOINT
N_AC_021400_1_0010101_01_00
Jacking for MaintenanceJacking Point Location
FIGURE-2-14-0-991-001-A01
2-14-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
POINT A DETAIL
Z−1 979.8Z−1 987
FR8
A
SPHERICAL RADIUS19 mm (0.75 in)
A
N_AC_021400_1_0030101_01_00
B
B
Jacking for MaintenanceForward Jacking Point
FIGURE-2-14-0-991-003-A01
2-14-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
LOWER SURFACE
A
WING JACK PAD
POINT BB’ DETAIL
Z−895
Z−828.35
RE
AR
SP
AR
DA
TU
M
INTERSECTION WITH REARSPAR DATUM
RIB9
SPHERICAL RADIUS32 mm (1.26 in)
A
A
EXAMPLE
B
B
N_AC_021400_1_0560101_01_00
Jacking for MaintenanceWing Jacking Points
FIGURE-2-14-0-991-056-A01
2-14-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
Z−744.932
SPHERICAL RADIUS 19 mm (0.75 in)(19 D535−71 595)
X =
35
106
A
Z−729.441
A
N_AC_021400_1_0570101_01_00
(4.95 in)
125.67 mm
Jacking for MaintenanceSafety Stay
FIGURE-2-14-0-991-057-A01
2-14-0Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
M
L
THE CENTER LINE (CL) IS A FICTITIOUS LINE AROUND WHICH THE AIRCRAFT IS BUILT.SAFETY STAY IS NOT USED FOR JACKING.SEE SECTION 1−10, FOR GROUND CLEARANCES A/C ON JACKS.
NOTE:
L M
1 560 mm(61.42 in)
2 846 mm(112.05 in)
3 047 mm(119.96 in)
2 620 mm(103.15 in)
3 772 mm(148.50 in)
3 859 mm(151.93 in)
1 931 mm(76.02 in)
3 082 mm(121.34 in)
3 169 mm(124.76 in)
1 545 mm(60.83 in)
2 761 mm(108.70 in)
2 892 mm(113.86 in)
N
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED AND
AIRCRAFT ON WHEELS, NLG SHOCK ABSORBER DEFLATED
AIRCRAFT ON JACKS, CENTER LINE (CL) PARALLEL TO GROUNDSHOCK ABSORBERS EXTENDED MAIN WHEEL CLEARANCE(STANDARD TIRES) (49 x 17) 120 mm (4.72 in) FOR EXTENDED
AIRCRAFT ON WHEELS, (STANDARD TIRES) AT MAX.PERMITTED WEIGHT FOR JACKING
FLAT TIRES
AND RETRACTED LANDING GEARS
AND FLAT TIRES
N
N_AC_021400_1_0040101_01_00
Jacking for MaintenanceJacking Design
FIGURE-2-14-0-991-004-A01
2-14-0Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
Jacking for Wheel Change
1. General
Landing gear jacking will be required especially for replacing wheels and brake unit components.
The maximum permitted aircraft weight for jacking is 53 000 kg (116 845 lb).
2. Main Gear Jacking
The main gears are normally jacked up by placing a jack directly under the ball pad.
The ball spherical radius is 19 mm (0.75 in).
It is also possible to jack the main gear using a cantilever jack.
3. Nose Gear Jacking
For nose gear jacking a 19 mm (0.75 in) radius ball pad is fitted under the lower end of the shockabsorber sliding tube. Jacking can be accomplished either by placing a jack directly under the ballpad, or using an adapter fitting provided with an identical ball pad.
2-14-0Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:
45 x 16 R20
552 mm(21.73 in)
38 mm(1.5 in)
DIA. BALL
25 mm (1 in)
218 mm(8.58 in)
180 mm(7.09 in)
ON THE RIM
200 mm(7.87 in)FULLY
RETRACTED
49 x 19 R20
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES.TWIN WHEEL TRACK IS 927 mm (36.5 in).
THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)CLEARANCE BETWEEN THE TIRE AND GROUND.
600 mm(23.62 in)FULLY
EXTENDED
N_AC_021400_1_0120101_01_00
FLAT TIRES
INFLATED TIRES
Landing Gear Jacking for Wheel ChangeMLG Jacking Point Location - Twin Wheels
FIGURE-2-14-0-991-012-A01
2-14-0Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_021400_1_0130101_01_00
MLG TIRE 49 x 19 R20
643 mm(25.32 in)
TWIN WHEEL TRACK
927 mm(36.5 in)
DOUBLE FLAT MLG TIRES
MIN
FORK
CONTOUR OF TIRES ON GROUND
CANTILEVERARM
25 mm(1 in)
1 620 mm(63.78 in)
25 mm(1 in)MIN
25 mm(1 in) APPROX
409 mm(16.1 in)
218 mm (8.58 in)(180 mm (7.09 in)
ON RIM)
552 mm(21.73 in)
FWD
Landing Gear Jacking for Wheel ChangeMLG Jacking with Cantilever Jack - Twin Wheels
FIGURE-2-14-0-991-013-A01
2-14-0Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
32
80 90 100 110 120 130 140 150 (x1 000 lbs)
AIRCRAFT GROSS WEIGHT
30
28
26
22
20
18
16
1435 40 45 50 55 60 65 70 (x1 000 kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x1 0
00 k
g)
24
CG POSITION15.0% MAC18.7% MAC25.0% MAC31.0% MAC37.0% MAC
N_AC_021400_1_0140101_01_00
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking Points - Twin Wheels
FIGURE-2-14-0-991-014-A01
2-14-0Page 11
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
APPROX326 mm
(12.83 in)38 mm(1.5 in)
DIA. BALLSAE AS 33559
25 mm(1 in)
128 mm(5.04 in)
40 mm(1.57 in)
THE FLAT TIRES VIEW SHOWS THE MINIMUM HEIGHT TO ENGAGE JACK WITH 2 FLAT TIRES.THE INFLATED TIRES VIEW SHOWS THE JACKING HEIGHT TO GIVE 25 mm (1 in)CLEARANCE BETWEEN THE TIRE AND GROUND.
NOTE:
500 mm (19.69 in)
264 mm MIN (10.39 in)289 mm MAX (11.38 in)
INFLATED TIRESFLAT TIRES
198 mm(7.8 in)
FWD
N_AC_021400_1_0150101_01_00
A
A
Landing Gear Jacking for Wheel ChangeNLG Jacking - Point LocationFIGURE-2-14-0-991-015-A01
2-14-0Page 12
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
12
10
8
6
4
2
14
35 40 45 50 55 60 65 70
CG POSITION15.0% MAC18.7% MAC25.0% MAC31.0% MAC37.0% MAC
80 90 100 110 120 130 140 150 (x1 000 lbs)
AIRCRAFT GROSS WEIGHT
(x1 000 kg)
LOA
D A
T J
AC
KIN
G P
OIN
T (
x1 0
00 k
g)
N_AC_021400_1_0160101_01_00
Landing Gear Jacking for Wheel ChangeLoads at NLG Jacking PointsFIGURE-2-14-0-991-016-A01
2-14-0Page 13
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0 General Information
**ON A/C A318-100
General Information
1. This section gives standard day temperatures.
Section 3-2 indicates payload range information at specific altitudes recommended for long rangecruise with a given fuel reserve condition.
Section 3-3 represents FAR take-off runway length requirements at ISA and ISA +15˚C (+59˚F) forCFM56 and PW 6000 series engine conditions for FAA certification.
Section 3-4 represents FAR landing runway length requirements for FAA certification.
Section 3-5 indicates final approach speeds.
Standard day temperatures for the altitudes shown are tabulated below:
Standard day temperatures for the altitude
Altitude Standard Day Temperature
FEET METERS ˚F ˚C0 0 59.0 15.02000 610 51.9 11.14000 1219 44.7 7.16000 1829 37.6 3.18000 2438 30.5 -0.8
3-1-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-0 Payload / Range
**ON A/C A318-100
Payload / Range
1. Payload / Range
3-2-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1 ISA Conditions
**ON A/C A318-100
ISA Conditions
1. This section gives the payload / range at ISA conditions.
3-2-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
50 40 30 20 10 0
20 10 0
(100
0 lb
)(1
000
kg)
PA
YLO
AD
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
010
0020
0030
0040
00
7000
6000
5000
4000
3000
2000
1000
0R
AN
GE
(KM
)
RA
NG
E(N
M)
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
NO
TE
:
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ftIN
TE
RN
AT
ION
AL
RE
SE
RV
ES
:E
N R
OU
TE
10%
FLI
GH
T T
IME
OV
ER
SH
OO
T
59t
63t
68t
107
PA
SS
EN
GE
RS
N_AC_030201_1_0010101_01_00
Payload / RangeCFM56 series engine
FIGURE-3-2-1-991-001-A01
3-2-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
50 40 30 20 10 0
20 10 0
(100
0 lb
)(1
000
kg)
PA
YLO
AD
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
010
0020
0030
0040
00
7000
6000
5000
4000
3000
2000
1000
0R
AN
GE
(KM
)
RA
NG
E(N
M)
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
NO
TE
:
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ftIN
TE
RN
AT
ION
AL
RE
SE
RV
ES
:E
N R
OU
TE
10%
FLI
GH
T T
IME
OV
ER
SH
OO
T
59t
63t
68t
107
PA
SS
EN
GE
RS
N_AC_030201_1_0020101_01_00
Payload / RangePW 6000 series engine
FIGURE-3-2-1-991-002-A01
3-2-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-0 FAR / JAR Takeoff Weight Limitation
**ON A/C A318-100
FAR / JAR Take-off Weight Limitation
1. FAR / JAR Take-off Weight Limitation
3-3-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1 ISA Conditions
**ON A/C A318-100
ISA Conditions
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30
40
50
60
70
80
90 200
190
180
170
160
150
140
130
120
110
100
90
80
704
1
6 8 10 12 14
2 3 4 5
16
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
864
02
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
N_AC_030301_1_0010101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA Conditions -- CFM56 series engine
FIGURE-3-3-1-991-001-A01
3-3-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30
40
50
60
70
80
90 200
190
180
170
160
150
140
130
120
110
100
90
80
704
1
6 8 10 12 14
2 3 4 5
16
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
2 4 6
8
0
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
N_AC_030301_1_0020101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA Conditions -- PW 6000 series engine
FIGURE-3-3-1-991-002-A01
3-3-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2 ISA +15˚C (+59˚F) Conditions
**ON A/C A318-100
ISA +15˚C (+59˚F) Conditions
1. This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions.
3-3-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30
40
50
60
70
80
90 200
190
180
170
160
150
140
130
120
110
100
90
80
704
1
6 8 10 12 14
2 3 4 5
16
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
864
02
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
N_AC_030302_1_0010101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56 series engine
FIGURE-3-3-2-991-001-A01
3-3-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30
40
50
60
70
80
90 200
190
180
170
160
150
140
130
120
110
100
90
80
704
1
6 8 10 12 14
2 3 4 5
16
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
8
642
N_AC_030302_1_0020101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- PW 6000 series engine
FIGURE-3-3-2-991-002-A01
3-3-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-0 FAR / JAR Landing Field Length
**ON A/C A318-100
FAR / JAR Landing Field Length
1. FAR / JAR Landing Field Length
3-4-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1 ISA Conditions
**ON A/C A318-100
ISA Conditions
1. This section gives the landing field length.
3-4-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
LENGTH(1000 m)
LANDING FIELD(1000 ft)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
12
10
8
6
4
2 1.0
1.5
2.0
2.5
3.0
3.5
35 40 45 50 55 60 65
1401301201101009080
GROSS WEIGHT(1000 kg)
GROSS WEIGHT(1000 lb)
02468
AIRFIELD ELEVATION(1000 ft)
N_AC_030401_1_0010101_01_00
FAR / JAR Landing Field LengthCFM56-5B series engine
FIGURE-3-4-1-991-001-A01
3-4-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
12
10
8
6
4
265605550454035
2
1.5
2.0
2.5
3.0
3.5
86420
LENGTH(1000 m)LENGTH
(1000 ft)
LANDING FIELD
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
GROSS WEIGHT(1000 kg)
PRESSURE ALTITUDE(1000 ft)
80 90 100 110 120 130 140GROSS WEIGHT
(1000 lb)
N_AC_030401_1_0020101_01_00
FAR / JAR Landing Field LengthPW 6000 series engine
FIGURE-3-4-1-991-002-A01
3-4-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0 Final Approach Speed
**ON A/C A318-100
Final Approach Speed
1. This section gives the final approach speed.
3-5-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
90
100
110
120
130
140
35 40 45 50 55 60 65
1401301201101009080
GROSS WEIGHT(1000 kg)
GROSS WEIGHT(1000 lb)
C.A.S (Kts)
N_AC_030500_1_0010101_01_00
Final Approach SpeedCFM56-5B8 and CFM56-5B9 series engine
FIGURE-3-5-0-991-001-A01
3-5-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
90
100
110
120
130
140
35 40 45 50 55 60 65
1401301201101009080
GROSS WEIGHT(1000 kg)
GROSS WEIGHT(1000 lb)
C.A.S (Kts)
N_AC_030500_1_0020101_01_00
Final Approach SpeedPW 6000 series engine
FIGURE-3-5-0-991-002-A01
3-5-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A318-100
General Information
1. This section provides airplane turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.
In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the using airlines prior to layout planning.
4-1-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0 Turning Radii
**ON A/C A318-100
Turning Radii
1. This section gives the turning radii.
4-2-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
R6
R4
R5
R3
R2
R1
NOTE:
TURN TYPE:
1. ASYMMETRIC THRUST DIFFERENTIAL BRAKING
FOR STEERING DIMENSION TABLE SEE SHEET 2.
N_AC_040200_1_0010101_01_02
10.25 m(33.63 ft)
50°
60°
70°
(PIVOTTING ON ONE MAIN GEAR).
2. SYMMETRIC THRUST NO BRAKING.
7.59 m(24.9 ft)
Turning Radii, No Slip AngleFIGURE-4-2-0-991-001-A01
4-2-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
MA
XIM
UM
RA
MP
WE
IGH
T
EF
FE
CT
IVE
ST
EE
RIN
G A
NG
LE(d
eg)
mft
ft
ft
m
mm
ft
mft
mft
R6
TH
SR
5R
3N
LGR
2LM
LG
mft
R1
RM
LG
ST
EE
RIN
G
(deg
)A
NG
LEW
ING
TIP
FE
NC
ES
HA
RK
LET
R4
− W
ING
NO
SE
TY
PE
TU
RN
OF
75 (
MA
X)
7065605550454025 3020
70.3
8.2
270.
6
1.3
2.3
3.4
4.6
6.1
7.7
9.7
19.8
15.4
26.1
211
.03637394043465055708310
3
21.2
6972757983879399118
132
152
22.0
7215
.852
18.2
60
66.6
62.2
57.6
52.9
48.2
43.4
38.6
24.1
19.3
8.9
9.9
11.0
12.2
13.7
15.3
17.3
27.3
23.0
33.7
2932364045505790 75111
48111520253265 5186
11.3
11.8
12.3
13.1
14.0
15.2
16.7
21.5
25.4
31.3
21.9
22.9
24.0
25.2
26.6
28.2
30.2
35.8
40.2
46.5
22.8
23.7
24.8
26.0
27.4
29.1
31.1
36.7
41.0
47.3
757881859095102
120
135
155
16.0
16.2
16.6
17.2
17.9
18.8
20.0
24.0
27.5
33.0
525355565962667990108
18.7
19.2
19.9
20.7
21.7
22.9
24.5
29.1
32.9
38.6
6163656871758095108
127
29.0
22 2 2 2 2 2 2 2 2 2 2
3512
.261
107
33.8
19.8
6540
18.7
32.7
33.5
110
21.7
7126
.487
75 (
MA
X)
7065605550
71.8
7.8
0.3
1.2
2.2
3.3
4.6
6.0
10.9
20.9
21.7
7115
.751
18.1
59
67.3
62.8
57.9
53.1
48.3
8.8
9.7
10.9
12.2
13.6
11.3
11.7
12.3
13.0
14.0
21.8
22.7
23.9
25.1
26.5
22.6
23.6
24.7
26.0
27.4
7477818590
15.9
16.2
16.6
17.1
17.8
5253555658
18.6
19.2
19.9
20.7
21.7
61636568711 1 1 1 1 1
261
363738404346
687175788287
2932364045
47111520
AB
OV
E 5
0°, A
IRLI
NE
S M
AY
US
E T
YP
E 1
OR
TY
PE
2 T
UR
NS
DE
PE
ND
ING
ON
TH
E S
ITU
AT
ION
.T
YP
E 1
TU
RN
S U
SE
:T
HE
TU
RN
ON
LY.
