@AIRBUSA319
AIRCRAFT CHARACTERISTICSAIRPORT AND MAINTENANCE PLANNING
AC
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© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.Customer Services
Technical Data Support and Services31707 Blagnac Cedex
FRANCE
Issue: Jul 01/95 Rev: Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 11 - 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
@A319AIRCRAFT 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
@A319AIRCRAFT 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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Power Plant Handling - MajorDimensions - IAE V2500 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - MajorDimensions - IAE V2500 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - FanCowls - IAE V2500 Series Engine
N ILLUSTRATION ADDED
FIGURE Power Plant Handling - ThrustReverser Halves - IAE V2500 SeriesEngine
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
FIGURE Loads at the Aircraft JackingPoints - Wing Jacking Point and ForwardFuselage Jacking Point
N ILLUSTRATION ADDED
FIGURE Jacking for Maintenance -Location of Shoring Cradles
N ILLUSTRATION ADDED
Jacking for Wheel Change N
HIGHLIGHTSPage 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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
FIGURE Landing Gear Jacking for WheelChange - Loads at MLG Jacking Points -Twin Wheels
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at MLG Jacking Points -75 500 kg
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
FIGURE Landing Gear Jacking for WheelChange - Loads at NLG Jacking Points -75 500 kg
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 N
FIGURE Visibility from Cockpit in StaticPosition
N ILLUSTRATION ADDED
HIGHLIGHTSPage 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Binocular Visibility ThroughWindows from Captain Eye Position
N ILLUSTRATION ADDED
Section 4-5 R
Subject 4-5-1
FIGURE 135˚ Turn - Runway to Taxiway- Cockpit Over Centerline Method
R
FIGURE 135˚ Turn - Runway to Taxiway- Judgemental Oversteering Method
R
Subject 4-5-2
FIGURE 90˚ Turn - Runway to Taxiway -Cockpit Over Centerline Method
R
FIGURE 90˚ Turn - Runway to Taxiway -Judgemental Oversteering Method
R
Subject 4-5-3
FIGURE 180˚ Turn on a Runway - Edgeof Runway Method
R ILLUSTRATION REVISED
Subject 4-5-4 N
135˚ Turn - Taxiway to Taxiway N
FIGURE 135˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
N ILLUSTRATION ADDED
Subject 4-5-5 N
90˚ Turn - Taxiway to Taxiway N
FIGURE 90˚ Turn - Taxiway to Taxiway- Cockpit Over Centerline Method
N ILLUSTRATION ADDED
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
HIGHLIGHTSPage 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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
FIGURE Typical Ramp Layout - OpenApron - ULD Loading
N ILLUSTRATION ADDED
Subject 5-1-3 R
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
N
FIGURE Turn Round Stations - FullServicing (36 Min.)
N ILLUSTRATION ADDED
Subject 05-02-01 D
Section 5-3 R
Subject 5-3-0 R
Terminal Operation - Minimum ServicingTurn Round Time
N
FIGURE Turn Round Stations - MinimumServicing (21 Min.)
N ILLUSTRATION ADDED
Subject 05-03-01 D
Section 5-4
Subject 5-4-1
HIGHLIGHTSPage 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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
FIGURE Ground Service Connections -Overpressure Protector and NACA FlameArrestor
N ADDED OVERPRESSURE PROTECTORAND NACA FLAME ARRESTORILLUSTRATION.ILLUSTRATION ADDED
Subject 5-4-8
Potable Water System R NOTE AMENDED
Section 5-5
Subject 5-5-0
Engine Starting Pneumatic Requirements R CROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Engine Starting PneumaticRequirements
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) -- IAE V2500series engine
R
Subject 5-5-2 R
Medium Ambient Temperatures R DESCRIPTION TITLE UPDATED
HIGHLIGHTSPage 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Engine Starting PneumaticRequirements - Medium AmbientTemperature +15˚C (+59˚F) -- CFM56series engine
R
FIGURE Engine Starting PneumaticRequirements - Medium AmbientTemperature +15˚C (+59˚F) -- IAEV2500 series engine
R
Subject 5-5-3 R
High Ambient Temperatures R DESCRIPTION TITLE UPDATED
FIGURE Engine Starting PneumaticRequirements - High AmbientTemperature +55˚C (+131˚F) -- CFM56series engine
R
FIGURE Engine Starting PneumaticRequirements - High AmbientTemperature +50˚C (+122˚F) -- IAEV2500 series engine
R
Section 5-6
Subject 5-6-0
Ground Pneumatic Power Requirements R DELETED THE AIRFLOW DATA TABLE.ADDED A NOTE FOR GROUNDPNEUMATIC POWER REQUIREMENTS.PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
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.
HIGHLIGHTSPage 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 7
Section 7-3
Subject 7-3-0
FIGURE Maximum Pavement Loads R ILLUSTRATION REVISED
Section 7-4
Subject 7-4-1
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
FIGURE Landing Gear Loading onPavement
R
Section 7-5
Subject 7-5-1
FIGURE Flexible Pavement Requirements R
Section 7-6
Subject 7-6-1
FIGURE Flexible Pavement Requirements- LCN Conversion
R
Section 7-7
Subject 7-7-1
FIGURE Rigid Pavement Requirements(PCA)
R
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.
FIGURE Rigid Pavement Requirements -LCN Conversion
R
HIGHLIGHTSPage 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Section 7-9
Subject 7-9-1
FIGURE Aircraft Classification Number --Flexible Pavement
R
Subject 7-9-2
FIGURE Aircraft Classification Number --Rigid Pavement
R
CHAPTER 8 R
Section 8-0 N
Subject 8-0-0 N
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
HIGHLIGHTSPage 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Structural Break-in Points N ILLUSTRATION ADDED
HIGHLIGHTSPage 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 11 - 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
@A319AIRCRAFT 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
@A319AIRCRAFT 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
@A319AIRCRAFT 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 - IAE V2500Series Engine
N Jun 01/12
FIGURE Power Plant Handling - Major Dimensions - IAE V2500Series Engine
N Jun 01/12
FIGURE Power Plant Handling - Fan Cowls - IAE V2500 SeriesEngine
N Jun 01/12
FIGURE Power Plant Handling - Thrust Reverser Halves - IAE V2500Series 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
L.E.C.Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Loads at the Aircraft Jacking Points - Wing Jacking Pointand Forward Fuselage Jacking Point
N Jun 01/12
FIGURE Jacking for Maintenance - Location of Shoring Cradles N Jun 01/12
Jacking for Wheel Change N Jun 01/12
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 - Loads at MLGJacking Points - 75 500 kg
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
FIGURE Landing Gear Jacking for Wheel Change - Loads at NLGJacking Points - 75 500 kg
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 - CFM56-5A series engine Dec 01/07
FIGURE Payload / Range - CFM56-5B series engine Dec 01/07
FIGURE Payload / Range - IAE V2500-A5 series engine Dec 01/07
Subject 3-3-0
FAR / JAR Take-off Weight Limitation Dec 01/07
Subject 3-3-1
L.E.C.Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
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 --IAE V2500 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
FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C(+59˚F) Conditions -- IAE V2500 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 - CFM56-5A series engine Dec 01/07
FIGURE FAR / JAR Landing Field Length - IAE V2500 series engine Dec 01/07
Subject 3-5-0
Final Approach Speed Dec 01/07
FIGURE Final Approach Speed - CFM56-5A series engine Dec 01/07
FIGURE Final Approach Speed - IAE V2500 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
L.E.C.Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Minimum Turning Radii R Jun 01/12
Subject 4-4-0
Visibility from Cockpit in Static Position N Jun 01/12
FIGURE Visibility from Cockpit in Static Position N 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
Subject 4-5-1
135˚ Turn - Runway to Taxiway Dec 01/07
FIGURE 135˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
FIGURE 135˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
R Jun 01/12
Subject 4-5-2
90˚ Turn - Runway to Taxiway Dec 01/07
FIGURE 90˚ Turn - Runway to Taxiway - Cockpit Over CenterlineMethod
R Jun 01/12
FIGURE 90˚ Turn - Runway to Taxiway - Judgemental OversteeringMethod
R Jun 01/12
Subject 4-5-3
180˚ Turn on a Runway Dec 01/07
FIGURE 180˚ Turn on a Runway - Edge of Runway Method R Jun 01/12
Subject 4-5-4
135˚ Turn - Taxiway to Taxiway N Jun 01/12
FIGURE 135˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
N Jun 01/12
Subject 4-5-5
90˚ Turn - Taxiway to Taxiway N Jun 01/12
FIGURE 90˚ Turn - Taxiway to Taxiway - Cockpit Over CenterlineMethod
N Jun 01/12
Subject 4-6-0
L.E.C.Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
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 Runway Length Alterations - Line Up Distances -- 90˚ Turn Dec 01/07
FIGURE Runway Length Alterations - Line Up Distances -- 180˚ Turn 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
FIGURE Typical Ramp Layout - Open Apron - ULD Loading N 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 N Jun 01/12
FIGURE Turn Round Stations - Full Servicing (36 Min.) N Jun 01/12
Subject 5-3-0
Terminal Operation - Minimum Servicing Turn Round Time N Jun 01/12
FIGURE Turn Round Stations - Minimum Servicing (21 Min.) N Jun 01/12
Subject 5-4-0
Ground Service Connections Dec 01/07
Subject 5-4-1
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CONTENT CHGCODE
LAST REVISIONDATE
Ground Service Connections Layout R Jun 01/12
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 R Jun 01/12
FIGURE Ground Service Connections - Potable Water Ground ServicePanel
Sep 01/10
L.E.C.Page 9
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CONTENT CHGCODE
LAST REVISIONDATE
Subject 5-4-9
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 -- IAE V2500Series Engine
Sep 01/10
FIGURE Ground Service Connections - IDG Oil Tank -- IAE V2500Series Engine
Sep 01/10
FIGURE Ground Service Connections - Starter Oil Tank -- IAE V2500Series Engine
Sep 01/10
FIGURE Ground Service Connections - APU Oil Tank Sep 01/10
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 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) -- IAE V2500 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) -- IAE V2500 series engine
R Jun 01/12
Subject 5-5-3
High Ambient Temperatures R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - High AmbientTemperature +55˚C (+131˚F) -- CFM56 series engine
R Jun 01/12
FIGURE Engine Starting Pneumatic Requirements - High AmbientTemperature +50˚C (+122˚F) -- IAE V2500 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
L.E.C.Page 11
Jun 01/12
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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 -- IAE V2500series 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 -- IAEV2500 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 -- IAE V2500series engine
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
FIGURE Engine Exhaust Temperatures - Takeoff Power -- IAE V2500series 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 - IAE V2500 series engine Dec 01/07
Subject 6-3-0
Danger Areas of Engines Dec 01/07
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CONTENT CHGCODE
LAST REVISIONDATE
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 - IAE V2500 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 - IAE V2500 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
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
FIGURE Landing Gear Footprint - Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint May 01/11
FIGURE Landing Gear Footprint May 01/11
Subject 7-3-0
Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads May 01/11
L.E.C.Page 13
Jun 01/12
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads R Jun 01/12
FIGURE Maximum Pavement Loads May 01/11
FIGURE 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 - Landing Gear Loadingon 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 - Landing Gear Loadingon Pavement
May 01/11
L.E.C.Page 14
Jun 01/12
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon 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 R Jun 01/12
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement R Jun 01/12
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement R Jun 01/12
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
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 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 May 01/11
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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 May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements May 01/11
FIGURE Flexible Pavement Requirements R Jun 01/12
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 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
FIGURE Flexible Pavement Requirements - LCN Conversion May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement 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
FIGURE Flexible Pavement Requirements - LCN Conversion R Jun 01/12
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 - FlexiblePavement 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
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
L.E.C.Page 17
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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
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
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) R Jun 01/12
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
L.E.C.Page 18
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CONTENT CHGCODE
LAST REVISIONDATE
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
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
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE 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
Subject 7-8-3
Radius of Relative Stiffness (Other values of ”E” and ”L”) May 01/11
Subject 7-8-4
L.E.C.Page 19
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CONTENT CHGCODE
LAST REVISIONDATE
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
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
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
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement May 01/11
L.E.C.Page 20
Jun 01/12
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CONTENT CHGCODE
LAST REVISIONDATE
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
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
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement R Jun 01/12
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement May 01/11
L.E.C.Page 21
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CONTENT CHGCODE
LAST REVISIONDATE
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
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 22
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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
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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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@A319AIRCRAFT 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
6-1-5 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
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-1 Radius of Relative Stiffness
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0 Purpose
**ON A/C A319-100
Purpose
1. GeneralThe A319 AIRCRAFT CHARACTERISTICS -- AIRPORT AND MAINTENANCE PLANNING (AC)manual is issued for the A319-100 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 A319-100 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:- Sharklets- New Engine Option (neo)The A320 Family wider fuselage, advanced troubleshooting and Cargo Loading System enable easyand cost effective ground handling, whilst minimizing aircraft turn round time.
This document does not include the A319neo which is under development.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services
1-1-0Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
1, Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-0 General Aircraft Characteristics
**ON A/C A319-100
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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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-1-1 General Aircraft Characteristics Data
**ON A/C A319-100
General Airplane Characteristics Data
1. The following table provides characteristics of A319-100 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004
Kilograms 64 400 70 400 75 900 68 400 68 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds141 978 155 205 167 331 150 796 150 796
Kilograms 64 000 70 000 75 500 68 000 68 000Maximum Takeoff Weight(MTOW) Pounds 141 096 154 324 166 449 149 914 149 914
Kilograms 61 000 61 000 62 500 61 000 62 500Maximum Landing Weight(MLW) Pounds 134 482 134 482 137 789 134 482 137 789
Kilograms 57 000 57 000 58 500 57 000 58 500Maximum Zero FuelWeight (MZFW) Pounds 125 663 125 663 128 970 125 663 128 970
Aircraft CharacteristicsWV005 WV006 WV007 WV008 WV009
Kilograms 70 400 73 900 75 900 64 400 66 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds155 205 162 922 167 331 141 978 146 387
Kilograms 70 000 73 500 75 500 64 000 66 000Maximum Takeoff Weight(MTOW) Pounds 154 324 162 040 166 449 141 096 145 505
Kilograms 62 500 62 500 61 000 62 500 62 500Maximum Landing Weight(MLW) Pounds 137 789 137 789 134 482 137 789 137 789
Kilograms 58 500 58 500 57 000 58 500 58 500Maximum Zero FuelWeight (MZFW) Pounds 128 970 128 970 125 663 128 970 128 970
Aircraft CharacteristicsWV011 WV012
Kilograms 66 400 62 400Maximum Ramp Weight (MRW)Maximum Taxi Weight (MTW) Pounds 146 387 137 568
Kilograms 66 000 62 000Maximum Takeoff Weight (MTOW)
Pounds 145 505 136 686
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsWV011 WV012
Kilograms 61 000 61 000Maximum Landing Weight (MLW)
Pounds 134 482 134 482Kilograms 57 000 57 000Maximum Zero Fuel Weight (MZFW)
Pounds 125 663 125 663
2. The following table provides characteristics of A319-100 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard SeatingCapacity
Single-class156
Liters 23 859US gallons 6 303
Kilograms(density =0.785 kg/l)
18 729
Usable Fuel Capacity
Pounds 41 290Cubic meters 285Pressurized Fuselage
Volume (A/C nonequipped)
Cubic feet10 065
Cubic meters 120Passenger CompartmentVolume Cubic feet 4 238
Cubic meters 9Cockpit VolumeCubic feet 318Cubic meters 8.52Usable Volume, FWD
CC Cubic feet 300Cubic meters 11.92Usable Volume, AFT CCCubic feet 421Cubic meters 7.22Usable Volume, Bulk CCCubic feet 255Cubic meters 10.63Water Volume, FWD CCCubic feet 375.4Cubic meters 13.91Water Volume, AFT CCCubic feet 491.2Cubic meters 7.51Water Volume, Bulk CCCubic feet 265.2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0 General Aircraft Dimensions
**ON A/C A319-100
General Aircraft Dimensions
1. This section provides General Aircraft Dimensions.
2-2-0Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
4.14
m(1
3.58
ft)
OPTIONAL
11.04 m(36.22 ft)
5.07 m(16.63 ft)
5.87
m(1
9.26
ft)
N_AC_020200_1_0020101_01_03
12.45 m(40.85 ft)
34.10 m(111.88 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)
General Aircraft DimensionsWing Tip Fence (Sheet 1 of 4)
FIGURE-2-2-0-991-002-A01
2-2-0Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
33.84 m(111.02 ft)
9.6 m(31.5 ft)
9.52 m(31.23 ft)
CFM56
V2500
11.9
1 m
(39.
07 ft
)
8.30
m(2
7.23
ft)
5.75
m(1
8.86
ft)
3.95
m(1
2.96
ft)
4.87
m(1
5.98
ft)
N_AC_020200_1_0020103_01_00
General Aircraft DimensionsWing Tip Fence (Sheet 2 of 4)
FIGURE-2-2-0-991-002-A01
2-2-0Page 3
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
4.14
m(1
3.58
ft)
OPTIONAL
11.04 m(36.23 ft)
5.07 m(16.63 ft)
5.87
m(1
9.26
ft)
N_AC_020200_1_0020102_01_01
7.59 m(24.90 ft)
0.93 m(3.05 ft)
0.50 m(1.64 ft)
12.45 m
(40.85 ft)
35.80 m
(117.45 ft)
8.95 m(29.36 ft)
3.79 m(12.43 ft)
2.43 m(7.97 ft)
General Aircraft DimensionsSharklet (Sheet 3 of 4)
FIGURE-2-2-0-991-002-A01
2-2-0Page 4
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
33.84 m(111.02 ft)
9.6 m(31.5 ft)
9.52 m(31.23 ft)
CFM56
V2500
11.9
1 m
(39.
07 ft
)
8.30
m(2
7.23
ft)
5.75
m(1
8.86
ft)
3.95
m(1
2.96
ft)
4.87
m(1
5.98
ft)
16.2
9 m
(53.
44 ft
)1.
