Airbus a319 airplane characteristics for airport planning

@AIRBUSA319

AIRPLANE CHARACTERISTICSFOR AIRPORT PLANNING

AC

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© AIRBUS S.A.S. 2005. All rights reserved.

AIRBUS S.A.S.Customer Services

Technical Data Support and Services31707 Blagnac Cedex

FRANCE

Issue: Jul 01/95 Rev: May 01/11

@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING

HIGHLIGHTS

Revision No. 10 - May 01/11

LOCATIONS CHGCODE

DESCRIPTIONS OF CHANGE

CHAPTER 2

Section 2-1

Subject 2-1-1

General Airplane Characteristics Data R

Section 2-2

Subject 2-2-0

FIGURE General Airplane Dimensions -General Airplane Dimensions

R ILLUSTRATION REVISEDILLUSTRATION REVISED

Section 2-3

Subject 2-3-0

Ground Clearances R NOTE AMENDED

FIGURE Ground Clearances - GroundClearances

R ILLUSTRATION REVISED ANDCOMPLETED

Section 2-7 R

Subject 02-07-06 D

CHAPTER 4

Section 4-5 R

Subject 04-05-04 D

Subject 04-05-05 D

CHAPTER 6

Section 6-1 R

Subject 06-01-03 D

Subject 06-01-04 D

CHAPTER 7

Section 7-1

Subject 7-1-0

General Information R

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LOCATIONS CHGCODE


FIGURE Aircraft Codes - Aircraft Codes N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED

Section 7-2

Subject 7-2-0

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

FIGURE Landing Gear Footprint -Landing Gear Footprint

R ILLUSTRATION REVISED








N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED


N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED

Section 7-3

Subject 7-3-0

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

FIGURE Maximum Pavement Loads -Maximum Pavement Loads

N ILLUSTRATION ADDED









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LOCATIONS CHGCODE










Section 7-4

Subject 7-4-0

Landing Gear Loading on Pavement R

Subject 7-4-1

Landing Gear Loading on Pavement R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement














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LOCATIONS CHGCODE


















Section 7-5

Subject 7-5-0

Flexible Pavement Requirements - U.S.Army Corps of Engineers Design Method

R

Subject 7-5-1

Flexible Pavement Requirements - U.S.Army Corps of Engineers Design Method

R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED

FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements




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Section 7-6

Subject 7-6-0

Flexible Pavement Requirements - LCNConversion

R

Subject 7-6-1

Flexible Pavement Requirements - LCNConversion


FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion






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LOCATIONS CHGCODE


Section 7-7

Subject 7-7-0

Rigid Pavement Requirements - PortlandCement Association Design Method

R

Subject 7-7-1

Rigid Pavement Requirements - PortlandCement Association Design Method


FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)


















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LOCATIONS CHGCODE














Section 7-8

Subject 7-8-0

Rigid Pavement Requirements - LCNConversion

R

Subject 7-8-2

Rigid Pavement Requirements - LCNConversion


FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion






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LOCATIONS CHGCODE


Subject 7-8-3

Radius of Relative Stiffness (Other valuesof ”E” and ”L”)

R

Subject 7-8-4

FIGURE Radius of Relative Stiffness -(Effect E and µ on ”L” values)


Section 7-9

Subject 7-9-0

ACN/PCN Reporting System R

Subject 7-9-1

Aircraft Classification Number - FlexiblePavement


FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement














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LOCATIONS CHGCODE


















Subject 7-9-2

Aircraft Classification Number - RigidPavement


FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement






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LIST OF EFFECTIVE CONTENT

Revision No. 10 - May 01/11

CONTENT CHGCODE

LAST REVISIONDATE

CHAPTER 1

Subject 1-1-0

Purpose Dec 01/07

Subject 1-2-0

Introduction Dec 01/07

CHAPTER 2

Subject 2-1-0

General Airplane Characteristics Dec 01/07

Subject 2-1-1

General Airplane Characteristics Data R May 01/11

Subject 2-2-0

General Airplane Dimensions Dec 01/07

FIGURE General Airplane Dimensions - General Airplane Dimensions R May 01/11

Subject 2-3-0

Ground Clearances R May 01/11

FIGURE Ground Clearances - Ground Clearances R May 01/11

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

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 - PassengerCompartment Cross-section

Sep 01/10

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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 Dec 01/07

Subject 2-6-1

Lower Deck Cargo Compartments Dec 01/07

FIGURE Lower Deck Cargo Compartments - Lower Deck CargoCompartments Dimensions

Dec 01/07

FIGURE Lower Deck Cargo Compartments - Lower Deck CargoCompartments Containers

Dec 01/07

Subject 2-7-0

Doors Clearances Dec 01/07

Subject 2-7-1

Forward Passenger / Crew Doors Dec 01/07

FIGURE Doors Clearances - Forward Passenger / Crew Doors Dec 01/07

Subject 2-7-2

Emergency Exits Dec 01/07

FIGURE Doors Clearances - Emergency Exits Dec 01/07

Subject 2-7-3

Aft Passenger / Crew Doors Dec 01/07

FIGURE Doors Clearances - Aft Passenger / Crew Doors Dec 01/07

Subject 2-7-4

Forward Cargo Compartment Door Dec 01/07

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

Subject 2-7-5

Aft Cargo Compartment Door Dec 01/07

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

Subject 2-7-7

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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

CHAPTER 3

Subject 3-1-0

General Information Dec 01/07

Subject 3-2-0

Payload / Range Dec 01/07

Subject 3-2-1

ISA Conditions Dec 01/07

FIGURE Payload / Range - CFM56-5A series engine Dec 01/07

FIGURE Payload / Range - CFM56-5B series engine Dec 01/07

FIGURE Payload / Range - IAE V2500-A5 series engine Dec 01/07

Subject 3-3-0

FAR / JAR Take-off Weight Limitation Dec 01/07

Subject 3-3-1


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

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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


FIGURE FAR / JAR Landing Field Length - CFM56-5A series engine Dec 01/07

FIGURE FAR / JAR Landing Field Length - IAE V2500 series engine Dec 01/07

Subject 3-5-0

Final Approach Speed Dec 01/07

FIGURE Final Approach Speed - CFM56-5A series engine Dec 01/07

FIGURE Final Approach Speed - IAE V2500 series engine Dec 01/07

CHAPTER 4

Subject 4-1-0

General Information Dec 01/07

Subject 4-2-0

Turning Radii Dec 01/07

FIGURE Turning Radii, no Slip Angle - Turning Radii, no Slip Angle Dec 01/07

FIGURE Turning Radii, no Slip Angle - Turning Radii, no Slip Angle Dec 01/07

Subject 4-3-0

Minimum Turning Radii Dec 01/07

FIGURE Minimum Turning Radii - Minimum Turning Radii Dec 01/07

Subject 4-4-0

Visibility from Cockpit in Static Position Dec 01/07

FIGURE Visibility from Cockpit in Static Position - Visibility fromCockpit in Static Position

Dec 01/07

Subject 4-5-0

Runway and Taxiway Turn Paths Dec 01/07

Subject 4-5-1

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135˚ Turn - Runway to Taxiway Dec 01/07

FIGURE 135˚ Turn - Runway to Taxiway - CG on Centerline Method Dec 01/07

FIGURE 135˚ Turn - Runway to Taxiway - NLG on CenterlineMethod

Dec 01/07

Subject 4-5-2

90˚ Turn - Runway to Taxiway Dec 01/07

FIGURE 90˚ Turn - Runway to Taxiway - CG on Centerline Method Dec 01/07

FIGURE 90˚ Turn - Runway to Taxiway - NLG on Centerline Method Dec 01/07

Subject 4-5-3

180˚ Turn on a Runway Dec 01/07

FIGURE 180˚ Turn on a 150 ft Runway - NLG on Centerline Method Dec 01/07

Subject 4-5-6

180˚ Turn on a Wide Runway Dec 01/07

FIGURE 180˚ Parallel Turn on a 150 ft Wide Runway - Edge ofRunway Method

Dec 01/07

Subject 4-6-0

Runway Holding Bay (Apron) Dec 01/07

FIGURE Runway Holding Bay (Apron) - Runway Holding Bay(Apron)

Dec 01/07

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

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Subject 5-1-2

Aircraft at the Gate Sep 01/10

FIGURE Aircraft at the Gate - Aircraft at the Gate Sep 01/10

Subject 5-1-3

Aircraft at an Open Apron Sep 01/10

FIGURE Aircraft at an Open Apron - Aircraft at an Open Apron(Bulk Loading)

Sep 01/10

FIGURE Aircraft at an Open Apron - Aircraft at an Open Apron(ULD Loading)

Sep 01/10

Subject 5-2-0

Terminal Operations - Full Servicing Turnaround Sep 01/10

Subject 5-2-1

Full Servicing Turnaround Charts Sep 01/10

FIGURE Turnaround Stations - Full Servicing (41 Min.) Sep 01/10

Subject 5-3-0

Terminal Operation Sep 01/10

Subject 5-3-1

Minimum Servicing Turnaround Chart Sep 01/10

FIGURE Turnaround Stations - Minimum Servicing (21 Min.) Sep 01/10

Subject 5-4-0

Ground Service Connections Dec 01/07

Subject 5-4-1

Ground Service Connections Layout Dec 01/07

FIGURE Ground Service Connections - Ground Service ConnectionsLayout

Dec 01/07

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

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Hydraulic System Sep 01/10

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 Sep 01/10

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 Sep 01/10

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

Subject 5-4-7

Pneumatic System Sep 01/10

Subject 5-4-8

Potable Water System Sep 01/10

FIGURE Ground Service Connections - Potable Water Ground ServicePanel

Sep 01/10

Subject 5-4-9

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

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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 Dec 01/07