TY
PE
2 T
UR
NS
US
E:
IT IS
PO
SS
IBLE
TO
GE
T L
OW
ER
VA
LUE
S T
HA
N T
HO
SE
FR
OM
TY
PE
1 B
Y A
PP
LYIN
G D
IFF
ER
EN
TIA
L B
RA
KIN
G D
UR
ING
NO
TE
:
N_AC_040200_1_0020101_01_01
TH
E W
HO
LE T
UR
N.
AS
YM
ME
TR
IC T
HR
US
T D
UR
ING
TH
E W
HO
LE T
UR
N; A
ND
DIF
FE
RE
NT
IAL
BR
AK
ING
TO
INIT
IAT
E
SY
MM
ET
RIC
TH
RU
ST
DU
RIN
G T
HE
WH
OLE
TU
RN
; AN
D N
O D
IFF
ER
EN
TIA
L B
RA
KIN
G A
T A
LL.
Turning Radii, No Slip AngleFIGURE-4-2-0-991-002-A01
4-2-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A318-100
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
R6
R3
R5
R4
10.3 m
PAVEMENTWIDTH FOR180° TURN
MINIMUM
(34 ft)
STEERINGANGLE 75°
A
EFFECTIVETURN
Y
NOTE:MEASURED FROM OUTSIDE FACE OF TIRE.MODEL 100 TURN DIMENSION SHOWN.THEORETICAL CENTER OF TURNFOR MINIMUM TURNING RADIUS.SLOW CONTINUOUS TURNING.APPROXIMATELY IDLE THRUSTON BOTH ENGINES.
NOSE GEAR RADII TRACK R3,
NOTE:BY APPLYING DIFFERENTIAL BRAKING DURING THE WHOLE TURN.IT IS POSSIBLE TO GET LOWER VALUES THAN THOSE FROM TYPE 1
TYPEOF
TURN
1
2
STEERINGANGLE(DEG)
75 (MAX)
75 (MAX)
EFFECTIVESTEERING
ANGLE
71.8°
70.3°
m
m
ft
ft
Y
3.4
3.7
11
12
A
19.0
19.4
62
64
R3NLG
10.9
11.0
36
36
R4 WINGWING TIPFENCE
20.9
21.2
68
69
SHARKLET
21.7
22.0
71
72
R5NOSE
15.7
15.8
51
52
R6THS
18.1
18.2
59
60
NO DIFFERENTIAL BRAKING.DRY SURFACE.
N_AC_040300_1_0010101_01_02
OUTSIDE FACE OF TIRE
Minimum Turning RadiiFIGURE-4-3-0-991-001-A01
4-3-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A318-100
Visibility from Cockpit in Static Position
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30°
20°
10.14 m(33 ft 3.24 in)
5.07 m(16 ft 7.56 in)
VISUAL ANGLES IN VERTICALPLANE THROUGH PILOTEYE POSITION.
NOT TO BE USED FORLANDING APPROACH VISIBILITY
DIMENSIONS ARE APPROXIMATE
2.41 m(7 ft 10.92 in)4.56 m
(14 ft 11.52 in)
111°
133°
CAPTAIN FIELD OF VIEW
133°
111°
MAX AFT VISION WITH HEAD TURNEDAROUND SPINAL COLUMN.WING TIP CAN BE SEEN WHEN HEAD IS MOVEDTO THE SIDE.
VISUAL ANGLES IN HORIZONTALPLANE THROUGH PILOTEYE POSITION.
FIRST OFFICERFIELD OF VIEW
0.53 m(1 ft 8.88 in)
46°
32°
33°
25°
32°
25°
VISUAL ANGLES IN PLANEPERPENDICULAR TOLONGITUDINAL AXIS.
46°
33°
WITH HEAD MOVED125 mm (5 in) OUTBOARD
NOTE:PILOT EYE POSITION WHEN PILOT’S EYES ARE IN LINE WITH THE RED AND WHITE BALLS.
ZONE THAT CANNOT BE SEEN
N_AC_040400_1_0010101_01_03
Visibility from Cockpit in Static PositionFIGURE-4-4-0-991-001-A01
4-4-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FIR
ST
OF
FIC
ER
FIX
ED
WIN
DO
WF
IRS
T O
FF
ICE
RS
LID
ING
WIN
DO
WF
IRS
T O
FF
ICE
RW
IND
SH
IELD
CA
PT
AIN
WIN
DS
HIE
LDC
AP
TA
IN S
LID
ING
WIN
DO
WC
AP
TA
INF
IXE
D W
IND
OW
PIL
OT
EY
E P
OS
ITIO
N(C
AP
TA
IN P
OS
ITIO
N)
AS
580
B
A32
0
CA
PT
AIN
FIE
LD O
F V
IEW
SH
OW
N.
FIR
ST
OF
FIC
ER
FIE
LD O
F V
IEW
SY
MM
ET
RIC
AL.
EX
AM
PLE
: WH
EN
CA
PT
AIN
TU
RN
S H
IS H
EA
D B
Y 8
0° L
EF
T, V
ISIB
ILIT
YW
ILL
BE
35°
UP
AN
D 2
5° D
OW
N T
HR
OU
GH
TH
E S
LID
ING
WIN
DO
W F
RA
ME
.
35°
30°
20°
10°
0° 10°
20°
25°
110°
100°
90°
80°
70°
50°
40°
30°
20°
10°
0°10
°20
°40
°50
°60
°80
°90
°10
0°13
0°12
0°60
°30
°70
°11
0°
N_AC_040400_1_0050101_01_00
Binocular Visibility Through Windows from Captain Eye PositionFIGURE-4-4-0-991-005-A01
4-4-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A318-100
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A318-100
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
15 m(50 ft)
RUNWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
TAXIWAYCENTERLINE
FAA LEAD−IN FILLET
L = 45 m (150 ft)
APPROX 5.7 m(19 ft)
30 m(100 ft)
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATH
N_AC_040501_1_0010101_01_02
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-001-A01
4-5-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RUNWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
FAA LEAD−IN FILLET
L = 45 m (150 ft)
APPROX 3.2 m(10 ft)
TAXIWAYCENTERLINE
30 m
NOTE: FAA GROUP III FACILITIES.
N_AC_040501_1_0110101_01_00
NLG PATH
MLG PATH
15 m(50 ft)
(100 ft)
135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-1-991-011-A01
4-5-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A318-100
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
APPROX 6.9 m(22 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
RUNWAY CENTERLINE
FAA LEAD−IN FILLETL = 45 m (150 ft)
30 m(100 ft)
TAXIWAY CENTERLINE
15 m(50 ft)
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATH
N_AC_040502_1_0010101_01_02
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-001-A01
4-5-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
APPROX 9.3 m(30 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
RUNWAY CENTERLINE
FAA LEAD−IN FILLETL = 45 m (150 ft)
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATH
30 m(100 ft)
15 m(50 ft)
N_AC_040502_1_0080101_01_00
90˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-2-991-008-A01
4-5-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A318-100
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30 m(100 ft)
NOTE: TYPE 1 VALUES.
7.4 m(24 ft) 3 m
(10 ft)
RUNWAY CENTERLINE
R3 = 10.9 m(36 ft)
R5 = 15.8 m(52 ft)
R4
N_AC_040503_1_0050101_01_00
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
WINGTIP FENCES:R4 = 20.9 m (69 ft)SHARKLETS:R4 = 21.7 m (71 ft)
180˚ turn on a RunwayEdge of Runway Method (Sheet 1 of 2)
FIGURE-4-5-3-991-005-A01
4-5-3Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30 m(100 ft)
NOTE: TYPE 1 VALUES.
RUNWAY CENTERLINE
6.23 m(20 ft)
4.76 m(16 ft)
25°
N_AC_040503_1_0050102_01_00
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
WINGTIP FENCES:R4 = 20.9 m (69 ft)SHARKLETS:R4 = 21.7 m (71 ft)
R3 = 10.9 m(36 ft)
R5 = 15.8 m(52 ft)
R4
180˚ turn on a RunwayCenter of Runway Method (Sheet 2 of 2)
FIGURE-4-5-3-991-005-A01
4-5-3Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4 135˚ Turn - Taxiway to Taxiway
**ON A/C A318-100
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway.
4-5-4Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FAA LEAD−IN FILLET
L = 45 m (150 ft)
APPROX 6.3 m(21 ft)
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
(100 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m
N_AC_040504_1_0010101_01_02
15 m(50 ft)
15 m(50 ft)
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-4-991-001-A01
4-5-4Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
FILLET R = 16.5 m
TURN R = 30 m
FAA LEAD−IN FILLET
APPROX 3.1 m(10 ft)
15 m(50 ft)
15 m(50 ft)
N_AC_040504_1_0010102_01_00
(55 ft)
(100 ft)
L = 45 m (150 ft)
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-4-991-001-A01
4-5-4Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5 90˚ Turn - Taxiway to Taxiway
**ON A/C A318-100
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-5Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
15 m(50 ft)
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATHTAXIWAY CENTERLINE
APPROX 6.4 m(21 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft) 15 m
(50 ft)
N_AC_040505_1_0010101_01_02
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-5-991-001-A01
4-5-5Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATHTAXIWAY CENTERLINE
APPROX 9.3 m(30 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft)
15 m(50 ft)
15 m(50 ft)
N_AC_040505_1_0010102_01_00
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-5-991-001-A01
4-5-5Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A318-100
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
4-6-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
6.1 m(20 ft)
RUNWAY CENTERLINETAXIWAY
CENTERLINE
6.1 m(20 ft)
190 m(625 ft)
23 m(75 ft)
45 m(150 ft)
HOLDING POINT
12.2 m(40 ft)
90 m(300 ft)61 m
(200 ft)
N_AC_040600_1_0010101_01_02
Runway Holding Bay (Apron)FIGURE-4-6-0-991-001-A01
4-6-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0 Parking
**ON A/C A318-100
Airplane Parking
1. The following figures and charts show the rectangular space required for parking against the terminalbuilding.
The rectangle includes allowance for swinging the airplane on arrival and departure.- Steering Geometry- Minimum Parking Space Requirements
4-7-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
0
20
40
80
120
140
160
180
200
100
60
0
10
20
30
40
50
60
0
10 20 30 40 50 60 70 80 90
300280260240220200180160140120100806040200
DISTANCE ALONG TERMINAL (m)
DISTANCE ALONG TERMINAL (ft)
NOTE: ± 75° NOSE WHEEL STEERING (POWER OUT).± 95° NOSE WHEEL STEERING (PUSH BACK, PUSH OUT).3.05 m (10 ft) TRAVEL WITH NOSE WHEEL STRAIGHT AHEAD BEFORE AND AFTER
PARKED POSITION.
4.5 m (15 ft) BUILDING CLEARANCE FOR NOSE−IN PARKING.7.5 m (25 ft) BUILDING CLEARANCE FOR OTHER PARKING POSITIONS.7.5 m (25 ft) AIRPLANE TO AIRPLANE CLEARANCE DURING PARKING MANOEUVRES.LIAISE WITH USER AIRLINE FOR SPECIFIC PLANNED OPERATION PROCEDURE.
DISTANCE OUTFROM TERMINAL
(ft) (m)
PARALLEL PARKPOWER OUT
45° ENTRYPOWER OUT
90° ENTRYPUSH OUT
45° ENTRYPUSH OUT
STRAIGHT ENTRYPUSH BACK
N_AC_040700_1_0010101_01_00
Airplane ParkingMinimum Parking Space Requirements
FIGURE-4-7-0-991-001-A01
4-7-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
35.95 m(117 ft 11.4 in)
48.94 m(160 ft 6.86 in)
STRAIGHT ENTRY−PUSH BACK
N_AC_040700_1_0020101_01_01
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-002-A01
4-7-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
48.94 m(160 ft 6.86 in)
57.56 m(188 ft 10.2 in)
PARALLEL IN−POWER OUT
N_AC_040700_1_0030101_01_01
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-003-A01
4-7-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
53.52 m(175 ft 6.96 in)
43.7 m(143 ft 4.32 in)
90° ENTRY−PUSH OUT
N_AC_040700_1_0040101_01_01
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-004-A01
4-7-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
41.55 m(136 ft 3.72 in)
58.61 m(192 ft 3.36 in)
45° ENTRY IN−POWER OUT
N_AC_040700_1_0050101_01_01
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-005-A01
4-7-0Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
31.07 m(101 ft 11.16 in)
41.57 m(136 ft 4.56 in)
45° ENTRY−PUSH OUT
N_AC_040700_1_0060101_01_01
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-006-A01
4-7-0Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
27.4 m(89 ft 10.8 in)
13.7 m(44 ft 10.8 in)
3.05 m
NOTE: 73.2° EFFECTIVE STEERING ANGLE.
END OF RUNWAY
EDGE OFRUNWAY
44.1 m(46 ft 3.6 in)
24.4 m(79 ft 10.8 in)
REF(10 ft)
REF3.05 m(10 ft) REF
3.05 m(10 ft)
N_AC_040700_1_0070101_01_01
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-007-A01
4-7-0Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RUNWAY WIDTH 60.0 m
ED
GE
OF
RU
NW
AY
20.9
m
10.6
m
3.05
mR
EF
END OF RUNWAY
(68
ft 4.
8 in
)
(34
ft 9.
6 in
)
NOTE: 73.2° EFFECTIVE STEERING ANGLE.
(10
ft)
(196 ft 10.8 in)
N_AC_040700_1_0080101_01_01
Airplane ParkingSteering Geometry
FIGURE-4-7-0-991-008-A01
4-7-0Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
**ON A/C A318-100
Terminal Servicing
1. GeneralThis chapter provides typical ramp layouts, corresponding minimum turnaround time estimations,locations of ground service points and service requirements.The information given in this chapter reflects ideal conditions. Actual ramp layouts and servicerequirements may vary according to local regulations, airline procedures and the airplane condition.- Section 5.1 shows typical ramp layouts for passenger aircraft at the gate or on an open apron.- Section 5.2 shows the minimum turnaround schedules for full servicing arrangements.- Section 5.3 shows the minimum turnaround schedule for reduced servicing arrangements.- Section 5.4 gives the locations of ground service connections, the standard of connections used
and typical capacities and requirements.- Section 5.5 provides the engine starting pneumatic requirements for different engine types and
different ambient temperatures.- Section 5.6 provides the air conditioning requirements for heating and cooling (pull-down and
pull-up) using ground conditioned air for different ambient temperatures.- Section 5.7 provides the air conditioning requirements for heating and cooling to maintain a
constant cabin air temperature using low pressure conditioned air.- Section 5.8 shows the ground towing requirements taking into account different ground surface
and aircraft conditions.
5-0-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-0 Servicing Arrangements
**ON A/C A318-100
Airplane Servicing Arrangements
1. GeneralThis chapter provides typical ramp layouts, showing the various GSE items in position during typicalturnaround scenarios for the passenger aircraft.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.
The associated turnaround chart for full servicing is given in section 5.2.The associated turnaround chart for minimum servicing arrangement is given in section 5.3.
5-1-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A318-100
Symbols Used on Servicing Diagrams
1. This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC AIR CONDITIONING UNITAS AIR STARTING UNITBULK BULK TRAINCAT CATERING TRUCKCB CONVEYOR BELTCLEAN CLEANING TRUCKFUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNITLD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLEPBB PASSENGER BOARDING BRIDGEPS PASSENGER STAIRSTOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE
5-1-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2 Typical Ramp Layout - Open Apron
**ON A/C A318-100
Typical Ramp Layout - Open Apron
1. This section gives the typical servicing arrangement for pax version (Open Apron).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance 7.5 m from the aircraft).No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks in positionon landing gears).
5-1-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_050102_1_0010101_01_03
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6
CAT
CAT
WV
LV
BULK
FUEL
CB
CB
ASTOW
GPU
BULK
PS
PS
AC
Typical Ramp LayoutOpen Apron - Bulk LoadingFIGURE-5-1-2-991-001-A01
5-1-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3 Typical Ramp Layout - Gate
**ON A/C A318-100
Typical Ramp Layout - Gate
1. This section give the typical servicing arrangement for pax version (Passenger Bridge).
The Stand Safety Line delimits the Aircraft Safety Area (minimum distance of 7.5 m from theaircraft). No vehicle must be parked in this area before complete stop of the aircraft (wheel chocks inposition on landing gears).
