aircraft characteristics airport and maintenance … · 2012-10-04 · @a321 aircraft...
TRANSCRIPT
@AIRBUSA321
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: Sep 30/92 Rev: Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HIGHLIGHTS
Revision No. 16 - 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.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
@A321AIRCRAFT 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 - Location 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
@A321AIRCRAFT 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
@A321AIRCRAFT 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
@A321AIRCRAFT 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
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at MLG Jacking Points
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - NLG Jacking - Point Location
N ILLUSTRATION ADDED
FIGURE Landing Gear Jacking for WheelChange - Loads at NLG Jacking Points
N ILLUSTRATION ADDED
CHAPTER 3 R
CHAPTER 4
Section 4-2
Subject 4-2-0
FIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISED
FIGURE Turning Radii, No Slip Angle R ILLUSTRATION REVISED
Section 4-3
Subject 4-3-0
FIGURE Minimum Turning Radii R
Section 4-4
Subject 4-4-0
Visibility from Cockpit in Static Position N
FIGURE Visibility from Cockpit in StaticPosition
N ILLUSTRATION ADDED
FIGURE Binocular Visibility ThroughWindows from Captain Eye Position
N ILLUSTRATION ADDED
Section 4-5 R
Subject 4-5-1
HIGHLIGHTSPage 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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
Subject 5-1-0 R
Subject 5-1-2 R
HIGHLIGHTSPage 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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 (51 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 (25 Min.)
N ILLUSTRATION ADDED
Subject 05-03-01 D
Section 5-4
Subject 5-4-1
Ground Service Connections Layout R DELETED GROUND SERVICECONNECTIONS LAYOUT TABLE.
HIGHLIGHTSPage 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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
@A321AIRCRAFT 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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 7
Section 7-8 R
Subject 07-08-00 D
Subject 7-8-1
FIGURE Radius of Relative Stiffness -(Reference: Portland Cement Association)
R
Subject 7-8-2
Rigid Pavement Requirements - LCNConversion
R MOVED THE TEXT FROM 7-8-0 TO 7-8-2.
CHAPTER 8 R
Section 8-0 N
Subject 8-0-0 N
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 and EmergencyExits
N ILLUSTRATION ADDED
FIGURE FWD and AFT Lower DeckCargo Doors
N ILLUSTRATION ADDED
FIGURE Control Panels N ILLUSTRATION ADDED
HIGHLIGHTSPage 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE APU Access Door N ILLUSTRATION ADDED
FIGURE Aircraft Ground Clearances N ILLUSTRATION ADDED
FIGURE Structural Break-in Points N ILLUSTRATION ADDED
HIGHLIGHTSPage 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 16 - 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
@A321AIRCRAFT 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 2-7-6
L.E.C.Page 2
Jun 01/12
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CONTENT CHGCODE
LAST REVISIONDATE
Bulk Cargo Compartment Door Dec 01/07
FIGURE Doors Clearances - Bulk Cargo Compartment Door Dec 01/07
Subject 2-7-7
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 - Location 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
L.E.C.Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Exterior Lighting N Jun 01/12
Subject 2-11-0
Antennas and Probes Location N Jun 01/12
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
L.E.C.Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
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
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
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at MLGJacking Points
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - NLG Jacking -Point Location
N Jun 01/12
FIGURE Landing Gear Jacking for Wheel Change - Loads at NLGJacking Points
N Jun 01/12
CHAPTER 3
Subject 3-1-0
General Information Dec 01/07
Subject 3-2-0
Payload / Range Dec 01/07
Subject 3-2-1
ISA Conditions Dec 01/07
FIGURE Payload / Range - CFM56-5B 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
@A321AIRCRAFT 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 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 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
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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
@A321AIRCRAFT 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 (51 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 (25 Min.) N Jun 01/12
Subject 5-4-0
Ground Service Connections Dec 01/07
Subject 5-4-1
L.E.C.Page 8
Jun 01/12
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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
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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
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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
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Exhaust Velocities - Ground Idle Power -- CFM56-5Bseries 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 --CFM56-5B series 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 -- CFM56-5Bseries engine
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 -- CFM56-5Bseries 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 - CFM56-5B 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
Subject 6-3-1
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CONTENT CHGCODE
LAST REVISIONDATE
Ground Idle Power Dec 01/07
FIGURE Danger Areas of Engines - CFM56-5B 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 - CFM56-5B 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 - 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 - Landing Gear Footprint May 01/11
Subject 7-3-0
Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads May 01/11
FIGURE Maximum Pavement Loads May 01/11
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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 - Maximum Pavement Loads May 01/11
Subject 7-4-0
Landing Gear Loading on Pavement May 01/11
Subject 7-4-1
Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
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 May 01/11
FIGURE Landing Gear Loading on Pavement May 01/11
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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 Requirement - Flexible PavementRequirements
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 Requirement - Flexible PavementRequirements
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
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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
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
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
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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) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
FIGURE Rigid Pavement Requirements (PCA) May 01/11
Subject 7-8-1
Radius of Relative Stiffness Dec 01/07
FIGURE Radius of Relative Stiffness - (Reference: Portland CementAssociation)
R Jun 01/12
Subject 7-8-2
Rigid Pavement Requirements - LCN Conversion R Jun 01/12
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion May 01/11
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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
Subject 7-8-3
Radius of Relative Stiffness (Other values of ”E” and ”L”) May 01/11
Subject 7-8-4
Radius of Relative Stiffness Dec 01/07
FIGURE Radius of Relative Stiffness - (Effect E and µ on ”L” values) May 01/11
Subject 7-9-0
ACN/PCN Reporting System May 01/11
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
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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
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
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
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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
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 and Emergency Exits 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
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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
2-7-6 Bulk 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
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3-3-1 ISA Conditions
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
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5-4-10 Vacuum Toilet System
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
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7-8-1 Radius of Relative Stiffness
7-8-2 Rigid Pavement Requirements - LCN Conversion
7-8-3 Radius of Relative Stiffness (Other values of E and L)
7-8-4 Radius of Relative Stiffness
7-9-0 ACN/PCN Reporting System
7-9-1 Aircraft Classification Number - Flexible Pavement
7-9-2 Aircraft Classification Number - Rigid Pavement
8 SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
10 AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCOPE
1-1-0 Purpose
**ON A/C A321-100 A321-200
Purpose
1. GeneralThe A321 AIRCRAFT CHARACTERISTICS -- AIRPORT AND MAINTENANCE PLANNING (AC)manual is issued for the A321-100 and A321-200 series aircraft, equipped with wing-tip fences orSharklets to provide necessary data to airport operators, airlines and Maintenance/RepairOrganizations (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 A321-100 and A321-200 AC equipped with Sharklets can besubject to change pending completion of the flight test phase. It is given for guidance only and doesnot constitute a contractual 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 A321neo which is under development.
Correspondence concerning this publication should be directed to:
AIRBUS S.A.S.Customer ServicesTechnical Data Support and Services
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1, Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT DESCRIPTION
2-1-0 General Aircraft Characteristics
**ON A/C A321-100 A321-200
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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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-1-1 General Aircraft Characteristics Data
**ON A/C A321-100 A321-200
General Airplane Characteristics Data
**ON A/C A321-100
1. The following table provides characteristics of A321-100 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV002 WV003 WV004 WV005
Kilograms 83 400 83 400 85 400 78 400 83 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds183 865 183 865 188 275 172 842 183 865
Kilograms 83 000 83 000 85 000 78 000 83 000Maximum TakeoffWeight (MTOW) Pounds 182 984 182 984 187 393 171 961 182 984
Kilograms 73 500 74 500 74 500 73 500 75 000Maximum LandingWeight (MLW) Pounds 162 040 164 244 164 244 162 040 165 347
Kilograms 69 500 70 500 70 500 69 500 71 000Maximum Zero FuelWeight (MZFW) Pounds 153 221 155 426 155 426 153 221 156 528
Aircraft CharacteristicsWV006 WV007 WV008
Kilograms 78 400 80 400 89 400Maximum Ramp Weight (MRW)Maximum Taxi Weight (MTW) Pounds 172 842 177 252 197 093
Kilograms 78 000 80 000 89 000Maximum Takeoff Weight(MTOW) Pounds 171 961 176 370 196 211
Kilograms 74 500 73 500 75 500Maximum Landing Weight(MLW) Pounds 164 244 162 040 166 449
Kilograms 70 500 69 500 71 500Maximum Zero Fuel Weight(MZFW) Pounds 155 426 153 221 157 630
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2. The following table provides characteristics of A321-200 Models, these data are specific to eachWeight Variant:
Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004
Kilograms 89 400 93 400 89 400 91 400 87 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds197 093 205 912 197 093 201 502 192 684
Kilograms 89 000 93 000 89 000 91 000 87 000Maximum TakeoffWeight (MTOW) Pounds 196 211 205 030 196 211 200 621 191 802
Kilograms 75 500 77 800 77 800 77 800 75 500Maximum LandingWeight (MLW) Pounds 166 449 171 520 171 520 171 520 166 449
Kilograms 71 500 73 800 73 800 73 800 71 500Maximum Zero FuelWeight (MZFW) Pounds 157 630 162 701 162 701 162 701 157 630
Aircraft CharacteristicsWV005 WV006 WV007 WV008 WV009
Kilograms 85 400 83 400 83 400 80 400 78 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds188 275 183 865 183 865 177 252 172 842
Kilograms 85 000 83 000 83 000 80 000 78 000Maximum TakeoffWeight (MTOW) Pounds 187 393 182 984 182 984 176 370 171 961
Kilograms 75 500 75 500 73 500 73 500 73 500Maximum LandingWeight (MLW) Pounds 166 449 166 449 162 040 162 040 162 040
Kilograms 71 500 71 500 69 500 69 500 69 500Maximum Zero FuelWeight (MZFW) Pounds 157 630 157 630 153 221 153 221 153 221
Aircraft CharacteristicsWV010 WV011
Kilograms 85 400 93 900Maximum Ramp Weight (MRW)Maximum Taxi Weight (MTW) Pounds 188 275 207 014
Kilograms 85 000 93 500Maximum Takeoff Weight (MTOW)
Pounds 187 393 206 132Kilograms 77 800 77 800Maximum Landing Weight (MLW)
Pounds 171 520 171 520
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
Aircraft CharacteristicsWV010 WV011
Kilograms 73 800 73 800Maximum Zero Fuel Weight (MZFW)
Pounds 162 701 162 701
**ON A/C A321-100
3. The following table provides characteristics of A321-100 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard SeatingCapacity
Single-class220
Liters 23 700 - 26 692* - 29 684**US gallons 6 261 - 7 051* - 7 842**
Kilograms(density =0.785 kg/l)
18 604 - 20 953* - 23 301**
Usable Fuel Capacity
Pounds 41 015 - 46 193* - 51 370**Cubic meters 418Pressurized Fuselage
Volume (A/C nonequipped)
Cubic feet14 762
Cubic meters 155Passenger CompartmentVolume Cubic feet 5 474
Cubic meters 9Cockpit VolumeCubic feet 318Cubic meters 22.81Usable Volume, FWD CCCubic feet 806Cubic meters 23.03Usable Volume, AFT CCCubic feet 814Cubic meters 5.88Usable Volume, Bulk CCCubic feet 208Cubic meters 25.42Water Volume, FWD CCCubic feet 897.7Cubic meters 25.69Water Volume, AFT CCCubic feet 907.2Cubic meters 7.76Water Volume, Bulk CCCubic feet 274
* OPTION: 1 ACT** OPTION: 2 ACT
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
4. The following table provides characteristics of A321-200 Models, these data are common to eachWeight Variant:
Aircraft CharacteristicsStandard SeatingCapacity
Single-class220
Liters 23 700 - 26 692* - 29 684**US gallons 6 261 - 7 051* - 7 842**
Kilograms(density =0.785 kg/l)
18 604 - 20 953* - 23 301**
Usable Fuel Capacity
Pounds 41 015 - 46 193* - 51 370**Cubic meters 418Pressurized Fuselage
Volume (A/C nonequipped)
Cubic feet14 762
Cubic meters 155Passenger CompartmentVolume Cubic feet 5 474
Cubic meters 9Cockpit VolumeCubic feet 318Cubic meters 22.81Usable Volume, FWD CCCubic feet 806Cubic meters 23.03Usable Volume, AFT CCCubic feet 814Cubic meters 5.88Usable Volume, Bulk CCCubic feet 208Cubic meters 25.42Water Volume, FWD CCCubic feet 897.7Cubic meters 25.69Water Volume, AFT CCCubic feet 907.2Cubic meters 7.76Water Volume, Bulk CCCubic feet 274
* OPTION: 1 ACT** OPTION: 2 ACT
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-2-0 General Aircraft Dimensions
**ON A/C A321-100 A321-200
General Aircraft Dimensions
1. This section provides General Aircraft Dimensions.
2-2-0Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
12.45 m(40.85 ft)
34.10 m(111.88 ft)
16.90 m(55.45 ft)
5.07 m(16.63 ft)
5.87
m(1
9.26
ft)
4.14
m(1
3.58
ft)
N_AC_020200_1_0050101_01_03
7.59 m(24.90 ft)
0.93 m(3.05 ft)
0.50 m(1.64 ft)
8.97 m(29.43 ft)
General Aircraft DimensionsWing Tip Fence (Sheet 1 of 4)
FIGURE-2-2-0-991-005-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
RELATED TO AIRCRAFT ATTITUDE AND WEIGHTN_AC_020200_1_0050104_01_00
44.50 m
(146 ft)
15.46 m
(50.72 ft)
15.39 m
(50.49 ft)
CFM56
V2500
11.9
1 m
(39.
07 ft
)
8.30
m
(27.
23 ft
)
5.75
m
(18.
86 ft
)
3.95
m
(12.
96 ft
)
4.87
m
(15.
98 ft
)
General Aircraft DimensionsWing Tip Fence (Sheet 2 of 4)
FIGURE-2-2-0-991-005-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
16.90 m
(55.45 ft)
5.07 m
(16.63 ft)
5.87
m
(19.
26 ft
)
4.14
m
(13.
58 ft
)
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)
N_AC_020200_1_0050103_01_01
8.97 m(29.43 ft)
3.79 m(12.43 ft)
2.43 m(7.97 ft)
General Aircraft DimensionsSharklet (Sheet 3 of 4)
FIGURE-2-2-0-991-005-A01
2-2-0Page 4
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
RELATED TO AIRCRAFT ATTITUDE AND WEIGHT
44.50 m(146 ft)
15.46 m(50.72 ft)
15.39 m(50.49 ft)
CFM56
V2500
11.9
1 m
(39.
07 ft
)
8.30
m
(27.
23 ft
)
5.75
m(1
8.86
ft)
3.95
m
(12.
96 ft
)
4.87
m
(15.
98 ft
)
N_AC_020200_1_0050105_01_00
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)
27.72 m(90.94 ft)
General Aircraft DimensionsSharklet (Sheet 4 of 4)
FIGURE-2-2-0-991-005-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-3-0 Ground Clearances
**ON A/C A321-100 A321-200
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
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
A
CG 25%m
FWD CG 17.5%ft
FWD CG 19% AFT CG 36.9%
11.486.896.046.53
19.6220.112.332.925.779.02
10.4311.557.41
BC1C2D1D2
E (CFM)E (IAE)
FF1F2F3G
3.392.001.731.885.876.030.600.781.652.643.073.412.16
3.482.071.791.825.935.960.610.791.632.633.053.382.10
3.472.051.781.825.925.960.600.781.622.623.05
12.24H 3.63 3.53
3.382.093.53
39.70J 11.99 11.86 11.8512.83K1 3.80 3.77 3.7616.01K2 4.77 4.74 4.7318.31L 5.47 5.34 5.347.64M 2.22 2.14 2.14
13.16N 3.90 3.91 3.9014.11P 4.19 4.30 4.29
AFT CG 38%
15.94Q 4.76 4.61 4.6111.71R 3.46 3.49 3.48
3.391.991.731.875.876.010.590.771.642.633.063.402.143.61
11.973.794.765.452.203.894.194.733.45
P B C1 R E N G D2 M Q JD1 C2
L F1 F2 F3 K1 K2F
3.502.101.841.995.986.130.710.891.762.753.183.522.263.73
12.103.914.885.582.334.014.304.863.57
11.126.565.686.17
19.2619.781.972.565.418.6610.0711.197.0911.9139.3412.4715.6517.957.28
12.8013.7515.6211.35
11.426.795.875.97
19.4619.552.002.595.358.6310.0111.096.8911.5838.9112.3715.5517.527.02
12.8314.1115.1211.45
11.126.535.686.14
19.2619.721.942.535.388.63
10.0411.157.02
11.8439.2712.4315.6217.887.22
12.7613.7515.5211.32
11.386.735.845.9719.4219.551.972.565.318.6010.0111.096.8611.5838.8812.3415.5217.527.02
12.8014.0715.1211.42
m ft m ft m ft m ft4.132.712.432.436.586.581.241.422.263.253.684.012.714.13
12.454.385.355.932.754.544.965.204.13
13.558.897.977.97
21.5921.594.074.667.41
10.6612.0713.168.8913.5540.8514.3717.5519.469.02
14.8916.2717.0613.55
m ft
NOTE: PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
A/C JACKED FDLA/CCONFIG−URATION
47 t 89 tMRW
94 tMRW
= 4.60 m(15.09 ft)
N_AC_020300_1_0050101_01_04
A H
Ground ClearancesFIGURE-2-3-0-991-005-A01
2-3-0Page 2
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_020300_1_0300101_01_00
A
CG 25%m
FWD CG 17.5%ft
FWD CG 19% AFT CG 36.9%
11.486.896.046.53
19.6220.112.332.925.779.02
10.4311.557.41
BC1C2D1D2
E (CFM)E (IAE)
FF1F2F3G
3.392.001.731.885.876.030.600.781.652.643.073.412.16
3.482.071.791.825.935.960.610.791.632.633.053.382.10
3.472.051.781.825.925.960.600.781.622.623.05
12.24H 3.63 3.53
3.382.093.53
39.70J 11.99 11.86 11.8513.71K1 4.07 4.04 4.0322.38K2 6.71 6.68 6.6718.31L 5.47 5.34 5.347.64M 2.22 2.14 2.14
13.16N 3.90 3.91 3.9014.11P 4.19 4.30 4.29
AFT CG 38%
15.94Q 4.76 4.61 4.6111.71R 3.46 3.49 3.48
3.391.991.731.875.876.010.590.771.642.633.063.402.143.61
11.974.066.705.452.203.894.194.733.45
3.502.101.841.995.986.130.710.891.762.753.183.522.263.73
12.104.186.825.582.334.014.304.863.57
11.126.565.686.17
19.2619.781.972.565.418.6610.0711.197.0911.9139.3413.3522.0117.957.28
12.8013.7515.6211.35
11.426.795.875.97
19.4619.552.002.595.358.6310.0111.096.8911.5838.9113.2521.9217.527.02
12.8314.1115.1211.45
11.126.535.686.14
19.2619.721.942.535.388.63
10.0411.157.02
11.8439.2713.3221.9817.887.22
12.7613.7515.5211.32
11.386.735.845.9719.4219.551.972.565.318.6010.0111.096.8611.5838.8813.2221.8817.527.02
12.8014.0715.1211.42
m ft m ft m ft m ft4.132.712.432.436.586.581.241.422.263.253.684.012.714.13
12.454.657.295.932.754.544.965.204.13
13.558.897.977.9721.5921.594.074.667.41
10.6612.0713.168.8913.5540.8515.2623.9219.469.02
14.8916.2717.0613.55
m ft
NOTE: PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL.