61 m
(5.2
8 ft)
3.22 m(10.56 ft)
1.64 m(5.38 ft)
21.85 m(71.69 ft)
N_AC_020200_1_0020104_01_00
General Aircraft DimensionsSharklet (Sheet 4 of 4)
FIGURE-2-2-0-991-002-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0 Ground Clearances
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
CG 28% FWD CG 21% FWD CG 21% AFT CG 36%
11.386.866.006.3619.5919.982.202.795.688.9610.3711.487.28
BC1C2D1D2
E (CFM)E (IAE)
FF1F2F3G
11.126.595.746.14
19.3619.751.942.565.458.73
10.1411.257.05
11.326.735.846.0419.4219.621.972.565.388.6610.0711.196.92
11.096.535.686.0419.2919.651.872.495.358.63
10.0411.196.96
11.256.665.775.9419.3619.521.902.495.318.569.97
13.558.897.977.9721.5921.594.074.667.41
10.6612.07
12.17H 11.98 11.75 11.84
11.09 13.166.86 8.8911.61 13.55
39.73J 39.53 39.14 39.40 39.01 40.8512.80K1 12.60 12.43 12.50 12.37 14.3715.98K2 15.78 15.65 15.68 15.55 17.5518.31L 18.14 17.75 17.98 17.62 19.4613.02N 12.80 12.83 12.73 12.73 14.8913.98P 13.68 13.98 13.65 13.91 16.2715.98Q 15.81 15.39 15.68 15.26 17.06
AFT CG 36%
P C1 B D1 E C2 D2 H Q J
L F F1 F2 F3 K1 K2
3.472.091.831.945.976.090.670.851.732.733.163.502.223.71
12.113.904.875.583.974.264.87
3.392.011.751.875.906.020.590.781.662.663.093.432.153.6512.053.844.815.533.904.174.82
3.452.051.781.845.925.980.600.781.642.643.073.412.113.5811.933.794.775.413.914.264.69
3.381.991.731.845.885.990.570.761.632.633.063.412.123.61
12.013.814.785.483.884.164.78
3.432.031.761.815.905.950.580.761.622.613.043.382.093.5411.893.774.745.373.884.244.65
4.132.712.432.436.586.581.241.422.263.253.684.012.714.13
12.454.385.355.934.544.965.20
m ft m ft m ft m ft m ft m ft
NOTE:
G
PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
A/C JACKED FDLA/CCONFIG−URATION
40 t 64 tMRW
74 tMRW
= 4.60 m(15.09 ft)
N
N_AC_020300_1_0020101_01_04
A
Ground ClearancesFIGURE-2-3-0-991-002-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
40 t
CG 28%
MRW64 t
FWD CG 21%
MRW74 t
FWD CG 21%
A/C JACKED FDL= 4.60 m(15.09 ft)AFT CG 36%
11.386.866.006.3619.5919.982.202.795.688.9610.3711.487.28
BC1C2D1D2
E (CFM)E (IAE)
FF1F2F3G
11.126.595.746.14
19.3619.751.942.565.458.73
10.1411.257.05
11.326.735.846.0419.4219.621.972.565.388.6610.0711.196.92
11.096.535.686.0419.2919.651.872.495.358.63
10.0411.196.96
11.256.665.775.94
19.3619.521.902.495.318.569.97
13.558.897.977.97
21.5921.594.074.667.41
10.6612.07
12.17H 11.98 11.75 11.84
11.09 13.166.86 8.8911.61 13.55
39.73J 39.53 39.14 39.40 39.01 40.8513.68K1 13.48 13.32 13.39 13.25 15.2622.34K2 22.15 22.01 22.05 21.92 23.9218.31L 18.14 17.75 17.98 17.62 19.4613.02N 12.80 12.83 12.73 12.73 14.8913.98P 13.68 13.98 13.65 13.91 16.2715.98Q 15.81 15.39 15.68 15.26 17.06
AFT CG 36%
3.472.091.831.945.976.090.670.851.732.733.163.502.223.7112.114.176.815.583.974.264.87
3.392.011.751.875.906.020.590.781.662.663.093.432.153.65
12.054.116.755.533.904.174.82
3.452.051.781.845.925.980.600.781.642.643.073.412.113.5811.934.066.715.413.914.264.69
3.381.991.731.845.885.990.570.761.632.633.063.412.123.6112.014.086.725.483.884.164.78
3.432.031.761.815.905.950.580.761.622.613.043.382.093.5411.894.046.685.373.884.244.65
4.132.712.432.436.586.581.241.422.263.253.684.012.714.13
12.454.657.295.934.544.965.20
m ft m ft m ft m ft m ft m ft
NOTE: PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
A/CCONFIG−URATION
P A C1 B E C2 G D2 H Q J
L F F1 F2 F3 K1 K2
D1
N_AC_020300_1_0280101_01_00
N
Ground ClearancesGround Clearances with Sharklets
FIGURE-2-3-0-991-028-A01
2-3-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
HEIGHT FROM GROUND
m ft m ft m ftABCD
2.052.772.813.65
1.962.682.723.56
1.942.662.703.52
6.73 6.43 6.36
11.5211.6811.98
9.099.22
8.798.92
8.738.86
MODEL 100 (64T MTOW)
2.052.772.813.65
1.952.672.713.55
1.932.652.693.51
6.73 6.40 6.33
11.5211.6511.98
9.099.22
8.768.81
8.698.83
MODEL 100 (70T MTOW)
2.072.792.833.67
1.942.672.703.54
1.932.652.693.51
6.79 6.36 6.33
11.5211.6112.04
9.159.28
8.768.86
8.698.83
MODEL 100 (75.5T MTOW)
DCBA
N_AC_020300_1_0110101_01_00
EFG
HEIGHT FROM GROUND
m ft m ft m ft
HEIGHT FROM GROUND
m ft m ft m ft
2.092.593.04
2.012.502.95
1.982.472.91 9.559.689.97
6.868.50
6.598.20
6.508.10
2.102.593.05
1.992.492.94
1.972.462.90 9.519.6510.01
6.898.50
6.538.17
6.468.07
2.112.613.06
1.992.482.93
1.972.462.91 9.559.6110.06
6.928.56
6.538.14
6.468.07
ABCDEFG
ABCDEFG
F GE
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
Ground ClearancesFlaps and Flap Track Fairings When Flaps Fully Extended
FIGURE-2-3-0-991-011-A01
2-3-0Page 4
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
HEIGHT FROM GROUND
KJ
m ft m ft m ftHJK
2.683.093.48
2.593.003.39
2.582.983.36
8.79 8.50 8.4610.1411.42
9.8411.12
9.7811.02
MODEL 100 (64T MTOW)
H
HEIGHT FROM GROUND
m ft m ft m ftHJK
2.683.093.49
2.582.993.38
2.572.973.35
8.79 8.46 8.4310.1411.45
9.8111.09
9.7410.99
MODEL 100 (70T MTOW)
HEIGHT FROM GROUND
m ft m ft m ftHJK
2.703.103.50
2.582.983.37
2.572.973.36
8.86 8.46 8.4310.1711.48
9.7811.06
9.7411.02
MODEL 100 (75.5T MTOW)
N_AC_020300_1_0120101_01_00
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
Ground ClearancesFlap Track Fairings Up
FIGURE-2-3-0-991-012-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
HEIGHT FROM GROUND
m ft m ft m ftLM
4.183.84
4.093.75
4.043.71
13.71 13.42 13.2512.60 12.30 12.17
MODEL 100 (64T MTOW)
HEIGHT FROM GROUND
m ft m ft m ftLM
4.183.84
4.073.73
4.033.70
13.71 13.35 13.2212.60 12.24 12.14
MODEL 100 (70T MTOW)
HEIGHT FROM GROUND
m ft m ft m ftLM
4.203.86
4.063.73
4.043.71
13.78 13.32 13.2512.66 12.24 12.17
MODEL 100 (75.5T MTOW)
ML
N_AC_020300_1_0130101_01_00
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
Ground ClearancesAileron Down
FIGURE-2-3-0-991-013-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
Q R S T U V WPN
N_AC_020300_1_0140101_01_00
4.01
3.75
14.70
14.27
13.35
13.16
12.30
4.51
4.39
4.26
4.13
3.98
3.92
3.66
14.80
14.40
13.98
13.55
13.06
12.86
12.01
4.47
4.35
4.23
4.10
3.96
3.90
3.65
14.67
14.27
13.88
13.10
12.99
12.80
11.98
13.814.21
4.35
4.48
4.60 15.09
4.07
m ft m m
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
Q
R
N
P
ft ft
U
V
S
T
W
14.30
4.47
4.27
14.67
14.01
4.42
4.23
14.50
13.884.36
4.56 14.96
MODEL 100 (64T MTOW)
Ground ClearancesAileron Up and Spoilers 1 to 5 Extended (Sheet 1 of 2)
FIGURE-2-3-0-991-014-A01
2-3-0Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
MODEL 100 (70T MTOW)
MODEL 100 (75.5T MTOW)
HEIGHT FROM GROUND
m ft m ft m ft
4.604.484.354.22
4.504.374.254.12
4.464.344.224.09
15.09 14.76 14.63
13.4213.5213.85
14.7014.27
14.3413.94
14.2413.85
4.07 3.97 3.95 12.9613.0213.354.01 3.91 3.89 12.7612.8313.163.75 3.65 3.64 11.9411.9812.30
HEIGHT FROM GROUND
m ft m ft m ft
4.624.494.374.23
4.494.374.244.11
4.474.354.234.10
15.16 14.73 14.67
13.1013.4813.88
14.7314.34
14.3413.91
14.2713.88
4.09 3.97 3.96 12.9913.0213.424.02 3.91 3.90 12.8012.8313.193.77 3.65 3.64 11.9411.9812.37
NPQRSTUVW
4.564.37
4.454.26
4.414.22
14.96 14.60 14.4714.34 13.98 13.85
4.584.38
4.444.25
4.424.23
15.03 14.57 14.5014.37 13.94 13.88
N_AC_020300_1_0140102_01_00
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
NPQRSTUVW
Ground ClearancesAileron Up and Spoilers 1 to 5 Extended (Sheet 2 of 2)
FIGURE-2-3-0-991-014-A01
2-3-0Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
D’ E’B’ C’A’ZX
F’ G’Y
N_AC_020300_1_0150101_01_00
HEIGHT FROM GROUND
m ft m ft m ft
3.06
3.36
3.61
2.98
3.28
3.53
2.99
3.27
3.52
10.04 9.78 9.81
11.5511.5811.84
11.02 10.76 10.73
3.86 3.78 3.75 12.3012.4012.66
2.552.97
2.482.89
2.502.91
8.37 8.14 8.209.74 9.48 9.55
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
XYZA’B’C’D’E’F’
MODEL 100 (64T MTOW)
4.10 4.01 3.98 13.0613.1613.45G’
Ground ClearancesSlats Extended (Sheet 1 of 2)FIGURE-2-3-0-991-015-A01
2-3-0Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
HEIGHT FROM GROUND
m ft m ft m ft2.562.973.06
3.36
2.472.882.97
3.27
2.492.902.98
3.26
8.40 8.10 8.17
10.7010.7311.02
9.7410.04
9.459.74
9.519.78
3.62 3.52 3.51 11.5211.5511.88
3.87 3.77 3.74 12.2712.3712.70
4.10 4.00 3.97 13.0213.1213.45
HEIGHT FROM GROUND
m ft m ft m ft2.572.983.07
3.37
2.472.882.97
3.26
2.492.892.97
3.26
8.43 8.10 8.17
10.7010.7011.06
9.7810.07
9.459.74
9.489.74
3.63 3.51 3.51 11.5211.5211.91
3.88 3.76 3.75 12.3012.3412.73
4.12 3.99 3.97 13.0213.0913.52
MODEL 100 (70T MTOW)
MODEL 100 (75.5T MTOW)
XYZ
B’C’
F’G’
A’
D’E’
N_AC_020300_1_0150102_01_00
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
MAXIMUM RAMPWEIGHT AFT CG
MAXIMUM RAMPWEIGHT FWD CG
A/C IN MAINTENANCECONFIGURATION
MID CG
XYZ
B’C’
F’G’
A’
D’E’
Ground ClearancesSlats Extended (Sheet 2 of 2)FIGURE-2-3-0-991-015-A01
2-3-0Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-0 Interior Arrangements
**ON A/C A319-100
Interior Arrangements
1. This section gives the standard interior arrangements configuration.
2-4-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1 Passenger Compartment Layout
**ON A/C A319-100
Typical Configuration
1. This section gives the typical interior configuration.
2-4-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
156
SE
AT
S A
LL T
OU
RIS
T C
LAS
S28
/30
in P
ITC
H. 6
AB
RE
AS
T. 3
.3
FW
D P
AS
SE
NG
ER
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
AF
T P
AS
SE
NG
ER
A A
A
A
G L
G L
A
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(2)
AA
TT
EN
DA
NT
SE
AT
(5)
N_AC_020401_1_0020101_01_02
Typical ConfigurationTypical Configuration Single-Class, High Density
FIGURE-2-4-1-991-002-A01
2-4-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
8 S
UP
ER
FIR
ST
CLA
SS
PA
SS
EN
GE
R S
EA
TS
(12
4 T
OT
AL)
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
116
EC
ON
OM
Y C
LAS
S
FIR
ST
36
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
N_AC_020401_1_0080101_01_00
G
A AL
LG
L
A
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(3)
AA
TT
EN
DA
NT
SE
AT
(3)
Typical ConfigurationTypical Configuration Two-Class
FIGURE-2-4-1-991-008-A01
2-4-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0 Passenger Compartment Cross Section
**ON A/C A319-100
Passenger Compartment Cross-section
1. This section gives the typical passenger compartment cross-section configuration.
2-5-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-0 Cargo Compartments
**ON A/C A319-100
Cargo Compartments
1. This section gives the cargo compartments locations, dimensions and loading combinations.
2-6-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
BU
LK C
AR
GO
CO
MP
AR
TM
EN
TF
WD
CA
RG
OC
OM
PA
RT
ME
NT
(2 C
ON
TA
INE
RS
)
AF
T C
AR
GO
CO
MP
AR
TM
EN
T(2
CO
NT
AIN
ER
S)
1.81
m(7
1.26
in)
3.35
m(1
31.8
9 in
)
7.67
m(3
01.9
7 in
)
1.81
m(7
1.26
in)
FR
24A
FR
34F
R47
FR
51/
FR
59F
R65
N_AC_020600_1_0020101_01_00
Cargo CompartmentsLocations, Dimensions and Loading Combinations
FIGURE-2-6-0-991-002-A01
2-6-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0 Door Clearances
**ON A/C A319-100
Doors Clearances
1. This section gives doors clearances.
2-7-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-1 Forward Passenger / Crew Doors
**ON A/C A319-100
Forward Passenger / Crew Doors
1. This section gives forward passenger / crew doors clearances.
2-7-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
0.03 m(1.18 in)
N_AC_020701_1_0020101_01_00
Doors ClearancesForward Passenger / Crew Doors
FIGURE-2-7-1-991-002-A01
2-7-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-2 Emergency Exits
**ON A/C A319-100
Emergency Exits
1. This section gives emergency exits doors clearances.
2-7-2Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
NOTE: ESCAPE SLIDE COMPARTMENT DOOROPENS ON WING UPPER SURFACE.
(FROM NOSE)12.83 m
(42 ft 1.11 in)
0.5 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
A
A
B
B
CL
(1ft 7.68 in)
0.85 m(2 ft 9.45 in)
(FRAME 47)B BA A
OPTIONAL
N_AC_020702_1_0030101_01_00
Doors ClearancesEmergency Exits
FIGURE-2-7-2-991-003-A01
2-7-2Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-3 Aft Passenger / Crew Doors
**ON A/C A319-100
Aft Passenger / Crew Doors
1. This section gives Aft passenger / crew doors clearances.
2-7-3Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
25.91 m(85 ft)
(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_0020101_01_00
Doors ClearancesAft Passenger / Crew DoorsFIGURE-2-7-3-991-002-A01
2-7-3Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-4 Forward Cargo Compartment Doors
**ON A/C A319-100
Forward Cargo Compartment Door
1. This section gives forward cargo compartment door clearances.
2-7-4Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
8.16 m(26 ft 9.25 in)
1.82 m(5 ft 11.65 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)
0.5 m(1 ft 7.68 in)
(FROM NOSE)
2−3
SEECHAPTER
A
A
FWD
A A
2.71 m(8 ft 10.69 in)
N_AC_020704_1_0020101_01_00
Doors ClearancesForward Cargo Compartment Door
FIGURE-2-7-4-991-002-A01
2-7-4Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-5 Aft Cargo Compartment Doors
**ON A/C A319-100
Aft Cargo Compartment Door
1. This section gives Aft cargo compartment door clearances.
2-7-5Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
20.58 m
(67ft 6.22 in)
1.82 m(5 ft 11.65 in)
(FROM NOSE)
FWD
A
A
1.6 m5 ft 2.93 in)
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
N_AC_020705_1_0020101_01_01
Doors ClearancesAft Cargo Compartment DoorFIGURE-2-7-5-991-002-A01
2-7-5Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-7 Main Landing Gear Doors
**ON A/C A319-100
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances.
2-7-7Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
NOTE: VALUE OF CG: 25% RC.
A
GROUND LINE
0.207 m(8.14 in)
0.485 m
(1 ft 7.09 in)
AIRCRAFT
1.23 m(4 ft 0.42 in)
0.14 m(5.51 in)
84°
1.942 m
(6 ft 4.45 in)
14.758 m(48 ft 5 in)
1.826 m(5 ft 11.88 in)
1.761 m(5 ft 9.32 in)
A
N_AC_020707_1_0020101_01_02
Doors ClearancesMain Landing Gear Doors
FIGURE-2-7-7-991-002-A01
2-7-7Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-8 Radome
**ON A/C A319-100
Radome
1. This section gives the radome clearances.
2-7-8Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
0.63 m(2 ft 0.79 in)
STA 3500FR1
65°
(5 ft 0.62 in)1.54 m
N_AC_020708_1_0020101_01_00
Doors ClearancesRadome
FIGURE-2-7-8-991-002-A01
2-7-8Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-9 APU and Nose Landing Gear Doors
**ON A/C A319-100
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances.
2-7-9Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
3.23
m(1
0 ft
7.16
in)
3.86
m(1
2 ft
7.96
in)
NOTE: VALUE OF CG : 25% RC.
1.5
m(4
ft 1
1 in
)
1.4
m(4
ft 7
.11
in)
FR80
FR84
N_AC_020709_1_0020101_01_00
Doors ClearancesAPU and Nose Landing Gear Doors
FIGURE-2-7-9-991-002-A01
2-7-9Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0 Escape Slides
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FWD CABIN ESCAPE SLIDE
OFF WING ESCAPE SLIDE
N_AC_020800_1_0030101_01_00
AFT CABINESCAPE SLIDE
Escape SlidesLocation
FIGURE-2-8-0-991-003-A01
2-8-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
EMERGENCY DESCENT DEVICETHROUGH WINDOW OPENING
GRID EQUALS 1 m (3.28 ft) IN REALITY
N_AC_020800_1_0040101_01_00
Escape SlidesDimensions
FIGURE-2-8-0-991-004-A01
2-8-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0 Landing Gear
**ON A/C A319-100
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 STA 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 a leg with a built-in shock absorber strut, carrying twin wheel withadequate 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
@A319AIRCRAFT 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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_020900_1_0060101_01_00
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
Landing GearMain Landing Gear - Twin Wheel (Sheet 1 of 2)
FIGURE-2-9-0-991-006-A01
2-9-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
DOORACTUATINGCYLINDER
FLAG
LOCKSTAYACTUATINGCYLINDER
GROUND LOCK SLEEVE
FLAG
BC
LOCKINGPIN
LOCKINGPIN
N_AC_020900_1_0060102_01_00
BOTTOM FILLING ANDCHARGING CONNECTIONMS28889
EDEXAMPLE
TOP FILLING AND CHARGING CONNECTION MS28889
Landing GearMain Landing Gear - Twin Wheel (Sheet 2 of 2)
FIGURE-2-9-0-991-006-A01
2-9-0Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_020900_1_0070101_01_00
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)
Landing GearMain Landing Gear Dimensions - Twin Wheel
FIGURE-2-9-0-991-007-A01
2-9-0Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_020900_1_0080101_01_00
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
Landing GearNose Landing Gear (Sheet 1 of 2)
FIGURE-2-9-0-991-008-A01
2-9-0Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
C
D
OPERATIONAL)
FLAG
DOWNLOCKSAFETY PIN
LOCKSTAY
B
CONNECTION MS28889FILLING AND CHARGING
N_AC_020900_1_0080102_01_00
Landing GearNose Landing Gear (Sheet 2 of 2)
FIGURE-2-9-0-991-008-A01
2-9-0Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_020900_1_0090101_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-2-9-0-991-009-A01
2-9-0Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
= =
==
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)
18.5
m(6
0.70
ft)
2.95
m(9
.68
ft)
3.76
m(1
2.34
ft)
3.79
m(1
2.43
ft)
6.49
m(2
1.29
ft)
2.5
m(8
.20
ft)7.