5-1-3Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_050103_1_0040101_01_02
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6
CAT
CAT
WV
LV
BULK
FUEL
CB
CB
TOW
GPU
PBB
BULK
AS
AC
Typical Ramp LayoutGate
FIGURE-5-1-3-991-004-A01
5-1-3Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0 Terminal Operations - Full Servicing
**ON A/C A318-100
Terminal Operations - Full Servicing Turn Round Time
1. This section provides typical turn round time chart showing the typical times for ramp activitiesduring aircraft turn round.
Actual times may vary due to each operator’s specific practice and operating conditions.
For each turn round time chart, the associated typical ramp layout is given in Section 5-1.
2. Assumptions for full turn round chart
A. PASSENGER HANDLING107 pax, all Y/CAll passengers deboard and board the aircraft1 Passenger Boarding Bridge (PBB) used at door L1Equipment positioning/removal + opening/closing door = 2 min
Deboarding:- 107 pax at door L1- Deboarding rate = 22 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 107 pax at door L1- Boarding rate = 18 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +2 min- No Passenger with Reduced Mobility
B. CARGO2 belt loadersEquipment positioning/removal + opening/closing door = +1 min
Cargo exchange:- 15 kg (33 lb) per pax- FWD cargo compartment: 700 kg (1543 lb)- AFT cargo compartment: 900 kg (1984 lb)- Bulk off-loading rate = 120 kg/min (265 lb/min)- Bulk loading rate = 100 kg/min (220 lb/min)
C. REFUELLING2 hoses, one side6624 l (1750 US gal) at 50 psi (3 bar)
5-2-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Dispenser positioning/removal = 4 min
D. CLEANINGPerformed in available time
E. CATERING1 catering truck for servicing galleys sequentially at doors R1 & R2Equipment positioning/removal + door opening/closing = 2 minTime to drive from one door to the other = 1 minFull Size Trolley Equivalent (FSTE) to unload and load:- 4 FSTE at door R1- 4 FSTE at door R2Time for trolley exchange = 1.5 min per FSTE
F. GROUND HANDLING SERVICINGStart of operations:- Bridges: t0 = 0- Other equipment: t = t0 + 1 minPotable water servicing: 100% uplift, 200 l (53 US gal), max filling pressure = 3.45 bar (50 psi)Toilet servicing: draining + rinsing = 5 min, max rinse & precharge pressure = 3.45 bar (50psi)
5-2-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
0 5 15 20 25 30 35 40
HEADCOUNTING
CATERING AT DOOR R2
CLEANING
CARGO FWD CC
REFUELLING
TOILET SERVICING
CARGO AFT CC
TRT: 34 min
10
CATERING AT DOOR R1
DEBOARDING/BOARDING AT DOOR L1
POTABLE WATERSERVICING
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
min
N_AC_050200_1_0040101_01_01
AVAILABLE TIME
Turn Round StationsFull Servicing (34 Min.)
FIGURE-5-2-0-991-004-A01
5-2-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0 Terminal Operation - Transit
**ON A/C A318-100
Terminal Operation - Minimum Servicing Turn Round Time
1. This section provides typical turn round time chart showing the typical times for ramp activitiesduring aircraft turn round.
Actual times may vary due to each operator’s specific practice and operating conditions.
For each turn round time chart, the associated typical ramp layout is given in Section 5-1.
2. Assumptions for minimum turn round chart
A. PASSENGER HANDLING132 pax, all Y/C2 Stairways used at doors L1 & L2Equipment positioning/removal + opening/closing door = 2 min
Deboarding:- 66 pax at door L1- 66 pax at door L2- Deboarding rate = 20 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 66 pax at door L1- 66 pax at door L2- Boarding rate = 15 pax/min per door- Last Pax Seating allowance (LPS) + headcounting = +2 min- No Passenger with Reduced Mobility
B. CARGO2 belt loadersEquipment positioning/removal + opening/closing door = +1 min
Cargo exchange:- 10 kg (22 lb) per pax- FWD cargo compartment: 660 kg (1455 lb)- AFT cargo compartment: 660 kg (1455 lb)- Bulk off-loading rate = 120 kg/min (265 lb/min)- Bulk loading rate = 100 kg/min (220 lb/min)
C. REFUELLING2 hoses, one side
5-3-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6624 l (1750 US gal) at 50 psi (3 bar)Dispenser positioning/removal = 4 min
D. CLEANINGPerformed in available time
E. CATERINGNo catering
F. GROUND HANDLING SERVICINGStart of operations:- Bridges: t0 = 0- Other equipment: t = t0 + 1 minNo potable water servicingNo toilet servicing
5-3-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
0 5 15 20 25 3010
TRT: 20 min
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
HEADCOUNTING
CATERING
CLEANING
CARGO FWD CC
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CARGO AFT CC
AVAILABLE TIME
AVAILABLE TIME
min
DEBOARDING/BOARDING AT DOOR L1
DEBOARDING/BOARDING AT DOOR L2
N_AC_050300_1_0010101_01_01
Turn Round StationsMinimum Servicing (20 Min.)FIGURE-5-3-0-991-001-A01
5-3-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-0 Ground Service Connections
**ON A/C A318-100
Ground Service Connections
1. Ground Service Connections.
5-4-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1 Ground Service Connections Layout
**ON A/C A318-100
Ground Service Connections Layout
1. This section gives the ground service connections layout.
5-4-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
1 3 6 7 11 12 2 4 14− −
67
6
7
13
10
1
10
13
14
CONNECTOR (LP) PANELS
EXTERNAL POWER RECEPTACLETOILET SERVICE DOORGROUNDING POINT NLGPOTABLE WATER SERVICE DOORGROUND SERVICE CONDITIONED AIR
IDG OIL FILLINGENGINE OIL FILLING CONNECTOR APU OIL FILLING
GRAVITY REFUEL
HYDRAULIC SYSTEM GROUND SERVICESGROUNDING POINT MLGREFUEL/DEFUEL CONNECTORSREFUEL/DEFUEL PANELGROUND AIR START CONNECTOR (HP)1 −
2 −3 −4 −5 −
8 −9 −
10 −11 −12 −
6 −7 −
13 −14 −
5 12
2
4
98
N_AC_050401_1_0010101_01_01
Ground Service ConnectionsGround Service Connections Layout
FIGURE-5-4-1-991-001-A01
5-4-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2 Grounding Points
**ON A/C A318-100
Grounding Points
1. Grounding Points.
DISTANCE: Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUNDOn Nose Landing Gearleg:
5.07 m(16.63 ft) on centerline
0.94 m(3.08 ft)
On left Main LandingGear leg:
15.32 m(50.26 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
On right Main LandingGear leg:
15.32 m(50.26 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).
B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for:- refuel/defuel operations,- maintenance operations,- bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.
5-4-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
(2)(1)
GROUND CABLE(OPTIONAL)
LANDINGGEAR
NOSE LANDING GEAR
MAIN LANDING GEAR
(1)
A
A
A
(1)
N_AC_050402_1_0010101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-001-A01
5-4-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE: R SIDE SYMMETRICAL
RIB20
RIB19
FWD
A
FOR SPECIFICATIONS REFERTO FLIGHT MANUAL
B
B
A
N_AC_050402_1_0020101_01_00
A
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-002-A01
5-4-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3 Hydraulic System
**ON A/C A318-100
Hydraulic System
1. Access.
FROM AIRPLANE CENTERLINE
ACCESSAFT OF NOSE
m (ft)RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green System:Access door 197CB
16.43(53.9)
1.27(4.17)
1.76(5.77)
Yellow System:Access door 198CB
16.43(53.9)
1.27(4.17)
1.76(5.77)
Blue System:Access door 197EB
16.96(55.64)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.
2. Reservoir Pressurization.On the air pressurization manifold:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Access door 195BB13.2(43.31)
0.25(0.82)
1.74(5.71)
NOTE : Distances are approximate.- One 1/4 in. AEROQUIP AE 96994E self-sealing connection common to the 3 reservoirs.
3. Accumulator Charging.Four (MS28889-1) connections (one for each accumulator) for:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Yellow Systemaccumulator:Access door 196BB
13.8(45.28)
0.25(0.82)
1.99(6.53)
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green Systemaccumulator:Left MLG door
14.3(46.92)
0.25(0.82)
3.2(10.5)
Blue Systemaccumulator:Access door 195BB
15.8(51.84)
0.25(0.82)
1.99(6.53)
Yellow System brakingaccumulator:Access door 196BB
13.8(45.28)
0.76(2.49)
1.74(5.71)
NOTE : Distances are approximate.
4. Reservoir Filling.On the Green system ground service panel:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Access door 197CB16.43(53.9)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.One 1/4 in. AEROQUIP AE96993E self-sealing connection for pressurized supply.One handpump filling connection for unpressurized (suction) supply.
5. Reservoir Drain.On 3/8 in. self-sealing connection on reservoir for:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Yellow System:Access door 196 BB -198 CB
13.8(45.27)
1.43(4.69)
1.9(6.23)
Green System:Left MLG door
14.3(46.92)
1.27(4.17)
2.61(8.56)
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Blue System:Access door 197 EB
16.96(55.64)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.
6. Ground Test.On each ground service panel:- One self-sealing connector AE80532N (suction).- One self-sealing connector AE80531K (delivery).
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RESERVOIR FILL SYSTEMHAND PUMP FILL CONNECTION
GROUND TESTPRESSURE
CONNECTION
GROUND TESTSUCTION
CONNECTIONRESERVOIR FILLCONNECTION
AE96993GM
GROUND SUPPLY
AE80531K AE80532N
1698GM
1008GM 1007GM 1006GM
197CB
A
AN_AC_050403_1_0040101_01_00
Hydraulic SystemGreen System Ground Service Panel
FIGURE-5-4-3-991-004-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
GROUND CONNECTIONSUCTION
GROUNDCONNECTION
DELIVERY
AE80531K
AE80532N
2006GM
2008GM
A
Z197
A
N_AC_050403_1_0050101_01_00
Hydraulic SystemBlue System Ground Service Panel
FIGURE-5-4-3-991-005-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
GROUND TESTPRESSURE CONNECTION
GROUND TESTSUCTION CONNECTION
AE80531K AE80532N
A
A
3008GM 3006GM
198CB
N_AC_050403_1_0060101_01_00
Hydraulic SystemYellow System Ground Service Panel
FIGURE-5-4-3-991-006-A01
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Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4 Electrical System
**ON A/C A318-100
Electrical System
1. Electrical System.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
A/C External Power:Access door 121AL
2.55(8.37) on centerline
2.00(6.56)
NOTE : Distances are approximate.
2. Technical SpecificationsThis chapter gives data related to the location of the ground service connections.
A. External Power Receptacle:- One Style3 ISO 461 receptacle - 90 KVA.
B. Power Supply:- Three-phase, 400 Hz, 115/200V
C. Electrical Connectors for Servicing:- AC outlets: HUBBELL 5258- DC outlets: HUBBELL 7472
D. Electrical Loads in Ground ConfigurationIn ground configuration, in addition to the power necessary for maintenance, all the circuits,except those which are connected to the engines, are supplied as in flight.In these conditions, the maximum power on ground is approximately 75 KVA; this value doesnot take into account the supply of the galleys, which according to the aircraft interior layout,may reach 30 KVA.
E. Electrical Power necessary for Maintenance at Line Stop and Workshops- Hydraulic electric-pumps: 34 KVA- Air Conditioning/Ventilation: 20.8 KVA- Fuel pumps: 12 KVA- Lighting commercial: 6.7 KVA- Lighting technical: 3 KVA- Ice and rain protection: 3 KVA- Cargo loading: 3 KVA- AFS, Flight controls, ADS, Recorders: 3.3 KVA- Communications: 1.3 KVA
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Radio navigation: 1.2 KVA.
5-4-4Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
108VU
A
N_AC_050404_1_0010101_01_01
A
121AL
Ground Service ConnectionsExternal Power ReceptaclesFIGURE-5-4-4-991-001-A01
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Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5 Oxygen System
**ON A/C A318-100
Oxygen System
1. Replenishment of high pressure oxygen source.
A. For the A318 aircraft (basic version), the oxygen source is replenished by replacing the oxygencylinder installed in the avionics compartment.
5-4-5Page 1
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6 Fuel System
**ON A/C A318-100
Fuel System
1. Refuel/Defuel Control Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Refuel/DefuelIntegrated Panel:Access door 192MB
14.01(45.96)
1.8(5.91)
1.8(5.91)
2. Refuel/Defuel Connectors.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Refuel/Defuel coupling,LeftAccess Door 522HB(Optional)
15.2(49.87)
9.83(32.25)
3.65(11.98)
Refuel/Defuel coupling,RightAccess Door 622HB
15.2(49.87)
9.83(32.25)
3.65(11.98)
Gravity Refuel Coupling16.71(54.82)
12.4(40.68)
12.4(40.68)
3.7(12.14)
A. Refuel/Defuel couplings:- Right wing: one standard ISO 45, 2.5 in.- Left wing: one optional standard ISO 45, 2.5 in.
B. Refuel pressure:- Maximum pressure: 3.45 bar (50 psi).
C. Refuel Flow:- 1400 l/minute (369.84 US gal/minute).
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3. Overpressure Protector and NACA Flame Arrestor.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Overpressure Protector 17.96(58.92)
14.9(48.88)
14.9(48.88)
4.32(14.17)
NACA Flame Arrestor 17.4(57.09)
13.7(44.95)
13.7(44.95)
4.02(13.19)
NOTE : Distances are approximate.
5-4-6Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
REFUEL/DEFUELCONTROL PANEL
NOTE: STANDARD CONFIGURATION OF REFUEL/DEFUEL PANEL.
A
FUELkg x 1000
QTY
RIGHTCTRLEFT
LEFT CTR RIGHT
LVLHI
OPEN
NORM
SHUT
OPEN
NORM
SHUT
REFUEL VALVESOPEN
NORM
SHUT
BATT POWERTESTHI LVL ON
OPEN LTS NORM
MODE SELECTREFUEL
OFF
DEFUEL / XFR
kg x 1000
PRESELECTED
DEC INC
ACTUALREFUEL
CKPT END
A
N_AC_050406_1_0010101_01_00
Ground Service ConnectionsRefuel/Defuel Panel
FIGURE-5-4-6-991-001-A01
5-4-6Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RIB15
RIB14
A
41QM
40QM
LEADINGEDGE
WING FRONTSPAR
A
N_AC_050406_1_0020101_01_00
Ground Service ConnectionsRefuel/Defuel Couplings
FIGURE-5-4-6-991-002-A01
5-4-6Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
RIB19
RIB20
A
ADAPTER(REF ONLY)
GROUND CONNECTION(REF ONLY)
44QM
(45QM)
AFWD
N_AC_050406_1_0030101_01_00
Ground Service ConnectionsGravity Refuel Couplings
FIGURE-5-4-6-991-003-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
A ALH SHOWN
RH SYMMETRICAL
FWD
NACA VENT INTAKE
NACA FLAME ARRESTOR
OVERPRESSURE PROTECTOR
N_AC_050406_1_0040101_01_00
B
C
RIB25RIB24
RIB23
RIB22
550CB (650CB)
550AB (650AB)
C
B
Ground Service ConnectionsOverpressure Protector and NACA Flame Arrestor
FIGURE-5-4-6-991-004-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7 Pneumatic System
**ON A/C A318-100
Pneumatic System
1. High Pressure Air Connectors.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
HP ConnectorAccess door 191DB
10.43(34.22)
0.84(2.76)
1.76(5.77)
NOTE : Distances are approximate.
A. Connector:- One standard MS33740, 3 in.
2. Low Pressure Air Connectors.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
LP ConnectorAccess door 191CB
9.9(32.48)
1.11(3.64)
1.73(5.68)
NOTE : Distances are approximate
A. Connector:- One standard SAE AS4262 type B, 8 in.
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8 Potable Water System
**ON A/C A318-100
Potable Water System
1. Potable Water Ground Service Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Potable WaterGround ServicePanel:Access door 171AL:
25.2(82.67)
0.3(0.98)
2.6(8.53)
NOTE : Distances are approximate
2. Potable Water Ground Drain Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Potable WaterGround ServicePanel:Access door 133AL:
11.4(37.4)
0.15(0.49)
1.75(5.74)
NOTE : Distances are approximate
3. Technical Specifications
A. Connectors:
(1) On the potable ground service panel (Access Door 171AL)- Fill/Drain Nipple 3/4 in (ISO 17775).- One ground pressurization connector.