Subject 5-5-1

Low Temperature -40˚C (-40˚F) Dec 01/07

FIGURE Engine Starting Pneumatic Requirements - Temperature-40˚C (-40˚F) -- CFM56 series engine

Dec 01/07

FIGURE Engine Starting Pneumatic Requirements - Temperature-40˚C (-40˚F) -- IAE V2500 series engine

Dec 01/07

Subject 5-5-2

Ambient Temperature +15˚C (+59˚F) Dec 01/07

FIGURE Engine Starting Pneumatic Requirements - Temperature+15˚C (+59˚F) -- CFM56 series engine

Dec 01/07

FIGURE Engine Starting Pneumatic Requirements - Temperature+15˚C (+59˚F) -- IAE V2500 series engine

Dec 01/07

Subject 5-5-3

High Temperature +50˚C (+122˚F) and +55˚C (+131˚F) Dec 01/07

FIGURE Engine Starting Pneumatic Requirements - Temperature+55˚C (+131˚F) -- CFM56 series engine

Dec 01/07

FIGURE Engine Starting Pneumatic Requirements - Temperature+50˚C (+122˚F) -- IAE V2500 series engine

Dec 01/07

Subject 5-6-0

Ground Pneumatic Power Requirements Dec 01/07

Subject 5-6-1

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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 - PreconditionedAirflow Requirements

Dec 01/07

Subject 5-8-0

Ground Towing Requirements Sep 01/10

FIGURE Ground Towing Requirements - Ground TowingRequirements

Sep 01/10

FIGURE Ground Towing Requirements - Typical Tow BarConfiguration 1

Sep 01/10

FIGURE Ground Towing Requirements - Typical Tow BarConfiguration 2

Sep 01/10

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

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

Dec 01/07

FIGURE Engine Exhaust Velocities - Ground Idle Power -- IAE V2500series engine

Dec 01/07

Subject 6-1-2

Engine Exhaust Temperatures Contours - Ground Idle Power Dec 01/07

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

Dec 01/07

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CONTENT CHGCODE

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FIGURE Engine Exhaust Temperatures - Ground Idle Power -- IAEV2500 series engine

Dec 01/07

Subject 6-1-5

Engine Exhaust Velocities Contours - Takeoff Power Dec 01/07

FIGURE Engine Exhaust Velocities - Takeoff Power -- CFM56 seriesengine

Dec 01/07

FIGURE Engine Exhaust Velocities - Takeoff Power -- IAE V2500series engine

Dec 01/07

Subject 6-1-6

Engine Exhaust Temperatures Contours - Takeoff Power Dec 01/07

FIGURE Engine Exhaust Temperatures - Takeoff Power -- CFM56series engine

Dec 01/07

FIGURE Engine Exhaust Temperatures - Takeoff Power -- IAE V2500series engine

Dec 01/07

Subject 6-2-0

Airport and Community Noise Dec 01/07

Subject 6-2-1

Noise Data Dec 01/07

FIGURE Airport and Community Noise - CFM56-5A series engine Dec 01/07

FIGURE Airport and Community Noise - CFM56-5B series engine Dec 01/07

FIGURE Airport and Community Noise - IAE V2500 series engine Dec 01/07

Subject 6-3-0

Danger Areas of Engines Dec 01/07

Subject 6-3-1

Ground Idle Power Dec 01/07

FIGURE Danger Areas of Engines - CFM56 series engine Dec 01/07

FIGURE Danger Areas of Engines - IAE V2500 series engine Dec 01/07

Subject 6-3-2

Takeoff Power Dec 01/07

FIGURE Danger Areas of Engines - CFM56 series engine Dec 01/07

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CONTENT CHGCODE

LAST REVISIONDATE

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 R May 01/11

FIGURE Aircraft Codes - Aircraft Codes N May 01/11

Subject 7-2-0

Landing Gear Footprint R May 01/11

FIGURE Landing Gear Footprint - Landing Gear Footprint R May 01/11




FIGURE Landing Gear Footprint - Landing Gear Footprint N May 01/11

FIGURE Landing Gear Footprint - Landing Gear Footprint N May 01/11

Subject 7-3-0

Maximum Pavement Loads R May 01/11

FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11








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Subject 7-4-0

Landing Gear Loading on Pavement R May 01/11

Subject 7-4-1

Landing Gear Loading on Pavement R May 01/11

FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement

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Subject 7-5-0

Flexible Pavement Requirements - U.S. Army Corps of EngineersDesign Method

R May 01/11

Subject 7-5-1

Flexible Pavement Requirements - U.S. Army Corps of EngineersDesign Method

R May 01/11

FIGURE Flexible Pavement Requirements - Flexible PavementRequirements

N May 01/11


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Subject 7-6-0

Flexible Pavement Requirements - LCN Conversion R May 01/11

Subject 7-6-1

Flexible Pavement Requirements - LCN Conversion R May 01/11

FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion

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Subject 7-7-0

Rigid Pavement Requirements - Portland Cement Association DesignMethod

R May 01/11

Subject 7-7-1

Rigid Pavement Requirements - Portland Cement Association DesignMethod

R May 01/11

FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)

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Subject 7-8-0

Rigid Pavement Requirements - LCN Conversion R May 01/11

Subject 7-8-1

Radius of Relative Stiffness Dec 01/07

FIGURE Radius of Relative Stiffness - (Reference: Portland CementAssociation)

Dec 01/07

Subject 7-8-2

Rigid Pavement Requirements - LCN Conversion R May 01/11

FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion

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Subject 7-8-3

Radius of Relative Stiffness (Other values of ”E” and ”L”) R May 01/11

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CONTENT CHGCODE

LAST REVISIONDATE

Subject 7-8-4

Radius of Relative Stiffness Dec 01/07

FIGURE Radius of Relative Stiffness - (Effect E and µ on ”L” values) R May 01/11

Subject 7-9-0

ACN/PCN Reporting System R May 01/11

Subject 7-9-1

Aircraft Classification Number - Flexible Pavement R May 01/11

FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement

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Subject 7-9-2

Aircraft Classification Number - Rigid Pavement R May 01/11

FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement

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CONTENT CHGCODE

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CHAPTER 8

Subject 8-1-0

Possible Future Derivative Airplane Dec 01/07

CHAPTER 9

Subject 9-1-0

Scaled Drawings Sep 01/10

FIGURE Scaled Drawing - Scaled Drawing Sep 01/10

FIGURE Scaled Drawing - Scaled Drawing Sep 01/10

L.E.C.Page 24

May 01/11


TABLE OF CONTENTS

1 SCOPE

1-1-0 Purpose

1-2-0 Introduction

2 AIRPLANE DESCRIPTION

2-1-0 General Airplane Characteristics

2-1-1 General Airplane Characteristics Data

2-2-0 General Airplane 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

2-6-1 Lower Deck Cargo Compartments

2-7-0 Door Clearances

2-7-1 Forward Passenger / Crew Doors

2-7-2 Emergency Exits

2-7-3 Aft Passenger / Crew Doors

2-7-4 Forward Cargo Compartment Doors

2-7-5 Aft Cargo Compartment Doors

2-7-7 Main Landing Gear Doors

2-7-8 Radome

2-7-9 APU and Nose Landing Gear Doors

3 AIRPLANE PERFORMANCE

3-1-0 General Information

3-2-0 Payload / Range

3-2-1 ISA Conditions

3-3-0 FAR / JAR Takeoff Weight Limitation


3-3-2 ISA +15˚C (+59˚F) Conditions

3-4-0 FAR / JAR Landing Field Length


3-5-0 Final Approach Speed

T.O.C.Page 1

May 01/11


4 GROUND MANEUVERING


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


4-5-3 180˚ Turn on a Runway

4-5-6 180˚ Turn on a Wide Runway

4-6-0 Runway Holding Bay (Apron)

4-7-0 Airplane Parking

5 TERMINAL SERVICING

5-0-0 TERMINAL SERVICING

5-1-0 Airplane Servicing Arrangements

5-1-1 Symbols Used on Servicing Diagrams

5-1-2 Typical Ramp Layout - Aircraft at the Gate

5-1-3 Typical Ramp Layout - Aircraft at an Open Apron

5-2-0 Terminal Operations - Full Servicing Turnaround

5-2-1 Full Servicing Turnaround Charts

5-3-0 Terminal Operation - Minimum Servicing Turnaround

5-3-1 Minimum Servicing Turnaround Chart

5-4-0 Ground Service Connections

5-4-1 Ground Service Connections Layout

5-4-2 Grounding Points

5-4-3 Hydraulic System

5-4-4 Electrical System

5-4-5 Oxygen System

5-4-6 Fuel System

5-4-7 Pneumatic System

5-4-8 Potable Water System

5-4-9 Oil System

5-4-10 Vacuum Toilet System

5-5-0 Engine Starting Pneumatic Requirements

5-5-1 Low Temperatures

5-5-2 Ambient Temperatures

5-5-3 High Temperatures

T.O.C.Page 2

May 01/11


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

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


7-2-0 Landing Gear Footprint

7-3-0 Maximum Pavement Loads

7-4-0 Landing Gear Loading on Pavement


7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method


7-6-0 Flexible Pavement Requirements - LCN Conversion


7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method


7-8-0 Rigid Pavement Requirements - LCN Conversion

7-8-1 Radius of Relative Stiffness


7-8-3 Radius of Relative Stiffness (Other values of E and L)


7-9-0 ACN/PCN Reporting System

T.O.C.Page 3

May 01/11


7-9-1 Aircraft Classification Number - Flexible Pavement

7-9-2 Aircraft Classification Number - Rigid Pavement

8 DERIVATIVE AIRPLANES

8-1-0 Possible Future Derivative Airplane

9 SCALED DRAWINGS

9-1-0 Scaled Drawings

T.O.C.Page 4

May 01/11


SCOPE

1-1-0 Purpose

**ON A/C A319-100

Purpose

1. GeneralThe A319 AIRPLANE CHARACTERISTICS (AC) manual is issued for the A319 basic versions toprovide the necessary data needed by airport operators and airlines for the planning of airportfacilities.