A/C JACKED FDLA/CCONFIG−URATION
47 t 89 tMRW
94 tMRW
= 4.60 m(15.09 ft)
F3F2F1FL
P A B C1 ER G M H Q JD1
K2
K1
C2N D2
Ground ClearancesGround Clearances with Sharklets
FIGURE-2-3-0-991-030-A01
2-3-0Page 3
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
m ft m m
A
B
C
D
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
E
H
J
F
G
1.95
2.84
2.71
3.74
1.83
2.73
2.60
3.62
1.80
2.70
2.57
3.58
6.40 6.00 5.91
11.7511.8812.27
9.32
8.89
8.96
8.53
8.86
8.43
2.49
3.53
2.37
3.41
2.34
3.37 11.0611.1911.58
8.17 7.78 7.68
1.91 1.79 1.76 5.775.876.27
2.31
2.96
2.19
2.84
2.15
2.79 9.159.329.71
7.58 7.19 7.05
ft ft
N_AC_020300_1_0220101_01_00
EB CFD AGJ H
Ground ClearancesFlaps and Flap Track Fairings When Flaps Fully Extended
FIGURE-2-3-0-991-022-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
2.68
3.07
3.46
2.57
2.96
3.35
2.56
2.94
3.32
8.79 8.43 8.40
10.07
11.35
9.71
10.99
9.65
10.89
L MK
N_AC_020300_1_0230101_01_00
m ft m ft m ft
K
L
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
M
Ground ClearancesFlap Track Fairings Up
FIGURE-2-3-0-991-023-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
4.15
3.81
4.03
3.70 12.14
13.22 4.00
3.67 12.04
13.1213.62
12.50
N P
N_AC_020300_1_0240101_01_00
m ft m ft m ft
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
N
P
Ground ClearancesAileron Down
FIGURE-2-3-0-991-024-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
4.04
3.74
14.63
14.24
13.39
13.25
12.27
4.48
4.35
4.23
4.10
3.97
3.94
3.63
14.70
14.27
13.88
13.45
13.02
12.93
11.91
4.45
4.32
4.20
4.07
3.95
3.92
3.61
14.60
14.17
13.78
13.35
12.96
12.86
11.84
13.784.20
4.34
4.46
4.59 15.06
4.08
VR T U W X Y
N_AC_020300_1_0250101_01_00
m ft m m
A/C IN MAINTENANCECONFIGURATION MID CG
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
X
Y
ft ft
4.33
4.53
14.21
4.42
4.22
14.50
13.85
4.37
4.19
14.34
13.75
14.86
SQ
Q
R
S
V
W
T
U
Ground ClearancesAileron Up and Spoilers 1 to 5 Extended
FIGURE-2-3-0-991-025-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
C’ E’
m ft m ft m ft
MAXIMUM RAMPWEIGHT FWD CG
MAXIMUM RAMPWEIGHT AFT CG
HEIGHT FROM GROUND
2.58
2.98
3.07
2.47
2.88
2.96
2.50
2.89
2.97
8.46 8.10 8.20
9.78
10.07
9.45
9.71
9.48
9.74
A’Z
B’ D’ F’ G’ H’
H’
J’
3.36
3.61
3.85
4.08 13.39
12.63
11.84
11.02 3.25
3.50
3.74
3.96 12.99
12.27
11.48
10.66 3.25
3.49
3.72
3.94 12.93
12.20
11.45
10.66
N_AC_020300_1_0260101_01_00
A/C IN MAINTENANCECONFIGURATION MID CG
J’
Z
A’
D’
B’
C’
E’
F’
G’
Ground ClearancesSlats Extended
FIGURE-2-3-0-991-026-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-0 Interior Arrangements
**ON A/C A321-100 A321-200
Interior Arrangements
1. This section gives the standard interior arrangements configuration.
2-4-0Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-4-1 Passenger Compartment Layout
**ON A/C A321-100 A321-200
Typical Configuration
1. This section gives the typical interior configuration.
2-4-1Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
G
FW
D P
AS
SE
NG
ER
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
/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
220
SE
AT
S A
LL T
OU
RIS
T C
LAS
S
28/2
9 in
PIT
CH
. 6 A
BR
EA
ST
. 3−
3
AA
AA
G L
AA
L LL
A
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(4)
AA
TT
EN
DA
NT
SE
AT
(7)
N_AC_020401_1_0040101_01_01
Typical ConfigurationTypical Configuration Single-Class, High Density
FIGURE-2-4-1-991-004-A01
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Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
FW
D P
AS
SE
NG
ER
EM
ER
GE
NC
Y E
XIT
/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
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
16 S
UP
ER
FIR
ST
16
9 E
CO
NO
MY
PA
SS
EN
GE
R S
EA
TS
(18
5 T
OT
AL)
SE
AT
PIT
CH
ES
: FIR
ST
36
in E
CO
NO
MY
32
in
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(3)
LLA
VA
TO
RY
(4)
AA
TT
EN
DA
NT
SE
AT
(6)
G LL
LLA
AA A
A
A
G
G
N_AC_020401_1_0060101_01_05
Typical ConfigurationTypical Configuration Two-Class
FIGURE-2-4-1-991-006-A01
2-4-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-5-0 Passenger Compartment Cross Section
**ON A/C A321-100 A321-200
Passenger Compartment Cross-section
1. This section gives the typical passenger compartment cross-section configuration.
2-5-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-6-0 Cargo Compartments
**ON A/C A321-100 A321-200
Cargo Compartments
1. This section gives the cargo compartments locations, dimensions and loading combinations.
2-6-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
1.81
m(7
1.26
in)
8.15
m(3
20.8
7 in
)11
.4 m
(448
.82
in)
0.86
m(3
3.85
in)
1.81
m(7
1.26
in)
FW
D C
AR
GO
CO
MP
AR
TM
EN
T(5
CO
NT
AIN
ER
S)
AF
T C
AR
GO
CO
MP
AR
TM
EN
T(5
CO
NT
AIN
ER
S)
BU
LK C
AR
GO
CO
MP
AR
TM
EN
T
FR
24A
FR
35.5
FR
47.2
FR
59F
R65
N_AC_020600_1_0040101_01_00
Cargo CompartmentsLocations, Dimensions and Loading Combinations
FIGURE-2-6-0-991-004-A01
2-6-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-0 Door Clearances
**ON A/C A321-100 A321-200
Doors Clearances
1. This section gives doors clearances.
2-7-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-1 Forward Passenger / Crew Doors
**ON A/C A321-100 A321-200
Forward Passenger / Crew Doors
1. This section gives forward passenger / crew doors clearances.
2-7-1Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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)
SEECHAPTER
2.375 m(7 ft 9.48 in)
2−3
1.85 m(6 ft 0.82 in)
0.03 m(1.18 in)
N_AC_020701_1_0040101_01_00
Doors ClearancesForward Passenger / Crew Doors
FIGURE-2-7-1-991-004-A01
2-7-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-2 Emergency Exits
**ON A/C A321-100 A321-200
Emergency Exits
1. This section gives emergency exits doors clearances.
2-7-2Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
2.38 m(7 ft 9.69 in)
2.36 m(7 ft 8.9 in)
0.39 m(1 ft 3.34 in)
0.39 m(1 ft 3.34 in)
0.4 m(1 ft 3.74 in)
0.56 m(1 ft 10 in)
CENTER OF FREE AISLE
13.844 m(45 ft 5 in)
24.791 m(81 ft 4 in)
0.83 m(2 ft 8.67 in)
1.73 m(5 ft 8.1 in)
FROM AIRCRAFT NOSE
FREE AISLE
FREE AISLE FREE AISLE
0.76 m(2 ft 5.91 in)
0.76 m(2 ft 5.91 in)
0.04 m(1.57 in)
0.04 m(1.57 in)
0.56 m(1 ft 10 in)
0.83 m(2 ft 8.67 in)
FROM AIRCRAFT NOSE
CENTER OF
LIMITCRITICAL CLEARANCECRITICAL CLEARANCE
LIMIT
1.73 m(5 ft 8.1 in)
0.43 m(1 ft 4.92 in)
1.52 m(4 ft 11.8 in)
(TOP OF FLOOR)1.52 m
(4 ft 11.8 in)
1.85 m(7.03 in)
2.36 m(7 ft 8.9 in)
A
A
B
B
A A
FWD
N_AC_020702_1_0050101_01_00
B B
Doors ClearancesEmergency Exits
FIGURE-2-7-2-991-005-A01
2-7-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-3 Aft Passenger / Crew Doors
**ON A/C A321-100 A321-200
Aft Passenger / Crew Doors
1. This section gives Aft passenger / crew doors clearances.
2-7-3Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
36.57 m(119 ft 11.7 in)
(FROM NOSE)
2.44 m(8 ft)
1.85 m(6 ft 0.82 in)
0.6 m(1 ft 11.6 in)
(1.18 in)0.03 m
FWD
A A
SEE
2−3CHAPTER
A
A
N_AC_020703_1_0040101_01_00
Doors ClearancesAft Passenger / Crew DoorsFIGURE-2-7-3-991-004-A01
2-7-3Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-4 Forward Cargo Compartment Doors
**ON A/C A321-100 A321-200
Forward Cargo Compartment Door
1. This section gives forward cargo compartment door clearances.
2-7-4Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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)
CFM ENGINE = 6.39 m (20 ft 11.56 in)V2500 ENGINE = 6.3 m (20 ft 8 in)
(FROM NOSE)
FWD
2.71 m(8 ft 10.69 in)
A
A
A A
2−3
SEECHAPTER
N_AC_020704_1_0040101_01_01
Doors ClearancesForward Cargo Compartment Door
FIGURE-2-7-4-991-004-A01
2-7-4Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-5 Aft Cargo Compartment Doors
**ON A/C A321-100 A321-200
Aft Cargo Compartment Door
1. This section gives Aft cargo compartment door clearances.
2-7-5Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
1.82 m(5 ft 11.65 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
29.62 m(97 ft 2.13 in)
A
A
A A
4.69 m(15 ft 4.64 in)
(FROM NOSE)
N_AC_020705_1_0040101_01_00
Doors ClearancesAft Cargo Compartment DoorFIGURE-2-7-5-991-004-A01
2-7-5Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-6 Bulk Cargo Compartment Doors
**ON A/C A321-100 A321-200
Bulk Cargo Compartment Door
1. This section gives the bulk cargo compartment door clearances.
2-7-6Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
0.95 m(3 ft 1.39 in)
0.89 m(2 ft 11 in)
FWD
2.19 m(7 ft 2.22 in)
8.76 m(28 ft 8.88 in)
0.77 m
(2 ft 6.31 in)A
A
2−3
SEECHAPTER A A
N_AC_020706_1_0020101_01_01
Doors ClearancesBulk Cargo Compartment Door
FIGURE-2-7-6-991-002-A01
2-7-6Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-7 Main Landing Gear Doors
**ON A/C A321-100 A321-200
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances.
2-7-7Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
20.62 m(67.6 ft)
1.826 m
(6 ft)
A
GROUND LINE
0.207 m(8.14 in)
0.485 m(1 ft 7.09 in)
NOTE: VALUE OF CG: 25% RC.AIRCRAFT
1.23 m(4 ft 0.42 in)
0.14 m(5.51 in)
84°
1.942 m
(6 ft 4.45 in)
1.761 m(5 ft 9.32 in)
A
N_AC_020707_1_0050101_01_02
Doors ClearancesMain Landing Gear Doors
FIGURE-2-7-7-991-005-A01
2-7-7Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-8 Radome
**ON A/C A321-100 A321-200
Radome
1. This section gives the radome clearances.
2-7-8Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
0.63 m(2 ft 0.79 in)
1.54 m(5 ft 0.62 in)
STA 3500FR1
65°
N_AC_020708_1_0040101_01_00
Doors ClearancesRadome
FIGURE-2-7-8-991-004-A01
2-7-8Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-7-9 APU and Nose Landing Gear Doors
**ON A/C A321-100 A321-200
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances.
2-7-9Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
FR80
FR84
3.42
m(1
1 ft
2.64
in)
4.05
m(1
3 ft
3.44
in)
NOTE: VALUE OF CG: 25% RC.
1.5
m(4
ft 1
1 in
)
1.4
m(4
ft 7
.11
in)
N_AC_020709_1_0040101_01_00
Doors ClearancesAPU and Nose Landing Gear Doors
FIGURE-2-7-9-991-004-A01
2-7-9Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-8-0 Escape Slides
**ON A/C A321-100 A321-200
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 four). Single lane escape slides are installed at
FWD/AFT emergency door.
2-8-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
FWD CABIN ESCAPE SLIDE
AFT CABIN
FWD EMERGENCY ESCAPE SLIDE
ESCAPE SLIDE
AFT EMERGENCY ESCAPE SLIDE
N_AC_020800_1_0070101_01_00
Escape SlidesLocation
FIGURE-2-8-0-991-007-A01
2-8-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
EMERGENCY DESCENT DEVICETHROUGH WINDOW OPENING
N_AC_020800_1_0080101_01_00
GRID EQUALS 1 m (3.28 ft) IN REALITY
Escape SlidesLocation
FIGURE-2-8-0-991-008-A01
2-8-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-9-0 Landing Gear
**ON A/C A321-100 A321-200
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 gear twin wheel landing gears are located under the wing and retract sidewaystowards the fuselage centerline.
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
@A321AIRCRAFT 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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
TORQUELINKS
DOWNLOCKACTUATOR
MAIN FITTING
SHOCK ABSORBER
SIDE STAY
D
ACTUATING CYLINDER
LOCK STAY
DAMPER
A
MAIN DOOR SHOWN OPEN IN GROUND MAINTENANCE POSITION.NOTE:
E
N_AC_020900_1_0160101_01_00
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-2-9-0-991-016-A01
2-9-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
DOORACTUATINGCYLINDER
FLAG
LOCKSTAYACTUATINGCYLINDER
GROUND LOCK SLEEVE
FLAG
BC
LOCKINGPIN
LOCKINGPIN
N_AC_020900_1_0160102_01_00
BOTTOM FILLING ANDCHARGING CONNECTIONMS28889
EDEXAMPLE
TOP FILLING AND CHARGING CONNECTION MS28889
Landing GearMain Landing Gear - Twin Wheel (Sheet 2 of 2)
FIGURE-2-9-0-991-016-A01
2-9-0Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
Y=COMPRESSED
EXTENDED
58.3
0 %
AM
C
3 795 mm
80°30RETRACTION
ANGLE
(36.50 in)927.10 mm
2 868.70 mm(112.94 in)
2 214 mm(87.17 in)
X= 24 513.89 mm(965.11 in)
470.52 mm(18.52 in)
(149.41 in)
N_AC_020900_1_0170101_01_00
Landing GearMain Landing Gear Dimensions - Twin Wheel
FIGURE-2-9-0-991-017-A01
2-9-0Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_020900_1_0180101_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-2-9-0-991-018-A01
2-9-0Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
TOWING LEVER
(NOSE WHEEL STREERINGNORMAL POSITION
(TOWING POSITION)SAFETY PIN
(NOSE WHEEL STEERING DEACTIVATED)TOWING POSITION
E
DOOR HINGE
NLG DOOR
NLG DOORSAFETY PIN
FLAG
LH SYMMETRICALRH SHOWN
FLAG
DOWNLOCKSAFETY PIN
LOCKSTAY
BC
D
OPERATIONAL)CONNECTION MS28889FILLING AND CHARGING
N_AC_020900_1_0180102_01_00
Landing GearNose Landing Gear (Sheet 2 of 2)
FIGURE-2-9-0-991-018-A01
2-9-0Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_020900_1_0190101_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-2-9-0-991-019-A01
2-9-0Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
=
==
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)
24.5
2 m
(80.
45 ft
)
24.3
7 m
(79.
95 ft
)
7.59
m(2
4.90
ft)
=
6.49
m(2
1.29
ft) 3.
79 m
(12.
43 ft
)3.76
m(1
2.34
ft) 2.