(2) On drain panel (Access Door 133AL)- Drain Nipple 3/4 in (ISO 17775)
B. Usable capacity:- Standard configuration - one tank:200 l (52.83 US gal)
C. Filling pressure:- 3.45 bar (50 psi).
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
D. Typical flow rate:- 50 l/min (13.21 US gal/min).
5-4-8Page 2
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
DRAIN CONNECTION
FILL ANDDRAIN PORT
GROUND CONNECTION
PRESSURIZATION
Z133
Z171
A
B
B
A
N_AC_050408_1_0010101_01_00
Ground Service ConnectionsPotable Water Ground Service Panel
FIGURE-5-4-8-991-001-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9 Oil System
**ON A/C A318-100
Oil System
1. Engine Oil Replenishment for CFM56 Series Engine (See FIGURE 5---9-99--001-A):One gravity filling cap and one pressure filling connection per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Engine Oil GravityFilling Cap:Access door: 437BL(LH),447BL (RH)
12.3(40.35)
6.63(21.75)
4.82(15.81)
1.46(4.79)
Engine Oil PressureFilling Port:
12.2(40.03)
6.49(21.29)
4.74(15.55)
1.42(4.66)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 19.6 l (5.18 US gal)- Usable: 9.46 l (2.50 US gal)
B. Maximum delivery pressure required: 25 psi (1.72 bar)Maximum delivery flow required: 180 l/h (47.55 US gal/h)
2. IDG Oil Replenishment for CFM56 Series Engine (See FIGURE 5---9-99--002-A):One pressure filling connection per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
IDG Oil PressureFilling Connection:Access door: 438DR(LH),448DR (RH)
11.4(37.4)
6.9(22.64)
5.52(18.11)
0.68(2.23)
NOTE : Distances are approximate
A. IDG oil tank capacity: 5 l (1.32 US gal)
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
B. Maximum servicing pressure: 5 to 40 psi (0.34 to 2.76 bar) at the IDG inlet.
3. Starter Oil Replenishment for CFM56 Series Engine (See FIGURE 5---9-99--003-A):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Starter Oil FillingConnection:
10.4(34.12)
5.3(17.39)
6.2(20.34)
0.76(2.49)
NOTE : Distances are approximate
A. Tank capacity: 0.8 l (0.206 US gal)
4. Engine Oil Replenishment for PW 6000 Series Engine (See FIGURE 5---9-99--004-A):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Engine Oil GravityFilling Cap:Access door: 438BR(LH),448BR (RH)
10.16(33.33)
4.8(15.75)
6.63(21.75)
1.8(5.9)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 18.36 l (4.85 US gal)- Usable: 23.50 l (6.21 US gal)- Engine oil tank capacity: 18.36 l (4.85 US gal)
1. IDG Oil Replenishment for PW 6000 Series Engine:One pressure filling connection per engine.
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
IDG Oil PressureFilling Connection:Access door 438DR(LH),448DR (RH)
10(32.81)
5.33(17.49)
6.17(20.24)
1.02(3.35)
NOTE : Distances are approximate
A. Tank capacity: 6.28 l (1.66 US gal)
B. Maximum servicing pressure: 35 psi (2.41 bar)
5. Starter Oil Replenishment for PW 6000 Series Engine (See FIGURE 5---9-99--006-A):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Starter Oil FillingConnection:
10.16(33.33)
5.84(19.16)
5.59(18.34)
1.02(3.35)
NOTE : Distances are approximate
A. Tank capacity: 0.35 l (0.09 US gal)
6. APU Oil System (See FIGURE 5---9-99--007-A):APU oil gravity filling cap.
AFT OF NOSEm (ft)
FROM AIRPLANECENTERLINE(LEFT HAND)
m (ft)
MEAN HEIGHT FROMGROUND
m (ft)
GTCP 36-30029.37(96.36)
0.3(0.98)
4.83(15.85)
APS 320029.37(96.36)
0.3(0.98)
4.78(15.68)
131-929.27(96.03)
0.35(1.15)
4.32(14.17)
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
NOTE : Distances are approximate
A. Tank capacity (usable):- APU type GTCP 36-300: 6.20 l (1.64 US gal)- APU type APS 3200: 5.40 l (1.43 US gal)- APU type 131-9: 6.25 l (1.65 US gal)
5-4-9Page 4
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ACCESS PANEL: 437BL (LEFT)447BL (RIGHT) OIL IN
VENT
OIL LEVELTRANSMITTER(OPTIONAL)
OIL CAP
SIGHT WINDOW
ANTI−SIPHONDEVICE
AIR PRESSURESWITCH NIPPLE
SELF−SEALING MAGNETICDRAIN PLUG
PRESSURE NIPPLE
OIL OUT
OIL/FUEL HEATEXCHANGER
SERVO FUELHEATER
A
A
B
FWD
B
N_AC_050409_1_0010101_01_00
Ground Service ConnectionsEngine Oil Tank -- CFM56 Series Engine
FIGURE-5-4-9-991-001-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
C
A
B
SIGHT GLASS
NOTE: ATHE YELLOW BAND, OIL SERVICINGIS REQUIRED.
BTHE GREEN AND YELLOW BANDS,OIL SERVICING IS NOT REQUIRED.
CTHE GREEN BAND, OIL SERVICINGIS REQUIRED.
1 − PRESSURE FILL VALVE2 − CASE DRAIN PLUG3 − DUST CAP4 − DUST CAP5 − OVERFLOW DRAIN VALVE6 − OIL LEVEL INDICATOR
(SIGHT GLASS)
1
2
34
5
6
A B
A
B
OVERFULL
ADDOIL
ADDOIL
CFM−56
IF THE OIL LEVEL IS ABOVE
IF THE OIL LEVEL IS WITHIN
IF THE OIL LEVEL IS BELOW
N_AC_050409_1_0020101_01_01
Ground Service ConnectionsIDG Oil Tank -- CFM56 Series Engine
FIGURE-5-4-9-991-002-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
DRAIN PORTAND MAGNETICPLUG
OVERFLOWPLUG
STARTER
OIL FILLERPLUG
A
A
N_AC_050409_1_0030101_01_02
Ground Service ConnectionsStarter Oil Tank -- CFM56 Series Engine
FIGURE-5-4-9-991-003-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
B
N−02463(0601)PW V
OIL
FULL FULL
LTRLOW
1
LOW
1
QTS
LEVEL
OIL TANK
CAP
A
SIGHT GLASS
B
N_AC_050409_1_0040101_01_02
Ground Service ConnectionsEngine Oil Tank -- PW 6000 Series Engine
FIGURE-5-4-9-991-004-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
IDG
N−01198 (0601)PW V
B
A
A
B
OVER FULL
ADDOIL
ADDOIL
IDG OVERFILLDRAIN VALVE
IDG OIL LEVELSIGHT GLASS
IDG PRESSUREFILL VALVE
N_AC_050409_1_0050101_01_01
Ground Service ConnectionsIDG Oil Tank -- PW 6000 Series Engine
FIGURE-5-4-9-991-005-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A
STARTER
MAGNETICCHIP COLLECTOR
FILLPLUG
OVERFLOWPLUG
N−01199 (1100)PW VA
N_AC_050409_1_0060101_01_00
Ground Service ConnectionsStarter Oil Tank -- PW 6000 Series Engine
FIGURE-5-4-9-991-006-A01
5-4-9Page 10
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FR80
Z316Z315
FR84
GRAVITYOIL FILLER
PRESSUREFILL PORT
OVERFLOWDRAIN VALVE
A
A
OIL LEVELSIGHT GLASS
N_AC_050409_1_0070101_01_00
Ground Service ConnectionsAPU Oil Tank
FIGURE-5-4-9-991-007-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10 Vacuum Toilet System
**ON A/C A318-100
Vacuum Toilet System
1. Vacuum Toilet System.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) R SIDEm (ft)
L SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Waste WaterGround ServicePanel:Access door 172AR
25.2(82.67)
0.8(2.62)
2.8(9.18)
NOTE : Distances are approximate
2. Technical Specifications
A. Connectors:- Draining: 4 in (ISO 17775).- Flushing and filling: 1 in (ISO 17775).
B. Usable waste tank capacity:- Standard configuration - on tank: 177 l (30.91 US gal).
C. Waste tank - Rinsing:- Operating pressure: 3.45 bar (50 psi).
D. Waste tank - Precharge:- 10 l (2.64 US gal).
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FILL AND RINSECONNECTION
TOILET DRAINCONNECTION
FR66 FR65
A
Z172
A
N_AC_050410_1_0010101_01_00
Ground Service ConnectionsWaste Water Ground Service Panel
FIGURE-5-4-10-991-001-A01
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A318-100
Engine Starting Pneumatic Requirements
1. Engine Starting Pneumatic Requirements.To determinate the airflow required at ground connection, refer to the example given in FIGURE 5---0-99--001-A.
For engine starting pneumatic requirements for:- Low ambient temperatures, refer to 5-5-1,- Medium ambient temperatures, refer to 5-5-2,- High ambient temperatures, refer to 5-5-3.
5-5-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
EXAMPLE TO DETERMINATE THE AIRFLOW REQUIRED AT THE FUSELAGE CONNECTION:−FOR AN AIR START UNIT DELIVERING 60 PSIA (4.14 BARS) AIR PRESSURE AT THE
FUSELAGE CONNECTOR
1. DRAW AN HORIZONTAL LINE FROM THE SUPPLIED AIR PRESSURE (60 PSIA (4.14 BARS)).2. FROM THE INTERSECTION WITH THE AIR SUPPLY TEMPERATURE AT FUSELAGE
CONNECTION (220°C (428°F)), DRAW A VERTICAL LINE.3. THE INTERSECTION WITH THE HORIZONTAL AXIS GIVES THE REQUIRED AIRFLOW AT GROUND
CONNECTION (78 kg/min (1.3 kg/s)).
−AT A SUPPLIED AIR TEMPERATURE OF 220°C (428°F) AT THE FUSELAGE CONNECTOR
N_AC_050500_1_0010101_01_00
220°C200°C
150°C
100°C
50°C
0°C
230
3
4
40
50
60
5
6
70
80
90
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
MIN. PRESSUREAT GROUND CONNECTION: 33 PSIG
RECOMMENDED PRESSURE:38 PSIG AT GROUNDCONNECTION
SEA LEVEL
Z = 8000 ft
40s
50s70s
35s
Z = 8000 ft
SEA LEVEL
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
ESTIMATED STARTINGTIMES UP TO IDLE
0.80 1.00 2.001.801.601.401.20 kg/s
48 60 8472 kg/min12010896
SEA LEVEL
MAXIM
UM T
EMPERATURE L
IMIT
AIR FLOW REQUIRED AT GROUND CONNECTION
Engine Starting Pneumatic RequirementsEngine Starting Pneumatic Requirements
FIGURE-5-5-0-991-001-A01
5-5-0Page 2
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-1 Low Ambient Temperatures
**ON A/C A318-100
Low Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature of -40˚C(-40˚F).
5-5-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
220°C
200°C
150°C
100°C
50°C
0°C
kg/mn1201089684726048
230
3
4
40
50
60
5
6
70
80
90
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
MIN. PRESSUREAT GROUND CONNECTION: 33 PSIG
RECOMMENDED PRESSURE:38 PSIG AT GROUNDCONNECTION
AIR FLOW REQUIRED AT GROUND CONNECTION
SEA LEVEL
Z = 8000 ft
40s
50s
70s
35S
SEA LEVEL
Z = 8000 ft
SEA LEVEL
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
MAXIM
UM T
EMPERATURE L
IMIT
ESTIMATED STARTINGTIMES UP TO IDLE
N_AC_050501_1_0010101_01_01
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- CFM56 series engine
FIGURE-5-5-1-991-001-A01
5-5-1Page 2
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
40 50 60 70 80 90 100 110 120 kg/min
1
2
3
4
5
6
7
100.0
PSIA
87.0
72.5
58.0
43.5
29.0
14.5
ABSOLUTE BARS −40°F (−40°C)
220°C200°C
150°C
100°C
50°C
0°CMAXIMUM TEMPERATURE LIM
IT
101.5
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
AIR SUPPLY PRESSUREAT GROUND CONNECTION
N−03649 (0402)PW V
MAXIMUM DESIGN DUCT PRESSURE
80s
70s
60s
50sESTIMATED STARTINGTIMES UP TO IDLE
AIR FLOW REQUIRED AT GROUND CONNECTION
N_AC_050501_1_0020101_01_00
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- PW 6000 series engine
FIGURE-5-5-1-991-002-A01
5-5-1Page 3
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-2 Medium Ambient Temperatures
**ON A/C A318-100
Medium Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature of +15˚C(+59˚F).
5-5-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
220°C
200°C
150°C
100°C
50°C
35S
0°C
kg/mn1201089684726048
230
3
4
40
50
60
5
6
70
80
90
PSIA ABSOLUTE BARS
MAXIM
UM T
EMPERATURE L
IMIT
MAXIMUM DUCT PRESSURE: 60 PSIG
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
AIR SUPPLY PRESSUREAT GROUND CONNECTION
RECOMMENDED PRESSURE:33 PSIG AT GROUNDCONNECTION
MIN. PRESSUREAT GROUND CONNECTION: 22 PSIG
SEA LEVEL
Z = 8000 ft
TIMES UP TO IDLEESTIMATED STARTING
40s
AIR FLOW REQUIRED AT GROUND CONNECTION
SEA LEVEL
Z = 8000 ft
SEA LEVEL
Z = 8000 ft
50s
60s
70s
N_AC_050502_1_0010101_01_01
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- CFM56 series engine
FIGURE-5-5-2-991-001-A01
5-5-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
40 50 60 70 80 90 100 110 120 kg/min
1
2
3
4
5
6
7
100.0
PSIA
87.0
72.5
58.0
43.5
29.0
14.5
ABSOLUTE BARS 59°F (15°C)
220°C200°C
150°C
100°C
50°C
0°CMAXIMUM TEMPERATURE LIM
IT
101.5
AIR SUPPLY PRESSUREAT GROUND CONNECTION AIR SUPPLY TEMPERATURE
AT FUSELAGE CONNECTION
N−02538 (0402)PW V
50s
60s
70s
80s
MAXIMUM DESIGN DUCT PRESSURE
ESTIMATED STARTINGTIMES UP TO IDLE
AIR FLOW REQUIRED AT GROUND CONNECTION
N_AC_050502_1_0020101_01_00
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- PW 6000 series engine
FIGURE-5-5-2-991-002-A01
5-5-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-3 High Ambient Temperatures
**ON A/C A318-100
High Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature upper:- +38˚C (+100˚F) -- PW 6000- +50˚C (+122˚F) -- CFM56
5-5-3Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
220°C
200°C
150°C
100°C
50°C
kg/mn1201089684726048
230
3
4
40
50
60
5
6
70
80
90
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
MINI. PRESSUREAT GROUND CONNECTION: 22 PSIG
RECOMMENDED PRESSURE:33 PSIG AT GROUNDCONNECTION
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
MAXIM
UM T
EMPERATURE L
IMIT
TIMES UP TO IDLEESTIMATED STARTING
40s
50s
60s
70s
Z = 8000 ft
SEA LEVEL
SEA LEVEL
Z = 8000 ft
Z = 8000 ft
SEA LEVEL
AIR FLOW REQUIRED AT GROUND CONNECTION
35s
MAXIMUM DUCT PRESSURE: 60 PSIG
N_AC_050503_1_0010101_01_00
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +50˚C (+122˚F) -- CFM56 series engine
FIGURE-5-5-3-991-001-A01
5-5-3Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
40 50 60 70 80 90 100 110 120 kg/min
1
2
3
4
5
6
7
100.0
PSIA
87.0
72.5
58.0
43.5
29.0
14.5
ABSOLUTE BARS 100°F (38°C)
220°C200°C
150°C
100°C
50°C
0°C
101.5
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
AIR SUPPLY PRESSUREAT GROUND CONNECTION
N−03650 (0402)PW V
MAXIMUM DESIGN DUCT PRESSURE
AIR FLOW REQUIRED AT GROUND CONNECTION
60s
50s
70s
80s
TIMES UP TO IDLEESTIMATED STARTING
MAXIMUM TEMPERATURE LIM
IT
N_AC_050503_1_0020101_01_00
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +38˚C (+100˚F) -- PW 6000 series engine
FIGURE-5-5-3-991-002-A01
5-5-3Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A318-100
Ground Pneumatic Power Requirements
1. Ground Pneumatic Power Requirements
NOTE : The air flow rates and temperature requirements given in sections 5.6 and 5.7 are given ataircraft connection.