59 m
(24.
90 ft
)
MA
IN J
AC
KIN
G P
OIN
T
FROM X0
18.6
5 m
(61.
19 ft
)
FW
D J
AC
KIN
G P
OIN
T
MA
IN J
AC
KIN
G P
OIN
T
N_AC_020900_1_0220101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-022-A01
2-9-0Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
18
.65
m(6
1.19
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_0230101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-023-A01
2-9-0Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0 Exterior Lighting
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10
12
6 75 4
9
13
8
8
2
N_AC_021000_1_0050101_01_00
11
1
3
111
3
RH
LH
RH
LH
Exterior LightingFIGURE-2-10-0-991-005-A01
2-10-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021000_1_0060101_01_00
2
1 3
55
7
Exterior LightingFIGURE-2-10-0-991-006-A01
2-10-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021000_1_0070101_01_00
109
1313
11 11
4
12
6
Exterior LightingFIGURE-2-10-0-991-007-A01
2-10-0Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
8 8
1514
15
N_AC_021000_1_0180101_01_00
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
Exterior LightingFIGURE-2-10-0-991-018-A01
2-10-0Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0 Antennas and Probes Location
**ON A/C A319-100
Antennas and Probes Location
1. This section gives the location of antennas and probes.
2-11-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RADIO ALTIMETER(2)
RADIO ALTIMETER(1)
VHF(2)
DME(2)
DME(1)
PITOT PROBE(1)
PITOT PROBE(3)
TAT PROBE
VHF(1)
WEATHER RADAR
TAT PROBE
PITOT PROBE(2)
GPS(2)
GPS(1)TCAS TOP
ATC(1)
ADF(1)
ELT
VHF(3)
ATC(2)
EMERGENCY STATIC PROBE
AOA SENSOR(1)
LOCGLIDE
STATIC PROBE(2)STATIC PROBE(1)
TCAS BOTTOM
MARKER
HF
VOREMERGENCY STATIC PROBE
AOA SENSOR(2)
STATIC PROBE(2)
STATIC PROBE(1)
AOA SENSOR(3) STBY
NOTE: DEPENDING ON AIRCRAFT CONFIGURATION
ATC(4)
ATC(3)
N_AC_021100_1_0020101_01_00
Antennas and ProbesLocation
FIGURE-2-11-0-991-002-A01
2-11-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0 Power Plant
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIR INTAKE FIXEDON ACCESS DOOR
RH ACCESS DOOR
CUT OUT SEALED WITHLABYRINTH GASKET
FRONTFIREWALL
UPPERFIREWALL
FIREWALL RH
LOUVER LH
REARFIREWALL
CUT OUT SEALED WITHLABYRINTH GASKET
B
A
A
/FR80
/FR84
STA33561
STA35211
Z310
LH ACCESS DOORNOTE: NOT SHOWN FOR CLARITY315AL
316AR
N_AC_021200_1_0030101_01_00
Auxiliary Power UnitAccess Doors
FIGURE-2-12-0-991-003-A01
2-12-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
OIL
CO
OLE
R O
UT
LET
AIR
INT
AK
E D
UC
T
AP
U−
FU
EL−
LIN
E
AIR
INT
AK
E H
OU
SIN
G
DIV
ER
TE
R
FR
ON
T F
IRE
WA
LL
BLE
ED
AIR
LIN
E
FIR
E E
XT
ING
UIS
HIN
GB
OT
TLE
GE
NE
RA
TO
R
AP
U S
US
PE
NS
ION
(7 R
OD
S)
AP
U
FIR
E O
VE
RH
EA
T D
ET
EC
TO
R
AP
U S
US
PE
NS
ION
(7 R
OD
S)
EX
HA
US
TM
UF
FLE
R
B
N_AC_021200_1_0040101_01_00
/ FR
84
/ FR
80
/ FR
78
/ FR
77
ST
A35
211
ST
A33
561
ST
A32
923
ST
A32
811
/ FR
87S
TA
3637
9
Auxiliary Power UnitGeneral Layout
FIGURE-2-12-0-991-004-A01
2-12-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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 - IAE 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:- low pressure compressor (fan and booster) assembly- LP compressor/intermediate case- No. 4 bearing and combustion section- high pressure compressor- HP turbine section- LP turbine section- accessory drives (gear box).
2-12-0Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
The four stage Low Pressure Compressor (LPC) is driven by a five stage Low Pressure Turbine(LPT) and the ten stage High Pressure Compressor (HPC) by a two stage High PressureTurbine (HPT). The HPT also drives a gearbox which, in turn drives the engines and aircraftmounted accessories. The two shafts are supported by five main bearings.The V2500 incorporates a Full Authority Digital Engine Control (FADEC) which governs allengine functions, including power management. Reverse thrust for braking the aircraft afterlanding is supplied by an integrated system which acts 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 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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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_0190101_01_00
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-019-A01
2-12-0Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FAN COWL
CENTERBODY
FANREVERSER
6°
PRIMARYNOZZLE
9.6 m(31.5 m)
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)
BLOCKER DOOREXTENDED
C C
1.9 m(6.2 ft)
2.07 m(6.8 ft)
2.1 m(6.9 ft)
A A
B B D D
1.6 m(5.2 ft)
1.2 m(3.9 ft)
1.8 m(5.9 ft)
N_AC_021200_1_0200101_01_00
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-020-A01
2-12-0Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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_0210101_01_00
Power Plant HandlingFan Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-021-A01
2-12-0Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021200_1_0220101_01_00
3.7 m(12.1 ft)
3.3 m(10.8 ft)
35°45°
1 m(3.3 ft)
(3 ft)0.9 m
CAUTION
DO 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)
Power Plant HandlingThrust Reverser Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-022-A01
2-12-0Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021200_1_0230101_01_00
3 101 mm(122.1 in)
1 715 mm(67.5 in)
ACCESSORYDRIVE
FAN AND BOOSTER COMPRESSOR COMBUSTOR HP
TURBINE
LP
TURBINE
TURBINE
FRAME
1 067 mm(42.0 in)
FWD
A
A
Power Plant HandlingMajor Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-023-A01
2-12-0Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021200_1_0240101_01_00
0.5°6°
5.26 m(17.27 ft)
1.50 m(4.95 ft)
5.25 m(17.23 ft)
2.01 6.58 0.99 3.25 1.10 3.63 1.41 4.62
W U V PPS
m ft m ft m ft m ft
ATCOMPONENT
INLETATTACH FLG
TORQUE BOX"V" BLADE
COMB. CHAMBERENTRY FLG
COMB. CHAMBEREXIT FLG
TEC FLGTURB. EXIT CASE
AFT ENDCNA
2.01 6.58 1.00 3.29 1.11 3.64 2.59 8.50
1.98 6.50 0.97 3.19 1.07 3.52 3.26 10.70
1.93 6.32 0.93 3.06 1.03 3.39 3.63 11.90
1.64 5.38 0.78 2.57 0.86 2.83 4.60 15.10
1.24 4.07 0.60 1.96 0.64 2.11 −−−− −−−−
W
U
V
F
F
E
E
D
D
C
C
B
B
A
A
DISTANCE FROMTHE NOSE
9.52 m(31.23 ft)
A−A
B−B
C−C
D−D
E−E
F−F
ALL SIZES GIVEN ON THIS ILLUSTRATION ARE APPROXIMATENOTE:
Power Plant HandlingMajor Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-024-A01
2-12-0Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021200_1_0250101_01_00
2 m
(6.6 ft)
CLOSEDWL100
1.2 m(3.9 ft)
GROUND
WL100
3.9 m
(12.8 ft)
FWD VIEW
FAN COWLOPEN 50°
0.67 m(2.2 ft)
APPROXIMATE DIMENSIONSNOTE:
1.6 m(5.2 ft)
Power Plant HandlingFan Cowls - IAE V2500 Series Engine
FIGURE-2-12-0-991-025-A01
2-12-0Page 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021200_1_0260101_01_00
1.1 m(3.6 ft)
THRUST REVERSEROPEN 45°
0.67 m(2.2 ft)
2 m
(6.6 ft)
AFT VIEW
WL100CLOSED
3.6 m
(11.8 ft)
0.9 m(3 ft)
WL100
APPROXIMATE DIMENSIONSNOTE:
1 m(3.3 ft)
Power Plant HandlingThrust Reverser Halves - IAE V2500 Series Engine
FIGURE-2-12-0-991-026-A01
2-12-0Page 13
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0 Leveling, Symmetry and Alignment
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021300_1_0020101_01_00
2LH
2RH
RIB10
RIB10 FR54 FR57
FR34
FR28
11
12
Location of the Leveling PointsFIGURE-2-13-0-991-002-A01
2-13-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0 Jacking
**ON A/C A319-100
Jacking for Maintenance
1. Jacking for Maintenance
A. General
The A319 aircraft can be jacked:- at not more than the maximum permitted aircraft weight for jacking 57 000 kg (125 663 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 is such that the jack may be placedbeneath the airplane under the most adverse conditions, namely, tires deflated and shock absorbersdepressurized.
2-14-0Page 1
Jun 01/12
@A319AIRCRAFT 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 57 000 kg (125 663 lb).Centerline at 4.6 mm (0.18 in) parallel to the ground.
3. Shoring Cradles
When it is necessary to support the aircraft in order to relieve the loads on the structureaccomplishment of modifications or major work, it is advisable to provide for adapters under thewings and the fuselage for an alternative means of lifting.
NOTE : Aircraft must not be lifted or supported by the wings or fuselage alone without support ofthe other.
A. Under the Fuselage
Frames which are capable of supporting loads are noted below as well as the maximumpermissible loads for each frame.
Under the Fuselage
Shoring Fittings (Per Side)
FR 8 3 000 daN (6 744 lbf)
FR 15 5 000 daN (11 240 lbf)
FR 21 2 000 daN (4 496 lbf)
FR 30 1 700 daN (3 822 lbf)
FR 62/63 4 200 daN (9 442 lbf)
2-14-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Under the Fuselage
Shoring Cradles
FR 8 1 700 daN (3 822 lbf)
FR 9 3 300 daN (7 419 lbf)
FR 28 1 300 daN (2 923 lbf)
FR 60 2 600 daN (5 845 lbf)
Under the Fuselage
Safety Stay Pad
FR 73/74 2 000 daN (4 496 lbf)
B. Under the Wings
Shoring cradles are used when it is necessary to stress-jack the aircraft to carry out maintenanceand repair work. These are used to oppose the deflections of the wings and reduce the stressesto an acceptable level at the area of maintenance and repair.
The shoring cradles, each with two adjustable pads, 152.4 mm (6.00 in) square, are positionedat three locations under each wing. These locations are detailed in Table 5.
The adjustable pads are faced with thin rubber and contact the wing profile at the datumintersections of the ribs and the front and rear spars (F/S and R/S).
Table 5 shows the maximum load limit allowed at each jack pad when the wings are supportedby the cradles. These load limits apply to all A319 aircraft and variants.
The maximum permitted load, as specified in Table 5, is for a wing with its engines removed.When the wing(s) are held with the shoring cradles, and with the engines installed, the level ofshear stress caused (at the front spar) is not permitted. The weight of the engine can also causea torsion load that will lift the rear spar from its cradle.
Thus it is recommended that you remove the applicable engine(s) before you use the shoringcradles. However, for minor repairs the engine may be installed if its full weight is held.
It is important that the loads at each rib position are not exceeded because damage to theaircraft may occur.
2-14-0Page 3
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Maximum Allowable Load at each Jack Pad
Maximum Stress Relief Jacking Forces (LIMIT)
Rib 4 Rib 13 Rib 22Configuration
F/Spar R/Spar F/Spar R/Spar F/Spar R/Spar
Engine &MLGRemoved
790 daN(1 776 lbf)
1 330 daN(2 990 lbf)
670 daN(1 506 lbf)
550 daN(1 236 lbf)
320 daN(719 lbf)
380 daN(854 lbf)
EngineRemoved
530 daN(1 191 lbf)
2 510 daN(5 643 lbf)
610 daN(1 371 lbf)
610 daN(1 371 lbf)
310 daN(697 lbf)
380 daN(854 lbf)
4. Airplane Jacking for Removal/Installation of Landing Gear Shock Absorbers
For removal/installation of the nose gear shock absorber with the gear fully extended and the wheelsremoved, the fuselage longitudinal datum line must be not less than 5 300 mm (208.66 in) above theground.
For removal/installation of the main landing gear shock absorber, after removing the bogie beam, thefuselage longitudinal datum line must be not less than 5 210 mm (205.12 in) above the ground.
For reference, for landing gear swinging tests, the fuselage longitudinal datum line must be not lessthan 4 600 mm (181.10 in) above the ground.
2-14-0Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
28.83 m(94.59 ft)
2.74 m(8.99 ft)
15.97 m(52.40 ft)
6.5 m(21.33 ft)
WING JACKING
FWD JACKINGPOINT SAFETY
POINT
WING JACKING
CL
POINT
POINT
N_AC_021400_1_0050101_01_00
Jacking for MaintenanceJacking Point Location
FIGURE-2-14-0-991-005-A01
2-14-0Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
N_AC_021400_1_0060101_01_00
POINT A DETAIL
Z−1 979.8Z−1 987
FR8
A
SPHERICAL RADIUS19 mm (0.75 in)
B
B
Jacking for MaintenanceForward Jacking Point
FIGURE-2-14-0-991-006-A01
2-14-0Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
A
N_AC_021400_1_0070101_01_00
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)
EXAMPLE
B
B
Jacking for MaintenanceWing Jacking Points
FIGURE-2-14-0-991-007-A01
2-14-0Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
A
Z−748.44
SPHERICAL RADIUS 19 mm (0.75 in)(19 D535−71 595)
X =
31
372
AN_AC_021400_1_0080101_01_00
(4.97 in)
126.15 mm
Jacking for MaintenanceSafety Stay
FIGURE-2-14-0-991-008-A01
2-14-0Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
M
N
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
L M
1 560 mm(61.42 in)
2 846 mm(112.05 in)
3 072 mm(120.94 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)
2 920 mm(114.96 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_AC_021400_1_0090101_01_00
Jacking for MaintenanceJacking Design
FIGURE-2-14-0-991-009-A01
2-14-0Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
20
30
40
50
LOA
D O
N W
ING
JA
CK
ING
PO
INT
S (
kg x
1 0
00) 70
55
40 3530
2520
15
70
65
60
55
50
45
40
35
300 4 5 6 7 8 9 10
20
30
40
50
60
70
80
90
AIR
CR
AF
T W
EIG
HT
(kg
x 1
000
)
PERMISSIBLE WIND SPEED (km/h)
AIRCRAFT CG (%RC)50
45
TIP UPSECURITYMARGIN
LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1000)
60
321
ASSUME AIRCRAFT WITH GROSS WEIGHT OF 47 000 kg AND CENTER OF GRAVITYAT 18 % RC . THE REACTION AT THE WING JACKING POINTS IS 41 500 kg(20 750 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGEJACKING POINT IS 5 500 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE THE WIND
A
BC
D
EXAMPLE:
SPEED MUST NOT BE IN EXCESS OF 84 km/h.
B
C
D
A
N_AC_021400_1_0100101_01_00
Loads at the Aircraft Jacking PointsWing Jacking Point and Forward Fuselage Jacking Point
FIGURE-2-14-0-991-010-A01
2-14-0Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
(SAFETY STAY)FR73 FR74/
FR60
FR9
FR28
RIB4
RIB13
RIB22
RIB13
RIB22
RIB4
N_AC_021400_1_0110101_01_00
NOTE:THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
Jacking for MaintenanceLocation of Shoring CradlesFIGURE-2-14-0-991-011-A01
2-14-0Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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 57 000 kg (125 663 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 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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 JACKTWIN WHEEL TRACK IS 927 mm (36.5 in).