95 m
(9.6
8 ft)
2.5
m(8
.20
ft)
MA
IN J
AC
KIN
G P
OIN
T
MA
IN J
AC
KIN
G P
OIN
TM
AIN
JA
CK
ING
PO
INT
FROM X0
FW
D J
AC
KIN
G P
OIN
T
N_AC_020900_1_0260101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-026-A01
2-9-0Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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)
24
.52
m(8
0.45
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_0270101_01_00
Landing Gear Maintenance PitsMaintenance Pit EnvelopesFIGURE-2-9-0-991-027-A01
2-9-0Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-10-0 Exterior Lighting
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
6 75
13
10
9
8
8
2
12
4
N_AC_021000_1_0130101_01_00
11
1
3
111
3
RH
LH
RH
LH
Exterior LightingFIGURE-2-10-0-991-013-A01
2-10-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
1
2
3
55
N_AC_021000_1_0140101_01_00
7
Exterior LightingFIGURE-2-10-0-991-014-A01
2-10-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
12
11
1313
4
11
9
N_AC_021000_1_0150101_01_00
6
10
Exterior LightingFIGURE-2-10-0-991-015-A01
2-10-0Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
1415 15
8 8
N_AC_021000_1_0200101_01_00
EXAMPLE FOR LIGHT N° 15
CEILING LIGHT
SPOT LIGHT
GROUND
Exterior LightingFIGURE-2-10-0-991-020-A01
2-10-0Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-11-0 Antennas and Probes Location
**ON A/C A321-100 A321-200
Antennas and Probes Location
1. This section gives the location of antennas and probes.
2-11-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
RADIO ALTIMETER(2)
DME(2)PITOT PROBE(1)
PITOT PROBE(3)
DME(1)
TAT PROBE
VHF(1)
TAT PROBE
PITOT PROBE(2)
ADF(1)
ATC(1)
GPS(2)
GPS(1)
VHF(3)
ATC(2)
RADIO ALTIMETER(1)
VHF(2)
WEATHER RADAR
EMERGENCY STATIC PROBE
AOA SENSOR(3) STBY
AOA SENSOR(1)
TCAS TOPELT
MARKER
TCAS BOTTOM
STATIC PROBE(1)
STATIC PROBE(2)
LOCGLIDE
HF
VOREMERGENCY STATIC PROBE
AOA SENSOR(2)
STATIC PROBE(2)
STATIC PROBE(1)
ATC(4)
ATC(3)
NOTE: DEPENDING ON AIRCRAFT CONFIGURATIONN_AC_021100_1_0040101_01_00
Antennas and ProbesLocation
FIGURE-2-11-0-991-004-A01
2-11-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-12-0 Power Plant
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AIR INTAKE FIXEDON ACCESS DOOR
CUT OUT SEALED WITHLABYRINTH GASKET
FRONTFIREWALL
FIREWALL
FIREWALL RH
LOUVER LH
REARFIREWALL
CUT OUT SEALED WITHLABYRINTH GASKET
LH ACCESS DOOR NOTE:
B
UPPER
A
/FR80
/ FR84
NOT SHOWN FOR CLARITY
Z310
STA45879
STA44229
A
315AL
RH ACCESS DOOR316AR
N_AC_021200_1_0070101_01_00
Auxiliary Power UnitAccess Doors
FIGURE-2-12-0-991-007-A01
2-12-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
FR
87/
ST
A47
047
FR
84/
ST
A45
879
FR
80/
ST
A44
229
FR
78/
ST
A43
591
FR
77/
ST
A43
479
N_AC_021200_1_0080101_01_00
Auxiliary Power UnitGeneral Layout
FIGURE-2-12-0-991-008-A01
2-12-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT 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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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_0350101_01_00
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-035-A01
2-12-0Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
FAN COWL
CENTERBODY
FANREVERSER
6°
(3.9 ft)
1.8 m(5.9 ft)
2.07 m(6.8 ft)
2.1 m(6.9 ft)
BLOCKER DOOREXTENDED
PRIMARYNOZZLE
15.46 m(50.7 ft)
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)
1.6 m(5.2 ft)
ENGINE AIRINLET COWL
A
A
B
B
C
C
D
D
0.57 m(1.9 ft)
A A
B B D DC CN_AC_021200_1_0360101_01_00
1.2 m
1.9 m(6.2 ft)
Power Plant HandlingMajor Dimensions - CFM56 Series Engine
FIGURE-2-12-0-991-036-A01
2-12-0Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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_0370101_01_00
Power Plant HandlingFan Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-037-A01
2-12-0Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
3.7 m(12.1 ft)
3.3 m(10.8 ft)
(3 ft)0.9 m
CAUTIONDO NOT ACTUATE SLATS:
− WITH THRUST REVERSER COWLS 45° OPEN POSITION− WITH BLOCKER DOORS OPEN AND THRUST REVERSER COWLS AT 35° AND 45° OPEN POSITION
APPROXIMATE DIMENSIONSNOTE:
GROUND
0.5 m(1.6 ft)
0.7 m(2.3 ft)
1 m(3.3 ft)
45°35°
1 m(3.3 ft)
N_AC_021200_1_0380101_01_00
Power Plant HandlingThrust Reverser Cowls - CFM56 Series Engine
FIGURE-2-12-0-991-038-A01
2-12-0Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_021200_1_0390101_01_00
FAN AND BOOSTER COMPRESSOR
COMBUSTOR
HPTURBINE
LPTURBINE
TURBINEFRAME
A
3 101 mm(122.1 in)
1 715 mm(67.5 in)
1 067 mm(42.0 in)
DRIVEACCESSORY
FWD
A
Power Plant HandlingMajor Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-039-A01
2-12-0Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
0.5°6°
C
C
D
D
E
E
F
F
U
V
5.26 m(17.26 ft)
1.50 m(4.92 ft)
5.25 m(17.22 ft)
W
B
BA
A
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
TCH 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 −−−− −−−−
15.37 m(50.43 ft)
DISTANCE FROMTHE NOSE
A−A
B−B
C−C
D−D
E−E
F−F
NOTE: ALL SIZES GIVEN ON THIS ILLUSTRATION ARE APPROXIMATE
N_AC_021200_1_0400101_01_00
Power Plant HandlingMajor Dimensions - IAE V2500 Series Engine
FIGURE-2-12-0-991-040-A01
2-12-0Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_021200_1_0410101_01_00
2 m
(6.6 ft)
CLOSEDWL100
1.6 m(5.2 ft) 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:
Power Plant HandlingFan Cowls - IAE V2500 Series Engine
FIGURE-2-12-0-991-041-A01
2-12-0Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
APPROXIMATE DIMENSIONSNOTE:N_AC_021200_1_0420101_01_00
1.1 m(3.6 ft)
1 m(3.3 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
Power Plant HandlingThrust Reverser Halves - IAE V2500 Series Engine
FIGURE-2-12-0-991-042-A01
2-12-0Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-13-0 Leveling, Symmetry and Alignment
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_021300_1_0050101_01_00
12
11
FR30
FR48
2LH
RIB10
2RH
RIB10
FR47
FR32
Location of the Leveling PointsFIGURE-2-13-0-991-005-A01
2-13-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
2-14-0 Jacking
**ON A/C A321-100 A321-200
Jacking for Maintenance
1. Jacking for Maintenance
A. General
The A321 aircraft can be jacked:- at no more than the maximum permitted aircraft weight for jacking (69 000 kg (152 119
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 middle 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 structure isprovided 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
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@A321AIRCRAFT 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)
33 400 daN(75 086 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 69 000 kg (152 119 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, shoring cradles shall be placed under each wing andfuselage as necessary.
NOTE : Aircraft must not be lifted or supported by the wings or fuselage alone without adequatesupport of the other.
A. Under the FuselageFrames 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 33 1 700 daN (3 822 lbf)
FR 62/63 4 200 daN (9 442 lbf)
2-14-0Page 2
Jun 01/12
@A321AIRCRAFT 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 29 to 34 1 330 daN (2 990 lbf) each
FR 56 to 60 2 600 daN (5 845 lbf) each
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 certainmaintenance and repair work. These are used to oppose the deflections of the wings and reducethe stresses to 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 A321 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 engines may be installed if their 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
Jun 01/12
@A321AIRCRAFT 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.
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
2.74 m(8.99 ft)
FWD JACKINGPOINT
21.83 m(71.62 ft)
WING JACKINGPOINT
6.5 m(21.33 ft)
WING JACKINGPOINT
SAFETYPOINT
39.5 m(129.59 ft)
CL
N_AC_021400_1_0380101_01_00
Jacking for MaintenanceJacking Point Location
FIGURE-2-14-0-991-038-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
A
N_AC_021400_1_0390101_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-2-14-0-991-039-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
A
A
N_AC_021400_1_0400101_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-2-14-0-991-040-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
Z−748.44
SPHERICAL RADIUS 19 mm (0.75 in)(19 D535−71 595)
X =
42
040
A
A
126.15 mm
N_AC_021400_1_0410101_01_00
(4.97 in)
Jacking for MaintenanceSafety Stay
FIGURE-2-14-0-991-041-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
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:
M
L
L M
FLAT TIRES
AND RETRACTED LANDING GEARS
AND FLAT TIRES
1 560 mm(61.42 in)
2 846 mm(112.05 in)
3 183 mm(125.31 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)
2 976 mm(117.17 in)
N
N
N_AC_021400_1_0420101_01_00
Jacking for MaintenanceJacking Design
FIGURE-2-14-0-991-042-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
80
70
60
50
40
30
200 3 4 5 6 7 8 9 101 2
30
35
40
45
50
55
60
65
70
75
80051015202530
354045
20
30
40
50
60
70
80
AIR
CR
AF
T W
EIG
HT
(kg
x 1
000)
AIRCRAFT CG (%RC)
PERMISSIBLE WIND SPEED (km/h)
LOA
D O
N W
ING
JA
CK
ING
PO
INT
S (
kg x
100
0)
LOAD ON FORWARD FUSELAGE JACKING POINT (kg x 1000)
TIP UPSECURITYMARGIN
ASSUME AIRCRAFT WITH GROSS WEIGHT OF 67 500 kg AND CENTER OF GRAVITYAT 23 % RC . THE REACTION AT THE WING JACKING POINTS IS 62 750 kg(31 375 kg PER SIDE) AND THE REACTION AT THE FORWARD FUSELAGEJACKING POINT IS 4 750 kg . IF THE AIRCRAFT MUST BE LIFTED OUTSIDE THE WIND
A
BC
D
EXAMPLE:
SPEED MUST NOT BE IN EXCESS OF 70 km/h.
N_AC_021400_1_0430101_01_00
A
C
D
B
Loads at the Aircraft Jacking PointsWing Jacking Point and Forward Fuselage Jacking Point
FIGURE-2-14-0-991-043-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
(SAFETY STAY)
RIB13
RIB22
RIB13
RIB22
RIB4
FR29
FR56
FR60
FR34
FR9
RIB4
N_AC_021400_1_0440101_01_00
NOTE: THE SHORING CRADLE MUST BE INSTALLED AT THE EXACT LOCATION OF THE FRAME.
FR73 FR74/
Jacking for MaintenanceLocation of Shoring CradlesFIGURE-2-14-0-991-044-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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 69 000 kg (152 119 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.
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
49 x 18 R22
563 mm(22.17 in)
38 mm(1.5 in)
DIA. BALL
25 mm (1 in)
205 mm(8.07 in)
186 mm(7.32 in)
ON THE RIM
200 mm(7.87 in)FULLY
RETRACTED
1 270 x 455 R22
600 mm(23.62 in)FULLY
EXTENDED
TWIN WHEEL TRACK IS 927 mm (36.5 in).NOTE:
N_AC_021400_1_0240101_01_00
FLAT TIRES
INFLATED TIRES
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.
Landing Gear Jacking for Wheel ChangeMLG Jacking Point Location - Twin Wheels
FIGURE-2-14-0-991-024-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
MLG TIRE 1 270 x 455−R22
655 mm(25.79 in)
TWIN WHEEL TRACK
DOUBLE FLAT MLG TIRES
FORK
CONTOUR OF TIRES ON GROUND
CANTILEVERARM
1 620 mm(63.78 in)
APPROX
205 mm (8.07 in)(186 mm (7.32 in)
ON RIM)
563 mm(22.17 in)
FWD
N_AC_021400_1_0250101_01_00
25 mm(1 in)
927 mm(36.5 in)
MIN25 mm(1 in)MIN
25 mm(1 in)
409 mm(16.1 in)
Landing Gear Jacking for Wheel ChangeMLG Jacking with Cantilever Jack - Twin Wheels
FIGURE-2-14-0-991-025-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_021400_1_0260101_01_00
40 9050 60 70 8030
45
40
35
30
25
20
15
10
CG 40%CG 30%CG 25%
CG 20%CG 17%
AIRCRAFT WEIGHT
CG POSITION
LOAD AT MLGJACKING POINT
(x 1 000 kg)
180170160150140130120110100908070 x 1 000 lb190 200
x 1 000 kg
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking PointsFIGURE-2-14-0-991-026-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
45
40
35
30
25
20
15
10
50
40 9050 60 70 80
AIRCRAFT WEIGHT
LOAD AT MLGJACKING POINT
(x 1 000 kg) CG POSITION
CG 38.0%
CG 25.0%CG 17.5%
18017016015014013012011010090 x 1 000 lb190 200
x 1 000 kg
N_AC_021400_1_0270101_01_00
Landing Gear Jacking for Wheel ChangeLoads at MLG Jacking PointsFIGURE-2-14-0-991-027-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
APPROX326 mm
(12.83 in)38 mm(1.5 in)
DIA. BALLSAE AS 33559
25 mm(1 in)
128 mm(5.07 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:
FWD
500 mm (19.69 in)
289 mm MAX (11.38 in)
INFLATED TIRESFLAT TIRES
198 mm(7.8 in)
264 mm MIN (10.39 in)
N_AC_021400_1_0280101_01_00
A
A
Landing Gear Jacking for Wheel ChangeNLG Jacking - Point LocationFIGURE-2-14-0-991-028-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
LOAD ATJACKING POINT
(x 1 000 kg) CG POSITION
CG 17.5%
CG 25.0%
CG 38.0%
7
6
5
4
3
2
1
0
8
9
10
9050 60 70 8040
AIRCRAFT WEIGHT
18017016015014013012011010090 x 1 000 lb190 200
x 1 000 kg
N_AC_021400_1_0290101_01_00
Landing Gear Jacking for Wheel ChangeLoads at NLG Jacking PointsFIGURE-2-14-0-991-029-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT PERFORMANCE
3-1-0 General Information
**ON A/C A321-100 A321-200
General Information
1. This section gives standard day temperatures.
Section 3-2 indicates payload range information at specific altitudes recommended for long rangecruise with a given fuel reserve condition.
Section 3-3 represents FAR take-off runway length requirements at ISA and ISA +15˚C (+59˚F) forCFM56 and 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
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-0 Payload / Range
**ON A/C A321-100 A321-200
Payload / Range
1. Payload / Range
3-2-0Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-2-1 ISA Conditions
**ON A/C A321-100 A321-200
ISA Conditions
1. This section gives the payload / range at ISA conditions.
3-2-1Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
(1000 lbs) (1000 kg)
PAYLOAD
50
40
30
20
10
0
60
70
5
10
15
20
25
30
35
93.5t
89t
RANGE(NM)
500 1000 1500 2000 2500 3000 3500 4000
2000 4000 6000 8000
185 PASSENGERS
NOTE:
RANGE(KM)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
N_AC_030201_1_0100101_01_00
Payload / RangeCFM56-5B series engine
FIGURE-3-2-1-991-010-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
(1000 kg)
PAYLOAD
50
40
30
20
10
0
60
70
5
10
15
20
25
30
35
500 1000 1500 2000 2500 3000 3500 4000
2000 4000 6000 8000
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
93.5t
89t
(1000 lbs)
185 PASSENGERS
RANGE(NM)
RANGE(KM)
NOTE:
N_AC_030201_1_0110101_01_00
Payload / RangeIAE V2500-A5 series engineFIGURE-3-2-1-991-011-A01
3-2-1Page 3
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-0 FAR / JAR Takeoff Weight Limitation
**ON A/C A321-100 A321-200
FAR / JAR Take-off Weight Limitation
1. FAR / JAR Take-off Weight Limitation
3-3-0Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-1 ISA Conditions
**ON A/C A321-100 A321-200
ISA Conditions
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
16141210864
54321
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
RUNWAY LENGTH
1000 ft
1000 m
8
6
4
20
N_AC_030301_1_0070101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA Conditions -- CFM56 series engine
FIGURE-3-3-1-991-007-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
16141210864
54321
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
RUNWAY LENGTH
1000 ft
1000 m
8
6
4
2
0
N_AC_030301_1_0080101_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-3-3-1-991-008-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-3-2 ISA +15˚C (+59˚F) Conditions
**ON A/C A321-100 A321-200
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
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
4
1
6 8 10 12 14
2 3 4 5
16
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
200
190
180
170
160
150
140
130
120
110
210
220
230
40
50
60
70
80
90
100
110
8
6
4
2
0
N_AC_030302_1_0070101_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-3-3-2-991-007-A01
3-3-2Page 2
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
16141210864
54321
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
RUNWAY LENGTH
1000 ft
1000 m
8
6
4
2
0
N_AC_030302_1_0080101_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-3-3-2-991-008-A01
3-3-2Page 3
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-0 FAR / JAR Landing Field Length
**ON A/C A321-100 A321-200
FAR / JAR Landing Field Length
1. FAR / JAR Landing Field Length
3-4-0Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-4-1 ISA Conditions
**ON A/C A321-100 A321-200
ISA Conditions
1. This section gives the landing field length.
3-4-1Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
F.A
.R. L
AN
DIN
G F
IELD
LE
NG
TH
GROSS WEIGHT
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
km 1000 ft
2.5
2
1.5
13
4
5
6
7
8
80 100 120 140 160 180
30 40 50 60 70 80 90
(1000 lb)
GROSS WEIGHT(1000 kg)
10 8 6 42
SEALEVEL
N_AC_030401_1_0070101_01_00
ISA CONDITIONSSLATS 27 DEG.FLAPS 40 DEG.
AIRFIELD ELEVATION(1000 ft)
FAR / JAR Landing Field LengthCFM56 series engine
FIGURE-3-4-1-991-007-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AIRFIELD ELEVATION(1000 ft)
ISA CONDITIONSSLATS 27 DEG.FLAPS 40 DEG.
SEA
GROSS WEIGHT
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
km 1000 ft
2.5
2
1.5
13
4
5
6
7
8
80 100 120 140 160 180
30 40 50 60 70 80 90
10 8 6 4
2
(1000 lb)
GROSS WEIGHT(1000 kg)
LEVEL
N_AC_030401_1_0080101_01_00
F.A
.R. L
AN
DIN
G F
IELD
LE
NG
TH
FAR / JAR Landing Field LengthIAE V2500 series engine
FIGURE-3-4-1-991-008-A01
3-4-1Page 3
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
3-5-0 Final Approach Speed
**ON A/C A321-100 A321-200
Final Approach Speed
1. This section gives the final approach speed.
3-5-0Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
10080 100 120 140 160 180 200
GROSS WEIGHT(1000 lb)
GROSS WEIGHT(1000 kg)
110
120
130
140
150
160
C.A.S (Kts)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
40 50 60 70 80 90 100
LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 40 DEG.
SEA LEVEL
N_AC_030500_1_0070101_01_00
Final Approach SpeedCFM56 series engine
FIGURE-3-5-0-991-007-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
10080 100 120 140 160 180 200
GROSS WEIGHT(1000 lb)
GROSS WEIGHT(1000 kg)
110
120
130
140
150
160
C.A.S (Kts)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
40 50 60 70 80 90 100
LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 40 DEG.
SEA LEVEL
N_AC_030500_1_0080101_01_00
Final Approach SpeedIAE V2500 series engine
FIGURE-3-5-0-991-008-A01
3-5-0Page 3
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-2-0 Turning Radii
**ON A/C A321-100 A321-200
Turning Radii
1. This section gives the turning radii.
4-2-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
R4
R3
16.9 m
(55.45 ft)
(24.9 ft)7.59 m
R6
R5
R1
R2
50°
60°
70°
N_AC_040200_1_0070101_01_02
NOTE:
TURN TYPE:
1. ASYMMETRIC THRUST DIFFERENTIAL BRAKING
FOR STEERING DIMENSION TABLE SEE SHEET 2.