5-6-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-1 Heating
**ON A/C A318-100
Heating
1. This section provides the ground pneumatic power requirements heating.
5-6-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
3040
50T
IME
(m
in)
0.5
0.42
9
0.51
5
0.60
0.68
6
0.72
2
1.0
0.85
8
1.2
1.03
0.94
4
1.11
5
1.20
1
1.5
1.28
7
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
TOTAL AIRFLOW
(lb/s
)
2.59
2.15
1.72
1.28
1.5
2.0
2.5
3.0
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
TIM
E T
O H
EA
T C
AB
IN T
O 2
1°C
(69
.8°
F O
N G
RO
UN
D)
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T −
23°
C (
−9.
4°F
)T
EM
PE
RA
TU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N: 7
0°C
(15
8°F
)E
MP
TY
CA
BIN
ELE
CT
RIC
AL
LOA
D =
270
0 W
RE
CIR
CU
LAT
ION
: ON
NO
T O
TH
ER
HE
AT
LO
AD
CABIN AIRFLOW
N_AC_050601_1_0010101_01_01
Ground Pneumatic Power RequirementsHeating
FIGURE-5-6-1-991-001-A01
5-6-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-2 Cooling
**ON A/C A318-100
Cooling
1. This section provides the ground pneumatic power requirements cooling.
5-6-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
40T
IME
(m
in)
0.5
0.42
9
0.51
5
0.60
0.68
6
0.72
2
1.0
0.85
8
1.2
1.03
0.94
4
1.11
5
1.20
1
1.5
1.28
7
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
TOTAL AIRFLOW
(lb/s
)
2.59
2.15
1.72
1.28
1.5
2.0
2.5
3.0
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
TIM
E T
O C
OO
L C
AB
IN T
O 2
7°C
(80
.6°
F O
N G
RO
UN
D)
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T −
38°
C (
−10
0.4°
F)
TE
MP
ER
AT
UR
E A
T G
RO
UN
D C
ON
NE
CT
ION
: 1.5
°C
(34
.7°
F)
EM
PT
Y C
AB
INE
LEC
TR
ICA
L LO
AD
= 2
000
WS
UN
= 4
990
WR
EC
IRC
ULA
TIO
N: O
N
CABIN AIRFLOW
N_AC_050602_1_0010101_01_01
Ground Pneumatic Power RequirementsCooling
FIGURE-5-6-2-991-001-A01
5-6-2Page 2
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A318-100
Preconditioned Airflow Requirements
1. This section gives the preconditioned airflow requirements for cabin air conditioning.
5-7-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2.59
2.1
5
1.7
2
1.2
8
3.0
2.5
2.0
1.5
1.2
87
1.1
15
1.2
01
1.0
3
0.94
4
0.85
8
0.72
2
0.68
6
0.60
0.5
15
0.42
9
1.5
0.5
1.0
1.2
TOTAL AIRFLOW
CABIN AIRFLOW
CABIN AIRFLOW
TOTAL AIRFLOW(kg/s
)
30−3
0−4
0−2
0−1
01
020
40 0
−40
0
−10
50
10
10
0
INLE
T F
LOW
TE
MP
ER
AT
UR
E
NO
TE
:
(°C
)
(°F
)
(lb
/s)
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
OA
T =
−40°
C (−
40°F
)
OA
T =
−23
°C (
−9.4
°F)
OA
T =
−30°
C (−
22°F
)
CU
RV
E 2
, 3, 4
CA
BIN
AT
21°
C (
69.8
°F
)
RE
CIR
CU
LAT
ION
: ON
NO
OT
HE
R H
EA
T L
OA
D
ELE
CT
RIC
AL
LOA
D =
380
0 W
NO
PA
SS
EN
GE
R O
R C
AB
IN
LP
GR
OU
ND
CO
NN
EC
TIO
N M
AX
IMU
M P
RE
SS
UR
E 4
0 M
B
CU
RV
E 1
: C
AB
IN A
T 2
7°C
(80
.6°
F)
134
PA
SS
EN
GE
R, 4
CA
BIN
AT
TE
ND
AN
TS
, 3 C
RE
W M
EM
BE
RS
BR
IGH
T D
AY
SO
LAR
LO
AD
: 297
5 W
ELE
CT
RIC
AL
LOA
D =
620
0 W
RE
CIR
CU
LAT
ION
: ON
OA
T (
OU
TS
IDE
AM
BIE
NT
TE
MP
ER
AT
UR
E)
= 3
8°C
(10
0.4°
F)
AT
TE
ND
AN
TS
N_AC_050700_1_0010101_01_01
Preconditioned Airflow RequirementsFIGURE-5-7-0-991-001-A01
5-7-0Page 2
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A318-100
Ground Towing Requirements
1. GeneralThis section provides information on aircraft towing.This aircraft is designed with means for conventional or towbarless towing.Information/procedures can be found for both in chapter 9 of the Aircraft Maintenance Manual.Status on towbarless towing equipment qualification can be found in SIL 09-002.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a tow bar attached to the nose gear leg (refer to AMM chap 9 for conditions andlimitations).One tow bar fitting is installed at the front of the leg.The main landing gears have attachment points for towing or debogging (for details, refer to chapter07 of the Aircraft Recovery Manual).
A. The first part of this section shows the chart to determine the draw bar pull and tow tractormass requirements as function of the following physical characteristics:- Aircraft weight.- Number of engines at idle.- Slope.The chart is based on the engine type with the highest idle thrust level.
B. The second part of this section supplies guidelines for the tow bar.
NOTE : Information on aircraft towing procedures and corresponding aircraft limitations aregiven in chapter 9 on the Aircraft Maintenance Manual.
The aircraft tow bar shall respect the following norms:- SAE AS1614 C, ”Main Line Aircraft Tow Bar Attach Fitting Interface”.- SAE ARP1915 D, ”Aircraft Tow Bar”.- ISO 8267-1, ”Aircraft - Tow bar attachment fitting - Interface requirements - Part 1: Main
line aircraft”.- ISO 9667, ”Aircraft ground support equipment - Tow bars”.- IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Tow
bar”.A conventional type tow bar is required which should be equipped with a damping system toprotect the nose gear against jerks and with towing shear pins:- A traction shear pin calibrated at 9425 daN (21188 lbf).- A torsion pin calibrated at 826 m.daN (7311 lbf.in).The towing head is designed according to SAE AS1614 C (Aircraft Weight Category I).
5-8-0Page 1
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@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10
0 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0
35404550556065
TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]
DRAWBAR PULL [ t ] A/C WEIGHT [ t ]
0
1.5% SLOPE60 tons
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A318 AT 60 t, AT 1.5% SLOPE,1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (60 t)− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%)− FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL NO OF ENGINES AT IDLE = 2− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER OF ENGINES (1)− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5.1 t)− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS
THE RECOMMENDED MINIMUM TRACTOR WEIGHT (9 t)
ICE m = 0.05
1 ENGINE ON5
5.1
WE
T C
ON
CR
ET
E m
= 0
.57
HA
RD
SN
OW
m =
0.2
AT IDLE
DR
Y C
ON
CR
ET
E m
= 0
.8
BREAKAWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 616 daN
9.0
N_AC_050800_1_0010101_01_04
Ground Towing RequirementsFIGURE-5-8-0-991-001-A01
5-8-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0 De-Icing and External Cleaning
**ON A/C A318-100
De-Icing and External Cleaning
1. De-Icing and External Cleaning on GroundThe mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heightsup to approximately 13 m (42.65 ft).
2. De-Icing
Wing Top Surface(Both Sides)
Wingtip Devices(Both Inside andOutside Surfaces)
(Both Sides)
HTP Top Surface(Both Sides)
VTP(Both Sides)AIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A318 99.7 1073.16 1.8 19.38 27 290.63 46.2 497.29A318 Sharklet 99.7 1073.16 9.6 103.33 27 290.63 46.2 497.29
Fuselage Top Surface(Top Third - 120˚ Arc)
Nacelle and Pylon(Top Third - 120˚ Arc)
(All Engines)Total De-Iced Area
AIRCRAFT TYPE
m2 ft2 m2 ft2 m2 ft2
A318 111.9 1204.48 23.6 254.03 310 3337A318 Sharklet 111.9 1204.48 23.6 254.03 318 3423
NOTE : Dimensions are approximate
3. External Cleaning
Wing TopSurface
(Both Sides)
Wing LowerSurface
(Including FlapTrack Fairing)(Both Sides)
Wingtip Devices(Both Inside and
OutsideSurfaces)
(Both Sides)
HTP TopSurface
(Both Sides)
HTP LowerSurface
(Both Sides)AIRCRAFT
TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2 m2 ft2
A318 99.7 1073.16 103.4 1112.99 1.8 19.38 27 290.63 27 290.63A318 Sharklet 99.7 1073.16 103.4 1112.99 9.6 103.33 27 290.63 27 290.63
VTP(Both Sides)
Fuselage andBelly Fairing
Nacelle and Pylon(All Engines) Total Cleaned Area
AIRCRAFT TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A318 46.2 497.29 343.2 3694.17 73.2 787.92 723 7782
5-9-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
VTP(Both Sides)
Fuselage andBelly Fairing
Nacelle and Pylon(All Engines) Total Cleaned Area
AIRCRAFT TYPE
m2 ft2 m2 ft2 m2 ft2 m2 ft2
A318 Sharklet 46.2 497.29 343.2 3694.17 73.2 787.92 731 7868
NOTE : Dimensions are approximate
5-9-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A318-100
Engine Exhaust Velocities and Temperatures
1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway, Maximum Takeoff conditions.
6-1-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A318-100
Engine Exhaust Velocities Contours - Ground Idle Power
1. This section gives engine exhaust velocities contours at ground idle power.
6-1-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ELE
VA
TIO
N
FE
ET
40 30 20 10 0036912
mft
PLA
NA
IRP
LAN
E
V (
M/S
)
GR
OU
ND
PLA
NE
ME
TE
RS
40 30 20 10 0036912
mft
4530
2520
1510
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
4530
2520
1510
N_AC_060101_1_0010101_01_00
Engine Exhaust VelocitiesGround Idle Power -- CFM56 series engine
FIGURE-6-1-1-991-001-A01
6-1-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AIR
PLA
NE
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
102
MP
H62
MP
H34
MP
H20
MP
H
PLA
NC
ON
VE
RS
ION
FA
CT
OR
1 M
PH
= 1
.6 k
m/h
102
MP
H62
MP
H34
MP
H20
MP
H
015
3046
61
250
300
050
100
150
200
7691
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
PW
A 6
000
− G
RO
UN
D ID
LEA
LL V
ELO
CIT
Y V
ALU
ES
AR
E IN
ST
AT
UE
MIL
ES
PE
R H
OU
R.
NO
TE
:
(18)60
(12)40 (6
)20 0
(18)60
(12)40 (6
)20 0
N_AC_060101_1_0020101_01_00
Engine Exhaust VelocitiesGround Idle Power -- PW 6000 series engine
FIGURE-6-1-1-991-002-A01
6-1-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A318-100
Engine Exhaust Temperatures Contours - Ground Idle Power
1. This section gives engine exhaust temperatures contours at ground idle power.
6-1-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ELE
VA
TIO
N
FE
ET 40 30 20 10 0
036912
mft
PLA
NA
IRP
LAN
E
GR
OU
ND
PLA
NE
ME
TE
RS
mft
400
350
325
300
40 30 20 10 0036912
3000
lbs
OF
TH
RU
ST
T (
°K
)
400
350
325
300
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
N_AC_060102_1_0010101_01_00
Engine Exhaust TemperaturesGround Idle Power -- CFM56 series engine
FIGURE-6-1-2-991-001-A01
6-1-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AIR
PLA
NE
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
N
PW
A 6
000
− G
RO
UN
D ID
LEA
LL T
EM
PE
RA
TU
RE
S A
RE
IN F
AH
RE
NH
EIT
(C
ELS
IUS
).N
OT
E:
160°
F(7
1°C
)10
0°F
(38°
C)
160°
F(7
1°C
)10
0°F
(38°
C)
015
3046
61
250
300
050
100
150
200
7691
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
(18)60
(12)40 (6)
20 0
(18)60
(12)40 (6)
20 0
N_AC_060102_1_0020101_01_00
Engine Exhaust TemperaturesGround Idle Power -- PW 6000 series engine
FIGURE-6-1-2-991-002-A01
6-1-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3 Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A318-100
Engine Exhaust Velocities Contours - Breakaway Power
1. This section gives engine exhaust velocities contours at breakaway power.
6-1-3Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
40 30 20 10 0036912
mft
PLA
NA
IRP
LAN
E
GR
OU
ND
PLA
NE
ME
TE
RS
40 30 20 10 0036912
mft
(38%
N1)
NO
TE
:−
add
+ 1
% N
1 pe
r +
15°
C (
27°
F)
AB
OV
E IS
A T
EM
PE
RA
TU
RE
CO
ND
ITIO
NS
− a
dd +
1%
N1
per
2000
ft
3000
lbs
OF
TH
RU
ST
V (
M/S
)
4020
15
4020
15
N_AC_060103_1_0010101_01_00
Engine Exhaust VelocitiesBreakaway Power -- CFM56 series engine
FIGURE-6-1-3-991-001-A01
6-1-3Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
PW
A 6
000
− B
RE
AK
AW
AY
PO
WE
RA
LL V
ELO
CIT
Y V
ALU
ES
AR
E IN
ST
AT
UE
MIL
ES
PE
R H
OU
R.
NO
TE
:
AIR
PLA
NE
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
102
MP
H62
MP
H34
MP
H20
MP
H
PLA
NC
ON
VE
RS
ION
FA
CT
OR
1 M
PH
= 1
.6 k
m/h
102
MP
H62
MP
H34
MP
H20
MP
H
015
3046
61
250
300
050
100
150
200
7691
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
(18)60
(12)40 (6
)20 0
(18)60
(12)40 (6
)20 0
N_AC_060103_1_0020101_01_00
Engine Exhaust VelocitiesBreakaway Power -- PW 6000 series engine
FIGURE-6-1-3-991-002-A01
6-1-3Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4 Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A318-100
Engine Exhaust Temperatures Contours - Breakaway Power
1. This section gives engine exhaust temperatures contours at breakaway power.
6-1-4Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
40 30 20 10 0036912
mft
PLA
NA
IRP
LAN
E
3000
lbs
OF
TH
RU
ST
GR
OU
ND
PLA
NE
ME
TE
RS
40 30 20 10 0036912
mft
T (
°K
)40
035
032
530
0
400
350
325
300
N_AC_060104_1_0010101_01_00
Engine Exhaust TemperaturesBreakaway Power -- CFM56 series engine
FIGURE-6-1-4-991-001-A01
6-1-4Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
PW
A 6
000
− B
RE
AK
AW
AY
PO
WE
RA
LL T
EM
PE
RA
TU
RE
S A
RE
IN F
AH
RE
NH
EIT
(C
ELS
IUS
).N
OT
E:
AIR
PLA
NE
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
PLA
N
160°
F(7
1°C
)10
0°F
(38°
C)
160°
F(7
1°C
)10
0°F
(38°
C)
015
3046
61
250
300
050
100
150
200
7691
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
(18)60
(12)40 (6
)20 0
(18)60
(12)40 (6
)20 0
N_AC_060104_1_0020101_01_00
Engine Exhaust TemperaturesBreakaway Power -- PW 6000 series engine
FIGURE-6-1-4-991-002-A01
6-1-4Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A318-100
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power.
6-1-5Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
450
420
390
360
330
300
270
240
210
180
150
120
9060
30
010
020
030
040
050
070
060
080
090
010
0011
0012
0013
0014
0015
00
ME
TE
RS
FE
ET
ftm
V =
40
m/s
V =
20
m/s
V =
12
m/s
V =
40
m/s
V =
20
m/s
V =
12
m/s
PLA
NA
IRP
LAN
E
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
TA
KE
OF
F P
OW
ER
INC
LUD
ES
(W
OR
ST
CA
SE
)G
RO
UN
D P
LAN
EH
EA
DW
IND
(20
KT
S.)
mft
42 36 30 24 18 12 6 0
140
120
100 80 60 40 200
42 36 30 24 18 12 6 0
140
120
100 80 60 40 200
N_AC_060105_1_0010101_01_00
Engine Exhaust VelocitiesTakeoff Power -- CFM56 series engine
FIGURE-6-1-5-991-001-A01
6-1-5Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
015
3046
61
250
300
AIR
PLA
NE
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
050
100
150
200
7691
0
CO
NV
ER
SIO
N F
AC
TO
R1
MP
H =
1.6
km
/h
PW
A 6
000
− T
AK
EO
FF
ALL
VE
LOC
ITY
VA
LUE
S A
RE
IN S
TA
TU
E M
ILE
S P
ER
HO
UR
.N
OT
E:
150
MP
H10
2 M
PH
62 M
PH
34 M
PH
TO
320
ft (9
8 m
)20
MP
H T
O40
0 ft
(122
m)
150
MP
H10
2 M
PH
62 M
PH
34 M
PH
TO
320
ft (9
8 m
)20
MP
H T
O40
0 ft
(122
m)
60(1
8) 40 (12) 20 (6
)FE
ET
(ME
TE
RS
)
060 (18) 40 (12) 20 (6
)FE
ET
(ME
TE
RS
)
FE
ET
(ME
TE
RS
)
PLA
N
N_AC_060105_1_0020101_01_00
Engine Exhaust VelocitiesTakeoff Power -- PW 6000 series engine
FIGURE-6-1-5-991-002-A01
6-1-5Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A318-100
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power.