WITH 2 FLAT TIRES.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_0170101_01_00
INFLATED TIRES
FLAT TIRES
Landing Gear Jacking for Wheel ChangeMLG Jacking Point Location - Twin Wheels
FIGURE-2-14-0-991-017-A01
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Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021400_1_0180101_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)APPROX
409 mm(16.1 in)
218 mm (8.58 in)(180 mm (7.09 in)
ON RIM)
552 mm(21.73 in)
FWD
MIN25 mm(1 in)
Landing Gear Jacking for Wheel ChangeMLG Jacking with Cantilever Jack - Twin Wheels
FIGURE-2-14-0-991-018-A01
2-14-0Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_021400_1_0190101_01_00
x1 000 lb
x1 000 kg
AIRCRAFT WEIGHTMODEL 100
70 80 90 100 110 120 130 140 150 160 170 180
30 8040 50 60 70
5
10
15
20
25
30
35
40
40%
30%25%20%14%
CGPOSITION
LOAD AT MLGJACKING POINT
1 000 kg
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking Points - Twin Wheels
FIGURE-2-14-0-991-019-A01
2-14-0Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
36.0% CG
26.0% CG
21.0% CG
14.0% CG
45 50 55 60 65 70 75 8018
20
22
24
26
28
30
32
34
36
LOAD AT MLGJACKING POINT
1 000 kg
CGPOSITION
N_AC_021400_1_0200101_01_00
x1 000 lb
x1 000 kg
180170160150140130120110100
AIRCRAFT WEIGHT
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking Points - 75 500 kg
FIGURE-2-14-0-991-020-A01
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Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
APPROX326 mm
(12.83 in)DIA. BALL
SAE AS 33559
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
FWD
N_AC_021400_1_0210101_01_00
A
A
25 mm(1 in)
38 mm(1.5 in)
198 mm(7.8 in)
Landing Gear Jacking for Wheel ChangeNLG Jacking - Point LocationFIGURE-2-14-0-991-021-A01
2-14-0Page 17
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
x1 000 kg
AIRCRAFT WEIGHTMODEL 100
30 8040 50 60 70
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
CGPOSITION
14%
20%
25%
30%
40%
N_AC_021400_1_0220101_01_00
180170160150140130120110100908070x1 000 lb
LOAD AT NLGJACKING POINT
1 000 kg
Landing Gear Jacking for Wheel ChangeLoads at NLG Jacking PointsFIGURE-2-14-0-991-022-A01
2-14-0Page 18
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
36.0% CG
26.0% CG
21.0% CG
14.0% CG
45 50 55 60 65 70 75 803
4
5
6
7
8
9
10
11
12
LOAD AT NLGJACKING POINT
1 000 kg
CGPOSITION
N_AC_021400_1_0230101_01_00
x1 000 lb
x1 000 kg
180170160150140130120110100
AIRCRAFT WEIGHT
Landing Gear Jacking for Wheel ChangeLoads at NLG Jacking Points - 75 500 kg
FIGURE-2-14-0-991-023-A01
2-14-0Page 19
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0 General Information
**ON A/C A319-100
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) forCFM56-5A, CFM56-5B and IAE V2500 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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-0 Payload / Range
**ON A/C A319-100
Payload / Range
1. Payload / Range
3-2-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1 ISA Conditions
**ON A/C A319-100
ISA Conditions
1. This section gives the payload / range at ISA conditions.
3-2-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
50 40 30 20 10 0
20 10 00
1000
2000
3000
4000
010
0020
0030
0040
0050
0060
0070
00
(100
0 lb
)(1
000
kg)
PA
YLO
AD
RA
NG
E(K
M)
RA
NG
E(N
M)
MA
X T
AK
E−
OF
F W
EIG
HT
145
504
lb(6
6 00
0 kg
)
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
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
124
PA
SS
EN
GE
RS
64t
75.5
t
70t
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
:
N_AC_030201_1_0030101_01_00
Payload / RangeCFM56-5A series engine
FIGURE-3-2-1-991-003-A01
3-2-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
50 40 30 20 10 0
20 10 00
1000
2000
3000
4000
010
0020
0030
0040
0050
0060
0070
00
(100
0 lb
)(1
000
kg)
PA
YLO
AD
RA
NG
E(K
M)
RA
NG
E(N
M)
MA
X T
AK
E−
OF
F W
EIG
HT
145
504
lb(6
6 00
0 kg
)
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
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
124
PA
SS
EN
GE
RS
64t
75.5
t
70t
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
:
N_AC_030201_1_0040101_01_00
Payload / RangeCFM56-5B series engine
FIGURE-3-2-1-991-004-A01
3-2-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
50 40 30 20 10 0
20 10 00
1000
2000
3000
4000
010
0020
0030
0040
0050
0060
0070
00
(100
0 lb
)(1
000
kg)
PA
YLO
AD
RA
NG
E(K
M)
RA
NG
E(N
M)
MA
X T
AK
E−
OF
F W
EIG
HT
145
504
lb(6
6 00
0 kg
)
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
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
124
PA
SS
EN
GE
RS
64t
75.5
t
70t
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
:
N_AC_030201_1_0050101_01_00
Payload / RangeIAE V2500-A5 series engineFIGURE-3-2-1-991-005-A01
3-2-1Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-0 FAR / JAR Takeoff Weight Limitation
**ON A/C A319-100
FAR / JAR Take-off Weight Limitation
1. FAR / JAR Take-off Weight Limitation
3-3-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1 ISA Conditions
**ON A/C A319-100
ISA Conditions
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
86420
N_AC_030301_1_0030101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA Conditions -- CFM56 series engine
FIGURE-3-3-1-991-003-A01
3-3-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
0
86
24
N_AC_030301_1_0040101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA Conditions -- IAE V2500 series engine
FIGURE-3-3-1-991-004-A01
3-3-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2 ISA +15˚C (+59˚F) Conditions
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
0
8642
N_AC_030302_1_0030101_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-3-3-2-991-003-A01
3-3-2Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
0
86
24
N_AC_030302_1_0040101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- IAE V2500 series engine
FIGURE-3-3-2-991-004-A01
3-3-2Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-0 FAR / JAR Landing Field Length
**ON A/C A319-100
FAR / JAR Landing Field Length
1. FAR / JAR Landing Field Length
3-4-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1 ISA Conditions
**ON A/C A319-100
ISA Conditions
1. This section gives the landing field length.
3-4-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
3.0
3.5
4.0
4.5
5.0
5.5
6.0
160140120100806040GROSS WEIGHT
(1000 lb)
F.A
.R L
AN
DIN
G L
EN
GT
H (
1000
ft)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
ISA CONDITIONSSLATS 27 DEG.FLAPS 35 DEG.
PRESSURE ALTITUDE(1000 ft)
10
6
SEA
4 2
8
LEVEL
N_AC_030401_1_0030101_01_00
FAR / JAR Landing Field LengthCFM56-5A series engine
FIGURE-3-4-1-991-003-A01
3-4-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
5.5
5.0
4.5
4.0
3.5
3.0160
GROSS WEIGHT(1000 lb)140120100806040
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
10 8 6 4 2SEA
PRESSURE ALTITUDE(1000 ft)
ISA CONDITIONSSLATS 27 DEG.FLAPS 35 DEG.
LEVEL
N_AC_030401_1_0040101_01_00
F.A
.R L
AN
DIN
G L
EN
GT
H (
1000
ft)
FAR / JAR Landing Field LengthIAE V2500 series engine
FIGURE-3-4-1-991-004-A01
3-4-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0 Final Approach Speed
**ON A/C A319-100
Final Approach Speed
1. This section gives the final approach speed.
3-5-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
20018016014012010080100
110
120
130
140
150
160
170
C.A.S. (Kts)
GROSS WEIGHT(1000 lb)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 35DEG.
SEA LEVEL
N_AC_030500_1_0030101_01_00
Final Approach SpeedCFM56-5A series engine
FIGURE-3-5-0-991-003-A01
3-5-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
20018016014012010080100
110
120
130
140
150
160
170
C.A.S. (Kts)
GROSS WEIGHT(1000 lb)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 35 DEG.
SEA LEVEL
N_AC_030500_1_0040101_01_00
Final Approach SpeedIAE V2500 series engine
FIGURE-3-5-0-991-004-A01
3-5-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0 Turning Radii
**ON A/C A319-100
Turning Radii
1. This section gives the turning radii.
4-2-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
R4
R6
R5
R3
R2
R1
60°70°
NOTE:
1.
2.
TURN TYPE:
ASYMMETRIC THRUST DIFFERENTIALBRAKING (PIVOTTING ON ONE MAIN GEAR).
SYMMETRIC THRUST NO BRAKING.
FOR STEERING DIMENSION TABLE SEE SHEET 2.
N_AC_040200_1_0030101_01_02
50°
11.04 m(36.22 ft)
7.59 m(24.9 ft)
Turning Radii, No Slip AngleFIGURE-4-2-0-991-003-A01
4-2-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
GA
NG
LE(d
eg)
TY
PE
TU
RN
OF
WIN
GT
IPF
EN
CE
SH
AR
KLE
T
R4
− W
ING
NO
SE
75 (
MA
X)
706560555045403525 3020 7067
.79.
030
1.4
0.8
1.6
2.6
3.8
5.2
6.7
8.5
10.6
16.7
13.3
21.4
28.2
51
12.1
403940414346495359667689110
22.0
7270737680848995102
111
122
137
159
22.8
7516
.755
20.0
66
70.3
66.9
62.5
57.9
53.2
48.4
43.6
38.8
29.1
33.9
24.3
19.4
8.4
9.2
10.2
11.4
12.7
14.3
16.1
18.2
24.3
20.9
29.0
35.8
283034374247536080 6995117
359131722283555 447092
222222222222
11.8
12.2
12.6
13.2
14.0
15.0
16.3
17.9
20.1
23.0
27.2
33.5
21.4
22.2
23.2
24.4
25.7
27.2
29.0
31.1
33.7
37.1
41.8
48.6
22.3
23.0
24.0
25.2
26.5
28.0
29.8
31.9
34.6
38.0
42.6
49.4
73767983879298105
113
125
140
162
16.6
16.8
17.1
17.5
18.1
18.9
19.8
21.2
23.0
25.6
29.3
35.2
5455565859626569758496116
19.7
20.1
20.7
21.4
22.3
23.3
24.6
26.2
28.3
31.1
35.1
41.2
656668707376818693102
115
135
75 (
MA
X)
65605550
0.5
2.5
3.7
5.1
6.6
3841434649
6976808489
71.9
63.1
58.3
53.5
48.6
8.1
10.1
11.3
12.6
14.2
2733374147
28121722
11111
11.7
12.5
13.2
14.0
14.9
21.1
23.1
24.3
25.6
27.1
22.0
23.9
25.1
26.4
28.0
7278828792
16.5
17.1
17.5
18.1
18.8
5456575962
19.6
20.6
21.3
22.2
23.2
6468707376
N_AC_040200_1_0040101_01_01
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
:
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-4-2-0-991-004-A01
4-2-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A319-100
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_040300_1_0020101_01_02
R6
R3
R5
R4
11.0 m
PAVEMENTWIDTH FOR180° TURN
MINIMUM
(36 ft)
STEERINGANGLE 75°
A
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 ALL 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
71.9°
70.3°
m
m
ft
ft
Y
3.6
3.9
12
13
A
20.1
20.5
66
67
R3NLG
11.7
11.8
38
39
R4 WINGWING TIPFENCE
21.1
21.4
69
70
SHARKLET
22.0
22.3
72
73
R5NOSE
16.5
16.6
54
54
R6THS
19.6
19.7
64
65
NO DIFFERENTIAL BRAKING.DRY SURFACE.
EFFECTIVETURN
Y
OUTSIDE FACE OF TIRE
Minimum Turning RadiiFIGURE-4-3-0-991-002-A01
4-3-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A319-100
Visibility from Cockpit in Static Position
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A319-100
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A319-100
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FAA LEAD−IN FILLET
L = 45 m (150 ft)
TAXIWAYCENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
APPROX 5.1 m(17 ft)
30 m
NOTE: FAA GROUP III FACILITIES.
RUNWAY CENTERLINE
NLG PATH
MLG PATH
15 m(50 ft)
(100 ft)
N_AC_040501_1_0020101_01_02
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-002-A01
4-5-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FAA LEAD−IN FILLET
L = 45 m (150 ft)
RUNWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
APPROX 3.2 m(10 ft)
TAXIWAYCENTERLINE
30 m
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATH
15 m(50 ft)
(100 ft)
N_AC_040501_1_0030101_01_02
135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-1-991-003-A01
4-5-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A319-100
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
APPROX 6.4 m(21 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_0020101_01_01
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-002-A01
4-5-2Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
APPROX 9 m(29 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_0030101_01_01
90˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-2-991-003-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A319-100
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
30 m(100 ft)
NOTE: TYPE 1 VALUES.
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
RUNWAY CENTERLINE
R3 = 11.7 m(39 ft)
R5 = 16.5 m(55 ft)
R4
3 m(10 ft)
6.6 m(22 ft)
N_AC_040503_1_0010101_01_02
WINGTIP FENCES:R4 = 21.1 m (70 ft)SHARKLETS:R4 = 22 m (72 ft)
180˚ Turn on a RunwayEdge of Runway Method (Sheet 1 of 2)
FIGURE-4-5-3-991-001-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
30 m(100 ft)
NOTE: TYPE 1 VALUES.
RUNWAY CENTERLINE
5.22 m(17 ft)
4.75 m(16 ft)
25°
N_AC_040503_1_0010102_01_00
R3 = 11.7 m(38 ft)
R5 = 16.5 m(55 ft)
R4
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
WINGTIP FENCES:R4 = 21.1 m (70 ft)SHARKLETS:R4 = 22 m (72 ft)
180˚ Turn on a RunwayCenter of Runway Method (Sheet 2 of 2)
FIGURE-4-5-3-991-001-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4 135˚ Turn - Taxiway to Taxiway
**ON A/C A319-100
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway.
4-5-4Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FAA LEAD−IN FILLET
APPROX 5.8 m(19 ft)
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
15 m(50 ft)
15 m(50 ft)
N_AC_040504_1_0050101_01_00
L = 45 m (150 ft)
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-4-991-005-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
FAA LEAD−IN FILLET
TURN R = 30 m
FILLET R = 16.5 m
APPROX 3.3 m(11ft)
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
15 m(50 ft)
15 m(50 ft)
N_AC_040504_1_0050102_01_00
(55 ft)
(100 ft)
L = 45 m (150 ft)
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-4-991-005-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5 90˚ Turn - Taxiway to Taxiway
**ON A/C A319-100
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-5Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATHTAXIWAY CENTERLINE
APPROX 6.1 m(20 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft)
N_AC_040505_1_0030101_01_00
15 m(50 ft)
15 m(50 ft)
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-5-991-003-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATHTAXIWAY CENTERLINE
APPROX 9 m(29 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft)
N_AC_040505_1_0030102_01_00
15 m(50 ft)
15 m(50 ft)
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-5-991-003-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A319-100
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
4-6-0Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RUNWAY CENTERLINETAXIWAY
CENTERLINE
HOLDING POINT
90 m
NOTE: LAYOUT IN ACCORDANCE WITH THE REQUIREMENTS OF NAS 3601, CHAPTER 4,AND AN/865, CHAPTER 3.OUTER PARKED AIRCRAFT TURNED THRU MIN. TURN RADIUS TO PARKED POSITION.
N_AC_040600_1_0020101_01_02
61 m(200 ft)
23 m(75 ft)
45 m(150 ft)
6.1 m(20 ft)
6.1 m(20 ft)
190 m(625 ft)
12.2 m(40 ft)
(300 ft)
Runway Holding Bay (Apron)FIGURE-4-6-0-991-002-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0 Parking
**ON A/C A319-100
Airplane Parking
1. The following figures and charts show the rectangular space required for parking against the terminalbuilding.
AIRPLANE MODEL MAX. EFF. STEERING MIN. LINE UP DISTANCE
90˚ TURN ANGLE DEGREESTODAm (ft)
ASDAm (ft)
A319 6912.07(39.6)
23.11(75.8)
AIRPLANEMODEL
MIN. LINE UP DISTANCE
REQUIREDMIN.
PAVEMENTWIDTH
NOMINAL LINE UP DISTANCE
180˚ TURNTODAm (ft)
ASDAm (ft)
m (ft)TODAm (ft)
ASDAm (ft)
A31915.34(50.3)
26.38(86.5)
27.4(89.9)
21.58(70.8)
32.62(107.0)
Abbreviations:- TODA (Take-Off Distance Adjustment)- ASDA (Accelerate-Stop Distance Adjustment)
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
RUNWAY WIDTH 60.00 m
ED
GE
OF
RU
NW
AY
29.3
5 m
(REF)
18.3
1 m
END OF RUNWAY
NOTE:
3.05
m(R
EF
)
69° STEERING AND NO SLIP ON NLG TIRES.
(10.
0 ft)
(96
ft 3.
6 in
)
(60.
0 ft)
(196 ft 10.8 in)
3.05 m(10.0 ft)
N_AC_040700_1_0090101_01_01
Runway Length AlterationsLine Up Distances -- 90˚ TurnFIGURE-4-7-0-991-009-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
END OF RUNWAY
EDGE OFRUNWAY
27.41 m(90.0 ft)
16.60 m(54 ft 6 in)
3.05 m(10.0 ft)(REF)3.05 m
(10.0 ft)
NOTES: 69° STEERING AND NO SLIP ON NLG TIRES.
32.62 m(107.0 ft)
21.58 m(70 ft 9.6 in)
(REF)
3.05 m(10.0 ft)(REF)
N_AC_040700_1_0100101_01_01
Runway Length AlterationsLine Up Distances -- 180˚ Turn
FIGURE-4-7-0-991-010-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
**ON A/C A319-100
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.
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-0 Servicing Arrangements
**ON A/C A319-100
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.
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A319-100
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
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2 Typical Ramp Layout - Open Apron
**ON A/C A319-100
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 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).
5-1-2Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_050102_1_0020101_01_03
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6
BULK
BULK
CAT
CAT
LV
FUEL
WV
ASTOW
GPU
CB
CB
PS
PS
AC
Typical Ramp LayoutOpen Apron - Bulk LoadingFIGURE-5-1-2-991-002-A01
5-1-2Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_050102_1_0080101_01_00
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6
CAT
CAT
LV
ULD
FUEL
ULD
WV
ASTOW
GPU
PS
PS
LD CL
LD CL
AC
Typical Ramp LayoutOpen Apron - ULD LoadingFIGURE-5-1-2-991-008-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3 Typical Ramp Layout - Gate
**ON A/C A319-100
Typical Ramp Layout - Gate
1. This section gives 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
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_050103_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
LV
ULD
FUEL
ULD
PBB
WV
TOW
GPU
N_AC_050103_1_0010101_01_03
LD CL
LD CL
AS
AC
Typical Ramp LayoutGate
FIGURE-5-1-3-991-001-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0 Terminal Operations - Full Servicing
**ON A/C A319-100
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 HANDLING124 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:- 124 pax at door L1- Deboarding rate = 22 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 124 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 cargo loadersEquipment positioning/removal + opening/closing door = +1 min
Cargo exchange:- FWD cargo compartment: 2 LD3- AFT cargo compartment: 2 LD3
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
C. REFUELLING2 hoses, one side
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@A319AIRCRAFT 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. 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
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
0 5 15 20 25 30 35 40
TRT: 36 min
10
HEADCOUNTING
CATERING AT DOOR R2
CLEANING
CARGO FWD CC
REFUELLING
TOILET SERVICING
CARGO AFT CC
CATERING AT DOOR R1
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
DEBOARDING/BOARDING AT DOOR L1
POTABLE WATERSERVICING
N_AC_050200_1_0050101_01_01
min
AVAILABLE TIME
Turn Round StationsFull Servicing (36 Min.)
FIGURE-5-2-0-991-005-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0 Terminal Operation - Transit
**ON A/C A319-100
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 HANDLING156 pax, all Y/C2 Stairways used at doors L1 & L2Equipment positioning/removal + opening/closing door = 2 min
Deboarding:- 78 pax at door L1- 78 pax at door L2- Deboarding rate = 20 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 78 pax at door L1- 78 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 cargo loadersEquipment positioning/removal + opening/closing door = +1 min
Cargo exchange:- FWD cargo compartment: 2 LD3- AFT cargo compartment: 2 LD3
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
C. REFUELLING2 hoses, one side6624 l (1750 US gal) at 50 psi (3 bar)Dispenser positioning/removal = 4 min
D. CLEANINGNo cleaning
E. CATERINGNo catering
F. GROUND HANDLING SERVICINGStart of operations:- Bridges: t0 = 0- Other equipment: t = t0 + 1 minNo potable water servicingNo toilet servicing
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
0 5 15 20 25 3010
TRT: 21 min
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
AVAILABLE TIME
AVAILABLE TIME
min
N_AC_050300_1_0020101_01_01
HEADCOUNTING
CATERING
CLEANING
CARGO FWD CC
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CARGO AFT CC
DEBOARDING/BOARDING AT DOOR L1
DEBOARDING/BOARDING AT DOOR L2
Turn Round StationsMinimum Servicing (21 Min.)FIGURE-5-3-0-991-002-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-0 Ground Service Connections
**ON A/C A319-100
Ground Service Connections
1. Ground Service Connections.
5-4-0Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-1 Ground Service Connections Layout
**ON A/C A319-100
Ground Service Connections Layout
1. This section gives the ground service connections layout.
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1 3 11 12 2 4 14−
1 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 −
13
10
10
13
67
6
7
6 7−
5 8 12 4
29
N_AC_050401_1_0020101_01_01
Ground Service ConnectionsGround Service Connections Layout
FIGURE-5-4-1-991-002-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-2 Grounding Points
**ON A/C A319-100
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:
16.11 m(52.85 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
On right Main LandingGear leg:
16.11 m(52.85 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.