(PIVOTTING ON ONE MAIN GEAR).
2. SYMMETRIC THRUST NO BRAKING.
APPLICABLE FOR A321−100 AND A321−200.
Turning Radii, No Slip AngleFIGURE-4-2-0-991-007-A01
4-2-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
MA
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R6
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mft
R1
RM
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ST
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706560555045403525 3020
73.1
71.6
67.4
63.0
58.3
53.6
48.8
44.0
39.2
29.4
34.3
24.5
19.6
22222222222
2.0
2.5
3.9
5.5
7.3
9.4
11.7
14.4
17.6
21.7
26.9
34.0
44.3
78131824313847587188112
145
9.6
10.1
11.5
13.1
14.9
16.9
19.3
22.0
25.2
29.3
34.5
41.6
51.9
32333843495663728396113
136
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17.8
17.9
18.4
19.1
20.0
21.2
22.7
24.6
27.0
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34.7
41.1
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58596163667074818999114
135
166
22.6
23.1
24.5
26.1
27.8
29.8
32.1
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38.1
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47.3
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747680859198105
114
125
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155
178
212
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23.9
25.3
26.9
28.6
30.7
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35.6
38.9
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7778838894101
108
117
128
141
158
181
215
22.6
22.7
23.1
23.6
24.3
25.3
26.5
28.1
30.2
33.1
37.2
43.1
52.3
747476778083879299109
122
141
172
24.5
24.7
25.4
26.3
27.4
28.6
30.2
32.1
34.6
37.8
42.2
48.5
57.9
80818386909499105
114
124
139
159
190
7065605550
1
68.4
63.6
58.8
54.0
49.1
11111
75 (
MA
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3.6
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11.5
1217233038
11.2
12.9
14.7
16.8
19.1
3742485563
18.3
19.0
19.9
21.1
22.6
6062656974
24.1
25.8
27.6
29.7
32.0
79859197105
25.0
26.6
28.5
30.5
32.8
828793100
108
23.0
23.5
24.2
25.2
26.4
7577808387
25.3
26.2
27.2
28.5
30.1
8386899499
N_AC_040200_1_0080101_01_01
AB
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Turning Radii, No Slip AngleFIGURE-4-2-0-991-008-A01
4-2-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A321-100 A321-200
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
R6
R3
R5
R416.9 m
PAVEMENTWIDTH FOR180° TURN
MINIMUM
NOTE:MEASURED FROM OUTSIDE FACE OF TIRE.THEORETICAL CENTER OF TURNFOR MINIMUM TURNING RADIUS.SLOW CONTINUOUS TURNING,APPROXIMATELY IDLE THRUSTON ALL ENGINES.NO DIFFERENTIAL BRAKING.
NOSE GEAR RADII TRACK
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
73.1°
71.6°
m
m
ft
ft
Y
5.1
5.6
17
18
A
27.7
28.3
91
93
R3NLG
17.8
17.9
58
59
R4 WINGWING TIPFENCE
22.6
23.1
74
76
SHARKLET
23.4
23.9
77
78
R5NOSE
22.6
22.7
74
74
R6THS
24.5
24.7
80
81
(55 ft)
STEERINGANGLE 75°
Y
A
OUTSIDE FACE OF TIRE
EFFECTIVETURN
N_AC_040300_1_0040101_01_02
Minimum Turning RadiiFIGURE-4-3-0-991-004-A01
4-3-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A321-100 A321-200
Visibility from Cockpit in Static Position
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
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IND
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PIL
OT
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TA
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ITIO
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AS
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CA
PT
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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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A321-100 A321-200
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A321-100 A321-200
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
FAA LEAD−IN FILLET
L = 45 m (150 ft)
30 m
TAXIWAYCENTERLINE
RUNWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
APPROX 1.9 m(6 ft)
NOTE: FAA GROUP III FACILITIES.
ADDITIONAL FILLET TO MEET3 m (10 ft) EDGE CLEARANCE
N_AC_040501_1_0060101_01_02
NLG PATH
MLG PATH
15 m(50 ft)
(100 ft)
135˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-1-991-006-A01
4-5-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
RUNWAY CENTERLINE
TURN R = 30 m(100 ft)
FILLET R = 16.5 m(55 ft)
FAA LEAD−IN FILLET
L = 45 m (150 ft)
APPROX 3 m(10 ft)
TAXIWAYCENTERLINE
30 m
NOTE: FAA GROUP III FACILITIES.
N_AC_040501_1_0070101_01_02
NLG PATH
MLG PATH
15 m(50 ft)
(100 ft)
135˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-1-991-007-A01
4-5-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A321-100 A321-200
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
APPROX 3.7 m(12 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.N_AC_040502_1_0060101_01_02
NLG PATH
MLG PATH
30 m(100 ft)
15 m(50 ft)
90˚ Turn - Runway to TaxiwayCockpit Over Centerline Method
FIGURE-4-5-2-991-006-A01
4-5-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
APPROX 9.2 m(30 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
RUNWAY CENTERLINE
FAA LEAD−IN FILLETL = 45 m (150 ft)
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.N_AC_040502_1_0070101_01_02
NLG PATH
MLG PATH
30 m(100 ft)
15 m(50 ft)
90˚ Turn - Runway to TaxiwayJudgemental Oversteering Method
FIGURE-4-5-2-991-007-A01
4-5-2Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A321-100 A321-200
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
45 m(150 ft)
RUNWAY CENTERLINE
3.45 m(11 ft)
14.9 m(49 ft)
R3 = 17.6 m(58 ft)
R5 = 22.6 m(74 ft)
NOTE: TYPE 1 VALUES.
N_AC_040503_1_0020101_01_02
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
WINGTIP FENCES:R4 = 22.7 m (74 ft)SHARKLETS:R4 = 23.4 m (77 ft)
R4
180˚ Turn on a RunwayEdge of Runway Method (Sheet 1 of 2)
FIGURE-4-5-3-991-002-A01
4-5-3Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
12 m(39 ft)
45 m(150 ft)
4.4 m(14 ft)
NOTE: TYPE 1 VALUES.
6.3 m(21 ft)
RUNWAY CENTERLINE
25°
N_AC_040503_1_0020102_01_00
NLG PATH
WINGTIP PATH:
NOSE PATH
MLG PATH
WINGTIP FENCES:R4 = 22.7 m (74 ft)SHARKLETS:R4 = 23.4 m (77 ft)
R3 = 17.6 m(58 ft)
R5 = 22.6 m(74 ft)
R4
180˚ Turn on a RunwayCenter of Runway Method (Sheet 2 of 2)
FIGURE-4-5-3-991-002-A01
4-5-3Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-4 135˚ Turn - Taxiway to Taxiway
**ON A/C A321-100 A321-200
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway.
4-5-4Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
FAA LEAD−IN FILLET
APPROX 2.3 m(8 ft)
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
FILLET R = 16.5 m
TURN R = 30 m
ADDITIONAL FILLET TO MEET3 m (10 ft) EDGE CLEARANCE
15 m(50 ft)
15 m(50 ft)
N_AC_040504_1_0070101_01_00
L = 45 m (150 ft)
(55 ft)
(100 ft)
135˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-4-991-007-A01
4-5-4Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
NLG PATH
MLG PATH
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES
TAXIWAY CENTERLINE
FILLET R = 16.5 m
TURN R = 30 m
FAA LEAD−IN FILLET
APPROX 3 m
15 m(50 ft)
15 m(50 ft)
N_AC_040504_1_0070102_01_00
(55 ft)
(100 ft)
L = 45 m (150 ft)
(10 ft)
135˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-4-991-007-A01
4-5-4Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-5-5 90˚ Turn - Taxiway to Taxiway
**ON A/C A321-100 A321-200
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-5Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATHTAXIWAY CENTERLINE
APPROX 3.2 m(10 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft)
15 m(50 ft)
15 m(50 ft)
N_AC_040505_1_0040101_01_00
90˚ Turn - Taxiway to TaxiwayCockpit Over Centerline Method (Sheet 1 of 2)
FIGURE-4-5-5-991-004-A01
4-5-5Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
TAXIWAY CENTERLINE
NOTE: FAA GROUP III FACILITIES.
NLG PATH
MLG PATHTAXIWAY CENTERLINE
APPROX 9.1 m(30 ft)
FILLET R = 16.5 m(55 ft)
TURN R = 30 m(100 ft)
FAA LEAD−IN FILLETL = 45 m (150 ft)
15 m(50 ft)
15 m(50 ft)
N_AC_040505_1_0040102_01_00
90˚ Turn - Taxiway to TaxiwayJudgemental Oversteering Method (Sheet 2 of 2)
FIGURE-4-5-5-991-004-A01
4-5-5Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A321-100 A321-200
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
4-6-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
RUNWAY CENTERLINETAXIWAY
CENTERLINE
HOLDING POINT
12.2 m
NOTE: APPLICABLE FOR A321−100 AND A321−200.
N_AC_040600_1_0040101_01_02
61 m(200 ft)
190 m
23 m(75 ft)
45 m(150 ft)
90 m61 m
(200 ft)
6.1 m(20 ft)
6.1 m(20 ft)
190 m(625 ft)
(40 ft)
90 m(300 ft)
Runway Holding Bay (Apron)FIGURE-4-6-0-991-004-A01
4-6-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
4-7-0 Parking
**ON A/C A321-100 A321-200
Airplane Parking
1. The following figures and charts show the rectangular space required for parking against the terminalbuilding.
4-7-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
3.05 m(10 ft)(REF)
3.05 m(10 ft)
AIRPLANE MODEL MIN LINEUP DISTANCE
ASDAm (ft)
A321−100 ANDA321−200
ABREVIATIONS TODA (TAKEOFF DISTANCE ADJUSTMENT)ASDA (ACCELERATE−STOP DISTANCE ADJUSTMENT)
19.92 m(65 ft 4.8 in)
36.83 m(121 ft 2.4 in)
90°
MAX. EFF. STEERINGANGLE DEGREES
19.9(65.4)
36.8(121.2)75°
TODAm (ft)
LINEUP DISTANCES FOR A321−100 AND A321−200 USING 75° STEERING AND NO SLIP ON NOSE TIRES
60 m(196 ft 10.8 in)
RUNWAYWIDTH
(REF)
N_AC_040700_1_0110101_01_01
Runway Length AlterationsLine Up Distances -- 90˚ TurnFIGURE-4-7-0-991-011-A01
4-7-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
32.63 m(107 ft 1.2 in)
20.73 m(68 ft)
3.05 m(10 ft)(REF)
END OF RUNWAY
EDGE OFRUNWAY
AIRPLANE MODEL MIN LINEUP DISTANCE NOMINAL LINEUP DISTANCE
180° ASDAm (ft) m (ft) ASDA
m (ft)
A321−100 ANDA321−200
26.9(88.3)
43.8(143.8)
32.6(107.1) AS MINIMUM AS MINIMUM
ABREVIATIONS TODA (TAKEOFF DISTANCE ADJUSTMENT)ASDA (ACCELERATE−STOP DISTANCE ADJUSTMENT)
TODAm (ft)
TODAm (ft)
LINEUP DISTANCES FOR A321−100 AND A321−200USING 75° STEERING AND NO SLIP ON NOSE TIRES
REQ’D MIN PAVEMENT WIDTH
43.82 m(143 ft 9.6 in)
26.9 m(88 ft 3.6 in)
3.05 m(10 ft)(REF)3.05 m
(10 ft)(REF)
N_AC_040700_1_0120101_01_01
Runway Length AlterationsLine Up Distances -- 180˚ Turn
FIGURE-4-7-0-991-012-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
**ON A/C A321-100 A321-200
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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5-1-0 Servicing Arrangements
**ON A/C A321-100 A321-200
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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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A321-100 A321-200
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
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-2 Typical Ramp Layout - Open Apron
**ON A/C A321-100 A321-200
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).
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_050102_1_0050101_01_03
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6 AS
CAT
GPU
CAT
WV
LV
FUEL
CB
TOW
CB
BULK
BULK
PS
PS
AC
Typical Ramp LayoutOpen Apron - Bulk LoadingFIGURE-5-1-2-991-005-A01
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**ON A/C A321-100 A321-200
N_AC_050102_1_0100101_01_00
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6 AS
CAT
ULD
GPU
CAT
WV
LV
ULD
BULK
FUEL
CB
TOW
LD CL
PS
PS
LD CL
AC
Typical Ramp LayoutOpen Apron - ULD LoadingFIGURE-5-1-2-991-010-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-1-3 Typical Ramp Layout - Gate
**ON A/C A321-100 A321-200
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).
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**ON A/C A321-100 A321-200
STAND SAFETY LINE
NOTE: TYPICAL RAMP LAYOUTAPPLICABLE TO AIRCRAFTWITH OR WITHOUT SHARKLETS.
8METERS
FEET5 10 150 20
0 2 4 6 AS
CAT
ULD
GPU
CAT
WV
LV
ULD
PBB
BULK
FUEL
CB
TOW
N_AC_050103_1_0030101_01_03
LD CL
LD CL
AC
Typical Ramp LayoutGate
FIGURE-5-1-3-991-003-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-2-0 Terminal Operations - Full Servicing
**ON A/C A321-100 A321-200
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 HANDLING185 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:- 185 pax at door L1- Deboarding rate = 22 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 185 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 loaders + 1 belt loaderEquipment positioning/removal + opening/closing door = +1 minCargo exchange:- FWD cargo compartment: 5 LD3- AFT cargo compartment: 5 LD3- Bulk compartment: 500 kg (1102 lb)
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
Bulk off-loading/loading times:
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- Bulk off-loading rate = 120 kg/min (265 lb/min)- Bulk loading rate = 100 kg/min (220 lb/min)
C. REFUELLING2 hoses, one side7134 l (1885 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- 10 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)
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**ON A/C A321-100 A321-200
0 20 30 40
TRT: 51 min
10 50 60
CATERING AT DOOR R1
CATERING AT DOOR R2
CLEANING
CARGO FWD CC
BULK
REFUELLING
TOILET SERVICING
HEADCOUNTING
CARGO AFT CC
DEBOARDING/BOARDING AT DOOR L1
POTABLE WATERSERVICING
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
N_AC_050200_1_0070101_01_01
min
AVAILABLE TIME
Turn Round StationsFull Servicing (51 Min.)
FIGURE-5-2-0-991-007-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-3-0 Terminal Operation - Transit
**ON A/C A321-100 A321-200
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 HANDLING220 pax, all Y/C2 Stairways used at doors L1 & L2Equipment positioning/removal + opening/closing door = 2 min
Deboarding:- 110 pax at door L1- 110 pax at door L2- Deboarding rate = 20 pax/min per door- No Passenger with Reduced Mobility (PRM)
Boarding:- 110 pax at door L1- 110 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: 5 LD3- AFT cargo compartment: 5 LD3- Bulk cargo compartment: 500 kg (1102 lb)
LD3 off-loading/loading times:- Off-loading = 1.2 min/LD3- Loading = 1.4 min/LD3
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Bulk off-loading/loading times:- Off-loading rate = 120 kg/min (265 lb/min)- Loading rate = 100 kg/min (220 lb/min)
C. REFUELLING2 hoses, one side7134 l (1885 US gal) at 50 psi (3 bar)Dispenser positioning/removal = 4 min
D. CLEANINGPerformed in available time
E. CATERINGNo catering
F. GROUND HANDLING SERVICINGStart of operations:- Bridges: t0 = 0- Other equipment: t = t0 + 1 minNo potable water servicingNo toilet servicing
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**ON A/C A321-100 A321-200
0 5 15 20 25 3010
HEADCOUNTING
CATERING
CLEANING
CARGO FWD CC
BULK
REFUELLING
POTABLE WATER SERVICING
TOILET SERVICING
CARGO AFT CC
TRT: 25 min
POSITIONING/REMOVAL
ACTIVITY
CRITICAL PATH
DEBOARDING/BOARDING AT DOOR L1
DEBOARDING/BOARDING AT DOOR L2
min
AVAILABLE TIME
AVAILABLE TIME
N_AC_050300_1_0040101_01_01
Turn Round StationsMinimum Servicing (25 Min.)FIGURE-5-3-0-991-004-A01
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5-4-0 Ground Service Connections
**ON A/C A321-100 A321-200
Ground Service Connections
1. Ground Service Connections.
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5-4-1 Ground Service Connections Layout
**ON A/C A321-100 A321-200
Ground Service Connections Layout
1. This section gives the ground service connections layout.
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**ON A/C A321-100 A321-200
1 3 11 12 2 4 14−6 7−
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 −
114
13
10
10
13
67
6
7
5 8 12 4
9 2
N_AC_050401_1_0070101_01_01
Ground Service ConnectionsGround Service Connections Layout
FIGURE-5-4-1-991-007-A01
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5-4-2 Grounding Points
**ON A/C A321-100 A321-200
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:
21.97 m(72.08 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
On right Main LandingGear leg:
21.97 m(72.08 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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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
(2)(1)
GROUND CABLE(OPTIONAL)
LANDINGGEAR
NOSE LANDING GEAR
MAIN LANDING GEAR
(1)
A
A
A
(1)
N_AC_050402_1_0070101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-007-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
NOTE: R SIDE SYMMETRICAL
A
RIB20
RIB19
FWD
A
A
FOR SPECIFICATIONS REFERTO FLIGHT MANUAL
B
B
N_AC_050402_1_0080101_01_00
Ground Service ConnectionsGrounding Points
FIGURE-5-4-2-991-008-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-3 Hydraulic System
**ON A/C A321-100 A321-200
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
23.44(76.9)
1.27(4.17)
1.76(5.77)
Yellow System:Access door 198CB
23.44(76.9)
1.27(4.17)
1.76(5.77)
Blue System:Access door 197EB
24.49(80.35)
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 195BB19.92(65.35)
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
20.1(65.94)
0.25(0.82)
1.99(6.53)
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POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green Systemaccumulator:Left MLG door
21.04(69.03)
0.25(0.82)
3.2(10.5)
Blue Systemaccumulator:Access door 195BB
22.3(72.51)
0.25(0.82)
1.99(6.53)
Yellow System brakingaccumulator:Access door 196BB
20.165.94)
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 197CB23.44(76.9)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.One 1/4 in. AEROQUIP AE96993E self-sealing connection for pressurized supply.One handpump filling connection for unpressurized (suction) supply.