6-1-6Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
60 40 20 0
18 12 6 0E
LEV
AT
ION
GR
OU
ND
PLA
NE
ftm
2040
6080
100
120
140
160
TA
KE
OF
F P
OW
ER
INC
LUD
ES
(W
OR
ST
CA
SE
):
HE
AD
WIN
D (
20 K
TS
)
GR
OU
ND
PLA
NE
FE
ET
ME
TE
RS
0
T =
425
° K
T =
370
° K
T =
315
° K
T =
425
° K
T =
370
° K
T =
315
° K
AIR
PLA
NE
1020
3040
50
ftm
PLA
N
60 40 20 0
18 12 6 0
N_AC_060106_1_0010101_01_00
Engine Exhaust TemperaturesTakeoff Power -- CFM56 series engine
FIGURE-6-1-6-991-001-A01
6-1-6Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
PLA
N
200°
F(9
3°C
)10
0°F
(38°
C)
320°
F(1
60°
C)
(18)60
(12)40 (6
)20 0
015
3046
61
250
300
AIR
PLA
NE
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
050
100
150
200
7691
PW
A 6
000
− T
AK
EO
FF
ALL
TE
MP
ER
AT
UR
ES
AR
E IN
FA
HR
EN
HE
IT (
CE
LSIU
S).
NO
TE
:
320°
F(1
60°
C)
200°
F(9
3°C
)10
0°F
(38°
C)
FE
ET
(ME
TE
RS
)
(18)60
(12)40 (6
)20 0F
EE
T(M
ET
ER
S)
FE
ET
(ME
TE
RS
)
N_AC_060106_1_0020101_01_00
Engine Exhaust TemperaturesTakeoff Power -- PW 6000 series engine
FIGURE-6-1-6-991-002-A01
6-1-6Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-0 Airport and Community Noise
**ON A/C A318-100
Airport and Community Noise
1. Airport and Community Noise Data
This section gives data concerning engine maintenance run-up noise to permit evaluation of possibleattenuation requirements.
6-2-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-1 Noise Data
**ON A/C A318-100
Noise Data
1. Noise Data for CFM56-5A series engine
A. Description of test conditions:
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 3˚C (37˚F)- Relative humidity: 66%- Atmospheric pressure: 1016 hPa- Wind speed: Negligible- No rain
2. Noise Data for CFM56-5B series engine
A. Description of test conditions:
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 22˚C (72˚F)- Relative humidity: 42%- Atmospheric pressure: 1003 hPa- Wind speed: Negligible- No rain
3. Noise Data for PW 6000 series engine
A. Description of test conditions:
6-2-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 28˚C (82˚F)- Relative humidity: 47%- Atmospheric pressure: 1004 hPa- Wind speed: Negligible- No rain
6-2-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_060201_1_0010101_01_00
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
20.8% 90%
8082
8486
8890
9294
9698
100102
104106
108110
112
0°10°
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
350°340°
330°
320°
310°
300°
290°
280°
270°
250°
240°
230°
220°
210°
NOISE REFERENCEPOINT
260°78
Airport and Community NoiseCFM56-5A series engine
FIGURE-6-2-1-991-001-A01
6-2-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
18.9% 87%
8082
8486
8890
9294
9698
100102
104106
108110
112
0°10°
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
350°340°
330°
320°
310°
300°
290°
280°
270°
250°
240°
230°
220°
210°
NOISE REFERENCEPOINT
260°
N_AC_060201_1_0020101_01_00
78
Airport and Community NoiseCFM56-5B series engine
FIGURE-6-2-1-991-002-A01
6-2-1Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
0°10°
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
140°
150°
350°340°
330°
320°
23.4% 92.7%
8082
8486
8890
9294
9698
100102
104106
108110
112
310°
300°
290°
280°
270°
250°
230°
220°
210°
NOISE REFERENCEPOINT
260°
240°
130°
N_AC_060201_1_0030101_01_00
78
Airport and Community NoisePW 6000 series engine
FIGURE-6-2-1-991-003-A01
6-2-1Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A318-100
Danger Areas of Engines
1. Danger Areas of the Engines.
6-3-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1 Ground Idle Power
**ON A/C A318-100
Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions.
6-3-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
30°TO 55 m (180 ft) INCLUDES CROSS WIND EFFECT
1.5 m(5 ft)
(7.2 ft)R = 2.2 m
INTAKE SUCTION DANGERAREA
ENTRY CORRIDOR
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
NO
EN
TR
Y 1
7 m
(55
ft) A
FT
OF
NO
ZZ
LE45°
(20 ft)
6.1 m
N_AC_060301_1_0010101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE-6-3-1-991-001-A01
6-3-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FEET(METERS)
60(18)
50(15)
40(12)
30(9)
20(6)
10(3) 0
10(3)
20(6)
30(9)
40(12)
50(15)
60(18)
INTAKE SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST DANGER AREA (AFT OF EXHAUST NOZZLE):200 ft (61 m) − GROUND IDLE (20 kt HEADWIND)
3.3 ft(1 m)
R = 9 ft(2.74 m)
R = 9 ft(2.74 m)
3.3 ft(1 m)
30° 30°
N_AC_060301_1_0020101_01_01
Danger Areas of EnginesPW 6000 series engine
FIGURE-6-3-1-991-002-A01
6-3-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2 Takeoff Power
**ON A/C A318-100
Takeoff Power
1. This section gives danger areas of the engines at max takeoff conditions.
6-3-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
40°
30°
INLET SUCTION DANGERAREA
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
TO
275
m (
900
ft) A
FT
OF
FA
N N
OZ
ZLE
TO 150 m (500 ft) AFTOF FAN NOZZLE
R = 5.9 m(19.5 ft)
1.8 m(6 ft)
N_AC_060302_1_0010101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE-6-3-2-991-001-A01
6-3-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FEET(METERS)
60(18)
50(15)
40(12)
30(9)
20(6)
10(3) 0
10(3)
20(6)
30(9)
40(12)
50(15)
60(18)
INTAKE SUCTION DANGER AREA
ENTRY CORRIDOR
EXHAUST DANGER AREA (AFT OF EXHAUST NOZZLE):600 ft (183 m) − TAKE OFF POWER (20 kt HEADWIND)
6 ft(1.83 m)
R = 20 ft(6.10 m)
R = 20 ft(6.10 m)
6 ft(1.83 m)
30° 30°
N_AC_060302_1_0020101_01_01
Danger Areas of EnginesPW 6000 series engine
FIGURE-6-3-2-991-002-A01
6-3-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A318-100
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1 APU
**ON A/C A318-100
APU - APIC & GARRETT
1. This section gives APU exhaust velocities and temperatures.
6-4-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
0 PLAN 5 10 15 2520
0 16.404 32.808 49.212 65.616 82.02
0
0
FEET
0
5
ELEVATION
10
0
16.404
32.808
METERS
HEIGHT
m ft
FEET
METERS
5 10 15 20
16.404 32.808 49.212 65.616
80°C176°F
100°C212°F
120°C248°F
150°C302°F
200°C392°F
300°C572°F
45 m/s147 ft/s
30 m/s98 ft/s
20 m/s65 ft/s
10 m/s32 ft/s
5 m/s16 ft/s
N_AC_060401_1_0010101_01_00
Exhaust Velocities and TemperaturesAPU -- APIC & GARRETTFIGURE-6-4-1-991-001-A01
6-4-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A318-100
General Information
1. General Information
This brief description of the pavement charts that follow will help in their use for airport planning.
To aid in the interpolation between the discrete values shown, each airplane configuration is shownwith a minimum range of five loads on the main landing gear.
All curves on the charts represent data at a constant specified tire pressure with:- The airplane loaded to the maximum ramp weight.- The Center of Gravity (CG) at its maximum permissible aft position.
Pavement requirements for commercial airplanes are derived from the static analysis of loads imposedon the main landing gear struts.
The A/C codes are used for configuration management of chapter 07 only. There is no relationbetween these A/C codes and the ICAO A/C codes used for determining the airplane wing span andouter main gear wheel span as described in ICAO-Annex 14 Volume 1, Aerodrome Design andOperation Chapter 1.4, Table 1-1.
Section 7-2-0 presents basic data on the landing gear footprint configuration, maximum ramp weightsand tire sizes and pressures.
Section 7-3-0 shows maximum vertical and horizontal pavement loads for certain critical conditions atthe tire-ground interfaces.
Section 7-4-1 contain charts to find these loads throughout the stability limits of the airplane at reston the pavement.
These main landing gear loads are used as the point of entry to the pavement design charts whichfollow, interpolating load values where necessary.
Section 7-5-1 uses procedures in Instruction Report No S-77-1, ”Procedures for Development of CBRDesign Curves”, dated June 1977 and as modified according to the methods described in ICAOAerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCNMethod), and utilizing the alpha factors approved by ICAO in October 2007.
7-1-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The report was prepared by the U.S Army Corps Engineers Waterways Experiment Station, Soils andPavement Laboratory, Vicksburg, Mississippi.
The line showing 10 000 coverages is used to calculate Aircraft Classification Number (ACN).
The procedure that follows is used to develop flexible pavement design curves such as shown inSection 7-5-1.- With the scale for pavement thickness at the bottom and the scale for CBR at the top, an
arbitrary line is drawn representing 10 000 coverages.- Incremental values of the weight on the main landing gear are then plotted.- Annual departure lines are drawn based on the load lines of the weight on the main landing gear
that is shown on the graph.
Section 7-7-1 gives the rigid pavement design curves that have been prepared with the use of theWestergaard Equation. This is in general accordance with the procedures outlined in the PortlandCement Association publications, ”Design of Concrete Airport Pavement”, 1973 and ”ComputerProgram for Airport Pavement Design”, (Program PDILB), 1967 both by Robert G. Packard.
The procedure that follows is used to develop rigid pavement design curves such as shown in Section7-7-1.- With the scale for pavement thickness to the left and the scale for allowable working stress to the
right, an arbitrary load line is drawn. This represents the maximum weight to be shown for themain landing gear .
- All values of the subgrade modulus (k values) are then plotted- Additional load lines for the incremental values of weight on the main landing gear are drawn on
the basis of the curve for k = 300 already shown on the graph.
All Load Classification Number (LCN) curves shown in Section 7-6-1 and Section 7-8-2 have beendeveloped from a computer program based on data provided in International Civil AviationOrganisation (ICAO) document 7920-AN/865/2, Aerodrome Manual, Part 2, ”Aerodrome PhysicalCharacteristics”, Second Edition, 1965.
The flexible pavement charts, section 7-6-1, show LCN against equivalent single wheel load andequivalent single wheel load against pavement thickness.
The rigid pavement charts in section 7-8-2 show LCN against equivalent single wheel load andequivalent single wheel load against radius of relative stiffness.
Section 7-9-0 gives ACN data prepared in accordance with the ACN/PCN system as referenced inICAO Annex 14, ”Aerodromes”, Volume 1 Fourth Edition July 2004, incorporating Amendments 1 to6.The ACN/PCN system gives a standardized international airplane/pavement rating system replacingthe various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout the world.
7-1-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.
An aircraft having an ACN equal to or less than the PCN can operate without restriction on thepavement.
Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.The derived single wheel is defined as the load on a single tire inflated to 1.25 Mpa (181 psi) thatwould have the same pavement requirements as the aircraft.
Computationally, the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1for flexible pavements to calculate ACN values.The Airport Authority must decide on the method of pavement analysis and the results of theirevaluation shown as follows:
PCNPAVEMENT
TYPESUBGRADECATEGORY
TIRE PRESSURE CATEGORY EVALUATION METHOD
R -- Rigid A -- High W -- No Limit T -- Technical
F -- Flexible B -- Medium X -- To 1.5 Mpa (217 psi) U -- Using Aircraft
C -- Low Y -- To 1 Mpa (145 psi)
D -- Ultra Low Z -- To 0.5 Mpa (73 psi)
Section 7-9-1, shows the aircraft ACN values for flexible pavements.
The four subgrade categories are:- A. High Strength CBR 15- B. Medium Strength CBR 10- C. Low Strength CBR 6- D. Ultra Low Strength CBR 3
Section 7-9-2, shows the aircraft ACN values for rigid pavements.
The four subgrade categories are:- A. High Strength Subgrade k = 150 MN/m3 (550 pci)- B. Medium Strength Subgrade k = 80 MN/m3 (300 pci)- C. Low Strength Subgrade k = 40 MN/m3 (150 pci)- D. Ultra Low Strength Subgrade k = 20 MN/m3 (75 pci)
7-1-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
MODEL WVAIRCRAFT
CODEA318−100 06 CA318−100 00 DA318−100 07 EA318−100 01 FA318−100 02 GA318−100 08 HA318−100 03 IA318−100 04 JA318−100 05 K
NOTE:
NOTE:CHAPTER 07 ONLY.THERE IS NO RELATION BETWEEN THESE A/C CODES AND THE ICAO A/C CODES USED FOR DETERMINING THE AIRPLANE WING SPAN ANDOUTER MAIN GEAR WHEEL SPAN AS DESCRIBED IN ICAO−ANNEX 14 VOLUME 1, AERODROME DESIGN AND OPERATION CHAPTER 1.4, TABLE 1−1.
FOR WEIGHT VARIANT DEFINITION, REFER TO CHAPTER 02−01−01.
THE A/C CODES ARE USED FOR CONFIGURATION MANAGEMENT OF
N_AC_070100_1_0010101_01_00
Aircraft CodesFIGURE-7-1-0-991-001-A01
7-1-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A318-100
Landing Gear Footprint
1. This section gives Landing Gear Footprint.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-2-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A/C CODE
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
12.3 bar (178 psi)
MAIN GEAR TIRE PRESSURE 10.2 bar (148 psi)
46 x 17 R20(46 x 16 − 20)
30 x 8.8 R15(30 x 8.8 − 15)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
C
SEE SECTION 7−4−1
927 mm(36.5 in)
500 mm(19.7 in)
10 252 mm
7 590 mm(24 ft 10.8 in)
(33 ft 7.6 in)
N_AC_070200_1_0010101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-001-A01
7-2-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
927 mm(36.5 in)
500 mm(19.7 in)
10 252 mm
A/C CODE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
D − E − F − G
30 x 8.8 R15(30 x 8.8 − 15)
12.8 bar (186 psi)
MAIN GEAR TIRE PRESSURE 11.4 bar (165 psi)
(33 ft 7.6 in)
46 x 17 R20(46 x 16 − 20)
7 590 mm(24 ft 10.8 in)
SEE SECTION 7−4−1
N_AC_070200_1_0020101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-002-A01
7-2-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
927 mm(36.5 in)
500 mm(19.7 in)
10 252 mm
7 590 mm(24 ft 10.8 in)
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
30 x 8.8 R15(30 x 8.8 − 15)
13.5 bar (196 psi)
MAIN GEAR TIRE PRESSURE 12.4 bar (180 psi)
46 x 17 R20(46 x 16 − 20)
(33 ft 7.6 in)
A/C CODE H − I − J − K
SEE SECTION 7−4−1
N_AC_070200_1_0030101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-003-A01
7-2-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A318-100
Maximum Pavement Loads
1. This section gives Maximum Pavement Loads.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-3-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
C56
400
VM
G (
PE
R S
TR
UT
)V
NG
124
350
23 2
5010
550
35 8
7516
270
56 0
7525
430
19 3
258
760
44 8
5020
340
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
(MG
)M
AX
IMU
M V
ER
TIC
AL
MA
IN G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T A
FT
CG
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
MR
W =
56
400
kgM
RW
= 5
9 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
14
% M
AC
AT
A/C
WE
IGH
T =
56
400
kgF
WD
CG
= 1
5 %
MA
C A
T A
/C W
EIG
HT
= 5
9 40
0 kg
D E60
450
27 4
3021
025
9 54
048
375
21 9
40
MR
W =
61
400
kgF
WD
CG
= 1
5 %
MA
C A
T A
/C W
EIG
HT
= 6
1 40
0 kg
MR
W =
56
400
kgM
RW
= 5
9 40
0 kg
AF
T C
G =
35
% M
AC
AT
A/C
WE
IGH
T =
56
400
kgA
FT
CG
= 3
3.9
% M
AC
AT
A/C
WE
IGH
T =
59
400
kgM
RW
= 6
1 40
0 kg
AF
T C
G =
32.