This document conforms to NAS 3601.

CORRESPONDENCECorrespondence concerning this publication should be directed to:

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

1-1-0Page 1

May 01/11


1-2-0 Introduction

**ON A/C A319-100

Introduction

1. General

This manual comprises 9 chapters with a List of Effective Pages (LEP) at the beginning of themanual and a Table Of Content (TOC) at the beginning of each chapter.

Chapter 1: SCOPE

Chapter 2: AIRPLANE DESCRIPTION

This chapter contains general dimensional and other basic aircraft data.

It covers:- aircraft dimensions and ground clearances,- passenger and cargo compartment arrangement.

Chapter 3: AIRPLANE PERFORMANCE

This chapter indicates the aircraft performance.

It covers:- payload range,- takeoff and landing runway requirements,- landing approach speed.

Chapter 4: GROUND MANEUVERING

This chapter provides the aircraft turning capability and maneuvering characteristics on the ground.

It includes:- turning radii and visibility from the cockpit,- runway and taxiway turn path.

Chapter 5: TERMINAL SERVICING

This chapter provides information for the arrangement of ground handling and servicing equipments.

It covers:- location and connections of ground servicing equipments,

1-2-0Page 1

May 01/11


- engine starting pneumatic and preconditioned airflow requirements.

Chapter 6: OPERATING CONDITIONS

This chapter contains data and safety/environmental precautions related to engine and APUoperation on the ground.

It covers:- contour size and shape of the jet engine exhaust velocities and temperature,- noise data.

Chapter 7: PAVEMENT DATA

This chapter contains the pavement data helpful for airport planning.

It gives:- landing gear foot print and static load,- charts for flexible pavements with Load Classification Number (LCN),- charts for rigid pavements with LCN,- Aircraft Classification Number (ACN), Pavement Classification Number (PCN), reporting system

for flexible and rigid pavements.

Chapter 8: DERIVATIVE AIRPLANES

This chapter gives relevant data of possible A319 new version with the associated size change.

Chapter 9: SCALED DRAWING

This chapter contains different A319 scaled drawings.

1-2-0Page 2

May 01/11


AIRPLANE DESCRIPTION

2-1-0 General Airplane Characteristics

**ON A/C A319-100

General Airplane Characteristics

1. General Airplane CharacteristicsThe weight terms used throughout this manual are given below together with their respectivedefinitions.

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

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

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

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

Operational Empty Weight (OEW):Weight of structure, powerplant, furnishings, systems, and other items of equipment that are anintegral part of a particular aircraft configuration plus the operator’s items. The operator’s items arethe flight and cabin crew and their baggage, unusable fuel, engine oil, emergency equipment, toiletchemical and fluids, galley structure, catering equipment, passenger seats and life vests, documents,etc.

Maximum Payload:Maximum Zero Fuel Weight (MZFW) minus Operational Empty Weight (OEW).

Maximum Seating Capacity:Maximum number of passengers specifically certified or anticipated for certification.

Maximum Cargo Volume:Maximum usable volume available for cargo.

Usable Fuel:Fuel available for aircraft propulsion.

2-1-0Page 1

May 01/11


2-1-1 General Airplane Characteristics Data

**ON A/C A319-100

General Airplane Characteristics Data

1. The following table provides characteristics of A319-100 Models, these data are specific to eachWeight Variant:

Aircraft CharacteristicsWV000 WV001 WV002 WV003 WV004

Kilograms 64 400 70 400 75 900 68 400 68 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)

Pounds141 978 155 205 167 331 150 796 150 796

Kilograms 64 000 70 000 75 500 68 000 68 000Maximum Takeoff Weight(MTOW) Pounds 141 096 154 324 166 449 149 914 149 914

Kilograms 61 000 61 000 62 500 61 000 62 500Maximum Landing Weight(MLW) Pounds 134 482 134 482 137 789 134 482 137 789

Kilograms 57 000 57 000 58 500 57 000 58 500Maximum Zero FuelWeight (MZFW) Pounds 125 663 125 663 128 970 125 663 128 970

CFM Engines 39 725 kg (87 579 lb)Estimated OperationalEmpty Weight (OEW) IAE Engines 39 826 kg (87 801 lb)

Kilograms 17 275 18 775 17 275 18 775Estimated MaximumPayload CFM 56 Pounds 38 085 41 392 38 085 41 392

Kilograms 17 174 18 674 17 174 18 674Estimated MaximumPayload IAE V2500 Pounds 37 862 41 169 37 862 41 169


Kilograms 70 400 73 900 75 900 64 400 66 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)

Pounds155 205 162 922 167 331 141 978 146 387

Kilograms 70 000 73 500 75 500 64 000 66 000Maximum Takeoff Weight(MTOW) Pounds 154 324 162 040 166 449 141 096 145 505

Kilograms 62 500 62 500 61 000 62 500 62 500Maximum Landing Weight(MLW) Pounds 137 789 137 789 134 482 137 789 137 789

Kilograms 58 500 58 500 57 000 58 500 58 500Maximum Zero FuelWeight (MZFW) Pounds 128 970 128 970 125 663 128 970 128 970

CFM Engines 39 725 kg (87 579 lb)Estimated OperationalEmpty Weight (OEW) IAE Engines 39 826 kg (87 801 lb)

2-1-1Page 1

May 01/11



Kilograms 18 775 17 275 18 775Estimated MaximumPayload CFM 56 Pounds 41 392 38 085 41 392

Kilograms 18 674 17 174 18 674Estimated MaximumPayload IAE V2500 Pounds 41 169 37 862 41 169

Aircraft CharacteristicsWV011 WV012

Kilograms 66 400 62 400Maximum Ramp Weight (MRW)Maximum Taxi Weight (MTW) Pounds 146 387 137 568

Kilograms 66 000 62 000Maximum Takeoff Weight (MTOW)

Pounds 145 505 136 686Kilograms 61 000 61 000Maximum Landing Weight (MLW)

Pounds 134 482 134 482Kilograms 57 000 57 000Maximum Zero Fuel Weight (MZFW)

Pounds 125 663 125 663CFM Engines 39 725 kg (87 579 lb)Estimated Operational Empty Weight

(OEW) IAE Engines 39 826 kg (87 801 lb)

Kilograms 17 275Estimated Maximum Payload CFM 56

Pounds 38 085Kilograms 17 174Estimated Maximum Payload IAE

V2500 Pounds 37 862

2. The following table provides characteristics of A319-100 Models, these data are common to eachWeight Variant:

Aircraft CharacteristicsStandard SeatingCapacity

Single-class156

Liters 23 859US gallons 6 303

Kilograms(density =0.785 kg/l)

18 729

Usable Fuel Capacity

Pounds 41 290Cubic meters 285Pressurized Fuselage

Volume (A/C nonequipped)

Cubic feet10 065

2-1-1Page 2

May 01/11


Aircraft CharacteristicsCubic meters 120Passenger Compartment

Volume Cubic feet 4 238Cubic meters 9Cockpit VolumeCubic feet 318Cubic meters 8.52Usable Volume, FWD

CC Cubic feet 300Cubic meters 11.92Usable Volume, AFT CCCubic feet 421Cubic meters 7.22Usable Volume, Bulk CCCubic feet 255Cubic meters 10.63Water Volume, FWD CCCubic feet 375.4Cubic meters 13.91Water Volume, AFT CCCubic feet 491.2Cubic meters 7.51Water Volume, Bulk CCCubic feet 265.2

2-1-1Page 3

May 01/11


2-2-0 General Airplane Dimensions

**ON A/C A319-100

General Airplane Dimensions

1. This section provides General Airplane Dimensions.

2-2-0Page 1

May 01/11


**ON A/C A319-100

CFM56

V2500

3020100SCALE FEET

(13.58 ft)4.14 m

NOTE:SEE CHAPTER 2−7FOR DOOR SIZE

(111.02 ft)

2−3

SEECHAPTER

(12.96 ft)3.95 m

(31.23 ft)9.52 m

(31.5 ft)