5. Reservoir Drain.On 3/8 in. self-sealing connection on reservoir for:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Yellow System:Access door 196 BB -198 CB
20.1(65.94)
1.43(4.69)
1.90(6.23)
Green System:Left MLG door
21.04(69.03)
1.27(4.17)
2.61(8.56)
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POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Blue SystemAccess door 197 EB
24.49(80.35)
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).
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**ON A/C A321-100 A321-200
RESERVOIR FILL SYSTEMHAND PUMP FILL CONNECTION
GROUND TESTPRESSURE
CONNECTION
GROUND TESTSUCTION
CONNECTIONRESERVOIR FILLCONNECTION
AE96993GM
GROUND SUPPLY
AE80531K AE80532N
1698GM
1008GM 1007GM 1006GM
197CB
A
AN_AC_050403_1_0040101_01_00
Hydraulic SystemGreen System Ground Service Panel
FIGURE-5-4-3-991-004-A01
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**ON A/C A321-100 A321-200
GROUND CONNECTIONSUCTION
GROUNDCONNECTION
DELIVERY
AE80531K
AE80532N
2006GM
2008GM
A
Z197
A
N_AC_050403_1_0050101_01_00
Hydraulic SystemBlue System Ground Service Panel
FIGURE-5-4-3-991-005-A01
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**ON A/C A321-100 A321-200
GROUND TESTPRESSURE CONNECTION
GROUND TESTSUCTION CONNECTION
AE80531K AE80532N
A
A
3008GM 3006GM
198CB
N_AC_050403_1_0060101_01_00
Hydraulic SystemYellow System Ground Service Panel
FIGURE-5-4-3-991-006-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-4 Electrical System
**ON A/C A321-100 A321-200
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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- Radio navigation: 1.2 KVA.
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**ON A/C A321-100 A321-200
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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5-4-5 Oxygen System
**ON A/C A321-100 A321-200
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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5-4-6 Fuel System
**ON A/C A321-100 A321-200
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
20.65(67.75)
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)
21.84(71.65)
9.83(32.25)
3.65(11.98)
Refuel/Defuel coupling,RightAccess Door 622HB
21.84(71.65)
9.83(32.25)
3.65(11.98)
Gravity Refuel Coupling23.35(76.61)
12.4(40.68)
12.4(40.68)
3.7(12.14)
A. Refuel/Defuel couplings:- Right wing: one standard ISO 45, 2.5 in.- Left wing: one optional standard ISO 45, 2.5 in.
B. Refuel pressure:- Maximum pressure: 3.45 bar (50 psi).
C. Refuel Flow:- 1400 l/minute (369.84 US gal/minute).
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@A321AIRCRAFT 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 24.61(80.74)
14.9(48.88)
14.9(48.88)
4.32(14.17)
NACA Flame Arrestor 24.05(78.90)
13.7(44.95)
13.7(44.95)
4.02(13.19)
NOTE : Distances are approximate.
5-4-6Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-7 Pneumatic System
**ON A/C A321-100 A321-200
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
17.25(56.59)
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
16.72(54.86)
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);
5-4-7Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-8 Potable Water System
**ON A/C A321-100 A321-200
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)
Access door 171AL:38.2(125.33)
0.3(0.98)
2.6(8.53)
NOTE : Distances are approximate
A. Connector:- Fill/Drain Nipple 3/4 in. (ISO 17775)
B. Usable capacity- Standard configuration - one tank:2000 l (52.83 US gal)
C. Filling pressure:- 3.45 bar (50 psi)
D. Typical flow rate:- 50 l/min (13.21 US gal/min)
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).
5-4-8Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- 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).
D. Typical flow rate:- 50 l/min (13.21 US gal/min).
5-4-8Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-9 Oil System
**ON A/C A321-100 A321-200
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)
17.38(57.02)
6.63(21.75)
4.82(15.81)
1.46(4.79)
Engine Oil PressureFilling Port:
17.26(56.62)
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 (SeeFIGURE 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)
16.46(54)
6.9(22.64)
5.52(18.11)
0.68(2.23)
NOTE : Distances are approximate
5-4-9Page 1
Jun 01/12
@A321AIRCRAFT 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:
16.81(55.15)
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)
16.5(54.13)
6.56(21.52)
4.92(16.14)
1.22(4)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 28 l (7.39 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: 2506-2 plus one overflow connection: 2505-2..
5-4-9Page 2
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@A321AIRCRAFT 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:
17.06(55.97)
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:
19.66(64.5)
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 36-30042.42(139.17)
0.3(0.98)
4.83(15.85)
APS 320042.42(139.17)
0.3(0.98)
4.78(15.68)
131-942.32(138.84)
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)
5-4-9Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
- APU type 131-9: 6.25 l (1.65 US gal)
5-4-9Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
5-4-9Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
’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
5-4-9Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
5-4-9Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-4-10 Vacuum Toilet System
**ON A/C A321-100 A321-200
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
38.2(125.33)
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
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A321-100 A321-200
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--004-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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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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_0040101_01_00
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
Engine Starting Pneumatic RequirementsFIGURE-5-5-0-991-004-A01
5-5-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-1 Low Ambient Temperatures
**ON A/C A321-100 A321-200
Low Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature of -40˚C(-40˚F).
5-5-1Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
220°C
200°C
150°C
100°C
50°C
MAXIM
UM T
EMPERATURE L
IMIT
TIMES UP TO IDLEESTIMATED STARTING
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
70s
AIR FLOW REQUIRED AT GROUND CONNECTION
GROUND CONNECTION:MIN PRESSURE AT
SEA LEVELZ = 8000 ft
SEA LEVEL
30 40 50 60 80 90 100 110 12070
2
3
4
5
4.5
6
7
6.5
5.5
2.5
3.5
30
40
50
60
70
80
90
100
0°C
33 PSIG
38 PSIG ATRECOMMENDED PRESSURE:
GROUND CONNECTION
60s
35s
40s
Z = 8000 ft
Z = 8000 ft
SEA LEVEL
50s
N_AC_050501_1_0070101_01_00
MAXIMUM DUCT PRESSURE: 60 PSIG
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- CFM56 series engine
FIGURE-5-5-1-991-007-A01
5-5-1Page 2
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
90
80
70
60
50
40
30 2
3
4
5
6
40 50 60 70 80 90 100 110 120
AIR SUPPLY PRESSUREAT GROUND CONNECTION
220°C
200°C
150°C
100°C
50°C
MAXIMUM T
EMPERATURE LIMIT
MAXIMUM DUCT PRESSURE
AIR FLOW REQUIRED AT GROUND CONNECTION
PSIA ABSOLUTE BARS
75s
70s
65s
60s
0°C
kg/mn
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
ESTIMATED STARTINGTIMES UP TO IDLE
N_AC_050501_1_0080101_01_00
Engine Starting Pneumatic RequirementsLow Ambient Temperature -40˚C (-40˚F) -- IAE V2500 series engine
FIGURE-5-5-1-991-008-A01
5-5-1Page 3
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-2 Medium Ambient Temperatures
**ON A/C A321-100 A321-200
Medium Ambient Temperatures
1. This section provides the engine starting pneumatic requirements for a temperature of +15˚C(+59˚F).
5-5-2Page 1
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
220°C
200°C
150°C
100°C
50°CMAXIM
UM T
EMPERATURE L
IMIT
TIMES UP TO IDLEESTIMATED STARTING
PSIA ABSOLUTE BARSAIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
70s
AIR FLOW REQUIRED AT GROUND CONNECTION
GROUND CONNECTION:MIN PRESSURE AT
SEA LEVEL
Z = 8000 ft
SEA LEVEL
0°C
22 PSIG
33 PSIG ATRECOMMENDED PRESSURE:
GROUND CONNECTION60s
Z = 8000 ft
2
2.5
3
3.5
4
7
6.5
6
5.5
5
4.5
100
90
80
70
60
50
40
30
30 40 50 60 70 80 90 100 110 120
Z = 8000 ft
SEA LEVEL
50s
40s
35s
MAXIMUM DUCT PRESSURE: 60 PSIG
N_AC_050502_1_0070101_01_00
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- CFM56 series engine
FIGURE-5-5-2-991-007-A01
5-5-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
220°C200°C
150°C
100°C
50°C
0°CMAXIMUM DUCT PRESSURE
TIMES UP TO IDLEESTIMATED STARTING
AIR FLOW REQUIRED AT GROUND CONNECTION
60s
230
3
4
5
6
90
80
70
60
50
40
55s
50s
45s
MAXIMUM T
EMPERATURE LIMIT
40 50 60 70 80 90 100 110 120
N_AC_050502_1_0080101_01_00
Engine Starting Pneumatic RequirementsMedium Ambient Temperature +15˚C (+59˚F) -- IAE V2500 series engine
FIGURE-5-5-2-991-008-A01
5-5-2Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-5-3 High Ambient Temperatures
**ON A/C A321-100 A321-200
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
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
220°C200°C
150°C
100°C
50°C
MAXIM
UM T
EMPERATURE L
IMIT
TIMES UP TO IDLEESTIMATED STARTING
PSIA ABSOLUTE BARS
70s
AIR FLOW REQUIRED AT GROUND CONNECTION
GROUND CONNECTION:MIN PRESSURE AT
22 PSIG
33 PSIG ATRECOMMENDED PRESSURE:
GROUND CONNECTION60s
50s
40s
35s
30
40
50
60
70
80
90
100 7
6
4
3
2
30 40 50 60 70 80 90 100 110 120
2.5
3.5
4.5
5
5.5
6.5
Z = 8000 ft
SEA LEVEL
Z = 8000 ft
SEA LEVEL
Z = 8000 ft
SEA LEVEL
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
N_AC_050503_1_0070101_01_00
MAXIMUM DUCT PRESSURE: 60 PSIG
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +55˚C (+131˚F) -- CFM56 series engine
FIGURE-5-5-3-991-007-A01
5-5-3Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
220°C
200°C
150°C
100°C
50°C
TIMES UP TO IDLEESTIMATED STARTING
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
AIR FLOW REQUIRED AT GROUND CONNECTION
0°C
60s
55s
2
3
4
5
6
90
80
70
60
50
40
30
40 50 60 70 80 90 100 110 120
50s
45s
MAXIMUM DUCT PRESSURE
MAXIMUM T
EMPERATURE LIMIT
N_AC_050503_1_0080101_01_00
Engine Starting Pneumatic RequirementsHigh Ambient Temperature +50˚C (+122˚F) -- IAE V2500 series engine
FIGURE-5-5-3-991-008-A01
5-5-3Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-1 Heating
**ON A/C A321-100 A321-200
Heating
1. This section provides the ground pneumatic power requirements heating.
5-6-1Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
TOTAL AIRFLOW(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
0.5
30
TIM
E T
O H
EA
T C
AB
IN T
O 2
1°C
(69
.8°
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
)
1.34(lb
/s)
4050
0.44
9
0.53
9
0.62
8
0.71
8
0.80
8
0.89
8
0.98
8
1.07
7
1.16
7
1.25
7
1.34
7
1.0
1.2
1.5
1.80
2.26
2.71
3.0
2.5
2.0
1.5
CABIN AIRFLOW
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 =
410
0 W
RE
CIR
CU
LAT
ION
: ON
NO
OT
HE
R H
EA
T L
OA
D
N_AC_050601_1_0040101_01_01
Ground Pneumatic Power RequirementsHeating
FIGURE-5-6-1-991-004-A01
5-6-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-2 Cooling
**ON A/C A321-100 A321-200
Cooling
1. This section provides the ground pneumatic power requirements cooling.
5-6-2Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
1.5
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
)
(lb/s
)
0.44
9
0.53
9
0.62
8
0.71
8
0.80
8
0.89
8
0.98
8
1.07
7
1.16
7
1.25
7
1.34
7
1.2
1.0
0.5
3040
50
1.34
1.80
2.26
2.71
3.0
2.5
2.0
1.5
CABIN AIRFLOW
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
N_AC_050602_1_0040101_01_01
Ground Pneumatic Power RequirementsCooling
FIGURE-5-6-2-991-004-A01
5-6-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A321-100 A321-200
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 0.449 0.990 -56.4 -69.50.6 1.32 0.539 1.188 -41.8 -43.20.7 1.54 0.628 1.385 -31.3 -24.30.8 1.76 0.718 1.583 -23.5 -10.30.9 1.98 0.808 1.781 -17.5 0.51.0 2.20 0.898 1.980 -12.7 9.11.1 2.43 0.988 2.178 -8.8 16.21.2 2.65 1.077 2.374 -5.5 22.11.3 2.87 1.167 2.573 -2.7 27.11.4 3.09 1.257 2.771 -0.4 31.31.5 3.31 1.347 2.970 1.7 35.1
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 0.449 0.990 32.6 90.70.6 1.32 0.539 1.188 30.5 86.90.7 1.54 0.628 1.385 29.0 84.20.8 1.76 0.718 1.583 27.9 82.20.9 1.98 0.808 1.781 27.1 80.81.0 2.20 0.898 1.980 26.4 79.51.1 2.43 0.988 2.178 25.9 78.61.2 2.65 1.077 2.374 25.4 77.71.3 2.87 1.167 2.573 25.0 77.01.4 3.09 1.257 2.771 24.7 76.5
5-7-0Page 1
Jun 01/12
@A321AIRCRAFT 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 1.347 2.970 24.4 75.9
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 0.449 0.990 38.4 101.10.6 1.32 0.539 1.188 35.3 95.50.7 1.54 0.628 1.385 33.1 91.60.8 1.76 0.718 1.583 31.5 88.70.9 1.98 0.808 1.781 30.2 86.41.0 2.20 0.898 1.980 29.2 84.61.1 2.43 0.988 2.178 28.4 83.11.2 2.65 1.077 2.374 27.7 81.91.3 2.87 1.167 2.573 27.1 80.81.4 3.09 1.257 2.771 26.6 79.91.5 3.31 1.347 2.970 26.2 79.2
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 0.449 0.990 46.6 115.90.6 1.32 0.539 1.188 42.2 108.00.7 1.54 0.628 1.385 39.0 102.20.8 1.76 0.718 1.583 36.6 97.90.9 1.98 0.808 1.781 34.7 94.51.0 2.20 0.898 1.980 33.2 91.81.1 2.43 0.988 2.178 32.0 89.61.2 2.65 1.077 2.374 31.0 87.81.3 2.87 1.167 2.573 30.2 86.41.4 3.09 1.257 2.771 29.5 85.1
5-7-0Page 2
Jun 01/12
@A321AIRCRAFT 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 1.347 2.970 28.8 83.8
NOTE : Data for stabilized conditions see 5-7-0.
5-7-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
TOTAL AIRFLOW
(kg/
s)TOTAL AIRFLOW
CABIN AIRFLOW
(lb/s
)
(°C
)IN
LET
FLO
WT
EM
PE
RA
TU
RE
(°F
)
−40
−30
−20
−10
010
2030
40
100
5010
0−
10−
40
1.34
1.80
2.26
2.71
3.0
2.5
2.0
1.5
0.44
9
0.53
9
0.62
8
0.71
8
0.80
8
0.89
8
0.98
8
1.07
7
1.16
7
1.25
7
1.34
7
0.5
1.0
1.2
1.5
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
NO
TE
:LP
GR
OU
ND
CO
NN
EC
TIO
N M
AX
IMU
M P
RE
SS
UR
E 4
0 m
b
CABIN AIRFLOW
CU
RV
E 1
: CA
BIN
AT
29°
C (
84.2
°F
)19
9 P
AS
SE
NG
ER
S, 6
CA
BIN
AT
TE
ND
AN
TS
, 3 C
RE
W M
EM
BE
RS
BR
IGH
T D
AY
SO
LAR
LO
AD
: 499
0 W
ELE
CT
RIC
AL
LOA
D =
780
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)
OA
T =
−23
°C
(−
9.4°
F)
OA
T =
−30
°C
(−
22°
F)
OA
T =
−40
°C
(−
40°
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 =
570
0 W
RE
CIR
CU
LAT
ION
: ON
NO
PA
SS
EN
GE
R O
R C
AB
INA
TT
EN
DA
NT
S
CU
RV
E 2
, 3, 4
N_AC_050700_1_0040101_01_01
Preconditioned Airflow RequirementsFIGURE-5-7-0-991-004-A01
5-7-0Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A321 AT 80 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 (80 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 (6.5 t)− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS
THE RECOMMENDED MINIMUM TRACTOR WEIGHT (11.5 t)
95
657075808590
10
0 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0
5
011.47
DR
Y C
ON
CR
ET
E m
= 0
.8
BREAKAWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 525 daN
WE
T C
ON
CR
ET
E m
= 0
.57
HA
RD
SN
OW
m =
0.2
ICE m = 0.05
1 ENGINE ON1.5% SLOPE
80 tons
DRAWBAR PULL [ t ] A/C WEIGHT [ t ]
6.5
TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]AT IDLE
N_AC_050800_1_0010401_01_03
Ground Towing RequirementsFIGURE-5-8-0-991-001-D01
5-8-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0 De-Icing and External Cleaning
**ON A/C A321-100 A321-200
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
A321 102.6 1104.38 1.8 19.38 27 290.63 43 462.85A321 Sharklet 102.6 1104.38 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
A321 167.4 1801.88 23.6 254.03 365 3929A321 Sharklet 167.4 1801.88 23.6 254.03 373 4015
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
A321 102.6 1104.38 108.8 1171.11 1.8 19.38 27 290.63 27 290.63A321 Sharklet 102.6 1104.38 108.8 1171.11 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
A321 43 462.85 509.6 5485.29 73.2 787.92 895 9634
5-9-0Page 1
Jun 01/12
@A321AIRCRAFT 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
A321 Sharklet 43 462.85 509.6 5485.29 73.2 787.92 902 9709
NOTE : Dimensions are approximate
5-9-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
PLA
NA
IRP
LAN
E
V (
m/s
)
GR
OU
ND
PLA
NE
ME
TE
RS
4530
2520
1510
40 30 20 10 0036912
mft
40 30 20 10 0036912
mft
N_AC_060101_1_0070101_01_00
4530
2520
1510
Engine Exhaust VelocitiesGround Idle Power -- CFM56-5B series engine
FIGURE-6-1-1-991-007-A01
6-1-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
GR
OU
ND
IDLE
TH
RU
ST
FE
ET
050
100
150
200
7590
PLA
N
34 M
PH
20 M
PH
68 M
PH
ftm
60
15 10 5 0
40 20 0
ftm
60
15 10 5 0
40 20 0
N_AC_060101_1_0080101_01_00
Engine Exhaust VelocitiesGround Idle Power -- IAE V2500 series engine
FIGURE-6-1-1-991-008-A01
6-1-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
mft
PLA
NA
IRP
LAN
E
T (
°K
)
GR
OU
ND
PLA
NE
ME
TE
RS40 30 20 10 0
036912
mft
400
350
325
300
40 30 20 10 0036912
400
350
325
300
N_AC_060102_1_0070101_01_00
Engine Exhaust TemperaturesGround Idle Power -- CFM56-5B series engine
FIGURE-6-1-2-991-007-A01
6-1-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
FE
ET
050
100
150
200
7590
45°
C35
°C
25°
C
ftm
60
15 10 5 0
40 20 0
N_AC_060102_1_0080101_01_00
Engine Exhaust TemperaturesGround Idle Power -- IAE V2500 series engine
FIGURE-6-1-2-991-008-A01
6-1-2Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A321-100 A321-200
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power.