9 %
MA
C A
T A
/C W
EIG
HT
= 6
1 40
0 kg
59 4
0013
0 95
023
900
10 8
4037
150
16 8
5058
750
26 6
5020
350
9 23
047
000
21 3
20
61 4
0013
5 37
524
700
11 2
0038
350
17 4
00
N_AC_070300_1_0200101_01_00
V
H
(1)
A/C
CO
DE
C D E
(2)
C D E
Maximum Pavement LoadsMaximum Pavement LoadsFIGURE-7-3-0-991-020-A01
7-3-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
F61
900
VM
G (
PE
R S
TR
UT
)V
NG
136
475
24 9
0011
290
38 6
7517
540
60 9
0027
620
21 2
009
620
48 7
0022
100
(NG
)M
AX
IMU
M V
ER
TIC
AL
NO
SE
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
FO
RW
AR
D C
G
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
MR
W =
61
900
kgM
RW
= 6
3 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
15
% M
AC
AT
A/C
WE
IGH
T =
61
900
kgF
WD
CG
= 1
5 %
MA
C A
T A
/C W
EIG
HT
= 6
3 40
0 kg
G H63
150
28 6
4022
075
10 0
1050
525
22 9
20
MR
W =
64
400
kgF
WD
CG
= 1
5.8
% M
AC
AT
A/C
WE
IGH
T =
64
400
kg
MR
W =
61
900
kgM
RW
= 6
3 40
0 kg
AF
T C
G =
32.
7 %
MA
C A
T A
/C W
EIG
HT
= 6
1 90
0 kg
AF
T C
G =
32
% M
AC
AT
A/C
WE
IGH
T =
63
400
kgM
RW
= 6
4 40
0 kg
AF
T C
G =
32
% M
AC
AT
A/C
WE
IGH
T =
64
400
kg
63 4
0013
9 77
525
475
11 5
6039
575
17 9
5062
175
28 2
0021
725
9 85
049
725
22 5
60
64 4
0014
1 97
525
400
11 5
2039
700
18 0
10
N_AC_070300_1_0210101_01_00
V
(MG
)V
H
(1)
A/C
CO
DE
F G H
(2)
F G H
Maximum Pavement LoadsMaximum Pavement LoadsFIGURE-7-3-0-991-021-A01
7-3-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
I64
900
VM
G (
PE
R S
TR
UT
)V
NG
143
075
25 3
5011
500
39 7
7518
040
63 6
5028
870
22 2
2510
090
50 9
2523
090
(NG
)M
AX
IMU
M V
ER
TIC
AL
NO
SE
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
FO
RW
AR
D C
G
(MG
)M
AX
IMU
M V
ER
TIC
AL
MA
IN G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T A
FT
CG
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
MR
W =
64
900
kgM
RW
= 6
6 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
16.
2 %
MA
C A
T A
/C W
EIG
HT
= 6
4 90
0 kg
FW
D C
G =
15
% M
AC
AT
A/C
WE
IGH
T =
63
000
kg
J K67
100
30 4
3023
425
10 6
3053
675
24 3
40
MR
W =
68
400
kgF
WD
CG
= 1
5 %
MA
C A
T A
/C W
EIG
HT
= 6
3 00
0 kg
MR
W =
64
900
kgM
RW
= 6
6 40
0 kg
AF
T C
G =
32
% M
AC
AT
A/C
WE
IGH
T =
64
900
kgA
FT
CG
= 3
2 %
MA
C A
T A
/C W
EIG
HT
= 6
6 40
0 kg
MR
W =
68
400
kgA
FT
CG
= 3
2 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
66 4
0014
6 37
525
325
11 4
9039
275
17 8
2065
125
29 5
4022
750
10 3
2052
100
23 6
30
68 4
0015
0 80
025
325
11 4
9039
250
17 8
10
N_AC_070300_1_0220101_01_00
V V
H
(1)
A/C
CO
DE
I J K
(2)
I J K
Maximum Pavement LoadsMaximum Pavement LoadsFIGURE-7-3-0-991-022-A01
7-3-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A318-100
Landing Gear Loading on Pavement
1. General
In the example shown in Section 7-4-1 Landing Gear Loading on Pavement, A/C Code C, the GrossAircraft Weight is 48 000 kg (105 825 lb) and the percentage of weight on the Main Landing Gear is90.2 %.
For these conditions, the total weight on the Main Landing Gear is 43 280 kg (95 425 lb).
7-4-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-1 Landing Gear Loading on Pavement
**ON A/C A318-100
Landing Gear Loading on Pavement
1. This section gives Landing Gear Loading on Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-4-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
90 92 94 96 9835
40
45
50
55
6010 20 30 40 50
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
35
40
45
50
55
60
TAKE OFF
A/C CODE C
CG FOR ACNCALCULATIONS
MZFW = 53 000 kg
MTOW/MLW = 56 000 kg
LANDING
N_AC_070401_1_0290101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-029-A01
7-4-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
90 92 94 96 9835
40
45
55
50
6010 20 30 40 50
PERCENTAGE MAC
35
40
45
50
55
60
AIR
CR
AF
T G
RO
SS
WE
IGH
T−
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
A/C CODE D
MTOW = 59 000 kg
CG FOR ACNCALCULATIONS
MLW = 56 000 kg
LANDING
TAKE OFF
N_AC_070401_1_0300101_01_00
MZFW = 53 000 kg
Landing Gear Loading on PavementFIGURE-7-4-1-991-030-A01
7-4-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 10090 92 94 96 9835 35
65 65
40
45
50
55
40
45
50
55
6060
PERCENTAGE OF WEIGHT ON MAIN GEAR
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
10 20 30 40 50
PERCENTAGE MAC
A/C CODE E
MTOW = 61 000 kg
MLW = 56 000 kg
MZFW = 53 000 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
N_AC_070401_1_0310101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-031-A01
7-4-1Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 10090 92 94 96 9835 35
65 65
40
45
50
55
40
45
50
55
6060
PERCENTAGE OF WEIGHT ON MAIN GEAR
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
10 20 30 40 50
PERCENTAGE MAC
A/C CODE F
MTOW = 61 500 kg
MLW = 56 000 kg
MZFW = 53 000 kg
CG FOR ACNCALCULATIONSLANDING
TAKE OFF
N_AC_070401_1_0320101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-032-A01
7-4-1Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 10090 92 94 96 9835 35
65 65
40
45
50
55
40
45
50
55
6060
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
10 20 30 40 50
PERCENTAGE MAC
A/C CODE G
MTOW = 63 000 kg
MLW = 57 500 kg
CG FOR ACNCALCULATIONS
N_AC_070401_1_0330101_01_00
MZFW = 54 500 kg
LANDING
TAKE OFF
PERCENTAGE OF WEIGHT ON MAIN GEAR
Landing Gear Loading on PavementFIGURE-7-4-1-991-033-A01
7-4-1Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 10090 92 94 96 9835 35
65 65
40
45
50
55
40
45
50
55
6060
PERCENTAGE OF WEIGHT ON MAIN GEAR
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
10 20 30 40 50
PERCENTAGE MAC
A/C CODE H
MTOW = 64 000 kg
CG FOR ACNCALCULATIONSLANDING
TAKE OFF
MLW = 56 000 kg
MZFW = 53 000 kg
N_AC_070401_1_0340101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-034-A01
7-4-1Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 10090 92 94 96 9835 35
65 65
40
45
50
55
40
45
50
55
6060
PERCENTAGE OF WEIGHT ON MAIN GEAR
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
10 20 30 40 50
PERCENTAGE MAC
CG FOR ACNCALCULATIONS
TAKE OFF
LANDING
MTOW = 64 500 kg
A/C CODE I
MLW = 57 500 kg
MZFW = 54 500 kg
N_AC_070401_1_0350101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-035-A01
7-4-1Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 10090 92 94 96 9835 35
65 65
40
45
50
55
40
45
50
55
6060
PERCENTAGE OF WEIGHT ON MAIN GEAR
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
10 20 30 40 50
PERCENTAGE MAC
A/C CODE J
CG FOR ACNCALCULATIONS
TAKE OFF
LANDING
MLW = 57 500 kg
MTOW = 66 000 kg
MZFW = 54 500 kg
70 70
N_AC_070401_1_0360101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-036-A01
7-4-1Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
78 80 82 84 86 88 10090 92 94 96 9835 35
65 65
40
45
50
55
40
45
50
55
6060
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
10 20 30 40 50
PERCENTAGE MAC
70 70
MTOW = 68 000 kg
TAKE OFF
CG FOR ACNCALCULATIONS
MZFW = 54 500 kg
MLW = 57 500 kg
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE K
N_AC_070401_1_0370101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-037-A01
7-4-1Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A318-100
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
1. General
In order to determine a particular Flexible Pavement Thickness, the Subgrade Strength (CBR), theAnnual Departure Level and the weight on one Main Landing Gear must be known.
In the example shown in Section 7-5-1 Flexible Pavement Requirements, A/C Code C for:- a CBR value of 10- an Annual Departure Level of 25 000- the Load on one MLG of 20 000 kg (44 100 lb).
For these conditions, the Flexible Pavement Thickness is 40.9 cm (16.1 in).
The line showing 10 000 Coverages is used to calculate the Aircraft Classification Number (ACN).
7-5-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A318-100
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
1. This section gives Flexible Pavement Requirements.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-5-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 10.2 bar (148 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE C ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
WEIGHT ON ONE MAIN LANDING GEAR25 430 kg (56 075 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
N_AC_070501_1_0290101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-029-A01
7-5-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
N_AC_070501_1_0300101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE D
WEIGHT ON ONE MAIN LANDING GEAR26 650 kg (58 750 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-030-A01
7-5-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE E
WEIGHT ON ONE MAIN LANDING GEAR27 430 kg (60 450 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
N_AC_070501_1_0310101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-031-A01
7-5-1Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
[INCHES]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
SUBGRADE STRENGTH − CBR
A/C CODE F
WEIGHT ON ONE MAIN LANDING GEAR27 620 kg (60 900 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)
N_AC_070501_1_0320101_01_00
10 000 kg (22 050 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-032-A01
7-5-1Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE G
28 200 kg (62 175 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
N_AC_070501_1_0330101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-033-A01
7-5-1Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE H
WEIGHT ON ONE MAIN LANDING GEAR28 640 kg (63 150 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
N_AC_070501_1_0340101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-034-A01
7-5-1Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE I
28 870 kg (63 650 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
WEIGHT ON ONE MAIN LANDING GEAR
N_AC_070501_1_0350101_01_00
Flexible Pavement RequirementsFlexible Pavement Requirements
FIGURE-7-5-1-991-035-A01
7-5-1Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE J
WEIGHT ON ONE MAIN LANDING GEAR29 540 kg (65 125 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
N_AC_070501_1_0360101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-036-A01
7-5-1Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
10 15 20 30 40 60 80 100 120 150 180
806050403020151063
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE K
WEIGHT ON ONE MAIN LANDING GEAR30 430 kg (67 100 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
N_AC_070501_1_0370101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-037-A01
7-5-1Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A318-100
Flexible Pavement Requirements - LCN Conversion
1. General
In order to determine the airplane weight that can be accommodated on a particular FlexiblePavement, both the LCN of the pavement and the thickness (h) must be known.
In the example shown in Section 7-6-1 Flexible Pavement Requirements - LCN Conversion, A/C CodeC for:The thickness (h) is shown at 20 inches with an LCN of 47.7.For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).
7-6-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-1 Flexible Pavement Requirements - LCN Conversion
**ON A/C A318-100
Flexible Pavement Requirements - LCN Conversion
1. This section gives Flexible Pavement Requirements - LCN Conversion.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-6-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
0.2
bar
(148
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
25 4
30 k
g
(56
075
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
C
N_AC_070601_1_0320101_01_00
2 03
21
524
1 01
6
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-032-A01
7-6-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
26 6
50 k
g
(58
750
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
D
2 03
21
524
1 01
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Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-033-A01
7-6-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
27 4
30 k
g
(60
475
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
N_AC_070601_1_0340101_01_00
A/C
CO
DE
E
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-034-A01
7-6-1Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
27 6
20 k
g
(60
900
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
2 03
21
524
1 01
6
N_AC_070601_1_0350101_01_00
A/C
CO
DE
F
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-035-A01
7-6-1Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.4
bar
(165
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
28 2
00 k
g
(62
175
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
G
2 03
21
524
1 01
6
N_AC_070601_1_0360101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-036-A01
7-6-1Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.4
bar
(180
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
28 6
40 k
g
(63
150
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
2 03
21
524
1 01
6
N_AC_070601_1_0370101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-037-A01
7-6-1Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.4
bar
(180
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
I
2 03
21
524
1 01
6
N_AC_070601_1_0380101_01_00
WE
IGH
T O
N O
NE
MA
IN
28 8
70 k
g
(63
650
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-038-A01
7-6-1Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.4
bar
(180
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
29 5
40 k
g
(65
125
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
J
2 03
21
524
1 01
6
N_AC_070601_1_0390101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-039-A01
7-6-1Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.4
bar
(180
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
30 4
30 k
g
(67
075
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
10 0
00 k
g
(22
050
lb)
762
254
508
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
K
2 03
21
524
1 01
6
N_AC_070601_1_0400101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-040-A01
7-6-1Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A318-100
Rigid Pavement Requirements - Portland Cement Association Design Method
1. General
In order to determine a particular Rigid Pavement Thickness, the Subgrade Modulus (k), theallowable working stress and the weight on one Main Landing Gear must be known.
In the example shown in Section 7-7-1 Rigid Pavement Requirements (PCA), A/C Code C for:- a ”k” value of 150 MN/m3 (550 lbf/in3)- an allowable working stress of 31.6 kgf/cm2 (450 lbf/in2)- the load on one MLG of 20 000 kg (44 100 lb).For these conditions, the Rigid Pavement Thickness is 18.4 cm (7.2 in).