(18.86 ft)5.75 m

OPTIONAL

(16.63 ft)5.07 m

(36.225 ft)11.04 m

(111.88 ft)34.10 m

9.6 m

33.84 m

7.59 m(24.9 ft)

(40.85 ft)12.45 m

N_AC_020200_1_0020101_01_02

SCALE METERS90 3 6

General Airplane Dimensions(Sheet 1 of 2)FIGURE 1

2-2-0Page 2

May 01/11


**ON A/C A319-100

CFM56

NOTE:SEE CHAPTER 2−7FOR DOOR SIZE

(111.02 ft)33.84 m

(12.96 ft)3.95 m

(16.63 ft)5.07 m

(18.86 ft)5.75 m

9.6 m(31.5 ft)

V2500(31.23 ft)9.52 m

11.04 m(36.23 ft)

(40.85 ft)12.45 m

3020100SCALE FEETSCALE METERS

960 3

N_AC_020200_1_0020102_01_00

7.59 m(24.9 ft)

35.48 m(116.4 ft)

(13.58 ft)4.14 m

OPTIONAL

2−3

SEECHAPTER

General Airplane DimensionsSharklet Option (Sheet 2 of 2)

FIGURE 2

2-2-0Page 3

May 01/11


2-3-0 Ground Clearances

**ON A/C A319-100

Ground Clearances

1. This section gives the height of various points of the aircraft, above the ground, for different aircraftconfigurations.Dimensions in the tables are approximate and will vary with tire type, W&B and others specialconditions.The dimensions are given for:- The basic aircraft OWE with a mid CG,- the MRW for the lightest weight variant with a FWD CG and a AFT CG,- the MRW for the heaviest weight variant with a FWD CG and a AFT CG,- aircraft on jacks, FDL at 4.6m (15.09ft).

NOTE : Passenger and cargo door clearances are measured from the center of the door sill and fromfloor level.

2-3-0Page 1

May 01/11


**ON A/C A319-100

A

OWE39 725 kg

CG 28%

MRW (WV0)64 400 kg

FWD CG 21%

MRW (WV8)73 900 kg

FWD CG 21%

AC JACKED FDL= 4.60 m

AFT CG 36%

11.386.866.006.3619.5919.982.202.795.688.9610.3711.487.28

BC1C2D1D2

E (CFM)E (IAE)

FF1F2F3G

11.126.595.746.14

19.3619.751.942.565.458.73

10.1411.257.05

11.326.735.846.0419.4219.621.972.565.388.6610.0711.196.92

11.096.535.686.0419.2919.651.872.495.358.63

10.0411.196.96

11.256.665.775.9419.3619.521.902.495.318.569.97

13.558.897.977.9721.5921.594.074.667.41

10.6612.07

12.17H 11.98 11.75 11.84

11.09 13.166.86 8.8911.61 13.55

39.73J 39.53 39.14 39.40 39.01 40.8512.80K1 12.60 12.43 12.50 12.37 14.3715.98K2 15.78 15.65 15.68 15.55 17.5518.31L 18.14 17.75 17.98 17.62 19.4613.02N 12.80 12.83 12.73 12.73 14.8913.98P 13.68 13.98 13.65 13.91 16.2715.98Q 15.81 15.39 15.68 15.26 17.06

AFT CG 36%

P A C1 B D1 E N C2 D2 H Q J

L F F1 F2 F3 K1 K2

3.472.091.831.945.976.090.670.851.732.733.163.502.223.71

12.113.904.875.583.974.264.87

3.392.011.751.875.906.020.590.781.662.663.093.432.153.6512.053.844.815.533.904.174.82

3.452.051.781.845.925.980.600.781.642.643.073.412.113.5811.933.794.775.413.914.264.69

3.381.991.731.845.885.990.570.761.632.633.063.412.123.61

12.013.814.785.483.884.164.78

3.432.031.761.815.905.950.580.761.622.613.043.382.093.5411.893.774.745.373.884.244.65

4.132.712.432.436.586.581.241.422.263.253.684.012.714.13

12.454.385.355.934.544.965.20

m ft m ft m ft m ft m ft m ft

NOTE:

G

PASSENGER AND CARGO DOOR GROUND CLEARANCES ARE MEASUREDFROM THE CENTER OF THE DOOR SILL AND FROM FLOOR LEVEL N_AC_020300_1_0020101_01_03

Ground ClearancesFIGURE 1

2-3-0Page 2

May 01/11


2-4-0 Interior Arrangements

**ON A/C A319-100

Interior Arrangements

1. This section gives the standard interior arrangements configuration.

2-4-0Page 1

May 01/11


2-4-1 Passenger Compartment Layout

**ON A/C A319-100

Typical Configuration

1. This section gives the typical interior configuration.

2-4-1Page 1

May 01/11


**ON A/C A319-100

/CR

EW

DO

OR

EM

ER

GE

NC

Y E

XIT

/CR

EW

DO

OR

156

SE

AT

S A

LL T

OU

RIS

T C

LAS

S28

/30

in P

ITC

H. 6

AB

RE

AS

T. 3

.3

FW

D P

AS

SE

NG

ER

AF

T P

AS

SE

NG

ER

/CR

EW

DO

OR

EM

ER

GE

NC

Y E

XIT

/CR

EW

DO

OR

FW

D P

AS

SE

NG

ER

AF

T P

AS

SE

NG

ER

A A

A

A

G L

G L

A

ITE

MD

ES

IGN

AT

ION

GG

ALL

EY

(2)

LLA

VA

TO

RY

(2)

AA

TT

EN

DA

NT

SE

AT

(5)

N_AC_020401_1_0020101_01_02

Typical ConfigurationTypical Configuration Single-Class, High Density

FIGURE 1

2-4-1Page 2

May 01/11


**ON A/C A319-100

8 S

UP

ER

FIR

ST

CLA

SS

PA

SS

EN

GE

R S

EA

TS

(12

4 T

OT

AL)

SE

AT

PIT

CH

ES

:

/CR

EW

DO

OR

EM

ER

GE

NC

Y E

XIT

AF

T P

AS

SE

NG

ER

/CR

EW

DO

OR

FW

D P

AS

SE

NG

ER

116

EC

ON

OM

Y C

LAS

S

FIR

ST

36

inE

CO

NO

MY

32

in

AF

T P

AS

SE

NG

ER

EM

ER

GE

NC

Y E

XIT

/CR

EW

DO

OR

FW

D P

AS

SE

NG

ER

/CR

EW

DO

OR

N_AC_020401_1_0080101_01_00

G

A AL

LG

L

A

ITE

MD

ES

IGN

AT

ION

GG

ALL

EY

(2)

LLA

VA

TO

RY

(3)

AA

TT

EN

DA

NT

SE

AT

(3)

Typical ConfigurationTypical Configuration Two-Class

FIGURE 2

2-4-1Page 3

May 01/11


2-5-0 Passenger Compartment Cross Section

**ON A/C A319-100

Passenger Compartment Cross-section

1. This section gives the typical passenger compartment cross-section configuration.

2-5-0Page 1

May 01/11


**ON A/C A319-100

3.95(155.51)

Cargo CompartmentFloor

CABINFLOOR

Top of cargoCompartment

AircraftDatum

Windows

2.64

(103.94)

2.13(83.86)

1.60(62.99)

1.24(48.82)

NOTE: DIMENSIONS m (in)

0.49(19.29)

0.52(20.47)

N_AC_020500_1_0010101_01_01

3.45(135.83)

3.68

(144.88)

1.42(55.91)

Passenger Compartment Cross-sectionFIGURE 1

2-5-0Page 2

May 01/11


**ON A/C A319-100


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

2-5-0Page 3

May 01/11


**ON A/C A319-100


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 3

2-5-0Page 4

May 01/11


**ON A/C A319-100


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 4

2-5-0Page 5

May 01/11


2-6-0 Cargo Compartments

**ON A/C A319-100

Cargo Compartments

1. This section gives the cargo compartments location and dimensions.

2-6-0Page 1

May 01/11


2-6-1 Lower Deck Cargo Compartments

**ON A/C A319-100

Lower Deck Cargo Compartments

1. This section gives the lower deck cargo compartments.

2-6-1Page 1

May 01/11


**ON A/C A319-100

FWD CARGOCOMPARTMENT DOOR

AFT CARGOCOMPARTMENT DOOR

AFT CARGOCOMPARTMENTNO.3 AND NO.4

BULK CARGOCOMPARTMENTNO.5

FWD CARGOCOMPARTMENTNO.1

FR24A FR34 FR47/FR51FR59

FR65

CARGO COMPT.FLOOR

1.243 m(4 ft 0.9 in)

1.430 m(4 ft 8.3 in)2.630 m

(8 ft 7.5 in)

TOP CARGOCOMPT.