6-1-5Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
420
390
360
330
300
270
240
210
180
150
120
9060
30
0
100
200
300
400
500
700
600
800
900
1000
1100
1200
1300
1400
ME
TE
RS
FE
ET
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
450
1500
ftm
42 36 30 24 18 12 6 0
140
120
100 80 60 40 200
N_AC_060105_1_0070101_01_00
Engine Exhaust VelocitiesTakeoff Power -- CFM56-5B series engine
FIGURE-6-1-5-991-007-A01
6-1-5Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
PLA
N
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)
ftm
60
15 10 5 0
40 20 0
ftm
15 10 5 0
60 40 20 0
N_AC_060105_1_0080101_01_00
Engine Exhaust VelocitiesTakeoff Power -- IAE V2500 series engine
FIGURE-6-1-5-991-008-A01
6-1-5Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A321-100 A321-200
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power.
6-1-6Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
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
0
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
50
ftm
60
0
40 20 0
18 12 6
ftm
60
0
40 20 0
18 12 6
N_AC_060106_1_0070101_01_00
Engine Exhaust TemperaturesTakeoff Power -- CFM56-5B series engine
FIGURE-6-1-6-991-007-A01
6-1-6Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
ME
TE
RS
1530
4560
250
300
ELE
VA
TIO
N
FE
ET
5010
015
020
0
7590
PLA
N
00
65°
C55
°C
45°
C35
°C
25°
C
ftm
15 10 5 0
60 40 20 0
ftm
15 10 5 0
60 40 20 0
N_AC_060106_1_0080101_01_00
Engine Exhaust TemperaturesTakeoff Power -- IAE V2500 series engine
FIGURE-6-1-6-991-008-A01
6-1-6Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-0 Airport and Community Noise
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-2-1 Noise Data
**ON A/C A321-100 A321-200
Noise Data
1. 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: 20.3˚C (69˚F)- Relative humidity: 43%- Atmospheric pressure: 988 hPa- Wind speed: Negligible- No rain
2. Noise Data for IAE V2500 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: 12˚C (54˚F)- Relative humidity: 62.5%- Atmospheric pressure: 1000 hPa- Wind speed: Negligible- No rain
6-2-1Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
112110108106104102
10098969492908886848280
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°
260°
250°
240°
230°
220°
210°NOISE REFERENCEPOINT
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
96%21.6%
78
N_AC_060201_1_0100101_01_00
Airport and Community NoiseCFM56-5B series engine
FIGURE-6-2-1-991-010-A01
6-2-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
GROUND IDLE
N2
CURVE
MAX THRUST POSSIBLEON BRAKES
57.7% 92.5%
E.P.R 1.007 1.397
11811611411211010810610410210098969492908886848280
NOISE REFERENCEPOINT
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_0110101_01_00
Airport and Community NoiseIAE V2500 series engine
FIGURE-6-2-1-991-011-A01
6-2-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A321-100 A321-200
Danger Areas of Engines
1. Danger Areas of the Engines.
6-3-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1 Ground Idle Power
**ON A/C A321-100 A321-200
Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions.
6-3-1Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AREA
A
B
C
D (105−32)
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
RADIUS = 7.2 ft (2.2 m)
3.4 ft (1 m)
TO 199 ft (61 m)
CLOSE ENTRY CORRIDORFOR WIND DIRECTION > 90°
ENTRY CORRIDOREXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
INLET SUCTIONDANGER AREA
WIDTH72 ft (22 m)
E
45°
NO ENTRY 82 ft (25 m)AFT OF NOZZLE EXIT
B
C
D
65−20
N_AC_060301_1_0090101_01_01
Danger Areas of EnginesCFM56-5B series engine
FIGURE-6-3-1-991-009-A01
6-3-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
30°
TO 59 m (195 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
0.91 m(3 ft)
R = 5.79 m(19 ft)
ENTRY CORRIDOR
EXHAUST DANGER AREA
INTAKE SUCTION DANGER AREA GROUND IDLE
N_AC_060301_1_0100101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE-6-3-1-991-010-A01
6-3-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-2 Takeoff Power
**ON A/C A321-100 A321-200
Takeoff Power
1. This section gives danger areas of the engines at max takeoff conditions.
6-3-2Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
AREA
A
B
C
D (105−32)
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 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
RADIUS = 21.7 ft (6.6 m)
E
TO 1235 ft (376 m)
WIDTH192 ft (59 m)
NO ENTRY 775 ft (236 m)AFT OF NOZZLE EXIT
INLET SUCTIONDANGER AREA
65−20
A
B
C
D
N_AC_060302_1_0070101_01_01
Danger Areas of EnginesCFM56-5B series engine
FIGURE-6-3-2-991-007-A01
6-3-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
30°
TO 348 m (1150 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
1.68 m
(5.5 ft)
R = 5.79 m(19 ft)
ENTRY CORRIDOR
EXHAUST DANGER AREA
INTAKE SUCTION DANGER AREA
N_AC_060302_1_0080101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE-6-3-2-991-008-A01
6-3-2Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A321-100 A321-200
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-4-1 APU
**ON A/C A321-100 A321-200
APU - APIC & GARRETT
1. This section gives APU exhaust velocities and temperatures.
6-4-1Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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_0040101_01_00
Exhaust Velocities and TemperaturesAPU -- APIC & GARRETTFIGURE-6-4-1-991-004-A01
6-4-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A321-100 A321-200
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 use 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
@A321AIRCRAFT 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 with the ACN/PCN system as referenced inICAO Annex 14, ”Aerodromes”, Volume 1 Fourth Edition July 2004, incorporating Amendments 1 to6.
7-1-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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.
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 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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
WVAIRCRAFT
CODE04 C04 C04 C09 D06 E06 E06 E07 G07 G07 G08 H00 I00 I00 I07 J02 L02 L02 L05 M05 M
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.
05 M06 O06 O
WVAIRCRAFT
CODE03 P03 P03 P05 Q05 Q10 R10 R04 S04 S08 U08 U08 U00 V00 V02 X02 X02 X02 X03 Z03 Z01 AA01 AA11 AB11 AB
MODEL
A321−111A321−112A321−131A321−214A321−111A321−112A321−131A321−111A321−112A321−131A321−214A321−111A321−112A321−131A321−214A321−111A321−112A321−131A321−111A321−112A321−131A321−211A321−231
MODEL
A321−111A321−112A321−131A321−211A321−231A321−211A321−231A321−211A321−231A321−111A321−112A321−131A321−211A321−231A321−211A321−231A321−213A321−232A321−211A321−231A321−211A321−231A321−211A321−231
N_AC_070100_1_0040101_01_00
Aircraft CodesAircraft Codes
FIGURE-7-1-0-991-004-A01
7-1-0Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
C − D − E
10.1 bar (146 psi)
1 270 x 455 R22 (49 x 18 − 22)
12.8 bar (186 psi)
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
30 x 8.8 R15 (30 x 8.8 − 15)
927 mm(36.5 in)
500 mm(19.7 in)
16 905 mm(55 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0280101_01_00
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-028-A01
7-2-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
G − H − I − J − L − M − O
10.8 bar (157 psi)
1 270 x 455 R22 (49 x 18 − 22)
13.6 bar (197 psi)
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
30 x 8.8 R15 (30 x 8.8 − 15)
927 mm(36.5 in)
500 mm(19.7 in)
16 905 mm(55 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0290101_01_00
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-029-A01
7-2-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
P − Q − R
11 bar (160 psi)
1 270 x 455 R22 (49 x 18 − 22)
13.9 bar (202 psi)
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
30 x 8.8 R15 (30 x 8.8 − 15)
927 mm(36.5 in)
500 mm(19.7 in)
16 905 mm(55 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0300101_01_00
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-030-A01
7-2-0Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
S − U − V − X
11.6 bar (168 psi)
1 270 x 455 R22 (49 x 18 − 22)
14.6 bar (212 psi)
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
30 x 8.8 R15 (30 x 8.8 − 15)
927 mm(36.5 in)
500 mm(19.7 in)
16 905 mm(55 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0310101_01_00
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-031-A01
7-2-0Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
Z − AA − AB
11.6 bar (168 psi)
1 270 x 455 R22 (49 x 18 − 22)
15 bar (218 psi)
PERCENTAGE OF WEIGHT
ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
30 x 8.8 R15 (30 x 8.8 − 15)
927 mm(36.5 in)
500 mm(19.7 in)
16 905 mm(55 ft 5.6 in)
7 590 mm(24 ft 10.8 in)
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0320101_01_00
Landing Gear FootprintLanding Gear Footprint
FIGURE-7-2-0-991-032-A01
7-2-0Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
C78
400
VM
G (
PE
R S
TR
UT
)V
NG
172
850
18 6
758
480
35 1
2515
930
82 7
0037
510
26 8
5012
180
66 1
5030
010
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 =
78
400
kgM
RW
= 7
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 =
15.
4 %
MA
C A
T A
/C W
EIG
HT
= 7
8 40
0 kg
FW
D C
G =
15.
4 %
MA
C A
T A
/C W
EIG
HT
= 7
8 40
0 kg
D E
MR
W =
78
400
kgF
WD
CG
= 1
5.4
% M
AC
AT
A/C
WE
IGH
T =
78
400
kg
(2)
MR
W =
78
400
kgM
RW
= 7
8 40
0 kg
AF
T C
G =
41
% M
AC
AT
A/C
WE
IGH
T =
78
400
kgA
FT
CG
= 4
1 %
MA
C A
T A
/C W
EIG
HT
= 7
8 40
0 kg
MR
W =
78
400
kgA
FT
CG
= 4
1 %
MA
C A
T A
/C W
EIG
HT
= 7
8 40
0 kg
78 4
0017
2 85
018
675
8 47
035
075
15 9
1030
010
82 7
0037
510
26 8
5012
180
66 1
50
78 4
0017
2 85
018
675
8 48
035
125
15 9
3082
700
37 5
1026
850
12 1
8066
150
30 0
10
C D E C D E
A/C
CO
DE
N_AC_070300_1_0330101_01_00
Maximum Pavement LoadsMaximum Pavement LoadsFIGURE-7-3-0-991-033-A01
7-3-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
G80
400
VM
G (
PE
R S
TR
UT
)V
NG
177
250
18 7
508
510
35 6
0016
140
84 8
0038
470
27 5
5012
490
67 8
5030
780
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 =
80
400
kgM
RW
= 8
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 =
16.
3 %
MA
C A
T A
/C W
EIG
HT
= 8
0 40
0 kg
FW
D C
G =
16.
3 %
MA
C A
T A
/C W
EIG
HT
= 8
0 40
0 kg
H I
MR
W =
83
400
kgF
WD
CG
= 1
7.5
% M
AC
AT
A/C
WE
IGH
T =
83
400
kg
(2)
MR
W =
80
400
kgM
RW
= 8
0 40
0 kg
AF
T C
G =
41
% M
AC
AT
A/C
WE
IGH
T =
80
400
kgA
FT
CG
= 4
0.7
% M
AC
AT
A/C
WE
IGH
T =
80
400
kgM
RW
= 8
3 40
0 kg
AF
T C
G =
41
% M
AC
AT
A/C
WE
IGH
T =
83
400
kg
80 4
0017
7 25
018
750
8 51
035
550
16 1
2030
750
84 7
5038
440
27 5
5012
490
67 8
00
83 4
0018
3 87
518
900
8 57
036
300
16 4
7087
975
39 9
1028
575
12 9
6070
375
31 9
20
G H I G H I
A/C
CO
DE
N_AC_070300_1_0340101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-034-A01
7-3-0Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
J83
400
VM
G (
PE
R S
TR
UT
)V
NG
183
875
18 8
758
560
36 2
5016
440
87 6
7539
770
28 5
7512
960
70 1
5031
820
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 =
83
400
kgM
RW
= 8
3 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
17.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
3 40
0 kg
FW
D C
G =
17.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
3 40
0 kg
L M
MR
W =
83
400
kgF
WD
CG
= 1
7.5
% M
AC
AT
A/C
WE
IGH
T =
83
400
kg
(2)
MR
W =
83
400
kgM
RW
= 8
3 40
0 kg
AF
T C
G =
39.
7 %
MA
C A
T A
/C W
EIG
HT
= 7
9 53
8 kg
AF
T C
G =
41
% M
AC
AT
A/C
WE
IGH
T =
83
400
kgM
RW
= 8
3 40
0 kg
AF
T C
G =
41
% M
AC
AT
A/C
WE
IGH
T =
83
400
kg
83 4
0018
3 87
518
900
8 57
036
300
16 4
7031
920
87 9
7539
910
28 5
7512
960
70 3
75
J L M J L M
83 4
0018
3 87
518
900
8 57
036
300
16 4
7031
920
87 9
7539
910
28 5
7512
960
70 3
75
A/C
CO
DE
N_AC_070300_1_0350101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-035-A01
7-3-0Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
O83
400
VM
G (
PE
R S
TR
UT
)V
NG
183
875
18 8
758
560
36 2
5016
440
87 6
7539
770
28 5
7512
960
70 1
5031
820
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 =
83
400
kgM
RW
= 8
5 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 =
17.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
3 40
0 kg
FW
D C
G =
18.
3 %
MA
C A
T A
/C W
EIG
HT
= 8
5 40
0 kg
P Q
MR
W =
85
400
kgF
WD
CG
= 1
7.5
% M
AC
AT
A/C
WE
IGH
T =
85
400
kg
(2)
MR
W =
83
400
kgM
RW
= 8
5 40
0 kg
AF
T C
G =
39.
7 %
MA
C A
T A
/C W
EIG
HT
= 8
3 40
0 kg
AF
T C
G =
41
% M
AC
AT
A/C
WE
IGH
T =
85
400
kgM
RW
= 8
5 40
0 kg
AF
T C
G =
39.
1 %
MA
C A
T A
/C W
EIG
HT
= 8
5 40
0 kg
85 4
0018
8 27
518
950
8 60
036
775
16 6
8032
690
90 1
0040
860
29 2
5013
270
72 0
75
O P Q O P Q
85 4
0018
8 27
519
325
8 76
037
075
16 8
2032
530
89 6
5040
660
29 2
5013
270
71 7
00
A/C
CO
DE
N_AC_070300_1_0360101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-036-A01
7-3-0Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
R85
400
VM
G (
PE
R S
TR
UT
)V
NG
188
275
19 3
258
760
37 0
7516
820
89 6
5040
660
29 2
5013
270
71 7
0032
530
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 =
85
400
kgM
RW
= 8
7 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 =
17.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
5 40
0 kg
FW
D C
G =
17.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
7 40
0 kg
S U
MR
W =
89
400
kgF
WD
CG
= 1
7.5
% M
AC
AT
A/C
WE
IGH
T =
89
400
kg
(2)
MR
W =
85
400
kgM
RW
= 8
7 40
0 kg
AF
T C
G =
39.
1 %
MA
C A
T A
/C W
EIG
HT
= 8
5 40
0 kg
AF
T C
G =
38.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
7 40
0 kg
MR
W =
89
400
kgA
FT
CG
= 3
8 %
MA
C A
T A
/C W
EIG
HT
= 8
9 40
0 kg
87 4
0019
2 67
518
725
8 49
036
900
16 7
4033
440
92 1
5041
800
29 9
5013
580
73 7
25
R S U R S U
89 4
0019
7 10
020
225
9 18
038
850
17 6
2033
950
93 5
5042
440
30 6
2513
890
74 8
50
A/C
CO
DE
N_AC_070300_1_0370101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-037-A01
7-3-0Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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
V89
400
VM
G (
PE
R S
TR
UT
)V
NG
197
100
19 1
258
680
37 7
2517
110
94 1
2542
700
30 6
2513
890
75 3
0034
160
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 =
89
400
kgM
RW
= 8
9 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
17.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
9 40
0 kg
FW
D C
G =
17.
5 %
MA
C A
T A
/C W
EIG
HT
= 8
9 40
0 kg
X Z
MR
W =
91
400
kgF
WD
CG
= 1
7.5
% M
AC
AT
A/C
WE
IGH
T =
89
000
kg
(2)
MR
W =
89
400
kgM
RW
= 8
9 40
0 kg
AF
T C
G =
38
% M
AC
AT
A/C
WE
IGH
T =
89
400
kgA
FT
CG
= 3
8 %
MA
C A
T A
/C W
EIG
HT
= 8
9 40
0 kg
MR
W =
91
400
kgA
FT
CG
= 3
7.5
% M
AC
AT
A/C
WE
IGH
T =
91
400
kg
V X Z V X Z
91 4
0020
1 50
019
050
8 64
037
525
17 0
3034
880
96 1
2543
600
31 3
2514
200
76 9
00
A/C
CO
DE
89 4
0019
7 10
019
125
8 68
037
725
17 1
1094
125
42 7
0030
625
13 8
9075
300
34 1
60
A/C
CO
DE
N_AC_070300_1_0380101_01_00
Maximum Pavement LoadsFIGURE-7-3-0-991-038-A01
7-3-0Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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
AA
93 4
00
VM
G (
PE
R S
TR
UT
)V
NG
205
900
18 8
258
530
37 8
0017
140
98 1
0044
490
32 0
0014
510
78 4
7535
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 =
93
400
kgM
RW
= 9
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 =
19
% M
AC
AT
A/C
WE
IGH
T =
91
500
kgF
WD
CG
= 1
9.7
% M
AC
AT
A/C
WE
IGH
T =
91
500
kg
AB
(2)
MR
W =
93
400
kgM
RW
= 9
3 90
0 kg
AF
T C
G =
37
% M
AC
AT
A/C
WE
IGH
T =
93
400
kgA
FT
CG
= 3
6.9
% M
AC
AT
A/C
WE
IGH
T =
93
900
kg
AA
AB
AA
AB
A/C
CO
DE
93 9
0020
7 02
518
475
8 38
037
450
16 9
9098
575
44 7
2032
175
14 5
9078
875
35 7
70
A/C
CO
DE
N_AC_070300_1_0390101_01_00
Maximum Pavement LoadsMaximum Pavement LoadsFIGURE-7-3-0-991-039-A01
7-3-0Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A321-100 A321-200
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 60 000 kg (132 275 lb) and the percentage of weight on the Main Landing Gear is95.7 %.