7-7-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A318-100
Rigid Pavement Requirements - Portland Cement Association Design Method
1. This section gives Rigid Pavement Requirements.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-7-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
1436
33
31
29
27
24
22
20
17
15 200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 430 kg (56 075 lb)
A/C CODE CRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 10.2 bar (148 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0290101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-029-A01
7-7-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
26 655 kg (58 750 lb)
A/C CODE DRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0300101_01_00
36
33
31
29
27
24
22
20
17
15
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-030-A01
7-7-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
36
33
31
29
27
24
22
20
17
15
N_AC_070701_1_0310101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE E
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
27 425 kg (60 450 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-031-A01
7-7-1Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
36
33
31
29
27
24
22
20
17
15
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE F
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
27 620 kg (60 900 lb)
N_AC_070701_1_0320101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-032-A01
7-7-1Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.4 bar (165 psi)
36
33
31
29
27
24
22
20
17
15
N_AC_070701_1_0330101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE G
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
28 195 kg (62 175 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-033-A01
7-7-1Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE HRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
28 645 kg (63 150 lb)
N_AC_070701_1_0340101_01_00
36
33
31
29
27
24
22
20
17
15
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-034-A01
7-7-1Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
36
33
31
29
27
24
22
20
17
15
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE I
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
28 865 kg (63 650 lb)
N_AC_070701_1_0350101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-035-A01
7-7-1Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE JRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
29 535 kg (65 125 lb)
N_AC_070701_1_0360101_01_00
36
33
31
29
27
24
22
20
17
15
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-036-A01
7-7-1Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.4 bar (180 psi)
36
33
31
29
27
24
22
20
17
15
N_AC_070701_1_0370101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE K
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
30 430 kg (67 100 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-037-A01
7-7-1Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-1 Radius of Relative Stiffness
**ON A/C A318-100
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
d6.06.57.07.5
k=75 k=100 k=150 k=200 k=250 k=300 k=350 k=400 k=550
8.08.59.09.5
10.010.511.011.512.012.513.013.514.014.515.015.516.016.517.017.518.019.020.021.022.023.024.025.0
31.4833.4335.3437.2239.0640.8842.6744.4346.1847.9049.6051.2852.9454.5956.2257.8359.4361.0269.5964.1565.6967.2368.7570.2671.7674.7377.6680.5583.4186.2489.0491.81
29.3031.1132.8934.6336.3538.0439.7141.3542.9744.5746.1647.7249.2750.8052.3253.8255.3156.7858.2559.7061.1362.5663.9865.3866.7869.5472.2774.9677.6380.2682.8685.44
26.4728.1129.7231.2932.8534.3735.8837.3638.8340.2841.7143.1244.5245.9047.2748.6349.9851.3152.6353.9455.2456.5357.8159.0860.3462.8465.3067.7470.1472.5274.8777.20
24.6326.1627.6529.1230.5731.9933.3934.7736.1437.4838.8140.1341.4342.7243.9945.2646.5147.7548.9850.2051.4152.6153.8054.9856.1558.4860.7763.0465.2867.4969.6871.84
23.3024.7426.1527.5428.9130.2531.5832.8934.1735.4536.7137.9539.1840.4041.6142.8043.9845.1646.3247.4748.6249.7550.8852.0053.1155.3157.4759.6261.7363.8365.9067.95
22.2623.6424.9926.3227.6228.9130.1731.4232.6533.8735.0736.2637.4438.6039.7540.8942.0243.1544.2645.3646.4547.5448.6149.6850.7452.8454.9156.9658.9860.9862.9664.92
21.4222.7424.0425.3226.5827.8129.0330.2331.4232.5933.7534.8936.0237.1438.2539.3540.4441.5142.5843.6444.7045.7446.7747.8048.8250.8452.8454.8156.7558.6860.5862.46
20.7222.0023.2524.4925.7026.9028.0829.2430.3931.5232.6433.7434.8435.9236.9938.0639.1140.1541.1942.2143.2344.2445.2446.2347.2249.1751.1053.0154.8956.7558.5960.41
19.1320.3121.4722.6123.7424.8425.9327.0028.0629.1130.1431.1632.1733.1734.1635.1436.1237.0838.0338.9839.9240.8541.7842.7043.6145.4147.1948.9550.6952.4154.1155.79
L = Ed
= 24.1652dk
43
43
12 (1 − ) k2
RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES
E = YOUNG’S MODULUS = 4 x 10 psi
k = SUBGRADE MODULUS, lb/in
d = RIGID PAVEMENT THICKNESS, (in)
= POISSON’S RATIO = 0.15
WHERE6
3
N_AC_070801_1_0010101_01_01
Radius of Relative Stiffness(Reference: Portland Cement Association)
FIGURE-7-8-1-991-001-A01
7-8-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-2 Rigid Pavement Requirements - LCN Conversion
**ON A/C A318-100
Rigid Pavement Requirements - LCN Conversion
1. GeneralIn order to determine the airplane weight that can be accommodated on a particular Rigid Pavement,both the LCN of the pavement and the Radius of Relative Stiffness (L) must be known.
In the example shown in this section Rigid Pavement Requirements - LCN Conversion, A/C Code Cfor:- The Radius of Relative Stiffness is shown at 762 mm (30 in) with an LCN of 51.1.
For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-8-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
2 ba
r (1
48 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
N_AC_070802_1_0320101_01_00
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R25
430
kg
(5
6 07
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
C
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-032-A01
7-8-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R26
655
kg
(5
8 75
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
D
N_AC_070802_1_0330101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-033-A01
7-8-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R27
425
kg
(6
0 45
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
E
N_AC_070802_1_0340101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-034-A01
7-8-2Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R27
620
kg
(6
0 90
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
F
N_AC_070802_1_0350101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-035-A01
7-8-2Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R28
195
kg
(6
2 17
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
G
N_AC_070802_1_0360101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-036-A01
7-8-2Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R28
645
kg
(6
3 15
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
H
N_AC_070802_1_0370101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-037-A01
7-8-2Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R28
865
kg
(6
3 65
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
I
N_AC_070802_1_0380101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-038-A01
7-8-2Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R29
535
kg
(6
5 12
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
J
N_AC_070802_1_0390101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-039-A01
7-8-2Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
2030
4050
100
8070
6001020304050607080
6080
5040
3020
1005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
762
254
508
2 28
61
524
1 01
6
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R30
430
kg
(6
7 10
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
K
N_AC_070802_1_0400101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-040-A01
7-8-2Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-3 Radius of Relative Stiffness (Other values of E and L)
**ON A/C A318-100
Radius of Relative Stiffness (Other values of ”E” and ”L”)
1. General
The table of Section 7-8-1, Radius of Relative Stiffness, presents ”L” values based on Young’sModulus (E) of 4 000 000 psi and Poisson’s Ratio (µ) of 0.15.
To find ”L” values based on other values of ”E” and ”µ”, see Section 7-8-4.
For example, to find an ”L” value based on an ”E” of 3 000 000 psi, the ”E” factor of 0.931 ismultiplied by the ”L” value found in the table of Section 7-8-1.
The effect of variations of ”µ” on the ”L” value is treated in a similar manner.
7-8-3Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-4 Radius of Relative Stiffness
**ON A/C A318-100
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-4Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
E F
AC
TO
RF
AC
TO
R
EFFECT OF E ON L VALUES
0.00 0.05 0.10 0.15 0.20 0.25
1.015
1.010
1.005
1.000
0.995
0.80
0.85
0.90
0.95
1.00
1.05
1.10
0 1 2 3 4 5
EFFECT OF ON L VALUES
NOTE: BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF TABLE 7.8.1
E, Young’s Modulus (10 , PSI)
, Poisson’s Ratio
N_AC_070804_1_0010101_01_02
Radius of Relative Stiffness(Effect E and µ on ”L” values)
FIGURE-7-8-4-991-001-A01
7-8-4Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0 ACN/PCN Reporting System
**ON A/C A318-100
ACN/PCN Reporting System
1. General
To determine the ACN of an aircraft on flexible or rigid pavement, both the aircraft gross weight andthe subgrade strength must be known.
In the example shown in Section 7-9-1 Aircraft Classification Number -- Flexible Pavement, A/C CodeC, for an aircraft gross weight of 50 000 kg (110 225 lb) and low subgrade strength (code C), theACN for the flexible pavement is 25.5.
In the example shown in Section 7-9-2 Aircraft Classification Number -- Rigid Pavement, A/C CodeC, for an aircraft gross weight of 50 000 kg (110 225 lb) and medium subgrade strength (code B),the ACN for the rigid pavement is 25.5.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref.: ICAO Aerodrome Design Manual Part 3 Chapter 1 Second Edition 1983).
7-9-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-1 Aircraft Classification Number - Flexible Pavement
**ON A/C A318-100
Aircraft Classification Number - Flexible Pavement
1. This section gives the Aircraft Classification Number - Flexible Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-9-1Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
5550
4540
3510152025303540
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
2 ba
r (1
48 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
5 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
77
60
8899
110
121
132
(x 1
000
lb)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
C
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0420101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E C
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-042-A01
7-9-1Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
5550
4540
3510152025303540
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
3.93
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
77
60
8899
110
121
132
(x 1
000
lb)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
D
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0430101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E D
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-043-A01
7-9-1Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
5550
4540
3510152025303540
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2.93
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
77
60
8899
110
121
132
(x 1
000
lb)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
E
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0440101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-044-A01
7-9-1Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
6055
5040
3510152025303540
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
77
65
8811
012
113
214
3
(x 1
000
lb)
4599
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
F
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0450101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-045-A01
7-9-1Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
6055
5040
3510152025303540
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
77
65
8811
012
113
214
3
(x 1
000
lb)
4599
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
G
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0460101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-046-A01
7-9-1Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
(x 1
000
lb)
6055
5040
3510152025303545
77
65
8811
012
1
459913
214
3
40
A/C
CO
DE
H
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0470101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-047-A01
7-9-1Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
6055
5040
3510152025303545
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
77
70
8811
012
113
215
4
(x 1
000
lb)
4599
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
I
ALP
HA
FA
CT
OR
= 0
.9
65143
40
N_AC_070901_1_0480101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E I
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-048-A01
7-9-1Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
6055
5040
35
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
77
70
8811
012
113
215
4
(x 1
000
lb)
4599
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
J
ALP
HA
FA
CT
OR
= 0
.9
65143
10152025303545 40
N_AC_070901_1_0490101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-049-A01
7-9-1Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
6055
5040
35
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
77
70
8811
012
113
215
4
(x 1
000
lb)
4599
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
K
ALP
HA
FA
CT
OR
= 0
.9
65143
10152025303545 40
N_AC_070901_1_0500101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E K
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-050-A01
7-9-1Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-2 Aircraft Classification Number - Rigid Pavement
**ON A/C A318-100
Aircraft Classification Number - Rigid Pavement
1. This section gives the Aircraft Classification Number - Rigid Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-9-2Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
5 %
MA
C.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
10.
2 ba
r (1
48 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
152025303577
8899
110
121
132
4045
5055
60
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
C
N_AC_070902_1_0410101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E C
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-041-A01
7-9-2Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
3.93
% M
AC
.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
D
40
N_AC_070902_1_0420101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E D
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-042-A01
7-9-2Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2.93
% M
AC
.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
40
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
E
65143
N_AC_070902_1_0430101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-043-A01
7-9-2Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2.7
% M
AC
.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
40
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
F
65143
N_AC_070902_1_0440101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-044-A01
7-9-2Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
4 ba
r (1
65 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
40S
UB
GR
AD
E S
TR
EN
GT
HD
− K
= 2
0 M
N/m
(U
LTR
A L
OW
)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
G
65143
45
N_AC_070902_1_0450101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-045-A01
7-9-2Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
40S
UB
GR
AD
E S
TR
EN
GT
HD
− K
= 2
0 M
N/m
(U
LTR
A L
OW
)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
H
65143
45
N_AC_070902_1_0460101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-046-A01
7-9-2Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
40
65143
45
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
I
154
70
N_AC_070902_1_0470101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E I
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-047-A01
7-9-2Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
40
65143
45
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
J
154
70
N_AC_070902_1_0480101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-048-A01
7-9-2Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
2 %
MA
C.
1035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
4 ba
r (1
80 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1520253035
7788
9911
012
113
2
4045
5055
60
40
65143
45
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
A/C
CO
DE
K
154
70
N_AC_070902_1_0490101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E K
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-049-A01
7-9-2Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
**ON A/C A318-100
Scaled Drawings
1. This section provides the scaled drawings.
NOTE : When printing this drawing, make sure to adjust for proper scaling.
8-0-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
0 10 20 30 40 50FEET
0 5 10 15METERS
010
2030
4050
FE
ET
05
1015
ME
TE
RS
N_AC_080000_1_0010101_01_00
WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.NOTE:
Scaled DrawingFIGURE-8-0-0-991-001-A01
8-0-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A318-100
Aircraft Rescue and Fire Fighting
1. Aircraft Rescue and Fire Fighting ChartsThis sections gives data related to aircraft rescue and fire fighting.The figures contained in this section are the figures that are in the Aircraft Rescue and Fire FightingCharts poster available for download on AIRBUSWorld and the Airbus website.
10-0-0Page 1
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0010101_01_00
Front PageFIGURE-10-0-0-991-001-A01
10-0-0Page 2
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0020101_01_00
Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-002-A01
10-0-0Page 3
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0030101_01_00
Wheel Safety Area(Sheet 1 of 2)
FIGURE-10-0-0-991-003-A01
10-0-0Page 4
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0030102_01_00
Wheel Safety AreaRecommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-003-A01
10-0-0Page 5
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0040101_01_00
Composite MaterialsFIGURE-10-0-0-991-004-A01
10-0-0Page 6
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
A AB
B
N_AC_100000_1_0050101_01_00
LG Ground Lock Safety DevicesFIGURE-10-0-0-991-005-A01
10-0-0Page 7
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
C L
N_AC_100000_1_0060101_01_00
Evacuation/Escape Slide/RaftFIGURE-10-0-0-991-006-A01
10-0-0Page 8
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0070101_01_00
Pax/Crew DoorsFIGURE-10-0-0-991-007-A01
10-0-0Page 9
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0080101_01_00
Emergency Exit HatchFIGURE-10-0-0-991-008-A01
10-0-0Page 10
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
134A
R15
4AR
/
198C
B
N_AC_100000_1_0090101_01_00
FWD and AFT Lower Deck Cargo DoorsFIGURE-10-0-0-991-009-A01
10-0-0Page 11
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
FL
T IN
T
LIG
HT
TE
ST
CK
PT
CA
LL
RE
SE
T
AP
U S
HU
T O
FF
AP
U F
IRE
AD
IRU
&C
KP
T C
AL
LA
VN
CS
VE
NT
AV
AIL
NO
T IN
US
E
EL
T
108V
U
EX
T P
WR
ENG
MAS
TER
2M
ASTE
R 1
ON
OF
F
ON
OF
FM
OD
E
IGN
ENG 1
FIR
E
FA
ULT
FIR
E
FA
ULT
21
CR
AN
KS
TA
RT
ENG 2
NO
RM
A
D
RA
IN R
PL
NT
SL
OW
FA
ST
OF
FW
IPE
R
MA
IN S
TA
RT
12
EN
G
OV
RD
FA
UL
TA U T O
BLO
WE
R
OV
RD
FA
UL
TA U T O
EX
TR
AC
TV
EN
TIL
AT
ION
OF
F
CA
B F
AN
S
ON
ON
TE
ST
AF
T
DIS
CH
22V
U
HO
T
AF
T
CA
RG
O S
MO
KE
CO
LD
OF
F
FA
UL
T
HO
T A
IR
OF
F
FA
UL
T
AF
T IS
OL V
ALV
E
CA
RG
O
DIS
CH
SM
OK
E
FW
D
DIS
CH
DIS
CH
SM
OK
E
APU
SH
PU
SH
PU
SH
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
DIS
CH
SQ
UIB
AG
EN
T 1
AG
EN
T 2
AG
EN
T 1
AG
EN
T 2
TE
ST
TE
ST
TE
ST
AG
EN
T
F I R E
F I R E
AP
UFI
RE
FIR
EEN
G2
FIR
EEN
G1
B
C E
ED
B C
FA
ULT
FA
ULT
OF
F
OF
F
OF
F
FA
ULT
OF
F
FA
ULT
OF
F
FA
ULT
OF
F
FA
ULT
OF
F
FA
ULT
ALT
N
FA
ULT
ON
AV
AIL
E L E CID
G 2
GE
N 2
DC
BU
S 2
AC
ES
S F
EE
D
EX
T P
WR
AP
U G
EN
GE
N 1
BA
T 2
BA
T2
1B
AT
1
AC
BU
S 1
DC
BU
S 1
CO
MM
ER
CIA
L
GA
LY &
CA
B
IDG
1
E L E C
BU
S T
IEA U T O
VV
35V
U
OF
F
A U T O
AC
BU
S 2
AC E
SS B
US
ON
FA
ULT
ON
FA
ULT
ON
FA
ULT
ON
FA
ULT
ON
AN
TI IC
EPR
OBE
/WIN
DO
WH
EAT
EN
G 1
EN
G 2
WIN
GM
AN
V/S
CTL
MO
DE
SE
LLD
G E
LEV
AU
TOD
ITC
HIN
GC
ABIN
PR
ESS
UP
ON
A U T O
A U T O
25V
U
ON
FA
ULT
ON
AV
AIL
INT
LT
SIG
NS
APU
STB
Y C
OM
PA
SS
AN
N L
TD
OM
ETE
ST
BR
T
DIM
OFFDIM
BR
T
OFF
SE
AT
BE
LTS
NO
SM
OK
ING
EM
ER
EX
IT L
T
A U T OO
FFO
FF
ON
ON
ON
AR
M
OFF
BRT
OFFOV
HD
INTE
G L
T
MA
STE
R S
W
STA
RT
WIN
GN
AV
& L
OG
OS
TRO
BE
BE
AC
ON
OFF
OFF
OFF
ON
ON
ON
OFF
EXT
LT
A U T O
RW
Y T
UR
N O
FFO
NO
N
OFF
OFF
OFF
RETR
ACT
LAN
DL
RN
OS
ET.
O
TAX
I
ON
OF
F
N_AC_100000_1_0120101_01_00
Control PanelsFIGURE-10-0-0-991-012-A01
10-0-0Page 12
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
316A
R
A
315A
L
A
N_AC_100000_1_0130101_01_00
APU Access DoorFIGURE-10-0-0-991-013-A01
10-0-0Page 13
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0140101_01_00
Aircraft Ground ClearancesFIGURE-10-0-0-991-014-A01
10-0-0Page 14
Jun 01/12
@A318AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A318-100
N_AC_100000_1_0150101_01_00
Structural Break-in PointsFIGURE-10-0-0-991-015-A01
10-0-0Page 15
Jun 01/12