3.346 m(10 ft 11.7 in)

1.816 m(5 ft 11.5 in)

1.816 m(5 ft 11.5 in)

7.661 m(25 ft 1.6 in)

N_AC_020601_1_0020101_01_00

Lower Deck Cargo CompartmentsLower Deck Cargo Compartments Dimensions

FIGURE 1

2-6-1Page 2

May 01/11


**ON A/C A319-100

FWD CARGO COMPARTMENTS

2 CONTAINERS(NO.1)

FR24A FR34 FR47/FR51

FR59

FR65

CABIN FLOOR

AFT CARGO COMPARTMENTS

2 CONTAINERS(NO.4)

FR24A

1.14 m(3 ft 9 in)

1.14 m(3 ft 9 in)

1.53 m(5 ft 0.4 in) 2.45 m

(8 ft 0.5 in)1.53 m

(5 ft 0.4 in)2.01 m

(6 ft 6.9 in)

1.56 m(5 ft 1.5 in)

1.56 m(5 ft 1.5 in)

N_AC_020601_1_0030101_01_00

Lower Deck Cargo CompartmentsLower Deck Cargo Compartments Containers

FIGURE 2

2-6-1Page 3

May 01/11


2-7-0 Door Clearances

**ON A/C A319-100

Doors Clearances

1. This section gives doors clearances.

2-7-0Page 1

May 01/11


2-7-1 Forward Passenger / Crew Doors

**ON A/C A319-100

Forward Passenger / Crew Doors

1. This section gives forward passenger / crew doors clearances.

2-7-1Page 1

May 01/11


**ON A/C A319-100

CRITICAL

CLEARANCE LIMIT

0.61 m(2 ft)

0.48 m(1 ft 6.88 in)

2.54 m(8 ft 3.99 in)

5.02 m(16 ft 5.62 in)

1.8 m(5 ft 10.8 in) 0.81 m

(2 ft 7.8 in)

1.85 m(6 ft 0.82 in)

SEECHAPTER

2.375 m(7 ft 9.48 in)

2−3

0.03 m(1.18 in)

N_AC_020701_1_0020101_01_00

Doors ClearancesForward Passenger / Crew Doors

FIGURE 1

2-7-1Page 2

May 01/11


2-7-2 Emergency Exits

**ON A/C A319-100

Emergency Exits

1. This section gives emergency exits doors clearances.

2-7-2Page 1

May 01/11


**ON A/C A319-100

NOTE: ESCAPE SLIDE COMPARTMENT DOOROPENS ON WING UPPER SURFACE.

(FROM NOSE)12.83 m

(42 ft 1.11 in)

0.5 m

0.47 m(1ft 6.49 in)

1.23 m(4 ft 0.42 in)

0.2 m(7.87 in)

FWD

0.9 m(2 ft 11.4 in)

0.495 m(1ft 7.48 in)

(TOP OF FLOOR)

0.12 m(4.72 in)

SEESECTION

2−3

A

A

B

B

CL

(1ft 7.68 in)

0.85 m(2 ft 9.45 in)

(FRAME 47)B BA A

OPTIONAL

N_AC_020702_1_0030101_01_00

Doors ClearancesEmergency Exits

FIGURE 1

2-7-2Page 2

May 01/11


2-7-3 Aft Passenger / Crew Doors

**ON A/C A319-100

Aft Passenger / Crew Doors

1. This section gives Aft passenger / crew doors clearances.

2-7-3Page 1

May 01/11


**ON A/C A319-100

1.79 m(5 ft 10.46 in)

0.81 m(2 ft 7.88 in)

0.58 m(1 ft 10.8 in)

CRITICALCLEARANCE

LIMIT

25.91 m(85 ft)

(FROM NOSE)

2.44 m(8 ft)

1.85 m(6 ft 0.82 in)

0.6 m(1 ft 11.6 in)

(1.18 in)0.03 m

FWD

SEE

2−3CHAPTER

A A

A

A

N_AC_020703_1_0020101_01_00

Doors ClearancesAft Passenger / Crew Doors

FIGURE 1

2-7-3Page 2

May 01/11


2-7-4 Forward Cargo Compartment Doors

**ON A/C A319-100

Forward Cargo Compartment Door

1. This section gives forward cargo compartment door clearances.

2-7-4Page 1

May 01/11


**ON A/C A319-100

8.16 m(26 ft 9.25 in)

1.82 m(5 ft 11.65 in)

1.24 m(4 ft 0.81 in)

3.945 m(12 ft 11.3 in)

1.495 m(4 ft 10.84 in)

0.5 m(1 ft 7.68 in)

(FROM NOSE)

2−3

SEECHAPTER

A

A

FWD

A A

2.71 m(8 ft 10.69 in)

N_AC_020704_1_0020101_01_00

Doors ClearancesForward Cargo Compartment Door

FIGURE 1

2-7-4Page 2

May 01/11


2-7-5 Aft Cargo Compartment Doors

**ON A/C A319-100

Aft Cargo Compartment Door

1. This section gives Aft cargo compartment door clearances.

2-7-5Page 1

May 01/11


**ON A/C A319-100

20.58 m

(67ft 6.22 in)

1.82 m(5 ft 11.65 in)

(FROM NOSE)

FWD

A

A

1.6 m5 ft 2.93 in)

1.23 m(4 ft 0.42 in)

3.945 m

(12 ft 11.3 in)

1.43 m(4 ft 8.29 in)

2−3

SEECHAPTER

A A

FWD

N_AC_020705_1_0020101_01_01

Doors ClearancesAft Cargo Compartment Door

FIGURE 1

2-7-5Page 2

May 01/11


2-7-7 Main Landing Gear Doors

**ON A/C A319-100

Main Landing Gear Doors

1. This section gives the main landing gear doors clearances.

2-7-7Page 1

May 01/11


**ON A/C A319-100

NOTE: VALUE OF CG: 25% RC.

A

GROUND LINE

0.207 m(8.14 in)

0.485 m

(1 ft 7.09 in)

AIRCRAFT

1.23 m(4 ft 0.42 in)

0.14 m(5.51 in)

84°

1.942 m

(6 ft 4.45 in)

14.758 m(48 ft 5 in)

1.826 m(5 ft 11.88 in)

1.761 m(5 ft 9.32 in)

A

N_AC_020707_1_0020101_01_02

Doors ClearancesMain Landing Gear Doors

FIGURE 1

2-7-7Page 2

May 01/11


2-7-8 Radome

**ON A/C A319-100

Radome

1. This section gives the radome clearances.

2-7-8Page 1

May 01/11


**ON A/C A319-100

0.63 m(2 ft 0.79 in)

STA 3500FR1

65°

(5 ft 0.62 in)1.54 m

N_AC_020708_1_0020101_01_00

Doors ClearancesRadome

FIGURE 1

2-7-8Page 2

May 01/11


2-7-9 APU and Nose Landing Gear Doors

**ON A/C A319-100

APU and Nose Landing Gear Doors

1. This section gives APU and Nose Landing Gear doors clearances.

2-7-9Page 1

May 01/11


**ON A/C A319-100

3.23

m(1

0 ft

7.16

in)

3.86

m(1

2 ft

7.96

in)

NOTE: VALUE OF CG : 25% RC.

1.5

m(4

ft 1

1 in

)

1.4

m(4

ft 7

.11

in)

FR80

FR84

N_AC_020709_1_0020101_01_00

Doors ClearancesAPU and Nose Landing Gear Doors

FIGURE 1

2-7-9Page 2

May 01/11


AIRPLANE PERFORMANCE


**ON A/C A319-100

General Information

1. This section gives standard day temperatures.

Section 3-2 indicates payload range information at specific altitudes recommended for long rangecruise with a given fuel reserve condition.

Section 3-3 represents FAR take-off runway length requirements at ISA and ISA +15˚C (+59˚F) forCFM56-5A, CFM56-5B and IAE V2500 series engine conditions for FAA certification.

Section 3-4 represents FAR landing runway length requirements for FAA certification.

Section 3-5 indicates final approach speeds.

Standard day temperatures for the altitudes shown are tabulated below:

Standard day temperatures for the altitude

Altitude Standard Day Temperature

FEET METERS ˚F ˚C0 0 59.0 15.02000 610 51.9 11.14000 1219 44.7 7.16000 1829 37.6 3.18000 2438 30.5 -0.8

3-1-0Page 1

May 01/11


3-2-0 Payload / Range

**ON A/C A319-100

Payload / Range

1. Payload / Range

3-2-0Page 1

May 01/11



**ON A/C A319-100

ISA Conditions

1. This section gives the payload / range at ISA conditions.

3-2-1Page 1

May 01/11


**ON A/C A319-100

50 40 30 20 10 0

20 10 00

1000

2000

3000

4000

010

0020

0030

0040

0050

0060

0070

00

(100

0 lb

)(1

000

kg)

PA

YLO

AD

RA

NG

E(K

M)

RA

NG

E(N

M)

MA

X T

AK

E−

OF

F W

EIG

HT

145

504

lb(6

6 00

0 kg

)

200

NM

(37

0 K

M)

DIV

ER

SIO

N30

MIN

UT

ES

HO

LD A

T 1

500

ftA

PP

RO

AC

H A

ND

LA

ND

ING

CR

UIS

E C

ON

DIT

ION

SIS

A +

10°

M =

0.7

635

000

/39

000

ft

INT

ER

NA

TIO

NA

L R

ES

ER

VE

S :

EN

RO

UT

E 1

0% F

LIG

HT

TIM

EO

VE

RS

HO

OT

124

PA

SS

EN

GE

RS

64t

75.5

t

70t

TH

ES

E C

UR

VE

S A

RE

GIV

EN

FO

R IN

FO

RM

AT

ION

ON

LYT

HE

AP

PR

OV

ED

VA

LUE

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

G T

HE

AIR

CR

AF

T.