For these conditions the total weight on the Main Landing Gear is 57 420 kg (126 575 lb).
7-4-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-4-1 Landing Gear Loading on Pavement
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
80
35
40
45
50
55
60
65
70
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 = 73 500 kg
MZFW = 69 500 kg
MTOW = 78 000 kg
CG FOR ACNCALCULATIONS
5 15 25 35 45 55
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE C
LANDING
TAKE OFF
N_AC_070401_1_0650101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-065-A01
7-4-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
805 15 25 35 45 55
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
MZFW = 69 500 kg
LANDING
MTOW = 78 000 kg
A/C CODE D
MLW = 73 500 kg
CG FOR ACNCALCULATIONS
TAKE OFF
35
40
45
50
55
60
65
70
75
80
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
N_AC_070401_1_0660101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-066-A01
7-4-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
N_AC_070401_1_0670101_01_00
TAKE OFF
35
40
45
50
55
60
65
70
75
80
35
40
45
50
55
60
65
70
75
80
LANDING
MTOW = 78 000 kg
MLW = 74 500 kg
MZFW = 70 500 kg
CG FOR ACNCALCULATIONSA/C CODE E
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
86 88 90 92 94 96 98 100
5 15 25 35 45 55
Landing Gear Loading on PavementFIGURE-7-4-1-991-067-A01
7-4-1Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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 MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
80
85
35
40
45
50
55
60
65
70
75
80
855 15 25 35 45 55
MTOW = 80 000 kg
LANDING
MLW = 73 500 kg
TAKE OFF
A/C CODE G
MZFW = 69 500 kg
CG FOR ACNCALCULATIONS
N_AC_070401_1_0680101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-068-A01
7-4-1Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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
86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
80
85
35
40
45
50
55
60
65
70
75
80
855 15 25 35 45 55
MTOW = 80 000 kg
MLW = 73 500 kg
MZFW = 69 500 kg
LANDING
CG FOR ACNCALCULATIONS
A/C CODE H
TAKE OFF
N_AC_070401_1_0690101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-069-A01
7-4-1Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
N_AC_070401_1_0700101_01_00
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
MTOW = 83 000 kg
CG FOR ACN
MLW = 73 500 kg
CALCULATIONS
35
40
45
50
55
60
65
70
75
80
85
35
40
45
50
55
60
65
70
75
80
855 15 25 35 45 55
PERCENTAGE MAC
A/C CODE I
MZFW = 69 500 kg
TAKE OFF
Landing Gear Loading on PavementFIGURE-7-4-1-991-070-A01
7-4-1Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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 = 73 500 kg
MZFW = 69 500 kg
LANDING
MTOW = 83 000 kg
CG FOR ACNCALCULATIONS
35
40
45
50
55
60
65
70
75
80
85
35
40
45
50
55
60
65
70
75
80
855 15 25 35 45 55
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
PERCENTAGE MAC
A/C CODE J
TAKE OFF
N_AC_070401_1_0710101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-071-A01
7-4-1Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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
MTOW = 83 000 kg
MZFW = 70 500 kg
CG FOR ACNCALCULATIONS
MLW = 74 500 kg
35
40
45
50
55
60
65
70
75
80
85
35
40
45
50
55
60
65
70
75
80
85
86 88 90 92 94 96 98 100
5 15 25 35 45 55
PERCENTAGE MAC
A/C CODE L
TAKE OFF
LANDING
N_AC_070401_1_0720101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-072-A01
7-4-1Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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
MTOW = 83 000 kg
MLW = 75 000 kg
MZFW = 71 000 kg
86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
80
85
35
40
45
50
55
60
65
70
75
80
855 15 25 35 45 55
PERCENTAGE MAC
A/C CODE M
CG FOR ACNCALCULATIONS
TAKE OFF
LANDING
N_AC_070401_1_0730101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-073-A01
7-4-1Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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
MTOW = 83 000 kg
MLW = 75 500 kg
MZFW = 71 500 kg
86 88 90 92 94 96 98 10035
40
45
50
55
60
65
70
75
80
85
35
40
45
50
55
60
65
70
75
80
855 15 25 35 45 55
A/C CODE O
CG FOR ACNCALCULATIONS
TAKE OFF
LANDING
N_AC_070401_1_0740101_01_00
Landing Gear Loading on PavementLanding Gear Loading on Pavement
FIGURE-7-4-1-991-074-A01
7-4-1Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
35
40
45
50
55
60
65
70
75
80
85
90
35
MTOW = 85 000 kg
MLW = 74 500 kg
LANDING
TAKE OFF
MZFW = 70 500 kg
CG FOR ACNCALCULATIONS
A/C CODE P
35
40
45
50
55
60
65
70
75
80
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45 55
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)
N_AC_070401_1_0750101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-075-A01
7-4-1Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
80
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45 55
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)
MLW = 75 500 kg
CG FOR ACNCALCULATIONS
MZFW = 71 500 kg
MTOW = 85 000 kg
A/C CODE Q
LANDING
TAKE OFF
N_AC_070401_1_0760101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-076-A01
7-4-1Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
CG FOR ACNCALCULATIONS
MLW = 77 800 kg
MZFW = 73 800 kg
MTOW = 85 000 kg
TAKE OFF
LANDING
A/C CODE R
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
80
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45 55
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)
N_AC_070401_1_0770101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-077-A01
7-4-1Page 14
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
80
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45
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)
MTOW = 87 000 kg
MLW = 75 500 kg
MZFW = 71 500 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
A/C CODE S
N_AC_070401_1_0780101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-078-A01
7-4-1Page 15
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
A/C CODE U
MTOW = 89 000 kg
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45 55
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)
MLW = 75 500 kg
80
CG FOR ACNCALCULATIONS
MZFW = 71 500 kg
LANDING
TAKE OFF
N_AC_070401_1_0790101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-079-A01
7-4-1Page 16
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45
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)
80
CG FOR ACNCALCULATIONS
LANDING
A/C CODE V
MZFW = 71 500 kg
MLW = 75 500 kg
TAKE OFF
MTOW = 89 000 kg
N_AC_070401_1_0800101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-080-A01
7-4-1Page 17
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
N_AC_070401_1_0810101_01_00
MLW = 77 800 kg
CG FOR ACNCALCULATIONS
LANDING
MZFW = 73 800 kg
MTOW = 89 000 kg
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45
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)
80
A/C CODE X
TAKE OFF
Landing Gear Loading on PavementFIGURE-7-4-1-991-081-A01
7-4-1Page 18
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45
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) 80
MLW = 77 800 kg
CG FOR ACNCALCULATIONS
LANDING
MZFW = 73 800 kg
MTOW = 91 000 kg
TAKE OFF
95 95
A/C CODE Z
N_AC_070401_1_0820101_01_00
Landing Gear Loading on PavementFIGURE-7-4-1-991-082-A01
7-4-1Page 19
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
N_AC_070401_1_0830101_01_00
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45
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) 80
95 95
MLW = 77 800 kg
CG FOR ACNCALCULATIONS
LANDING
MTOW = 93 000 kg
TAKE OFF
MZFW = 73 800 kg
A/C CODE AA
Landing Gear Loading on PavementFIGURE-7-4-1-991-083-A01
7-4-1Page 20
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
N_AC_070401_1_0840101_01_00
35
40
45
50
55
60
65
70
75
80
85
90
3535
40
45
50
55
60
65
70
75
85
90
86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
5 15 25 35 45
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) 80
95 95
MLW = 77 800 kg
CG FOR ACNCALCULATIONS
LANDING
MZFW = 73 800 kg
TAKE OFF
MTOW = 93 500 kg
A/C CODE AB
Landing Gear Loading on PavementFIGURE-7-4-1-991-084-A01
7-4-1Page 21
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A321-100 A321-200
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 30 000 kg (66 150 lb).
For these conditions, the Flexible Pavement Thickness is 52.5 cm (20.7 in).
The line showing 10 000 Coverages is used to calculate the Aircraft Classification Number (ACN).
7-5-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
N_AC_070501_1_1080101_01_00
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
WEIGHT ON ONE MAIN LANDING GEAR37 510 kg (82 700 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE C
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
N_AC_070501_1_1080101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Flexible Pavement RequirementsFIGURE-7-5-1-991-108-A01
7-5-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
N_AC_070501_1_1090101_01_00
WEIGHT ON ONE MAIN LANDING GEAR37 510 kg (82 700 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE D
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Flexible Pavement RequirementsFIGURE-7-5-1-991-109-A01
7-5-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
WEIGHT ON ONE MAIN LANDING GEAR37 510 kg (82 700 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE E
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_1100101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-110-A01
7-5-1Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE G
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
WEIGHT ON ONE MAIN LANDING GEAR38 470 kg (84 800 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_1110101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-111-A01
7-5-1Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
WEIGHT ON ONE MAIN LANDING GEAR38 440 kg (84 750 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE H
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_1120101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-112-A01
7-5-1Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
WEIGHT ON ONE MAIN LANDING GEAR39 910 kg (87 975 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE I
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_1130101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-113-A01
7-5-1Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE J
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR39 770 kg (87 675 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
N_AC_070501_1_1140101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-114-A01
7-5-1Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
WEIGHT ON ONE MAIN LANDING GEAR39 910 kg (87 975 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE L
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_1150101_01_00
Flexible Pavement RequirementFlexible Pavement Requirements
FIGURE-7-5-1-991-115-A01
7-5-1Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
WEIGHT ON ONE MAIN LANDING GEAR39 910 kg (87 975 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE M
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_1160101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-116-A01
7-5-1Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
WEIGHT ON ONE MAIN LANDING GEAR39 770 kg (87 675 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
A/C CODE O
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070501_1_1170101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-117-A01
7-5-1Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 13.9 bar (202 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE P ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
40 860 kg (90 100 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
WEIGHT ON ONE MAIN LANDING GEAR
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
N_AC_070501_1_1180101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-118-A01
7-5-1Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 13.9 bar (202 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
40 660 kg (89 650 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE Q ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG WEIGHT ON ONE MAIN LANDING GEAR
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
N_AC_070501_1_1190101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-119-A01
7-5-1Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 13.9 bar (202 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE R ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
N_AC_070501_1_1200101_01_00
WEIGHT ON ONE MAIN LANDING GEAR40 660 kg (89 650 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-120-A01
7-5-1Page 14
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
N_AC_070501_1_1210101_01_00
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE S ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR41 800 kg (92 150 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-121-A01
7-5-1Page 15
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE U ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR42 440 kg (93 550 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
N_AC_070501_1_1220101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-122-A01
7-5-1Page 16
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE V ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR42 700 kg (94 125 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
N_AC_070501_1_1230101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-123-A01
7-5-1Page 17
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR42 700 kg (94 125 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
N_AC_070501_1_1240101_01_00
A/C CODE X
Flexible Pavement RequirementFlexible Pavement Requirements
FIGURE-7-5-1-991-124-A01
7-5-1Page 18
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 15 bar (218 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
N_AC_070501_1_1250101_01_00
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE Z ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR43 600 kg (96 125 lb)
25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)30 000 kg (66 150 lb)
Flexible Pavement RequirementsFIGURE-7-5-1-991-125-A01
7-5-1Page 19
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 15 bar (218 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE AA ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR44 490 kg (98 100 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
N_AC_070501_1_1260101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-126-A01
7-5-1Page 20
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1 270 x 455 R22 (49 x 18−22) TIRES
TIRE PRESSURE CONSTANT AT 15 bar (218 psi)
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
806050403020151063
FOR ACN CALCULATIONS10 000 COVERAGES USED
A/C CODE AB ALPHA FACTOR = 0.9
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES*1 2003 0006 00015 00025 000*20 YEAR PAVEMENT LIFE
WEIGHT ON ONE MAIN LANDING GEAR44 720 kg (98 575 lb)
30 000 kg (66 150 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)
35 000 kg (77 150 lb)
N_AC_070501_1_1270101_01_00
Flexible Pavement RequirementsFIGURE-7-5-1-991-127-A01
7-5-1Page 21
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A321-100 A321-200
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 73.5.
For these conditions, the weight on one Main Landing Gear is 35 000 kg (77 150 lb).
7-6-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-6-1 Flexible Pavement Requirements - LCN Conversion
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
37 5
10 k
g
(82
700
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
C
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
N_AC_070601_1_1110101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-111-A01
7-6-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
37 5
10 k
g
(82
700
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
D
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
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
N_AC_070601_1_1120101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-112-A01
7-6-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.8
bar
(186
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
37 5
10 k
g
(82
700
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
E
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
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
N_AC_070601_1_1130101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-113-A01
7-6-1Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.6
bar
(197
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
38 4
70 k
g
(84
800
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
G
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
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
N_AC_070601_1_1140101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-114-A01
7-6-1Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.6
bar
(197
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
38 4
40 k
g
(84
750
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
N_AC_070601_1_1150101_01_00
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
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
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-115-A01
7-6-1Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.6
bar
(197
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
39 9
10 k
g
(87
975
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
I
N_AC_070601_1_1160101_01_00
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
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
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-116-A01
7-6-1Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.6
bar
(197
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
39 7
70 k
g
(87
675
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
J
N_AC_070601_1_1170101_01_00
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
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
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-117-A01
7-6-1Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.6
bar
(197
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
39 9
10 k
g
(87
975
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
L
N_AC_070601_1_1180101_01_00
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
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
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-118-A01
7-6-1Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.6
bar
(197
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
WE
IGH
T O
N O
NE
MA
IN
39 9
10 k
g
(87
975
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
M
N_AC_070601_1_1190101_01_00
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
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
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-119-A01
7-6-1Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
35 30 25 20 15 10 580
120
6050
4030
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
4045
7010
0
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.6
bar
(197
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
90100
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
39 7
70 k
g
(87
675
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
O
N_AC_070601_1_1200101_01_00
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
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-120-A01
7-6-1Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
NO
TE
: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
Sec
ond
Edi
tion
1965
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
3.9
bar
(202
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
8010
060
5040
30
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
90100
A/C
CO
DE
P
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
40 8
60 k
g
(90
075
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
N_AC_070601_1_1210101_01_00
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-121-A01
7-6-1Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
3.9
bar
(202
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
Q
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
40 6
60 k
g
(89
650
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
N_AC_070601_1_1220101_01_00
8010
060
5040
30
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
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-122-A01
7-6-1Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
3.9
bar
(202
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
R
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
40 6
60 k
g
(89
650
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
N_AC_070601_1_1230101_01_00
8010
060
5040
30
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
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-123-A01
7-6-1Page 14
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
4.6
bar
(212
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
S
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
41 8
00 k
g
(92
150
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
8010
060
5040
30
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
7012
0
N_AC_070601_1_1240101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-124-A01
7-6-1Page 15
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
NO
TE
: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
Sec
ond
Edi
tion
1965
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
4.6
bar
(212
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
U
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
42 4
40 k
g
(93
575
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
8010
060
5040
30
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
7012
0
N_AC_070601_1_1250101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-125-A01
7-6-1Page 16
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
4.6
bar
(212
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
V
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
42 7
00 k
g
(94
125
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
N_AC_070601_1_1260101_01_00
8010
060
5040
30
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
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-126-A01
7-6-1Page 17
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
4.6
bar
(212
psi
)1
270
x 45
5 R
22 (
49 x
18−
22)
TIR
ES
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
X
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
42 7
00 k
g
(94
125
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
N_AC_070601_1_1270101_01_00
8010
060
5040
30
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
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-127-A01
7-6-1Page 18
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
5 ba
r (2
18 p
si)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
S
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
Z
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
43 6
00 k
g
(96
125
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
N_AC_070601_1_1280101_01_00
8010
060
5040
30
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
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-128-A01
7-6-1Page 19
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
5 ba
r (2
18 p
si)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
S
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
A/C
CO
DE
AA
35 30 25 20 15 1045 540
WE
IGH
T O
N O
NE
MA
IN
44 4
90 k
g
(98
075
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
N_AC_070601_1_1290101_01_00
8010
060
5040
30
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
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-129-A01
7-6-1Page 20
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
NO
TE
: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
Sec
ond
Edi
tion
1965
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
5 ba
r (2
18 p
si)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
S
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
10
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
)
90100
WE
IGH
T O
N O
NE
MA
IN
44 7
20 k
g
(98
600
lb)
35 0
00 k
g
(77
150
lb)
30 0
00 k
g
(66
150
lb)
25 0
00 k
g
(55
125
lb)
LAN
DIN
G G
EA
R
20 0
00 k
g
(44
100
lb)
A/C
CO
DE
AB
35 30 25 20 15 1045 540
N_AC_070601_1_1300101_01_00
8010
060
5040
30
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
7012
0
Flexible Pavement Requirements - LCN ConversionFIGURE-7-6-1-991-130-A01
7-6-1Page 21
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A321-100 A321-200
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 80 MN/m3 (300 lbf/in3)- an allowable working stress of 31.6 kgf/cm2 (450 lbf/in2)- the load on one MLG of 30 000 kg (66 150 lb).For these conditions, the Rigid Pavement Thickness is 24.9 cm (9.8 in).