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
(2)(1)
GROUND CABLE(OPTIONAL)
LANDINGGEAR
NOSE LANDING GEAR
MAIN LANDING GEAR
(1)
A
A
A
(1)
N_AC_050402_1_0030101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-003-A01
5-4-2Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
NOTE: R SIDE SYMMETRICAL
A
RIB20
RIB19
B
FWD
A
A
FOR SPECIFICATIONS REFERTO FLIGHT MANUAL
BN_AC_050402_1_0040101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-004-A01
5-4-2Page 3
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3 Hydraulic System
**ON A/C A319-100
Hydraulic System
1. Access.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green System:Access door 197CB
17.57(57.64)
1.27(4.17)
1.76(5.77)
Yellow System:Access door 198CB
17.57(57.64)
1.27(4.17)
1.76(5.77)
Blue System:Access door 197EB
18.92(60.07)
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 195BB14.05(46.1)
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
14.5(47.57)
0.25(0.82)
1.99(6.53)
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@A319AIRCRAFT 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
15.67(51.41)
0.25(0.82)
3.2(10.5)
Blue Systemaccumulator:Access door 195BB
14.31(46.95)
0.25(0.82)
1.99(6.53)
Yellow System brakingaccumulator:Access door 196BB
14.5(47.57)
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 197CB17.57(57.64)
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 196BB -198CB
14.5(47.57)
1.43(4.69)
1.90(6.23)
Green System:Left MLG door
15.67(51.41)
1.27(4.17)
2.61(8.56)
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@A319AIRCRAFT 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 197EB
18.92(62.07)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.On 3/8 in. self-sealing connection for the Blue system on:- Blue system ground service panel.
6. Ground Test.On each ground service panel:- One self-sealing connector AE80532N (suction).- One self-sealing connector AE80531K (delivery).
5-4-3Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-3Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-3Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-3Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4 Electrical System
**ON A/C A319-100
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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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- Radio navigation: 1.2 KVA.
5-4-4Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-5 Oxygen System
**ON A/C A319-100
Oxygen System
1. Oxygen System.
DISTANCE: Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDOne service connection(external charging in theavionics compartment)MS22066 Std.
3.45 m(11.32 ft)
1.15 m(3.77 ft)
2.60 m(8.53 ft)
3/8” UNF × 24 TPI
Nominal pressure: 1850 psi (127.55 bar)
Max fill pressure: 2035 psi (140.31 bar)
NOTE : Internal charging connection provided.
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Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-6 Fuel System
**ON A/C A319-100
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
14.8(48.56)
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)
15.99(52.46)
9.83(32.25)
3.65(11.98)
Refuel/Defuel coupling,RightAccess Door 622HB
15.99(52.46)
9.83(32.25)
3.65(11.98)
Gravity Refuel Coupling17.5(57.41)
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).
5-4-6Page 1
Jun 01/12
@A319AIRCRAFT 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 18.76(61.55)
14.9(48.88)
14.9(48.88)
4.32(14.17)
NACA Flame Arrestor 18.2(59.71)
13.7(44.95)
13.7(44.95)
4.02(13.19)
NOTE : Distances are approximate.
5-4-6Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-6Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-6Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7 Pneumatic System
**ON A/C A319-100
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
11.38(37.34)
0.84(2.76)
1.76(5.77)
NOTE : Distances are approximate.
A. Connector- One standard 3 in. ISO TC20 connection (MS33740) for engine starting and cabin air
preconditioning (HP) installed on the left side of the belly fairing
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
10.85(35.6)
1.11(3.64)
1.73(5.68)
NOTE : Distances are approximate.
A. Connector:- One standard 8 in. connection (SAE AS4262 type B) for cabin air preconditioning (LP)
installed on the left side of the belly fairing
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Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8 Potable Water System
**ON A/C A319-100
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:
27.5(90.22)
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:
11.8(38.71)
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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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
D. Typical flow rate:- 50 l/min (13.21 US gal/min).
5-4-8Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-8Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9 Oil System
**ON A/C A319-100
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)
11.56(37.79)
6.63(21.75)
4.82(15.81)
1.46(4.79)
Engine Oil PressureFilling Port:
11.4(37.4)
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: OMP 2506-18 plus one connection overflow: OMP2505-18.
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)
10.6(34.77)
6.9(22.64)
5.52(18.11)
0.68(2.23)
NOTE : Distances are approximate
5-4-9Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
A. Tank capacity: 5 l (1.32 US gal)
B. Delivery pressure required: 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:
11.04(37.4)
5.3(17.39)
6.2(20.34)
0.76(2.49)
NOTE : Distances are approximate
A. Tank capacity: 0.8 l (0.21 US gal)
4. Engine Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5---9-99--004-B):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 437BL(LH),447BL (RH)
10.64(34.9)
6.56(21.52)
4.92(16.14)
1.22(4)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 28 l (7.4 US gal)- Usable: 23.50 l (6.21 US gal)
1. IDG Oil Replenishment for IAE V2500 Series Engine:One pressure filling connection per engine: OMP 2506-2 plus one overflow connection: OMP 2505-2.
5-4-9Page 2
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@A319AIRCRAFT 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:
11.2(36.74)
5.42(17.78)
6.04(19.81)
0.8(2.62)
NOTE : Distances are approximate
A. Tank capacity: 4.1 l (1.08 US gal)
5. Starter Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5---9-99--006-B):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:
11.04(37.4)
5.3(17.39)
6.14(20.14)
0.75(2.46)
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 36-30031.76(104.19)
0.3(0.98)
4.83(15.85)
APS 320031.76(104.19)
0.3(0.98)
4.78(15.68)
131-931.66(103.87)
0.35(1.15)
4.32(14.17)
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)
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- APU type 131-9: 6.25 l (1.65 US gal)
5-4-9Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-9Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-9Page 7
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
’FULL’ LEVEL NOTCH27.3 LT29.0 US QTS6.0 IMP GAL(WITHIN 60 MIN FROM SHUTDOWN)
NOTCH ’3’20 LT22 US QTS4.5 IMP GAL
NOTCH ’1’26 LT27 US QTS5.7 IMP GALNOTCH ’2’
23 LT24 US QTS5.1 IMP GAL
FCOC
PRISMALITELEVEL INDICATOR
OIL TANK
GRAVITYFILLER CAP
ACCESS PANEL: 437BL (LEFT)447BL (RIGHT)
B
A
A
B
FWD
N_AC_050409_1_0040201_01_00
Ground Service ConnectionsEngine Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-9-991-004-B01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
THE OIL LEVEL MUST NOT BE INTHE YELLOW BAND BUT IT CANBE IMMEDIATELY ABOVE THELOWER LIMIT OF THE YELLOWBAND BECAUSE OF THE AIRCRAFTRAMP ANGLE
DO THE IDG SERVICINGTO GET THE CORRECT IDGOIL LEVEL.
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
INCORRECTLY FILLED IDG
THE OIL LEVEL MUST NOT BEIN THE RED BAND
PERFORM IDG OIL SERVICINGTO GET THE CORRECT IDG OIL LEVEL.DO NOT USE THE OVERFLOW DRAIN HOSETO GET THE CORRECT IDG OIL LEVEL.
AT ALL TIMES(HOT OR COLD OIL/IDG)
OIL LEVEL CAN BEIN THE GREEN BAND OR THEYELLOW BAND
AFTER ENGINESHUTDOWN
CORRECTLY FILLED IDG
OIL LEVELINDICATOR
DUST CAPPRESSUREFILL HOSE
OIL LEVEL MUST BE AT OR NEARTHE LINE BETWEEN THE YELLOW BANDAND THE GREEN BAND
(HOT OIL/IDG)
PRESSUREFILL VALVE
DUST CAP
OVER FLOWDRAIN VALVE
OVER FLOWDRAIN HOSE
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
IDG
B
BB
A
B
A
B
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
N_AC_050409_1_0050201_01_00
Ground Service ConnectionsIDG Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-9-991-005-B01
5-4-9Page 9
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
OIL OVERFLOWPOINT
SIGHT GLASS
EXTERNAL GEARBOX
OIL FILLING POINT
ADAPTER
B
A
B
THE STARTER IS FULL WHEN THE OIL LEVELSHOWS NOT LESS THAN 3/4 FULL
ON THE SIGHT GLASS
*
PNEUMATIC STARTERA
*
N_AC_050409_1_0060201_01_00
Ground Service ConnectionsStarter Oil Tank -- IAE V2500 Series Engine
FIGURE-5-4-9-991-006-B01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-9Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10 Vacuum Toilet System
**ON A/C A319-100
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
27.5(90.22)
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).
5-4-10Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
5-4-10Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A319-100
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--002-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
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
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
N_AC_050500_1_0020101_01_00
Engine Starting Pneumatic RequirementsFIGURE-5-5-0-991-002-A01
5-5-0Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-1 Low Ambient Temperatures
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_050501_1_0030101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
220°C
200°C
150°C
100°C
50°C
0°C
100
90
80
70
60
50
40
30 2
Z = 8000 ftSEA LEVEL
2.5
3
4
3.5
5
6
7
6.5
5.5
4.5
ESTIMATED STARTINGTIMES UP TO IDLE
30 40 50 60 70 80 90 100 110 120
AIR FLOW REQUIRED AT GROUND CONNECTION
kg/mn
MIN. PRESSUREAT GROUND CONNECTION: 33 PSIG
RECOMMENDED PRESSURE:38 PSIG ATGROUND CONNECTION
SEA LEVEL
Z = 8000 ft
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
MAXIM
UM T
EMPERATURE L
IMIT
35s
40s
50s
60s70s
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- CFM56 series engine
FIGURE-5-5-1-991-003-A01
5-5-1Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
TIMES UP TO IDLEESTIMATED STARTING
MAXIMUM T
EMPERATURE LIMIT
30
40
50
60
70
80
90
6
5
4
3
2
0°C
50°C
100°C
150°C
200°C220°C
40 50 60 70 80 90 100 110 120
MAXIMUM DUCT PRESSURE
AIR FLOW REQUIRED AT GROUND CONNECTION
70s
75s
60s
65s
N_AC_050501_1_0040101_01_00
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- IAE V2500 series engine
FIGURE-5-5-1-991-004-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-2 Medium Ambient Temperatures
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_050502_1_0030101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
PRESSURE: 33 PSIG ATRECOMMENDED
GROUND CONNECTION:MIN PRESSURE AT
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
22 PSIG
GROUND CONNECTION
TIMES UP TO IDLEESTIMATED STARTING
0°C
50°C
100°C
150°C
200°C
220°C
30
40
50
60
70
80
90
100
2
3
4
5
6
7
6.5
5.5
4.5
2.5
3.5
30 40 50 60 70 80 90 100 110 120
35s
40s
50s
60s
70s
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
MAXIM
UM T
EMPERATURE L
IMIT
AIR FLOW REQUIRED AT GROUND CONNECTION
SEA LEVEL
Z = 8000 ft
Z = 8000 ft
SEA LEVEL
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- CFM56 series engine
FIGURE-5-5-2-991-003-A01
5-5-2Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
220°C200°C
150°C
100°C
50°C
0°C
90
80
70
60
50
40
30 2
3
4
5
6
MAXIMUM DUCT PRESSUREMAXIM
UM TEMPERATURE LI
MIT
ESTIMATED STARTINGTIMES UP TO IDLE
AIR FLOW REQUIRED AT GROUND CONNECTION
40 50 60 70 80 100 110 12090 kg/mn
ABSOLUTE BARS
45s
50s
55s
60s
N_AC_050502_1_0040101_01_00
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- IAE V2500 series engine
FIGURE-5-5-2-991-004-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-3 High Ambient Temperatures
**ON A/C A319-100
High Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature upper:- +50˚C (+122˚F) -- IAE V2500- +55˚C (+131˚F) -- CFM56
5-5-3Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_050503_1_0030101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
30
40
50
60
70
80
90
100
2
3
4
5
6
7
2.5
3.5
4.5
5.5
6.5
30 40 50 60 70 80 90 100 110 120 kg/mn
PRESSURE: 33 PSIG ATRECOMMENDED
GROUND CONNECTION:MIN PRESSURE AT
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
22 PSIG
GROUND CONNECTION
TIMES UP TO IDLEESTIMATED STARTING
50°C
100°C
150°C
200°C220°C
AIR FLOW REQUIRED AT GROUND CONNECTION
Z = 8000 ft
SEA LEVEL
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
Z = 8000 ft
Z = 8000 ft
SEA LEVEL
35s
40s
50s
60s
70s
MAXIM
UM T
EMPERATURE L
IMIT
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +55˚C (+131˚F) -- CFM56 series engine
FIGURE-5-5-3-991-003-A01
5-5-3Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_050503_1_0040101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
MAXIMUM T
EMPERATURE LIMIT
0°C
50°C
100°C
150°C
200°C220°C
MAXIMUM DUCT PRESSURE
30
40
50
2
3
4
570
60
80
90
6
40 50 60 70 80 90 100 110 120
AIR FLOW REQUIRED AT GROUND CONNECTION
45s
50s
55s
60s
TIMES UP TO IDLEESTIMATED STARTING
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +50˚C (+122˚F) -- IAE V2500 series engine
FIGURE-5-5-3-991-004-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-1 Heating
**ON A/C A319-100
Heating
1. This section provides the ground pneumatic power requirements heating.
5-6-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
1.28
7
1.20
1
1.11
5
1.03
0.94
4
0.85
8
0.72
2
0.68
6
0.51
5
0.60
0.42
9
1.5
1.2
1.0
0.5
3040
50T
IME
(m
in)
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
1.28
1.72
2.15
2.59
3.0
2.5
2.0
1.5
(lb/s
)
CABIN AIRFLOW
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
OT
HE
R H
EA
T L
OA
D
N_AC_050601_1_0020101_01_01
Ground Pneumatic Power RequirementsHeating
FIGURE-5-6-1-991-002-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-2 Cooling
**ON A/C A319-100
Cooling
1. This section provides the ground pneumatic power requirements cooling.
5-6-2Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1.28
7
1.20
1
1.11
5
1.03
0.94
4
0.85
8
0.72
2
0.68
6
0.51
5
0.60
0.42
9
1.5
1.2
1.0
0.5
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
2030
40
TIM
E T
O C
OO
L C
AB
IN T
O 2
7°C
(80
.6°
F O
N G
RO
UN
D)
TIM
E (
min
)
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
1.28
1.72
2.15
2.59
3.0
2.5
2.0
1.5
(lb/s
)
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T 3
8°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_0020101_01_01
Ground Pneumatic Power RequirementsCooling
FIGURE-5-6-2-991-002-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A319-100
Preconditioned Airflow Requirements
1. This section gives the preconditioned airflow requirements for cabin air conditioning.
A. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 1TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 -40.4 -40.70.6 1.32 0.515 1.135 -28.5 -19.30.7 1.54 0.600 1.323 -20.1 -4.20.8 1.76 0.686 1.512 -13.9 7.00.9 1.98 0.772 1.702 -9.1 15.61.0 2.20 0.858 1.892 -5.3 22.51.1 2.43 0.944 2.081 -2.2 28.01.2 2.65 1.030 2.271 0.4 32.71.3 2.87 1.115 2.458 2.6 36.71.4 3.09 1.201 2.648 4.4 39.91.5 3.31 1.287 2.837 6.0 42.8
NOTE : Data for stabilized conditions see 5-7-0.
B. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 2TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 31.7 89.10.6 1.32 0.515 1.135 29.7 85.50.7 1.54 0.600 1.323 28.4 83.10.8 1.76 0.686 1.512 27.3 81.10.9 1.98 0.772 1.702 26.5 79.71.0 2.20 0.858 1.892 25.9 78.61.1 2.43 0.944 2.081 25.4 77.71.2 2.65 1.030 2.271 25.0 77.01.3 2.87 1.115 2.458 24.6 76.31.4 3.09 1.201 2.648 24.3 75.7
5-7-0Page 1
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
FRESH AIRFLOW CURVE 2TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
1.5 3.31 1.287 2.837 24.0 75.2
NOTE : Data for stabilized conditions see 5-7-0.
C. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 3TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 36.0 96.80.6 1.32 0.515 1.135 33.3 91.90.7 1.54 0.600 1.323 31.4 88.50.8 1.76 0.686 1.512 29.9 85.80.9 1.98 0.772 1.702 28.8 83.81.0 2.20 0.858 1.892 27.9 82.21.1 2.43 0.944 2.081 27.2 81.01.2 2.65 1.030 2.271 26.6 79.91.3 2.87 1.115 2.458 26.1 79.01.4 3.09 1.201 2.648 25.7 78.31.5 3.31 1.287 2.837 25.3 77.5
NOTE : Data for stabilized conditions see 5-7-0.
D. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 4TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 42.2 108.00.6 1.32 0.515 1.135 38.4 101.10.7 1.54 0.600 1.323 35.7 96.30.8 1.76 0.686 1.512 33.7 92.70.9 1.98 0.772 1.702 32.1 89.81.0 2.20 0.858 1.892 30.9 87.61.1 2.43 0.944 2.081 29.9 85.81.2 2.65 1.030 2.271 29.0 84.21.3 2.87 1.115 2.458 28.3 82.91.4 3.09 1.201 2.648 27.7 81.9
5-7-0Page 2
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
FRESH AIRFLOW CURVE 4TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
1.5 3.31 1.287 2.837 27.2 81.0
NOTE : Data for stabilized conditions see 5-7-0.