NO

TE

:

N_AC_030201_1_0030101_01_00

Payload / RangeCFM56-5A series engine

FIGURE 1

3-2-1Page 2

May 01/11


**ON A/C A319-100

50 40 30 20 10 0

20 10 00

1000

2000

3000

4000

010

0020

0030

0040

0050

0060

0070

00

(100

0 lb

)(1

000

kg)

PA

YLO

AD

RA

NG

E(K

M)

RA

NG

E(N

M)

MA

X T

AK

E−

OF

F W

EIG

HT

145

504

lb(6

6 00

0 kg

)

200

NM

(37

0 K

M)

DIV

ER

SIO

N30

MIN

UT

ES

HO

LD A

T 1

500

ftA

PP

RO

AC

H A

ND

LA

ND

ING

CR

UIS

E C

ON

DIT

ION

SIS

A +

10°

M =

0.7

635

000

/39

000

ft

INT

ER

NA

TIO

NA

L R

ES

ER

VE

S :

EN

RO

UT

E 1

0% F

LIG

HT

TIM

EO

VE

RS

HO

OT

124

PA

SS

EN

GE

RS

64t

75.5

t

70t

TH

ES

E C

UR

VE

S A

RE

GIV

EN

FO

R IN

FO

RM

AT

ION

ON

LYT

HE

AP

PR

OV

ED

VA

LUE

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

G T

HE

AIR

CR

AF

T.

NO

TE

:

N_AC_030201_1_0040101_01_00

Payload / RangeCFM56-5B series engine

FIGURE 2

3-2-1Page 3

May 01/11


**ON A/C A319-100

50 40 30 20 10 0

20 10 00

1000

2000

3000

4000

010

0020

0030

0040

0050

0060

0070

00

(100

0 lb

)(1

000

kg)

PA

YLO

AD

RA

NG

E(K

M)

RA

NG

E(N

M)

MA

X T

AK

E−

OF

F W

EIG

HT

145

504

lb(6

6 00

0 kg

)

200

NM

(37

0 K

M)

DIV

ER

SIO

N30

MIN

UT

ES

HO

LD A

T 1

500

ftA

PP

RO

AC

H A

ND

LA

ND

ING

CR

UIS

E C

ON

DIT

ION

SIS

A +

10°

M =

0.7

635

000

/39

000

ft

INT

ER

NA

TIO

NA

L R

ES

ER

VE

S :

EN

RO

UT

E 1

0% F

LIG

HT

TIM

EO

VE

RS

HO

OT

124

PA

SS

EN

GE

RS

64t

75.5

t

70t

TH

ES

E C

UR

VE

S A

RE

GIV

EN

FO

R IN

FO

RM

AT

ION

ON

LYT

HE

AP

PR

OV

ED

VA

LUE

AR

E S

TA

TE

D IN

TH

E "

OP

ER

AT

ING

MA

NU

ALS

" S

PE

CIF

IC T

O T

HE

AIR

LIN

E O

PE

RA

TIN

G T

HE

AIR

CR

AF

T.

NO

TE

:

N_AC_030201_1_0050101_01_00

Payload / RangeIAE V2500-A5 series engine

FIGURE 3

3-2-1Page 4

May 01/11


3-3-0 FAR / JAR Takeoff Weight Limitation

**ON A/C A319-100

FAR / JAR Take-off Weight Limitation

1. FAR / JAR Take-off Weight Limitation

3-3-0Page 1

May 01/11



**ON A/C A319-100

ISA Conditions

1. This section gives the take-off weight limitation at ISA conditions.

3-3-1Page 1

May 01/11


**ON A/C A319-100

RUNWAY LENGTH

1000 ft

1000 m

THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.

NOTE:

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

110

120

130

140

150

160

170

180

190

200

210

220

230

110

100

90

80

70

60

50

40

1 2 3

4 6 8 10 12 14

4 5

16

86420

N_AC_030301_1_0030101_01_00

1000 kg

TA

KE

−O

FF

WE

IGH

T

1000 lb

FAR / JAR Take-off Weight LimitationISA Conditions -- CFM56 series engine

FIGURE 1

3-3-1Page 2

May 01/11


**ON A/C A319-100

RUNWAY LENGTH

1000 ft

1000 m


NOTE:

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

110

120

130

140

150

160

170

180

190

200

210

220

230

110

100

90

80

70

60

50

40

1 2 3

4 6 8 10 12 14

4 5

16

0

86

24

N_AC_030301_1_0040101_01_00

1000 kg

TA

KE

−O

FF

WE

IGH

T

1000 lb

FAR / JAR Take-off Weight LimitationISA Conditions -- IAE V2500 series engine

FIGURE 2

3-3-1Page 3

May 01/11


3-3-2 ISA +15˚C (+59˚F) Conditions

**ON A/C A319-100

ISA +15˚C (+59˚F) Conditions

1. This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions.

3-3-2Page 1

May 01/11


**ON A/C A319-100

RUNWAY LENGTH

1000 ft

1000 m


NOTE:

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

110

120

130

140

150

160

170

180

190

200

210

220

230

110

100

90

80

70

60

50

40

1 2 3

4 6 8 10 12 14

4 5

16

0

8642

N_AC_030302_1_0030101_01_00

1000 kg

TA

KE

−O

FF

WE

IGH

T

1000 lb

FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56 series engine

FIGURE 1

3-3-2Page 2

May 01/11


**ON A/C A319-100

RUNWAY LENGTH

1000 ft

1000 m


NOTE:

AIR

PO

RT

PR

ES

SU

RE

ALT

ITU

DE

(10

00 ft

)

110

120

130

140

150

160

170

180

190

200

210

220

230

110

100

90

80

70

60

50

40

1 2 3

4 6 8 10 12 14

4 5

16

0

86

24

N_AC_030302_1_0040101_01_00

1000 kg

TA

KE

−O

FF

WE

IGH

T

1000 lb

FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- IAE V2500 series engine

FIGURE 2

3-3-2Page 3

May 01/11


3-4-0 FAR / JAR Landing Field Length

**ON A/C A319-100

FAR / JAR Landing Field Length

1. FAR / JAR Landing Field Length

3-4-0Page 1

May 01/11



**ON A/C A319-100

ISA Conditions

1. This section gives the landing field length.

3-4-1Page 1

May 01/11


**ON A/C A319-100

3.0

3.5

4.0

4.5

5.0

5.5

6.0

160140120100806040GROSS WEIGHT

(1000 lb)

F.A

.R L

AN

DIN

G L

EN

GT

H (

1000

ft)


NOTE:

ISA CONDITIONSSLATS 27 DEG.FLAPS 35 DEG.

PRESSURE ALTITUDE(1000 ft)

10

6

SEA

4 2

8

LEVEL

N_AC_030401_1_0030101_01_00

FAR / JAR Landing Field LengthCFM56-5A series engine

FIGURE 1

3-4-1Page 2

May 01/11


**ON A/C A319-100

5.5

5.0

4.5

4.0

3.5

3.0160

GROSS WEIGHT(1000 lb)140120100806040


NOTE:

10 8 6 4 2SEA

PRESSURE ALTITUDE(1000 ft)

ISA CONDITIONSSLATS 27 DEG.FLAPS 35 DEG.

LEVEL

N_AC_030401_1_0040101_01_00

F.A

.R L

AN

DIN

G L

EN

GT

H (

1000

ft)

FAR / JAR Landing Field LengthIAE V2500 series engine

FIGURE 2

3-4-1Page 3

May 01/11


3-5-0 Final Approach Speed

**ON A/C A319-100

Final Approach Speed

1. This section gives the final approach speed.

3-5-0Page 1

May 01/11


**ON A/C A319-100

20018016014012010080100

110

120

130

140

150

160

170

C.A.S. (Kts)

GROSS WEIGHT(1000 lb)


NOTE:

LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 35DEG.

SEA LEVEL

N_AC_030500_1_0030101_01_00

Final Approach SpeedCFM56-5A series engine

FIGURE 1

3-5-0Page 2

May 01/11


**ON A/C A319-100

20018016014012010080100

110

120

130

140

150

160

170

C.A.S. (Kts)

GROSS WEIGHT(1000 lb)


NOTE:

LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 35 DEG.

SEA LEVEL

N_AC_030500_1_0040101_01_00

Final Approach SpeedIAE V2500 series engine

FIGURE 2

3-5-0Page 3

May 01/11


GROUND MANEUVERING


**ON A/C A319-100

General Information

1. This section provides airplane turning capability and maneuvering characteristics.

For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.

In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the using airlines prior to layout planning.

4-1-0Page 1

May 01/11


4-2-0 Turning Radii

**ON A/C A319-100

Turning Radii

1. This section gives the turning radii.

4-2-0Page 1

May 01/11


**ON A/C A319-100

R4

R6

R5

NOTE:

1.

2.

TURN TYPE

ASYMMETRIC THRUST DIFFERENTIALBRAKING (PIVOTTING ON ONE MAIN GEAR).

SYMMETRIC THRUST NO BRAKING

11.04 m

FOR STEERING DIMENSION TABLE SEE SHEET 2.