7-7-0Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
N_AC_070701_1_1090101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAINLANDING GEAR
A/C CODE C
N_AC_070701_1_1090101_01_00
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
37 510 kg (82 700 lb)
20 000 kg (44 100 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-109-A01
7-7-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
N_AC_070701_1_1100101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAINLANDING GEAR
A/C CODE D
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
37 515 kg (82 700 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1100101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-110-A01
7-7-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 12.8 bar (186 psi)
N_AC_070701_1_1110101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAINLANDING GEAR
A/C CODE E
N_AC_070701_1_1110101_01_00
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
37 510 kg (82 700 lb)
20 000 kg (44 100 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-111-A01
7-7-1Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAINLANDING GEAR
A/C CODE G
N_AC_070701_1_1120101_01_00
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
38 470 kg (84 800 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-112-A01
7-7-1Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAINLANDING GEAR
A/C CODE H
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
38 440 kg (84 750 lb)
20 000 kg (44 100 lb)
N_AC_070701_1_1130101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-113-A01
7-7-1Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAINLANDING GEAR
A/C CODE I
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
39 905 kg (87 975 lb)
20 000 kg (44 100 lb)
N_AC_070701_1_1140101_01_00
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-114-A01
7-7-1Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE J
WEIGHT ON ONE MAINLANDING GEAR
N_AC_070701_1_1150101_01_00
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
39 770 kg (87 675 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-115-A01
7-7-1Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE L
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAINLANDING GEAR
N_AC_070701_1_1160101_01_00
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
39 905 kg (87 975 lb)
20 000 kg (44 100 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-116-A01
7-7-1Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE M
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAINLANDING GEAR
N_AC_070701_1_1170101_01_00
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
39 905 kg (87 975 lb)
20 000 kg (44 100 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-117-A01
7-7-1Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.6 bar (197 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE O
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAINLANDING GEAR
N_AC_070701_1_1180101_01_00
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
39 770 kg (87 675 lb)
20 000 kg (44 100 lb)
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-118-A01
7-7-1Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.9 bar (202 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
40 865 kg (90 100 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1190101_01_00
A/C CODE P
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-119-A01
7-7-1Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.9 bar (202 psi)
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
40 660 kg (89 650 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1200101_01_00
A/C CODE Q
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-120-A01
7-7-1Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 13.9 bar (202 psi)
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
40 660 kg (89 650 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1210101_01_00
A/C CODE R
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-121-A01
7-7-1Page 14
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
41 805 kg (92 150 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1220101_01_00
A/C CODE S
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-122-A01
7-7-1Page 15
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
42 435 kg (93 550 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1230101_01_00
A/C CODE U
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-123-A01
7-7-1Page 16
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
42 700 kg (94 125 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1240101_01_00
A/C CODE V
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-124-A01
7-7-1Page 17
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 14.6 bar (212 psi)
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
42 700 kg (94 125 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1250101_01_00
A/C CODE X
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-125-A01
7-7-1Page 18
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
43 595 kg (96 125 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1260101_01_00
A/C CODE Z
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-126-A01
7-7-1Page 19
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
44 490 kg (98 100 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1270101_01_00
A/C CODE AA
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-127-A01
7-7-1Page 20
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
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
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
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
1 270 x 455 R22 (49 x 18−22) TIRESTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
WEIGHT ON ONEMAIN LANDING GEAR
35 000 kg (77 150 lb)30 000 kg (66 150 lb)25 000 kg (55 125 lb)
44 715 kg (98 575 lb)
20 000 kg (44 100 lb)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_1280101_01_00
A/C CODE AB
Rigid Pavement Requirements (PCA)FIGURE-7-7-1-991-128-A01
7-7-1Page 21
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-1 Radius of Relative Stiffness
**ON A/C A321-100 A321-200
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-1Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
L = Ed
= 24.1652dk
43
43
12 (1 − ) k2
RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES
N_AC_070801_1_0040101_01_01
E = YOUNG’S MODULUS = 4 x 10 psi
k = SUBGRADE MODULUS, lb/in
d = RIGID PAVEMENT THICKNESS, (in)
= POISSON’S RATIO = 0.15
WHERE6
3
Radius of Relative Stiffness(Reference: Portland Cement Association)
FIGURE-7-8-1-991-004-A01
7-8-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-2 Rigid Pavement Requirements - LCN Conversion
**ON A/C A321-100 A321-200
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 78.3.
For these conditions, the weight on one Main Landing Gear is 35 000 kg (77 150 lb).
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-8-2Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
C
37 5
10 k
g
(82
700
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
RM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_1110101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-111-A01
7-8-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
D
37 5
15 k
g
(82
700
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
RM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_1120101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-112-A01
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Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
E
37 5
10 k
g
(82
700
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
RM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
N_AC_070802_1_1130101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-113-A01
7-8-2Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
G
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
N_AC_070802_1_1140101_01_00
38 4
70 k
g
(84
800
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-114-A01
7-8-2Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
H
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
38 4
40 k
g
(84
750
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1150101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-115-A01
7-8-2Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
I
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
39 9
05 k
g
(87
975
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1160101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-116-A01
7-8-2Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
J
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
N_AC_070802_1_1170101_01_00
39 7
70 k
g
(87
675
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-117-A01
7-8-2Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
L
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
39 9
05 k
g
(87
975
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1180101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-118-A01
7-8-2Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
M
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
N_AC_070802_1_1190101_01_00
39 9
05 k
g
(87
975
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-119-A01
7-8-2Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
O
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
39 7
70 k
g
(87
675
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1200101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-120-A01
7-8-2Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
P
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
N_AC_070802_1_1210101_01_00
40 8
65 k
g
(90
100
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-121-A01
7-8-2Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
Q
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
N_AC_070802_1_1220101_01_00
40 6
60 k
g
(89
650
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-122-A01
7-8-2Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
R
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
40 6
60 k
g
(89
650
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1230101_01_00
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
S
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
41 8
05 k
g
(92
150
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1240101_01_00
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Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
U
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
N_AC_070802_1_1250101_01_00
42 4
35 k
g
(93
550
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-125-A01
7-8-2Page 16
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
V
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
42 7
00 k
g
(94
125
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1260101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-126-A01
7-8-2Page 17
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
X
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
42 7
00 k
g
(94
125
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1270101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-127-A01
7-8-2Page 18
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
Z
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
43 5
95 k
g
(96
125
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1280101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-128-A01
7-8-2Page 19
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
AA
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
N_AC_070802_1_1290101_01_00
44 4
90 k
g
(98
100
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-129-A01
7-8-2Page 20
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
2030
4050
100
8070
602030405060708090
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
)
508
762
1 01
61
270
1 77
82
286
9010
080
7060
5040
93439 29 24 19 14
A/C
CO
DE
AB
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
44 7
15 k
g
(98
575
lb)
35 0
00 k
g
(77
150
lb)
20 0
00 k
g
(44
100
lb)
25 0
00 k
g
(55
125
lb)
30 0
00 k
g
(66
150
lb)
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
N_AC_070802_1_1300101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE-7-8-2-991-130-A01
7-8-2Page 21
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-3 Radius of Relative Stiffness (Other values of E and L)
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-8-4 Radius of Relative Stiffness
**ON A/C A321-100 A321-200
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-4Page 1
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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 0.20 0.25
EFFECT OF ON L VALUES
E, Young’s Modulus (10 , PSI)
EFFECT OF E ON L VALUES
BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF TABLE 7−8−1NOTE:
, Poisson’s Ratio
E F
acto
rF
acto
r
N_AC_070804_1_0040101_01_02
Radius of Relative Stiffness(Effect E and µ on ”L” values)
FIGURE-7-8-4-991-004-A01
7-8-4Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-0 ACN/PCN Reporting System
**ON A/C A321-100 A321-200
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 65 000 kg (143 300 lb) and low subgrade strength (code C), theACN for the flexible pavement is 38.3.
In the example shown in Section 7-9-2 Aircraft Classification Number -- Rigid Pavement, A/C CodeC, for an aircraft gross weight of 65 000 kg (143 300 lb) and medium subgrade strength (code B),the ACN for the rigid pavement is 39.7.
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-1 Aircraft Classification Number - Flexible Pavement
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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: 4
1 %
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
60
ALP
HA
FA
CT
OR
= 0
.9
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_1230101_01_00
A/C
CO
DE
C
ON
PA
VE
ME
NT
− A
/C C
OD
E C
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-123-A01
7-9-1Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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: 4
1 %
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
60
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
D
N_AC_070901_1_1240101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E D
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-124-A01
7-9-1Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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: 4
1 %
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
60
N_AC_070901_1_1250101_01_00
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
E
N_AC_070901_1_1250101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-125-A01
7-9-1Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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: 4
1 %
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
1431
4815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
G
N_AC_070901_1_1260101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-126-A01
7-9-1Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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: 4
0.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
1431
4815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
N_AC_070901_1_1270101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-127-A01
7-9-1Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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: 4
1 %
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
1431
4815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
I
ON
PA
VE
ME
NT
− A
/C C
OD
E I
N_AC_070901_1_1280101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-128-A01
7-9-1Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
9.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
1431
4815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
J
ON
PA
VE
ME
NT
− A
/C C
OD
E J
N_AC_070901_1_1290101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-129-A01
7-9-1Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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: 4
1 %
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
1431
4815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
L
N_AC_070901_1_1300101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-130-A01
7-9-1Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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: 4
1 %
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
1431
4815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
M
ON
PA
VE
ME
NT
− A
/C C
OD
E M
N_AC_070901_1_1310101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-131-A01
7-9-1Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
9.7
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
1431
4815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
ALP
HA
FA
CT
OR
= 0
.9
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
O
ON
PA
VE
ME
NT
− A
/C C
OD
E O
N_AC_070901_1_1320101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-132-A01
7-9-1Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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: 4
1 %
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
1211
2613
013
413
914
314
815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
90
192
196
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
P
65
ALP
HA
FA
CT
OR
= 0
.9
ON
PA
VE
ME
NT
− A
/C C
OD
E P
N_AC_070901_1_1330101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-133-A01
7-9-1Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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
9.1
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
7782
8690
9599
104
108
112
(x 1
000
lb)
117
1211
2613
013
413
914
314
815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
90
192
196
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
Q
65
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_1340101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Q
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-134-A01
7-9-1Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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
9.1
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
7782
8690
9599
104
108
112
(x 1
000
lb)
117
1211
2613
013
413
914
314
815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
90
192
196
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
R
65
ALP
HA
FA
CT
OR
= 0
.9
ON
PA
VE
ME
NT
− A
/C C
OD
E R
N_AC_070901_1_1350101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-135-A01
7-9-1Page 14
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8.53
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
7782
8690
9599
104
108
112
(x 1
000
lb)
117
1211
2613
013
413
914
314
815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
90
192
196
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
S
65
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_1360101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E S
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-136-A01
7-9-1Page 15
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8 %
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
1211
2613
013
413
914
314
815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
90
192
196
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
U
65
ALP
HA
FA
CT
OR
= 0
.9
ON
PA
VE
ME
NT
− A
/C C
OD
E U
N_AC_070901_1_1370101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-137-A01
7-9-1Page 16
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8 %
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
1211
2613
013
413
914
314
815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
90
192
196
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
V
65
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_1380101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E V
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-138-A01
7-9-1Page 17
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8 %
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
1211
2613
013
413
914
314
815
215
716
1
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
174
60
85
165
170
187
179
183
90
192
196
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
X
65
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_1390101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E X
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-139-A01
7-9-1Page 18
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
7.49
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
lb)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
A/C
CO
DE
Z
ALP
HA
FA
CT
OR
= 0
.9
1520253035404550
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
7065
6055
5045
4035
75
55
80
174
60
85
165
170
187
179
183
90
192
196
6520
120
5
95
N_AC_070901_1_1400101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Z
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-140-A01
7-9-1Page 19
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
7 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
(x 1
000
lb)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
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
A/C
CO
DE
AA
1520253035404550
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
7065
6055
5045
4035
75
55
80
174
60
85
165
170
187
179
183
90
192
196
6520
120
5
95
N_AC_070901_1_1410101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
A
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-141-A01
7-9-1Page 20
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
6.88
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
(x 1
000
lb)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
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
A/C
CO
DE
AB
1520253035404550
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
7065
6055
5045
4035
75
55
80
174
60
85
165
170
187
179
183
90
192
196
6520
120
5
95
N_AC_070901_1_1420101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
B
Aircraft Classification Number -- Flexible PavementFIGURE-7-9-1-991-142-A01
7-9-1Page 21
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
7-9-2 Aircraft Classification Number - Rigid Pavement
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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: 4
1 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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
60
80
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)
55
N_AC_070902_1_1640101_01_00
A/C
CO
DE
C
ON
PA
VE
ME
NT
− A
/C C
OD
E C
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-164-A01
7-9-2Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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: 4
1 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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
60
80
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)
55
N_AC_070902_1_1650101_01_00
A/C
CO
DE
D
ON
PA
VE
ME
NT
− A
/C C
OD
E D
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-165-A01
7-9-2Page 3
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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: 4
1 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
8 ba
r (1
86 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
60
80
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)
55
165
170
174
N_AC_070902_1_1660101_01_00
A/C
CO
DE
E
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-166-A01
7-9-2Page 4
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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: 4
1 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
60
80
55
179
183
187
85
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)
N_AC_070902_1_1670101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
A/C
CO
DE
G
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-167-A01
7-9-2Page 5
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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: 4
0.7
% M
AC
.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
60
80
55
179
183
187
85
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)
N_AC_070902_1_1680101_01_00
A/C
CO
DE
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-168-A01
7-9-2Page 6
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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: 4
1 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
60
80
55
179
183
187
85
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)
N_AC_070902_1_1690101_01_00
A/C
CO
DE
I
ON
PA
VE
ME
NT
− A
/C C
OD
E I
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-169-A01
7-9-2Page 7
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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
9.7
% M
AC
.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
60
80
55
179
183
187
85
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)
N_AC_070902_1_1700101_01_00
A/C
CO
DE
J
ON
PA
VE
ME
NT
− A
/C C
OD
E J
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-170-A01
7-9-2Page 8
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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: 4
1 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
60
80
55
179
183
187
85
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)
N_AC_070902_1_1710101_01_00
A/C
CO
DE
L
ON
PA
VE
ME
NT
− A
/C C
OD
E L
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-171-A01
7-9-2Page 9
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
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: 4
1 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
60
80
55
179
183
187
85
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)
N_AC_070902_1_1720101_01_00
A/C
CO
DE
M
ON
PA
VE
ME
NT
− A
/C C
OD
E M
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-172-A01
7-9-2Page 10
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
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
9.7
% M
AC
.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
6 ba
r (1
97 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
60
80
55
179
183
187
85
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)
N_AC_070902_1_1730101_01_00
A/C
CO
DE
O
ON
PA
VE
ME
NT
− A
/C C
OD
E O
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-173-A01
7-9-2Page 11
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(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
65 55
179
183
196
85
N_AC_070902_1_1740101_01_00
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)
192
187
A/C
CO
DE
P
60
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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: 4
1 %
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 P
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-174-A01
7-9-2Page 12
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
65 55
179
183
196
85
192
187
60
N_AC_070902_1_1750101_01_00
A/C
CO
DE
Q
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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
9.1
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
GO
N P
AV
EM
EN
T −
A/C
CO
DE
Q
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-175-A01
7-9-2Page 13
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
65 55
179
183
196
85
192
187
60
A/C
CO
DE
R
N_AC_070902_1_1760101_01_00
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
9 ba
r (2
02 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
9.1
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
GO
N P
AV
EM
EN
T −
A/C
CO
DE
R
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-176-A01
7-9-2Page 14
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
65 55
179
183
196
85
192
187
60
A/C
CO
DE
S
N_AC_070902_1_1770101_01_00
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8.53
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
GO
N P
AV
EM
EN
T −
A/C
CO
DE
S
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-177-A01
7-9-2Page 15
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
65 55
179
183
196
85
192
187
60
A/C
CO
DE
U
N_AC_070902_1_1780101_01_00
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8 %
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 U
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-178-A01
7-9-2Page 16
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
65 55
179
183
196
85
192
187
60
A/C
CO
DE
V
N_AC_070902_1_1790101_01_00
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8 %
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 V
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-179-A01
7-9-2Page 17
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
65 55
179
183
196
85
192
187
60
A/C
CO
DE
X
N_AC_070902_1_1800101_01_00
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
14.
6 ba
r (2
12 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
8 %
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 X
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-180-A01
7-9-2Page 18
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
1520253035404550
3545
5565
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
65 55
179
183
196
85
192
187
60
A/C
CO
DE
Z
N_AC_070902_1_1810101_01_00
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
7.49
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
GO
N P
AV
EM
EN
T −
A/C
CO
DE
Z
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-181-A01
7-9-2Page 19
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1535
4555
6575
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
179
183
196
85
192
187
201
206
2535455565
9540
5060
7080
90
203040506070
N_AC_070902_1_1820101_01_00N_AC_070902_1_1820101_01_00
A/C
CO
DE
AA
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
7 %
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 A
A
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-182-A01
7-9-2Page 20
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-200
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
N_AC_070902_1_1830101_01_00
1535
4555
6575
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
179
183
196
85
192
187
201
205
2535455565
9540
5060
7080
90
203040506070
A/C
CO
DE
AB
(x 1
000
lb)
1 27
0 x
455
R22
(49
x 1
8−22
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
15
bar
(218
psi
)
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
6.88
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
GO
N P
AV
EM
EN
T −
A/C
CO
DE
AB
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)
Aircraft Classification Number -- Rigid PavementFIGURE-7-9-2-991-183-A01
7-9-2Page 21
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
SCALED DRAWINGS
8-0-0 SCALED DRAWINGS
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
0 10 20 30 40 50FEET
0 5 10 15METERS
010
2030
4050
FE
ET
05
1015
ME
TE
RS
N_AC_080000_1_0040101_01_00
WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING.NOTE:
Scaled DrawingFIGURE-8-0-0-991-004-A01
8-0-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
AIRCRAFT RESCUE AND FIRE FIGHTING
10-0-0 AIRCRAFT RESCUE AND FIRE FIGHTING
**ON A/C A321-100 A321-200
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
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
N_AC_100000_1_0010401_01_00
Front PageFIGURE-10-0-0-991-001-D01
10-0-0Page 2
Jun 01/12
@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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N_AC_100000_1_0020401_01_00
Highly Flammable and Hazardous Materials and ComponentsFIGURE-10-0-0-991-002-D01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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N_AC_100000_1_0030101_01_00
Wheel Safety Area(Sheet 1 of 2)
FIGURE-10-0-0-991-003-A01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
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N_AC_100000_1_0030102_01_00
Wheel Safety AreaRecommendations (Sheet 2 of 2)
FIGURE-10-0-0-991-003-A01
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N_AC_100000_1_0040401_01_00
Composite MaterialsFIGURE-10-0-0-991-004-D01
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A AB
B
N_AC_100000_1_0050101_01_00
LG Ground Lock Safety DevicesFIGURE-10-0-0-991-005-A01
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**ON A/C A321-100 A321-200
C L
N_AC_100000_1_0060401_01_00
Evacuation/Escape Slide/RaftFIGURE-10-0-0-991-006-D01
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N_AC_100000_1_0070201_01_00
Pax/Crew Doors and Emergency ExitsFIGURE-10-0-0-991-007-B01
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@A321AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A321-100 A321-200
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
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**ON A/C A321-100 A321-200
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N_AC_100000_1_0120101_01_00
Control PanelsFIGURE-10-0-0-991-012-A01
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**ON A/C A321-100 A321-200
316A
R
A
315A
L
A
N_AC_100000_1_0130101_01_00
APU Access DoorFIGURE-10-0-0-991-013-A01
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N_AC_100000_1_0140401_01_00
Aircraft Ground ClearancesFIGURE-10-0-0-991-014-D01
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**ON A/C A321-100 A321-200
N_AC_100000_1_0150101_01_00
Structural Break-in PointsFIGURE-10-0-0-991-015-A01
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