5-7-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
1.28
7
1.20
1
1.11
5
1.03
0.94
4
0.85
8
0.72
2
0.68
6
0.51
5
0.60
1.28
1.72
2.15
2.59
3.0
2.5
2.0
1.5
(lb/s
)
0.42
9
CU
RV
E 2
, 3, 4
(°C
)IN
LET
FLO
WT
EM
PE
RA
TU
RE
(°F
)
NO
TE
:LP
GR
OU
ND
CO
NN
EC
TIO
N M
AX
IMU
M P
RE
SS
UR
E 4
0 m
b
0.5
1.0
1.2
1.5
−40
−30
−20
−10
010
2030
40
−40
−10
010
5010
0
OA
T =
−23
°C
(−
9.4°
F)
OA
T =
−30
°C
(−
22°
F)
OA
T =
−40
°C
(−
40°
F)
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
CABIN AIRFLOW
CU
RV
E 1
: CA
BIN
AT
27°
C (
80.6
°F
)13
4 P
AS
SE
NG
ER
S, 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
AIR
TE
MP
ER
AT
UR
E)
= 3
8°C
(10
0.4°
F)
CA
BIN
AT
21°
C (
69.8
°F
)
NO
OT
HE
R H
EA
T L
OA
D
ELE
CT
RIC
AL
LOA
D =
380
0 W
RE
CIR
CU
LAT
ION
: ON
NO
PA
SS
EN
GE
R O
R C
AB
INA
TT
EN
DA
NT
S
N_AC_050700_1_0020101_01_01
Preconditioned Airflow RequirementsFIGURE-5-7-0-991-002-A01
5-7-0Page 4
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A319-100
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
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
70
404550556065
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A319 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 (5.0 t)− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS
THE RECOMMENDED MINIMUM TRACTOR WEIGHT (8.8 t)
10
0 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0
5
0
TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]
1 ENGINE ON1.5% SLOPE
60 tons
DRAWBAR PULL [ t ] A/C WEIGHT [ t ]
5.0
8.83
WE
T C
ON
CR
ET
E m
= 0
.57
HA
RD
SN
OW
m =
0.2
ICE m = 0.05
AT IDLE
DR
Y C
ON
CR
ET
E m
= 0
.8BREAKAWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 525 daN
N_AC_050800_1_0010201_01_03
Ground Towing RequirementsFIGURE-5-8-0-991-001-B01
5-8-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0 De-Icing and External Cleaning
**ON A/C A319-100
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
A319 99.7 1073.16 1.8 19.38 27 290.63 43 462.85A319 Sharklet 99.7 1073.16 9.6 103.33 27 290.63 43 462.85
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
A319 122 1313.20 23.6 254.03 317 3412A319 Sharklet 122 1313.20 23.6 254.03 325 3498
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
A319 99.7 1073.16 103.4 1112.99 1.8 19.38 27 290.63 27 290.63A319 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
A319 43 462.85 373.6 4021.40 73.2 787.92 750 8073
5-9-0Page 1
Jun 01/12
@A319AIRCRAFT 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
A319 Sharklet 43 462.85 373.6 4021.40 73.2 787.92 758 8159
NOTE : Dimensions are approximate
5-9-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
V (
m/s
)
GR
OU
ND
PLA
NE
ME
TE
RS
40 30 20 10 0036912
mft
4525
2015
10
4530
2520
1510
30
N_AC_060101_1_0030101_01_00
Engine Exhaust VelocitiesGround Idle Power -- CFM56 series engine
FIGURE-6-1-1-991-003-A01
6-1-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
VE
LOC
ITY
= ft
/s (
m/s
)
FE
ET
050
100
150
200
7590
ftm
PLA
N
ftm
100
(30)
50 (15)
30 (9)
100
(30)
50 (15)
30 (9)
15 10 5 0
60 40 20 0
15 10 5 0
60 40 20 0
N_AC_060101_1_0040101_01_00
Engine Exhaust VelocitiesGround Idle Power -- IAE V2500 series engine
FIGURE-6-1-1-991-004-A01
6-1-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
400
350
325
300
400
350
325
300
T (
°K
)
N_AC_060102_1_0030101_01_00
Engine Exhaust TemperaturesGround Idle Power -- CFM56 series engine
FIGURE-6-1-2-991-003-A01
6-1-2Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
TE
MP
ER
AT
UR
E =
°K
FE
ET
050
100
150
200
7590
ftm
PLA
N
ftm
32531
830
830
0
325
318
300
308
15 10 5 0
60 40 20 0
15 10 5 0
60 40 20 0
N_AC_060102_1_0040101_01_00
Engine Exhaust TemperaturesGround Idle Power -- IAE V2500 series engine
FIGURE-6-1-2-991-004-A01
6-1-2Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A319-100
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power.
6-1-5Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
420
390
360
330
300
270
240
210
180
150
120
9060
3000
100
200
300
400
500
700
600
800
900
1000
1100
1200
1300
1400
ME
TE
RS
FE
ET
ftm
ft
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.)
m
42 36 30 24 18 12 6 0
140
120
100 80 60 40 200
140
120
100 80 60 40 200
42 36 30 24 18 12 6 0
N_AC_060105_1_0030101_01_00
Engine Exhaust VelocitiesTakeoff Power -- CFM56 series engine
FIGURE-6-1-5-991-003-A01
6-1-5Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
MA
XIM
UM
TA
KE
OF
F T
HR
US
T
FE
ET
050
100
150
200
7590
ftm
PLA
N
ftm
136
MP
H10
2 M
PH
68 M
PH
34 M
PH
20 M
PH
TO
990
ft (
301
m)
TO
575
ft (
175
m)
60
15 10 5 0
40 20 0 60
15 10 5 0
40 20 0
N_AC_060105_1_0040101_01_00
Engine Exhaust VelocitiesTakeoff Power -- IAE V2500 series engine
FIGURE-6-1-5-991-004-A01
6-1-5Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A319-100
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power.
6-1-6Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
60 40 20 0
ftm
18 12 6 0E
LEV
AT
ION
GR
OU
ND
PLA
NE
2040
6080
100
120
140
160
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.)
FE
ET
ME
TE
RS
PLA
N
T =
425
°K
T =
370
°K
T =
315
°K
T =
425
°K
T =
370
°K
T =
315
°K
AIR
PLA
NE
1020
3040
500
ftm
60 40 20 0
18 12 6 0
N_AC_060106_1_0030101_01_00
Engine Exhaust TemperaturesTakeoff Power -- CFM56 series engine
FIGURE-6-1-6-991-003-A01
6-1-6Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
ME
TE
RS
1530
4560
250
300
ELE
VA
TIO
N
FE
ET
5010
015
020
0
7590
ftm
PLA
N
ftm
00
65°
C55
°C
45°
C35
°C
25°
C
60
15 10 5 0
40 20 060
15 10 5 0
40 20 0
N_AC_060106_1_0040101_01_00
Engine Exhaust TemperaturesTakeoff Power -- IAE V2500 series engine
FIGURE-6-1-6-991-004-A01
6-1-6Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-0 Airport and Community Noise
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-1 Noise Data
**ON A/C A319-100
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 IAE V2500 series engine
A. Description of test conditions:
6-2-1Page 1
Jun 01/12
@A319AIRCRAFT 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: 27˚C (81˚F)- Relative humidity: 40%- Atmospheric pressure: 1000 hPa- Wind speed: Negligible- No rain
6-2-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
112110108106104102
98969492908886848280
100
150°
135°
120°
105°
90°
75°
60°
45°
30°
15°
0°
345°
330°
315°
300°
285°
270°
255°
240°
225°
210°
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
20.8% 90%
NOISE REFERENCEPOINT
78
N_AC_060201_1_0040101_01_00
Airport and Community NoiseCFM56-5A series engine
FIGURE-6-2-1-991-004-A01
6-2-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
8082
8486
8890
9294
96
0°10°
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
320°
310°
300°
290°
280°
270°
250°
240°
230°
220°
210°
NOISE REFERENCEPOINT
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
87%18.9%
260°
N_AC_060201_1_0050101_01_00
78
Airport and Community NoiseCFM56-5B series engine
FIGURE-6-2-1-991-005-A01
6-2-1Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
11811611411211010810610410210098969492908886848280
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
25.2% 94.4%
NOISE REFERENCEPOINT
E.P.R 1.012 1.564
150°
140°
130°
120°
110°
100°
90°
80°
70°
60°
50°
40°
30°
20°10°
0°350°
340°
330°
320°
310°
300°
290°
280°
270°
210°
220°
230°
240°
250°
260°78
N_AC_060201_1_0060101_01_00
Airport and Community NoiseIAE V2500 series engine
FIGURE-6-2-1-991-006-A01
6-2-1Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A319-100
Danger Areas of Engines
1. Danger Areas of the Engines.
6-3-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1 Ground Idle Power
**ON A/C A319-100
Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions.
6-3-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AREA
A
B
C
D65−20
E < 20 (32)
NOT TO SCALE
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV. 1951
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPEAIRCRAFT.
LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT
BEYOND DANGER AREA
APPROX. WINDVELOCITYMPH (km/h)
210−145(338−233)
145−105(233−169)
105−65(169−105)
EXHAUST DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET HAZARDDIMENSIONS CALCULATEDON 40 ft/sec (12 m/sec)CRITICAL VELOCITYWITH A 3 ft (0.9 m)ADJUSTMENT FOR SAFETY
WIDTH72 ft (22 m)
RADIUS = 7.2 ft (2.2 m)
NO ENTRY 82 ft (25 m)AFT OF NOZZLE EXIT
3.4 ft (1 m)
TO 199 ft (61 m)
45°CLOSE ENTRY CORRIDORFOR WIND DIRECTION
B
C
D
> 90°
E
ENTRY CORRIDOREXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
INLET SUCTIONDANGER AREA
(105−32)
N_AC_060301_1_0030101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE-6-3-1-991-003-A01
6-3-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
0.91 m(3 ft)
R = 5.79 m(19ft)
30°
TO 59 m (195 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA
EXHAUST DANGER AREA
ENTRY CORRIDOR
N_AC_060301_1_0040101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE-6-3-1-991-004-A01
6-3-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2 Takeoff Power
**ON A/C A319-100
Takeoff Power
1. This section gives danger areas of the engines at max takeoff conditions.
6-3-2Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AREA
A
B
C
D65−20
E < 20 (32)
NOT TO SCALE
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV. 1951
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPEAIRCRAFT.
LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT
BEYOND DANGER AREA
APPROX. WINDVELOCITYMPH (km/h)
210−145(338−233)
145−105(233−169)
105−65(169−105)
INLET SUCTIONDANGER AREA
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
EXHAUST DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET HAZARD DIMENSIONSBASED ON 40 ft/sec (12 m/sec)CRITICAL VELOCITY WITH A3 ft (0.9 m) ADJUSTMENTFOR SAFETY
WIDTH195 ft (59 m)
RADIUS = 19.5 ft (5.9 m)
NO ENTRY 684 ft (208 m)AFT OF NOZZLE EXIT
A
B
C
D
ETO 1160 ft (354 m)
(105−32)
N_AC_060302_1_0030101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE-6-3-2-991-003-A01
6-3-2Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1.68 m(5.5 ft)
R = 5.79 m(19ft)
30°TO 348 m (1150 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA
EXHAUST DANGER AREA
ENTRY CORRIDOR
N_AC_060302_1_0040101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE-6-3-2-991-004-A01
6-3-2Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A319-100
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1 APU
**ON A/C A319-100
APU - APIC & GARRETT
1. This section gives APU exhaust velocities and temperatures.
6-4-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
80°C176°F
100°C212°F
120°C248°F
150°C302°F
200°C392°F
300°C572°F
METERS
HEIGHT
m ft
FEET
METERS
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
5 10 15 20
16.404 32.808 49.212 65.616
N_AC_060401_1_0020101_01_00
Exhaust Velocities and TemperaturesAPU -- APIC & GARRETTFIGURE-6-4-1-991-002-A01
6-4-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A319-100
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
@A319AIRCRAFT 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 on the left and the scale for allowable working stress on
the right, an arbitrary load line is drawn. This represents the maximum weight to be shown forthe main 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 in 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 to the ACN/PCN system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 Fourth Edition July 2004, incorporating Amendments 1 to 6.
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
@A319AIRCRAFT 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 1.0 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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
MODELA319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−133A319−115A319−111A319−112A319−113A319−114A319−131A319−132A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
WV1212121212121212000000000000000008080808080808081111111111111111090909090909090903030303030303030404040404040404
AIRCRAFT CODECCCCCCDDEEFFFFFFGGGGGGHHIIIIIIJJKKKKKKLLMMNNNNNNOOPPPPPP
MODELA319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
A319−112−CJA319−114−CJA319−115−CJA319−132−CJA319−133−CJ
A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
A319−112−CJA319−114−CJA319−115−CJA319−132−CJA319−133−CJ
A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
A319−111−CJA319−112−CJA319−113−CJA319−114−CJA319−131−CJA319−132−CJ
WV0101010101010101050505050505050505050505050606060606060606070707070707070702020202020202020202020202101010101010
AIRCRAFT CODEQQRRRRRRSSSSSTTUUUUUUVVVVVVWWXXYYYYYYZZZZZ
AAAAABABABABABABACACACACACAC
NOTE: FOR WEIGHT VARIANT DEFINITION, REFER TO CHAPTER 02−01−01.
NOTE: THE A/C CODES ARE USED FOR CONFIGURATION MANAGEMENT OFCHAPTER 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. N_AC_070100_1_0020101_01_00
Aircraft CodesFIGURE-7-1-0-991-002-A01
7-1-0Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
500 mm(19.7 in)
11 039 mm
(36 ft 2.6 in)
7 590 mm(24 ft 10.8 in)
927 mm(36.5 in)
30 x 8.8 R15 (30 x 8.8 − 15)
11.4 bar (165 psi)
46 x 17 R20 (46 x 16 − 20)
11.9 bar (173 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
C − D − E − F − G − H
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0040101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-004-A01
7-2-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
11 039 mm
500 mm(19.7 in)
(36 ft 2.6 in)
927 mm(36.5 in)
7 590 mm(24 ft 10.8 in)
30 x 8.8 R15 (30 x 8.8 − 15)
12.1 bar (175 psi)
46 x 17 R20 (46 x 16 − 20)
12.5 bar (181 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
I − J − K − L − M − N − O − P
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0050101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-005-A01
7-2-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
30 x 8.8 R15 (30 x 8.8 − 15)
12.5 bar (181 psi)
46 x 17 R20 (46 x 16 − 20)
12.9 bar (187 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
500 mm(19.7 in)
11 039 mm
(36 ft 2.6 in)
7 590 mm(24 ft 10.8 in)
927 mm(36.5 in)
Q − R − T − U
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0060101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-006-A01
7-2-0Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
11 039 mm
500 mm(19.7 in)
(36 ft 2.6 in)
927 mm(36.5 in)
7 590 mm(24 ft 10.8 in)
30 x 8.8 R15 (30 x 8.8 − 15)
13.5 bar (196 psi)
46 x 17 R20 (46 x 16 − 20)
13.4 bar (194 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
V − W
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0070101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-007-A01
7-2-0Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
30 x 8.8 R15 (30 x 8.8 − 15)
13.9 bar (202 psi)
46 x 17 R20 (46 x 16 − 20)
13.8 bar (200 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
500 mm(19.7 in)
11 039 mm
(36 ft 2.6 in)
7 590 mm(24 ft 10.8 in)
927 mm(36.5 in)
S − Z − AC
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0250101_01_00
Landing Gear FootprintFIGURE-7-2-0-991-025-A01
7-2-0Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
11 039 mm
500 mm(19.7 in)
(36 ft 2.6 in)
927 mm(36.5 in)
7 590 mm(24 ft 10.8 in)
30 x 8.8 R15 (30 x 8.8 − 15)
13.2 bar (191 psi)
46 x 17 R20 (46 x 16 − 20)
13.8 bar (200 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
X − Y − AA − AB
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0260101_01_00
Landing Gear FootprintFIGURE-7-2-0-991-026-A01
7-2-0Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
C62
400
VM
G (
PE
R S
TR
UT
)V
NG
137
575
23 6
2510
720
36 5
0016
550
63 7
2528
900
21 3
759
700
50 9
7523
120
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
62
400
kgM
RW
= 6
2 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 =
62
400
kgF
WD
CG
= 2
0.4
% M
AC
AT
A/C
WE
IGH
T =
62
400
kg
D E64
925
29 4
5022
075
10 0
1051
925
23 5
60
A/C
CO
DE
C DM
RW
= 6
4 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgE
(2)
MR
W =
62
400
kgM
RW
= 6
2 40
0 kg
AF
T C
G =
39
% M
AC
AT
A/C
WE
IGH
T =
62
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 6
2 40
0 kg
C DM
RW
= 6
4 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgE
62 4
0013
7 57
520
200
9 17
033
075
15 0
0062
900
28 5
3021
375
9 70
050
325
22 8
20
64 4
0014
1 97
520
500
9 30
033
750
15 3
10
N_AC_070300_1_0230101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-023-A01
7-3-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
F64
400
VM
G (
PE
R S
TR
UT
)V
NG
141
975
20 5
009
300
33 7
5015
310
65 7
7529
830
22 0
7510
010
52 6
2523
860
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
64
400
kgM
RW
= 6
4 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 =
21
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
4 40
0 kg
G H64
925
29 4
5022
075
10 0
1051
925
23 5
60
A/C
CO
DE
F GM
RW
= 6
4 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgH
(2)
MR
W =
64
400
kgM
RW
= 6
4 40
0 kg
AF
T C
G =
39
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgA
FT
CG
= 3
9 %
MA
C A
T A
/C W
EIG
HT
= 6
4 40
0 kg
F GM
RW
= 6
4 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgH
64 4
0014
1 97
520
500
9 30
033
750
15 3
10
64 4
0014
1 97
520
500
9 30
033
750
15 3
1065
775
29 8
3022
075
10 0
1052
625
23 8
60
N_AC_070300_1_0240101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-024-A01
7-3-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
I66
400
VM
G (
PE
R S
TR
UT
)V
NG
146
375
21 1
259
580
34 8
0015
780
67 7
5030
730
22 7
5010
320
54 2
0024
590
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
66
400
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 =
21
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
6 40
0 kg
J K67
750
30 7
3022
750
10 3
2054
200
24 5
90
A/C
CO
DE
I JM
RW
= 6
6 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgK
(2)
MR
W =
66
400
kgM
RW
= 6
6 40
0 kg
AF
T C
G =
38.
8 %
MA
C A
T A
/C W
EIG
HT
= 6
6 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgI J
MR
W =
66
400
kgA
FT
CG
= 3
8.8
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgK
66 4
0014
6 37
521
125
9 58
034
800
15 7
8066
950
30 3
6022
750
10 3
2053
550
24 2
90
66 4
0014
6 37
521
125
9 58
034
800
15 7
80
N_AC_070300_1_0250101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-025-A01
7-3-0Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
L66
400
VM
G (
PE
R S
TR
UT
)V
NG
146
375
21 1
259
580
34 8
0015
780
66 9
5030
360
22 7
5010
320
53 5
5024
290
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
66
400
kgM
RW
= 6
8 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 =
21
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
M N68
400
150
800
21 7
509
860
35 7
7516
230
69 6
0031
570
23 4
2510
630
55 6
7525
250
A/C
CO
DE
L MM
RW
= 6
8 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgN
(2)
MR
W =
66
400
kgM
RW
= 6
8 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
L MM
RW
= 6
8 40
0 kg
AF
T C
G =
38.