(36 ft 2.64 in)

R3

Y

7.59 m(24 ft 10.8 in)

(MIN TURNING WIDTH)A

N_AC_040200_1_0030101_01_01

Turning Radii, no Slip AngleFIGURE 1

4-2-0Page 2

May 01/11


**ON A/C A319-100

MA

XIM

UM

RA

MP

WE

IGH

T

WT

.31%

A31

9−10

0

EF

FE

CT

IVE

ST

EE

RIN

G

WIT

H S

LIP

ON

NLG

mft

Y

−

75.0

0°

74.9

2°

66.0

1°

60.3

9°

55.3

2°

50.2

9°

45.2

5°

35.1

9°

40.2

2°

30.1

6°

25.1

3°

20.1

0°

71°

70°

70°

70°

65°

55°

50°

45°

40°

35°

30°

25°

20°

3.79

4.01

3.86

4.02

5.15

6.37

7.73

9.26

11.0

4

15.7

7

13.1

6

19.1

2

23.6

7

30.3

3

12.4

13.2

12.7

13.2

16.9

20.9

25.4

30.4

36.2

51.7

43.2

62.7

77.7

99.5

R3

R4

R5

R6

A

mft

mft

mft

mft

mft

12.0

4

12.1

1

12.0

6

13.1

2

12.5

5

13.1

1

13.8

4

14.7

8

15.9

8

19.6

1

17.5

4

22.4

5

26.4

9

32.6

4

39.5

39.7

39.6

39.7

41.2

43.0

45.4

48.5

52.4

64.4

57.6

73.6

86.9

107.

1

21.3

6

21.5

8

21.4

3

21.5

8

22.6

9

23.8

9

25.2

2

26.7

3

28.4

8

33.1

5

30.5

7

36.4

7

40.9

9

47.6

1

70.1

70.8

70.3

70.8

74.4

78.4

82.7

87.7

93.4

108.

8

100.

3

119.

7

134.

5

156.

2

16.5

5

16.6

0

16.5

7

16.6

1

16.9

1

17.3

3

17.8

7

18.5

9

19.5

3

22.5

4

20.8

0

25.0

0

28.6

4

34.3

4

54.3

54.5

54.4

54.5

55.5

56.8

58.6

61.0

64.1

74.0

68.2

82.0

94.0

112.

7

19.6

6

19.7

7

19.6

9

19.7

7

20.3

8

21.0

9

21.9

3

22.9

3

24.1

7

27.7

4

25.7

2

30.4

7

34.3

5

40.2

8

64.5

64.9

64.6

64.9

66.9

69.2

71.9

75.2

79.3

91.0

84.4

100.

0

112.

7

132.

1

20.3

5

20.6

4

20.4

4

20.6

4

22.2

1

24.0

0

26.0

8

28.5

5

31.5

3

39.8

9

35.2

1

46.0

8

54.6

7

67.4

9

66.8

67.7

67.1

67.7

72.9

78.7

85.6

93.7

103.

4

130.

9

115.

5

151.

2

179.

4

221.

4

AN

GLE

WT

.30.

3%A

319−

100

wv

002

TU

RN

TY

PE

TY

RE

S

1 2 2 2 2 2 2 2 2 22 2 2 2

−

75.0

0°

73.9

1°

65.9

2°

60.4

0°

55.3

2°

50.2

8°

45.2

4°

35.1

8°

40.2

1°

30.1

5°

25.1

2°

20.1

0°

ST

EE

RIN

G A

NG

LE

15.0

8°15

°41

.20

135.

243

.02

141.

158

.44

191.

744

.24

145.

150

.35

165.

288

.73

291.

12

15.0

7°

60°

N_AC_040200_1_0040101_01_00

Turning Radii, no Slip AngleFIGURE 2

4-2-0Page 3

May 01/11


4-3-0 Minimum Turning Radii

**ON A/C A319-100

Minimum Turning Radii

1. This section gives the minimum turning radii.

4-3-0Page 1

May 01/11


**ON A/C A319-100

NOTE:

R3

R5

11.04 m(36 ft 2.64 in)

Y A R3 R4 R5 R6EFFECTIVETURN ANGLE

20.44 12.06 21.43 16.57 19.6970.71° EFF

75° STEERED

Y A R3 R4 R5 R6EFFECTIVETURN ANGLE

75° STEERED

A319−100 wv002

A319−100

4.01 20.64 12.11 21.58 16.60 19.77

3.86m

(ft)

m

(12.7) (67.1) (39.6) (70.3) (54.4) (64.6)

(13.2) (67.7) (39.7) (70.8) (54.5) (64.9)

70.03° EFFST

Y

70.03°(70.71°)

EFFECTIVETURN

STEERINGANGLE 75°

A

R6

R4

Y A R3 R4 R5 R6

(ft)

Y

70.03°(70.71°)

EFFECTIVETURN

STEERINGANGLE 75°

A

NOSE GEAR RADII TRACK R3,MEASURED FROM OUTSIDE FACE OF TIRE.MODEL 100 TURN DIMENSION SHOWN(MODEL 100 wv002 IN BRACKETS).THEORETICAL CENTER OF TURNFOR MINIMUM TURNING RADIUS.SLOW CONTINUOUS TURNING.APPROXIMATELY IDLE THRUSTON ALL ENGINES.NO DIFFERENTIAL BRAKING.DRY SURFACE.

PAVEMENTWIDTH FOR180° TURN

MINIMUM

N_AC_040300_1_0020101_01_01

Minimum Turning RadiiFIGURE 1

4-3-0Page 2

May 01/11


4-4-0 Visibility from Cockpit in Static Position

**ON A/C A319-100

Visibility from Cockpit in Static Position

1. This section gives the visibility from cockpit in static position.

4-4-0Page 1

May 01/11


**ON A/C A319-100

133°

133°

111°

111°

33°

20°

4.56 m(14ft 11.52 in)

2.405 m(7 ft 10.7 in)

12.54 m

(41 ft 1.7 in)

5.07 m(16 ft 7.56 in)

3.91 m(12 ft 9.84 in)

OPTIONAL

NOTE:PILOT’S EYE POSITION

0.53 m(1 ft 8.76 in)

46°30’

32°30’

33°

27°30’ 27°30’

33°

46°30’

32°30’

N_AC_040400_1_0020101_01_02

Visibility from Cockpit in Static PositionFIGURE 1

4-4-0Page 2

May 01/11


4-5-0 Runway and Taxiway Turn Paths

**ON A/C A319-100

Runway and Taxiway Turn Paths

1. Runway and Taxiway Turn Paths.

4-5-0Page 1

May 01/11



**ON A/C A319-100

135˚ Turn - Runway to Taxiway

1. This section gives the 135˚ turn - runway to taxiway.

4-5-1Page 1

May 01/11


**ON A/C A319-100

MLG PATH

R = 15.24 m(50.0 ft)

5.67 m

13.21 m

6.93 m(22 ft 8.4 in)

AIRCRAFTCG

NOTE: CG ON CENTERLINE METHOD135° RUNWAY TO TAXIWAY TURN15° MAX STEERING ANGLE ONCENTERLINE RADIUS.A 34.25 m (112 ft 6 in)

(43 ft 3.6 in)

(18 ft 7.2 in)

6.65 m(21 ft 9.6 in)

22.86 m(75.0 ft)

TAXIWAY

R = 51.44 m

TAIL TIP PATH

R = 34.25 m

45.72 m(150.0 ft)

RUNWAY

135°

(168 ft 9.6 in)

WING TIP PATH

(112 ft 4.8 in)

R = 43.90 m(144.0 ft)

N_AC_040501_1_0020101_01_01

135˚ Turn - Runway to TaxiwayCG on Centerline Method

FIGURE 1

4-5-1Page 2

May 01/11


**ON A/C A319-100

MLG PATH

NOTE:

TAIL TIP PATH

WING TIP PATH

R = 15.24 m(50.0 ft)

NLG PATH

6.46 m

13.24 m

R = 43.87 m

R = 50.65 m

R = 34.25 m

5.64 m(18 ft 6 in)

(43 ft 4.8 in)

(21 ft 2.4 in)

(143 ft 10.8 in)

(166 ft 2.4 in)

(112 ft 4.8 in)

22.86 m(75.0 ft)

TAXIWAY

NLG ON CENTERLINE METHOD 135° RUNWAYTO TAXIWAY TURN 15° MAX STEERING ANGLE ONA 34.25 m (112 ft 6 in) CENTERLINE RADIUS.

45.72 m(150.0 ft)

RUNWAY

135°

N_AC_040501_1_0030101_01_01

135˚ Turn - Runway to TaxiwayNLG on Centerline Method

FIGURE 2

4-5-1Page 3

May 01/11



**ON A/C A319-100

90˚ Turn - Runway to Taxiway

1. This section gives the 90˚ turn - runway to taxiway.

4-5-2Page 1

May 01/11


**ON A/C A319-100

NOTE: C.G. ON CENTERLINE METHOD90° RUNWAY TO TAXIWAY TURN15° MAX. STEERING ANGLEON A 34.25 m (112 ft 6 in) CENTERLINE RAD.