1 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
N
68 4
0015
0 80
021
750
9 86
035
775
16 2
3068
975
31 2
8023
425
10 6
3055
175
25 0
20
N_AC_070300_1_0260101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-026-A01
7-3-0Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
O68
400
VM
G (
PE
R S
TR
UT
)V
NG
150
800
21 7
509
860
35 8
0016
240
68 9
7531
280
23 4
2510
630
55 1
7525
020
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
68
400
kgM
RW
= 6
8 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 =
21
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
P Q70
400
155
200
22 3
2510
120
36 7
5016
660
71 0
2532
210
24 1
2510
940
56 8
0025
770
A/C
CO
DE
O PM
RW
= 7
0 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgQ
(2)
MR
W =
68
400
kgM
RW
= 6
8 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgA
FT
CG
= 3
8.1
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgO P
MR
W =
70
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
0 40
0 kg
Q
68 4
0015
0 80
021
700
9 84
035
725
16 2
1069
625
31 5
8023
425
10 6
3055
700
25 2
60
N_AC_070300_1_0270101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-027-A01
7-3-0Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
R70
400
VM
G (
PE
R S
TR
UT
)V
NG
155
200
22 3
2510
120
36 7
2516
660
71 4
7532
420
24 1
2510
940
57 1
7525
940
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
70
400
kgM
RW
= 7
0 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 =
21
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
0 40
0 kg
T U70
400
155
200
22 3
2510
120
36 7
2516
660
71 4
7532
420
24 1
2510
940
57 1
7525
940
A/C
CO
DE
R TM
RW
= 7
0 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgU
(2)
MR
W =
70
400
kgM
RW
= 7
0 40
0 kg
AF
T C
G =
37.
5 %
MA
C A
T A
/C W
EIG
HT
= 7
0 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgR T
MR
W =
70
400
kgA
FT
CG
= 3
7.5
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgU
70 4
0015
5 20
022
325
10 1
2036
750
16 6
6071
025
32 2
1024
125
10 9
4056
800
25 7
70
N_AC_070300_1_0280101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-028-A01
7-3-0Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
V73
900
VM
G (
PE
R S
TR
UT
)V
NG
162
925
23 4
0010
610
38 5
0017
460
74 7
2533
890
25 3
2511
480
59 7
7527
110
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
73
900
kgM
RW
= 7
3 90
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 =
21
% M
AC
AT
A/C
WE
IGH
T =
73
900
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
3 90
0 kg
W X75
900
167
325
23 6
2510
720
39 4
0017
870
76 6
0034
750
26 0
0011
800
61 2
7527
800
A/C
CO
DE
V WM
RW
= 7
5 90
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
74
500
kgX
(2)
MR
W =
73
900
kgM
RW
= 7
3 90
0 kg
AF
T C
G =
36.
5 %
MA
C A
T A
/C W
EIG
HT
= 7
3 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
73
900
kgV W
MR
W =
75
900
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
5 90
0 kg
X
73 9
0016
2 92
523
400
10 6
1033
100
15 0
1074
550
33 8
2025
300
11 4
8059
625
27 0
50
N_AC_070300_1_0290101_01_01
Maximum Pavement LoadsFIGURE-7-3-0-991-029-A01
7-3-0Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
Y75
900
VM
G (
PE
R S
TR
UT
)V
NG
167
325
23 6
2510
720
39 4
0017
870
76 6
0034
750
26 0
0011
800
61 2
7527
800
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
75
900
kgM
RW
= 7
5 90
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 =
21
% M
AC
AT
A/C
WE
IGH
T =
74
500
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
4 50
0 kg
AA
75 9
0016
7 32
523
625
AB
75 9
0016
7 32
523
500
10 7
2039
400
17 8
7076
600
34 7
5026
000
11 8
0061
275
27 8
00
10 6
6039
100
17 7
4076
675
34 7
8026
000
11 8
0061
350
27 8
30
A/C
CO
DE
Y AA
MR
W =
75
900
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
4 50
0 kg
AB
(2)
MR
W =
75
900
kgM
RW
= 7
5 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
75
900
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
5 90
0 kg
Y AA
MR
W =
75
900
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
5 90
0 kg
AB
N_AC_070300_1_0300101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-030-A01
7-3-0Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
S70
400
VM
G (
PE
R S
TR
UT
)V
NG
155
200
25 4
5011
550
39 6
5017
990
71 1
0032
250
24 1
2510
940
56 8
7525
800
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
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
70
400
kgM
RW
= 7
5 90
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 =
67
500
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
4 50
0 kg
Z AC
77 7
0035
240
26 3
5011
950
62 1
5028
190
A/C
CO
DE
S ZM
RW
= 7
6 90
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
74
500
kgA
C
(2)
MR
W =
70
400
kgM
RW
= 7
5 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
5 90
0 kg
S ZM
RW
= 7
6 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
76
900
kgA
C
76 9
0016
9 52
523
500
10 6
6039
100
17 7
30
75 9
0016
7 52
523
500
10 6
6039
100
17 7
4076
675
34 7
8026
000
11 8
0061
350
27 8
30
N_AC_070300_1_0310101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-031-A01
7-3-0Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A319-100
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 is92.6 %.
For these conditions the total weight on the Main Landing Gear is 44 470 kg (98 025 lb).
7-4-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-1 Landing Gear Loading on Pavement
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE C
LANDING
TAKE OFF
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 62 000 kg
N_AC_070401_1_0380101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-038-A01
7-4-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 62 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE D
LANDING
TAKE OFF
N_AC_070401_1_0390101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-039-A01
7-4-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE MAC
10 20 30 40 50
A/C CODE E
MLW = 61 000 kg
MZFW = 57 000 kg
LANDING
TAKE OFF
CG FOR ACNCALCULATIONS
MTOW = 64 000 kg
N_AC_070401_1_0400101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-040-A01
7-4-1Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MTOW = 64 000 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
PERCENTAGE MAC
10 20 30 40 50
MLW = 61 000 kg
A/C CODE F
N_AC_070401_1_0410101_01_00
MZFW = 57 000 kg
Landing Gear Loading on PavementFIGURE-7-4-1-991-041-A01
7-4-1Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MLW = 62 500 kg
MTOW = 64 000 kg
MZFW = 58 500 kg
TAKE OFF
LANDING
PERCENTAGE MAC
10 20 30 40 50
N_AC_070401_1_0420101_01_00
CG FOR ACNCALCULATIONS
A/C CODE G
Landing Gear Loading on PavementFIGURE-7-4-1-991-042-A01
7-4-1Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MLW = 62 500 kg
MTOW = 64 000 kg
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE H
N_AC_070401_1_0430101_01_00
LANDING
TAKE OFF
Landing Gear Loading on PavementFIGURE-7-4-1-991-043-A01
7-4-1Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE I
N_AC_070401_1_0440101_01_00
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 66 000 kg
LANDING
TAKE OFF
LANDING
Landing Gear Loading on PavementLanding Gear Loading on Pavement
FIGURE-7-4-1-991-044-A01
7-4-1Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MTOW = 66 000 kg
MZFW = 57 000 kg
PERCENTAGE MAC
10 20 30 40 50
TAKE OFF
LANDING
A/C CODE J
MLW = 61 000 kg
CG FOR ACNCALCULATIONS
LANDING
N_AC_070401_1_0450101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-045-A01
7-4-1Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MTOW = 66 000 kg
MZFW = 58 500 kg
PERCENTAGE MAC
10 20 30 40 50
A/C CODE K
TAKE OFF
MLW = 62 500 kg
N_AC_070401_1_0460101_01_00
LANDINGLANDING
CG FOR ACNCALCULATIONS
Landing Gear Loading on PavementFIGURE-7-4-1-991-046-A01
7-4-1Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 58 500 kg
MTOW = 66 000 kg
TAKE OFF
CG FOR ACNCALCULATIONS
MLW = 62 500 kg
LANDING
PERCENTAGE MAC
10 20 30 40 50
A/C CODE L
N_AC_070401_1_0470101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-047-A01
7-4-1Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 57 000 kg
CG FOR ACNCALCULATIONS
MLW = 61 000 kg
PERCENTAGE MAC
10 20 30 40 50
A/C CODE M
MTOW = 68 000 kg
LANDING
TAKE OFF
N_AC_070401_1_0480101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-048-A01
7-4-1Page 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 57 000 kg
MTOW = 68 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE N
MLW = 61 000 kg
LANDING
TAKE OFF
N_AC_070401_1_0490101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-049-A01
7-4-1Page 13
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 58 500 kg
TAKE OFF
CG FOR ACNCALCULATIONS
MTOW = 68 000 kg
MLW = 62 500 kg
LANDING
PERCENTAGE MAC
10 20 30 40 50
A/C CODE O
N_AC_070401_1_0500101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-050-A01
7-4-1Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MTOW = 68 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE P
MZFW = 58 500 kg
MLW = 62 500 kg
LANDING
TAKE OFF
N_AC_070401_1_0510101_01_00
LANDING
Landing Gear Loading on PavementFIGURE-7-4-1-991-051-A01
7-4-1Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
A/C CODE Q
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 70 000 kg
N_AC_070401_1_0520101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-052-A01
7-4-1Page 16
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE R
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 70 000 kg
N_AC_070401_1_0530101_01_00
Landing Gear Loading on PavementLanding Gear Loading on Pavement
FIGURE-7-4-1-991-053-A01
7-4-1Page 17
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE S
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
MZFW = 58 500 kg
MLW = 62 500 kg
MTOW = 70 000 kg
PERCENTAGE MAC
N_AC_070401_1_0540101_01_00
Landing Gear Loading on PavementLanding Gear Loading on Pavement
FIGURE-7-4-1-991-054-A01
7-4-1Page 18
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
LANDING
TAKE OFF
CG FOR ACNCALCULATIONS
MLW = 62 500 kg
MTOW = 70 000 kg
MZFW = 58 500 kg
A/C CODE T
PERCENTAGE MAC
N_AC_070401_1_0550101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-055-A01
7-4-1Page 19
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE U
LANDING
TAKE OFF
MZFW = 58 500 kg
MLW = 62 500 kg
MTOW = 70 000 kg
CG FOR ACNCALCULATIONS
N_AC_070401_1_0560101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-056-A01
7-4-1Page 20
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
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)
75
55
60
65
70
40
45
50
75
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE V
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
MLW = 62 500 kg
MTOW = 73 500 kg
TAKE OFF
LANDING
N_AC_070401_1_0570101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-057-A01
7-4-1Page 21
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
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)
75
55
60
65
70
40
45
50
75
PERCENTAGE OF WEIGHT ON MAIN GEAR
MTOW = 73 500 kg
A/C CODE W
MLW = 62 500 kg
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
PERCENTAGE MAC
N_AC_070401_1_0580101_01_01
Landing Gear Loading on PavementFIGURE-7-4-1-991-058-A01
7-4-1Page 22
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE X
LANDING
TAKE OFF
MTOW = 75 500 kg
MLW = 61 000 kg
MZFW = 57 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
N_AC_070401_1_0590101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-059-A01
7-4-1Page 23
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
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)
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE Y
MLW = 61 000 kg
MZFW = 57 000 kg
MTOW = 75 500 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
N_AC_070401_1_0600101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-060-A01
7-4-1Page 24
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
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)
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE Z
MZFW = 58 500 kg
MLW = 62 500 kg
MTOW = 75 500 kg
LANDING
TAKE OFF CG FOR ACNCALCULATIONS
N_AC_070401_1_0610101_01_01
Landing Gear Loading on PavementFIGURE-7-4-1-991-061-A01
7-4-1Page 25
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
35
40
45
50
35
75
55
60
65
70
40
45
50
75
80
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)
MLW = 62 500 kg
MTOW = 75 500 kg
TAKE OFF
MZFW = 58 500 kg
LANDING
CG FOR ACNCALCULATIONS
10 20 30 40 5080
PERCENTAGE MAC
A/C CODE AA
N_AC_070401_1_0620101_01_00
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
Landing Gear Loading on PavementFIGURE-7-4-1-991-062-A01
7-4-1Page 26
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
35
40
45
50
35
75
55
60
65
70
40
45
50
75
8080
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)
MLW = 62 500 kg
MTOW = 75 500 kg
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
LANDING
10 20 30 40 50
PERCENTAGE MAC
A/C CODE AB
TAKE OFF
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
N_AC_070401_1_0630101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-063-A01
7-4-1Page 27
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
55
60
65
70
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
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)
PERCENTAGE OF WEIGHT ON MAIN GEAR
CG FOR ACNCALCULATIONS
LANDING
MTOW = 76 500 kg
TAKE OFF
10 20 30 40 50
PERCENTAGE MAC
A/C CODE AC
MLW = 62 500 kg
N_AC_070401_1_0640101_01_01
MZFW = 58 500 kg
Landing Gear Loading on PavementFIGURE-7-4-1-991-064-A01
7-4-1Page 28
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A319-100
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 41.4 cm (16.3 in).
The line showing 10 000 Coverages is used to calculate the Aircraft Classification Number (ACN).
7-5-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR28 900 kg (63 725 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)
A/C CODE C ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0380101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-038-A01
7-5-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR28 530 kg (62 900 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)
A/C CODE D ALPHA FACTOR = 0.9
N_AC_070501_1_0390101_01_00
FOR ACN CALCULATIONS10 000 COVERAGES USED
Flexible Pavement RequirementsFIGURE-7-5-1-991-039-A01
7-5-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 450 kg (64 925 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)
A/C CODE E ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0400101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-040-A01
7-5-1Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 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)
A/C CODE F ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0410101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-041-A01
7-5-1Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 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)
A/C CODE G ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0420101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-042-A01
7-5-1Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 450 kg (64 925 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)
A/C CODE H ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0430101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-043-A01
7-5-1Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 730 kg (67 750 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)
A/C CODE I ALPHA FACTOR = 0.9
N_AC_070501_1_0440101_01_00
FOR ACN CALCULATIONS10 000 COVERAGES USED
Flexible Pavement RequirementsFIGURE-7-5-1-991-044-A01
7-5-1Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 360 kg (66 950 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)
A/C CODE J ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0450101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-045-A01
7-5-1Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 730 kg (67 750 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)
A/C CODE K ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0460101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-046-A01
7-5-1Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 360 kg (66 950 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)
A/C CODE L ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0470101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-047-A01
7-5-1Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 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)
A/C CODE M ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0480101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-048-A01
7-5-1Page 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 570 kg (69 600 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)
A/C CODE N ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0490101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-049-A01
7-5-1Page 13
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 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)
A/C CODE O ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0500101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-050-A01
7-5-1Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 580 kg (69 625 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)
A/C CODE P ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0510101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-051-A01
7-5-1Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
N_AC_070501_1_0520101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE Q
32 210 kg (71 025 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
Flexible Pavement RequirementsFIGURE-7-5-1-991-052-A01
7-5-1Page 16
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
N_AC_070501_1_0530101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE R ALPHA FACTOR = 0.9
32 420 kg (71 475 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-7-5-1-991-053-A01
7-5-1Page 17
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR32 250 kg (71 100 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)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE S ALPHA FACTOR = 0.9
N_AC_070501_1_0540101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-054-A01
7-5-1Page 18
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR32 210 kg (71 025 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)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE T ALPHA FACTOR = 0.9
N_AC_070501_1_0550101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-055-A01
7-5-1Page 19
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR32 420 kg (71 475 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)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE U ALPHA FACTOR = 0.9
N_AC_070501_1_0560101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-056-A01
7-5-1Page 20
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR33 890 kg (74 725 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)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE V ALPHA FACTOR = 0.9
N_AC_070501_1_0570101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-057-A01
7-5-1Page 21
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
8060403020151063
8060403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR33 820 kg (74 550 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)
SUBGRADE STRENGTH − CBR
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRES
TIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
N_AC_070501_1_0580101_01_01
A/C CODE W ALPHA FACTOR = 0.9
ANNUAL DEPARTURES*
Flexible Pavement RequirementsFIGURE-7-5-1-991-058-A01
7-5-1Page 22
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 750 kg (76 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE X
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0590101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-059-A01
7-5-1Page 23
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 750 kg (76 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE Y
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0600101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-060-A01
7-5-1Page 24
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 780 kg (76 675 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE Z
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0610101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-061-A01
7-5-1Page 25
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 750 kg (76 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE AA
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0620101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-062-A01
7-5-1Page 26
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 780 kg (76 675 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE AB
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0630101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-063-A01
7-5-1Page 27
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR35 240 kg (77 700 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE AC
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0640101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-064-A01
7-5-1Page 28
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A319-100
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 52.3.
For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).
7-6-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-1 Flexible Pavement Requirements - LCN Conversion
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
1.9
bar
(173
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
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
WE
IGH
T O
N O
NE
MA
IN
28 9
00 k
g
(63
725
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)
A/C
CO
DE
C
N_AC_070601_1_0410101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-041-A01
7-6-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
1.9
bar
(173
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0420101_01_00
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
WE
IGH
T O
N O
NE
MA
IN
28 5
30 k
g
(62
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
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
D
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-042-A01
7-6-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
1.9
bar
(173
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
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
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)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
E
N_AC_070601_1_0430101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-043-A01
7-6-1Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
1.9
bar
(173
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
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
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)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
F
N_AC_070601_1_0440101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-044-A01
7-6-1Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
1.9
bar
(173
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0450101_01_00
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
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
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)
A/C
CO
DE
G
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-045-A01
7-6-1Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
1.9
bar
(173
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
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
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)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
N_AC_070601_1_0460101_01_00
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
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
R
10 0
00 k
g
(22
050
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
I
N_AC_070601_1_0470101_01_00
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0480101_01_00
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
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
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)
A/C
CO
DE
J
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-048-A01
7-6-1Page 9
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0490101_01_00
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
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
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
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
K
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-049-A01
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
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)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
L
N_AC_070601_1_0500101_01_00
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7-6-1Page 11
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0510101_01_00
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
WE
IGH
T O
N O
NE
MA
IN
31 2
80 k
g
(68
950
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)
A/C
CO
DE
M
Flexible Pavement Requirements - LCN ConversionFlexible Pavement Requirements - LCN Conversion
FIGURE-7-6-1-991-051-A01
7-6-1Page 12
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
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
WE
IGH
T O
N O
NE
MA
IN
31 5
70 k
g
(69
600
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)
A/C
CO
DE
N
N_AC_070601_1_0520101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-052-A01
7-6-1Page 13
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0530101_01_00
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
WE
IGH
T O
N O
NE
MA
IN
31 2
80 k
g
(68
950
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)
A/C
CO
DE
O
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-053-A01
7-6-1Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.5
bar
(181
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]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0540101_01_00
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
WE
IGH
T O
N O
NE
MA
IN
31 5
80 k
g
(69
625
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)
A/C
CO
DE
P
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-054-A01
7-6-1Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.9
bar
(187
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
32 2
10 k
g
(71
000
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
Q
N_AC_070601_1_0550101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-055-A01
7-6-1Page 16
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
2.9
bar
(187
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
32 4
20 k
g
(71
475
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
R
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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
3.8
bar
(200
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
32 2
50 k
g
(71
100
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
S
N_AC_070601_1_0570101_01_00
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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
2.9
bar
(187
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
32 2
10 k
g
(71
000
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
T
N_AC_070601_1_0580101_01_00
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**ON A/C A319-100
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
2.9
bar
(187
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
32 4
20 k
g
(71
475
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
U
N_AC_070601_1_0590101_01_00
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**ON A/C A319-100
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
3.4
bar
(194
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
33 8
90 k
g
(74
725
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
V
N_AC_070601_1_0600101_01_00
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**ON A/C A319-100
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
3.4
bar
(194
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
33 8
20 k
g
(74
550
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
W
N_AC_070601_1_0610101_01_01
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**ON A/C A319-100
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
3.8
bar
(200
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
34 7
50 k
g
(76
600
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
X
N_AC_070601_1_0620101_01_00
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
3.8
bar
(200
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
34 7
50 k
g
(76
600
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
Y
N_AC_070601_1_0630101_01_00
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
3.8
bar
(200
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
34 7
80 k
g
(76
675
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
Z
N_AC_070601_1_0640101_01_00
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
3.8
bar
(200
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
34 7
50 k
g
(76
600
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
AA
N_AC_070601_1_0650101_01_00
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@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
3.8
bar
(200
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
34 7
80 k
g
(76
675
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
AB
N_AC_070601_1_0660101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-066-A01
7-6-1Page 27
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
3.8
bar
(200
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
35 2
40 k
g
(77
700
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
AC
N_AC_070601_1_0670101_01_00
Flexible Pavement Requirements - LCN ConversionFlexible Pavement Requirements - LCN Conversion
FIGURE-7-6-1-991-067-A01
7-6-1Page 28
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A319-100
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 18.9 cm (7.4 in).
7-7-0Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR28 905 kg (63 725 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
A/C CODE C
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14
N_AC_070701_1_0380101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-038-A01
7-7-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE D
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR28 530 kg (62 900 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0390101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-039-A01
7-7-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE E
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 445 kg (64 925 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0400101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-040-A01
7-7-1Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE F
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0410101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-041-A01
7-7-1Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE G
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0420101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-042-A01
7-7-1Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE H
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 445 kg (64 925 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0430101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-043-A01
7-7-1Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE I
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 735 kg (67 750 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0440101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-044-A01
7-7-1Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE J
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 365 kg (66 950 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0450101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-045-A01
7-7-1Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE K
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 735 kg (67 750 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0460101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-046-A01
7-7-1Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE L
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 365 kg (66 950 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0470101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-047-A01
7-7-1Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE M
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0480101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-048-A01
7-7-1Page 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE N
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 565 kg (69 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0490101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-049-A01
7-7-1Page 13
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE O
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0500101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-050-A01
7-7-1Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE P
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
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
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 580 kg (69 625 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
N_AC_070701_1_0510101_01_00
10 000 kg (22 050 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-051-A01
7-7-1Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE QRIG
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 12.9 bar (187 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0520101_01_00
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)
32 210 kg (71 025 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-052-A01
7-7-1Page 16
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
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)
32 420 kg (71 475 lb)
A/C CODE R
N_AC_070701_1_0530101_01_00
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³ [lb/in
²]
[kg/
cm²]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-053-A01
7-7-1Page 17
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
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 SRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
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)
32 245 kg (71 100 lb)
[lb/in
²]
[kg/
cm²]
N_AC_070701_1_0540101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-054-A01
7-7-1Page 18
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
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)
32 210 kg (71 025 lb)
A/C CODE TRIG
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 12.9 bar (187 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0550101_01_00
[lb/in
²]
[kg/
cm²]
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-055-A01
7-7-1Page 19
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
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)
32 420 kg (71 475 lb)
A/C CODE URIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0560101_01_00
[lb/in
²]
[kg/
cm²]
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-056-A01
7-7-1Page 20
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE VRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
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)
33 895 kg (74 725 lb)
[lb/in
²]
[kg/
cm²]
N_AC_070701_1_0570101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-057-A01
7-7-1Page 21
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
20
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_0580101_01_01
A/C CODE W
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)
33 820 kg (74 550 lb)
30
40
50
60
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-058-A01
7-7-1Page 22
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE XRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0590101_01_00
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)
34 745 kg (76 600 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-059-A01
7-7-1Page 23
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE YRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
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)
34 745 kg (76 600 lb)
N_AC_070701_1_0600101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-060-A01
7-7-1Page 24
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE ZRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
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)
34 780 kg (76 675 lb)
N_AC_070701_1_0610101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-061-A01
7-7-1Page 25
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE AARIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
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)
34 745 kg (76 600 lb)
N_AC_070701_1_0620101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-062-A01
7-7-1Page 26
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE ABRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
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)
34 780 kg (76 675 lb)
N_AC_070701_1_0630101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-063-A01
7-7-1Page 27
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE ACRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0640101_01_00
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
35 240 kg (77 700 lb)
WEIGHT ON ONE MAIN LANDING GEAR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-064-A01
7-7-1Page 28
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-1 Radius of Relative Stiffness
**ON A/C A319-100
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-1Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
31.4833.4335.3437.2239.0640.8842.6744.4346.1847.9049.6051.2852.9454.5956.2257.8359.4361.0262.5964.1565.6967.2368.7570.2671.7674.7377.6680.5583.4186.2489.0491.81
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
19.1320.3121.4722.6123.7424.8425.9327.0028.0629.1130.1432.1632.1733.1734.1635.1436.1237.0838.0338.9839.9240.8541.7842.7043.6145.4147.1948.9550.6952.4154.1155.79
RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES
L =
E = YOUNG’S MODULUS = 4 x 10 psi
k = SUBGRADE MODULUS, lb/in
d = RIGID PAVEMENT THICKNESS, (in)
= POISSON’S RATIO = 0.15
Ed12 (1 − ) k2 = 24.1652
dk
WHERE
43
4
6
3
3
N_AC_070801_1_0020101_01_02
Radius of Relative Stiffness(Reference: Portland Cement Association)
FIGURE-7-8-1-991-002-A01
7-8-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-2 Rigid Pavement Requirements - LCN Conversion
**ON A/C A319-100
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 56.
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 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]
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
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
28 9
00 k
g
(63
725
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)
N_AC_070802_1_0410101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-041-A01
7-8-2Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 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]
A/C
CO
DE
D
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
28 5
30 k
g
(62
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
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0420101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-042-A01
7-8-2Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 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]
A/C
CO
DE
E
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
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)
N_AC_070802_1_0430101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-043-A01
7-8-2Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 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]
A/C
CO
DE
F
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
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)
N_AC_070802_1_0440101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-044-A01
7-8-2Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 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]
A/C
CO
DE
G
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
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)
N_AC_070802_1_0450101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-045-A01
7-8-2Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 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]
A/C
CO
DE
H
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
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)
N_AC_070802_1_0460101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-046-A01
7-8-2Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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]
A/C
CO
DE
I
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
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
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0470101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-047-A01
7-8-2Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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]
A/C
CO
DE
J
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
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)
N_AC_070802_1_0480101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-048-A01
7-8-2Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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]
A/C
CO
DE
K
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
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
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0490101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-049-A01
7-8-2Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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]
A/C
CO
DE
L
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
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)
N_AC_070802_1_0500101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-050-A01
7-8-2Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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
)
A/C
CO
DE
M
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
280
kg
(6
8 95
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
)
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
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0510101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-051-A01
7-8-2Page 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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
)
A/C
CO
DE
N
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
570
kg
(6
9 60
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
)
N_AC_070802_1_0520101_01_00
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
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-052-A01
7-8-2Page 13
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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
)
A/C
CO
DE
O
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
280
kg
(6
8 95
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
)
N_AC_070802_1_0530101_01_00
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
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-053-A01
7-8-2Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 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
)
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
N_AC_070802_1_0540101_01_00
A/C
CO
DE
P
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
580
kg
(6
9 62
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
)
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
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-054-A01
7-8-2Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 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
)
A/C
CO
DE
Q
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
210
kg
(7
1 00
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
)
N_AC_070802_1_0550101_01_00
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
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-055-A01
7-8-2Page 16
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 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
)
A/C
CO
DE
R
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
420
kg
(7
1 47
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
)
N_AC_070802_1_0560101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-056-A01
7-8-2Page 17
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 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
)
A/C
CO
DE
S
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
250
kg
(7
1 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
)
N_AC_070802_1_0570101_01_00
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
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-057-A01
7-8-2Page 18
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 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
)
A/C
CO
DE
T
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
210
kg
(7
1 00
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
)
N_AC_070802_1_0580101_01_00
10 0
00 k
g
(22
050
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-058-A01
7-8-2Page 19
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 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
)
A/C
CO
DE
U
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
420
kg
(7
1 47
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
)
N_AC_070802_1_0590101_01_00
10 0
00 k
g
(22
050
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-059-A01
7-8-2Page 20
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 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
)
A/C
CO
DE
V
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
33 8
90 k
g
(74
725
lb)
N_AC_070802_1_0600101_01_00
10 0
00 k
g
(22
050
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-060-A01
7-8-2Page 21
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
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
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
2 00
02
500
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R33
820
kg
(7
4 55
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
)
N_AC_070802_1_0610101_01_01
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
W
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T M
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
1 75
01
500
1 00
075
01
250
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-061-A01
7-8-2Page 22
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 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
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
X
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
750
kg
(7
6 60
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
)
N_AC_070802_1_0620101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-062-A01
7-8-2Page 23
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 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
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
Y
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
TW
EIG
HT
ON
ON
E M
AIN
LA
ND
ING
GE
AR
34 7
50 k
g
(76
600
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)
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0630101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-063-A01
7-8-2Page 24
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 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
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
Z
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
780
kg
(7
6 67
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
)
N_AC_070802_1_0640101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-064-A01
7-8-2Page 25
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 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
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
AA
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
750
kg
(7
6 60
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
)
N_AC_070802_1_0650101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-065-A01
7-8-2Page 26
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 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
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
AB
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
780
kg
(7
6 67
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
)
N_AC_070802_1_0660101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-066-A01
7-8-2Page 27
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 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
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
AC
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R35
240
kg
(7
7 70
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
)
N_AC_070802_1_0670101_01_00
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
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-067-A01
7-8-2Page 28
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-3 Radius of Relative Stiffness (Other values of E and L)
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-4 Radius of Relative Stiffness
**ON A/C A319-100
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-4Page 1
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
0.80
0.85
0.90
0.95
1.00
1.05
1.10
0 1 2 3 4 5
0.995
1.000
1.005
1.010
1.015
0.00 0.05 0.10 0.15 0.25
E F
AC
TO
R
BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF TABLE 7−8−1
EFFECT OF ON L VALUES
E, Young’s Modulus (10 , PSI)
EFFECT OF E ON L VALUES
, Poisson’s Ratio
FA
CT
OR
NOTE:
0.20
N_AC_070804_1_0020101_01_02
Radius of Relative Stiffness(Effect E and µ on ”L” values)
FIGURE-7-8-4-991-002-A01
7-8-4Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0 ACN/PCN Reporting System
**ON A/C A319-100
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 55 000 kg (121 250 lb) and low subgrade strength (code C), theACN for the flexible pavement is 29.9.
In the example shown in Section 7-9-2 Aircraft Classification Number -- Rigid Pavement, A/C CodeC, for an aircraft gross weight of 55 000 kg (121 250 lb) and medium subgrade strength (code B),the ACN for the rigid pavement is 30.8.
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-1 Aircraft Classification Number - Flexible Pavement
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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
9 %
MA
C.
ON
PA
VE
ME
NT
− A
/C C
OD
E C
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
N_AC_070901_1_0510101_01_00
A/C
CO
DE
C
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-051-A01
7-9-1Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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
6 %
MA
C.
ON
PA
VE
ME
NT
− A
/C C
OD
E D
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
D
N_AC_070901_1_0520101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-052-A01
7-9-1Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
E
ON
PA
VE
ME
NT
− A
/C C
OD
E E
N_AC_070901_1_0530101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-053-A01
7-9-1Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
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
9 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
A/C
CO
DE
F
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0540101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-054-A01
7-9-1Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
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
9 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
A/C
CO
DE
G
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0550101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-055-A01
7-9-1Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
A/C
CO
DE
H
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0560101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-056-A01
7-9-1Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
8.8
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
I
65
148
152
N_AC_070901_1_0570101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E I
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-057-A01
7-9-1Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
J
65
148
152
N_AC_070901_1_0580101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-058-A01
7-9-1Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
8.8
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
K
65
148
152
N_AC_070901_1_0590101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E K
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-059-A01
7-9-1Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
L
65
148
152
N_AC_070901_1_0600101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-060-A01
7-9-1Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
M
65
148
152
N_AC_070901_1_0610101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E M
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-061-A01
7-9-1Page 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
8.1
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
N
50
N_AC_070901_1_0620101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E N
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-062-A01
7-9-1Page 13
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
O
50
N_AC_070901_1_0630101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E O
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-063-A01
7-9-1Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
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
8.1
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
P
50
N_AC_070901_1_0640101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E P
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-064-A01
7-9-1Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E Q
75
N_AC_070901_1_0650101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Q
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-065-A01
7-9-1Page 16
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
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
7.5
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E R
75
N_AC_070901_1_0660101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E R
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-066-A01
7-9-1Page 17
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E S
75
N_AC_070901_1_0670101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E S
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-067-A01
7-9-1Page 18
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
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
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E T
75
N_AC_070901_1_0680101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E T
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-068-A01
7-9-1Page 19
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
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
7.5
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E U
75
N_AC_070901_1_0690101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E U
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-069-A01
7-9-1Page 20
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)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.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
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
6.52
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E V
75
N_AC_070901_1_0700101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E V
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-070-A01
7-9-1Page 21
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
7065
6055
5045
4035
75
1520253035404550
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
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
ON
PA
VE
ME
NT
− A
/C C
OD
E W
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)(x
1 0
00 lb
)
A/C
CO
DE
W
N_AC_070901_1_0710101_01_01
8090
100
110
120
130
140
150
160
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-071-A01
7-9-1Page 22
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1520253035404550
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
13.
8 ba
r (2
00 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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
X
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
)
ON
PA
VE
ME
NT
− A
/C C
OD
E X
N_AC_070901_1_0720101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-072-A01
7-9-1Page 23
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1520253035404550
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
13.
8 ba
r (2
00 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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
Y
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
)
N_AC_070901_1_0730101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Y
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-073-A01
7-9-1Page 24
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1520253035404550
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
13.
8 ba
r (2
00 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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
Z
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
)
N_AC_070901_1_0740101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Z
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-074-A01
7-9-1Page 25
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1520253035404550
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
13.
8 ba
r (2
00 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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
AA
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
)
N_AC_070901_1_0750101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
A
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-075-A01
7-9-1Page 26
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1520253035404550
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
13.
8 ba
r (2
00 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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
AB
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
)
N_AC_070901_1_0760101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
B
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-076-A01
7-9-1Page 27
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
1520253035404550
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
13.
8 ba
r (2
00 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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
AC
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
)
N_AC_070901_1_0770101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
C
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-077-A01
7-9-1Page 28
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-2 Aircraft Classification Number - Rigid Pavement
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
9 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
C
N_AC_070902_1_0500101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E C
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-050-A01
7-9-2Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
D
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0510101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E D
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-051-A01
7-9-2Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
E
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0520101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-052-A01
7-9-2Page 4
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
9 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
F
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0530101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-053-A01
7-9-2Page 5
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
9 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
G
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0540101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-054-A01
7-9-2Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
H
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
N_AC_070902_1_0550101_01_00
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-055-A01
7-9-2Page 7
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
8.8
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
I
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0560101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E I
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-056-A01
7-9-2Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
J
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0570101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-057-A01
7-9-2Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
8.8
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
K
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0580101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E K
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-058-A01
7-9-2Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
L
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0590101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-059-A01
7-9-2Page 11
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E M
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
M
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
N_AC_070902_1_0600101_01_00
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-060-A01
7-9-2Page 12
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
N
65
148
152
N_AC_070902_1_0610101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E N
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 38.
1 %
MA
C.
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-061-A01
7-9-2Page 13
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
O
65
148
152
N_AC_070902_1_0620101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E O
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-062-A01
7-9-2Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
P
65
148
152
N_AC_070902_1_0630101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E P
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 38.
1 %
MA
C.
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-063-A01
7-9-2Page 15
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
Q
75
N_AC_070902_1_0640101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E Q
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-064-A01
7-9-2Page 16
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
R
75
N_AC_070902_1_0650101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E R
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 37.
5 %
MA
C.
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-065-A01
7-9-2Page 17
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
S
75
N_AC_070902_1_0660101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E S
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-066-A01
7-9-2Page 18
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
T
75
N_AC_070902_1_0670101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E T
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-067-A01
7-9-2Page 19
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
U
75
N_AC_070902_1_0680101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E U
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 37.
5 %
MA
C.
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-068-A01
7-9-2Page 20
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
V
75
N_AC_070902_1_0690101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E V
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36.
52 %
MA
C.
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-069-A01
7-9-2Page 21
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)A
CN
WA
S D
ET
ER
MIN
ED
AS
RE
FE
RE
NC
ED
INIC
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.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.4
bar
(194
psi
)O
N P
AV
EM
EN
T −
A/C
CO
DE
W
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070902_1_0700101_01_01
1520253035404550
3540
4550
5560
6570
75
8090
100
110
120
130
140
150
160
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
A/C
CO
DE
W
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-070-A01
7-9-2Page 22
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
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
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
X
55
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)
80
N_AC_070902_1_0710101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E X
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-071-A01
7-9-2Page 23
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
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
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
Y
55
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)
80
N_AC_070902_1_0720101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Y
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-072-A01
7-9-2Page 24
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
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
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
Z
55
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)
80
N_AC_070902_1_0730101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Z
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-073-A01
7-9-2Page 25
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
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
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
AA
55
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)
80
N_AC_070902_1_0740101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
A
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-074-A01
7-9-2Page 26
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
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
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
AB
55
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)
80
N_AC_070902_1_0750101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
B
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-075-A01
7-9-2Page 27
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
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
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
AC
55
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)
80
N_AC_070902_1_0770101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
C
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-077-A01
7-9-2Page 28
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.NOTE:
0 10 20 30 40 50FEET
0 5 10 15METERS
010
2030
4050
FE
ET
05
1015
ME
TE
RS
N_AC_080000_1_0020101_01_00
Scaled DrawingFIGURE-8-0-0-991-002-A01
8-0-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_100000_1_0010201_01_00
Front PageFIGURE-10-0-0-991-001-B01
10-0-0Page 2
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_100000_1_0020201_01_00
Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-002-B01
10-0-0Page 3
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_100000_1_0040201_01_00
Composite MaterialsFIGURE-10-0-0-991-004-B01
10-0-0Page 6
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
C L
N_AC_100000_1_0060201_01_00
Evacuation/Escape Slide/RaftFIGURE-10-0-0-991-006-B01
10-0-0Page 8
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_100000_1_0070101_01_00
Pax/Crew DoorsFIGURE-10-0-0-991-007-A01
10-0-0Page 9
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_100000_1_0080201_01_00
Emergency Exit HatchFIGURE-10-0-0-991-008-B01
10-0-0Page 10
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
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
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_100000_1_0140201_01_00
Aircraft Ground ClearancesFIGURE-10-0-0-991-014-B01
10-0-0Page 14
Jun 01/12
@A319AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A319-100
N_AC_100000_1_0150101_01_00
Structural Break-in PointsFIGURE-10-0-0-991-015-A01
10-0-0Page 15
Jun 01/12
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