MLG PATH

22.86 m(75.0 ft)

TAXIWAY

6.94 m(22 ft 9.6 in)

R = 15.24 m(50.0 ft)

13.38 m(43 ft 10.8 in) 5.73 m

(18 ft 9.6 in) R = 43.73 m(143 ft 6 in)

45.72 m(150.0 ft)RUNWAY

R = 34.25 m

(112 ft 4.8 in)

TAIL TIP PATH

R = 51.38 m

(168 ft 7.2 in)

WING TIPPATH

N_AC_040502_1_0020101_01_00

90˚ Turn - Runway to TaxiwayCG on Centerline Method

FIGURE 1

4-5-2Page 2

May 01/11


**ON A/C A319-100

NOTE: NLG ON CENTERLINE METHOD90° RUNWAY TO TAXIWAY TURN15° MAX. STEERING ANGLEON A 34.25 m (112 ft 6 in) CENTERLINE RAD.

MLG PATH6.94 m

(22 ft 9.6 in)

NLG PATH

13.38 m(43 ft 10.8 in) 5.73 m

(18 ft 9.6 in) R = 43.73 m(143 ft 6 in)

22.86 m(75.0 ft)

TAXIWAY

R = 15.24 m(50.0 ft)

45.72 m(150.0 ft)RUNWAY

(112 ft 4.8 in)

R = 34.25 m

TAIL TIP PATH

R = 51.38 m

(168 ft 7.2 in)

WING TIPPATH

N_AC_040502_1_0030101_01_00

90˚ Turn - Runway to TaxiwayNLG on Centerline Method

FIGURE 2

4-5-2Page 3

May 01/11


4-5-3 180˚ Turn on a Runway

**ON A/C A319-100

180˚ Turn on a Runway

1. This section gives the 180˚ turn on a runway.

4-5-3Page 1

May 01/11


**ON A/C A319-100

NOSE PATH

NLG PATH

MLG PATH

4.12 m 3.32 m

10.0

7 m

5.27

m

3.65

m

WING TIPPATH

TAIL TIPPATH

NOTE:180° ANGLED TURN ON A 150 ft RUNWAY.40° MAX TURN ANGLE, 17.17 m (56 ft 4.08 in)CENTERLINE RADIUS.

NLG ON CENTERLINE METHOD.

(33

.0 ft

)

(17

ft 3.

6 in

)

(12

.0 ft

)

(10 ft 10.8 in)(13 ft 6 in)

15°

45.72 m(150.0 ft)

RUNWAY

N_AC_040503_1_0010101_01_01

180˚ Turn on a 150 ft RunwayNLG on Centerline Method

FIGURE 1

4-5-3Page 2

May 01/11


4-5-6 180˚ Turn on a Wide Runway

**ON A/C A319-100

180˚ Turn on a Wide Runway

1. This section gives the 180˚ turn on a wide runway.

4-5-6Page 1

May 01/11


**ON A/C A319-100

R = 30.52 m

NOSE TIP PATH

MLG PATH

TAIL TIPPATH

WING TIPPATH

3.21 m 4.14 m

9.03

m

4.23

m

4.53

m

NOTE: EDGE OF RUNWAY METHOD.180° PARALLEL TURN ON A 150 ft WIDE RUNWAY.40° MAX. TURN ANGLE ON A 17.17 m (56 ft 4.08 in)CENTERLINE RADIUS.

45.7 m(150.0 ft)

RUNWAY

NLG PATH

(110 ft 1.2 in)

(13 ft 7.2 in)(10 ft 6 in)

(29

ft 7.

2 in

)

(13

ft6 1

0.8

in)

(14

ft 10

.8 in

)

R = 25.72 m(84 ft 4.8 in)

N_AC_040506_1_0020101_01_01

180˚ Parallel Turn on a 150 ft Wide RunwayEdge of Runway Method

FIGURE 1

4-5-6Page 2

May 01/11


4-6-0 Runway Holding Bay (Apron)

**ON A/C A319-100

Runway Holding Bay (Apron)

1. This section gives the runway holding bay (Apron).

4-6-0Page 1

May 01/11


**ON A/C A319-100

6.10 m(20.0 ft)

NOTE:

6.10 m(20.0 ft)

LAYOUT IN ACCORDANCE WITH THEREQUIREMENTS OF NAS 3601, CHAPTER 4,AND AN/865, CHAPTER 3.OUTER PARKED AIRCRAFTTURNED THRU MIN.TURN RADIUS TO PARKED POSITION.

60.40 m(198 ft 2.4 in)

12.20 m(40.0 ft)

N_AC_040600_1_0020101_01_01

Runway Holding Bay (Apron)FIGURE 1

4-6-0Page 2

May 01/11


4-7-0 Airplane Parking

**ON A/C A319-100

Airplane Parking

1. The following figures and charts show the rectangular space required for parking against the terminalbuilding.

AIRPLANE MODEL MAX. EFF. STEERING MIN. LINE UP DISTANCE

90˚ TURN ANGLE DEGREESTODAm (ft)

ASDAm (ft)

A319 6912.07(39.6)

23.11(75.8)

AIRPLANEMODEL

MIN. LINE UP DISTANCE

REQUIREDMIN.

PAVEMENTWIDTH

NOMINAL LINE UP DISTANCE

180˚ TURNTODAm (ft)

ASDAm (ft)

m (ft)TODAm (ft)

ASDAm (ft)

A31915.34(50.3)

26.38(86.5)

27.4(89.9)

21.58(70.8)

32.62(107.0)

Abbreviations:- TODA (Take-Off Distance Adjustment)- ASDA (Accelerate-Stop Distance Adjustment)

4-7-0Page 1

May 01/11


**ON A/C A319-100

RUNWAY WIDTH 60.00 m

ED

GE

OF

RU

NW

AY

29.3

5 m

(REF)

18.3

1 m

END OF RUNWAY

NOTE:

3.05

m(R

EF

)

69° STEERING AND NO SLIP ON NLG TIRES.

(10.

0 ft)

(96

ft 3.

6 in

)

(60.

0 ft)

(196 ft 10.8 in)

3.05 m(10.0 ft)

N_AC_040700_1_0090101_01_01

Runway Length AlterationsLine Up Distances -- 90˚ Turn

FIGURE 1

4-7-0Page 2

May 01/11


**ON A/C A319-100

END OF RUNWAY

EDGE OFRUNWAY

27.41 m(90.0 ft)

16.60 m(54 ft 6 in)

3.05 m(10.0 ft)(REF)3.05 m

(10.0 ft)

NOTES: 69° STEERING AND NO SLIP ON NLG TIRES.

32.62 m(107.0 ft)

21.58 m(70 ft 9.6 in)

(REF)

3.05 m(10.0 ft)(REF)

N_AC_040700_1_0100101_01_01

Runway Length AlterationsLine Up Distances -- 180˚ Turn

FIGURE 2

4-7-0Page 3

May 01/11


TERMINAL SERVICING

5-0-0 TERMINAL SERVICING

**ON A/C A319-100

Terminal Servicing

1. GeneralThis chapter provides typical ramp layouts, corresponding minimum turnaround time estimations,locations of ground service points and service requirements.The information given in this chapter reflects ideal conditions. Actual ramp layouts and servicerequirements may vary according to local regulations, airline procedures and the airplane condition.- Section 5.1 shows typical ramp layouts for passenger aircraft at the gate or on an open apron.- Section 5.2 shows the minimum turnaround schedules for full servicing arrangements.- Section 5.3 shows the minimum turnaround schedule for reduced servicing arrangements.- Section 5.4 gives the locations of ground service connections, the standard of connections used

and typical capacities and requirements.- Section 5.5 provides the engine starting pneumatic requirements for different engine types and

different ambient temperatures.- Section 5.6 provides the air conditioning requirements for heating and cooling (pull-down and

pull-up) using ground conditioned air for different ambient temperatures.- Section 5.7 provides the air conditioning requirements for heating and cooling to maintain a

constant cabin air temperature using low pressure conditioned air.- Section 5.8 shows the ground towing requirements taking into account different ground surface

and aircraft conditions.

5-0-0Page 1

May 01/11


5-1-0 Airplane Servicing Arrangements

**ON A/C A319-100

Airplane Servicing Arrangements

1. GeneralThis chapter provides typical ramp layouts, showing the various GSE items in position during typicalturnaround scenarios for the passenger aircraft.

These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.

The associated turnaround chart for full servicing is given in section 5.2.The associated turnaround chart for minimum servicing arrangement is given in section 5.3.

5-1-0Page 1

May 01/11


5-1-1 Symbols Used on Servicing Diagrams

**ON A/C A319-100

Symbols Used on Servicing Diagrams

1. This table gives the symbols used on servicing diagrams.

Ground Support Equipment

AC AIR CONDITIONING UNITAS AIR STARTING UNITBULK BULK TRAINCAT CATERING TRUCKCB CONVEYOR BELTCLEAN CLEANING TRUCKFUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNITLD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLEPBB PASSENGER BOARDING BRIDGEPS PASSENGER STAIRSTOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE

5-1-1Page 1

May 01/11


5-1-2 Typical Ramp Layout - Aircraft at the Gate

**ON A/C A319-100

Aircraft at the Gate

1. This section gives the typical servicing arrangement for pax version (Passenger Bridge).

5-1-2Page 1

May 01/11


**ON A/C A319-100

2 40 12 180 66SCALE FEETSCALE METERS

LV

AC

TOW AS

FUEL

WV

CATPBB

LD CL

LD CL

CAT

ULD

ULD

GPU

N_AC_050102_1_0020101_01_02

Aircraft at the GateFIGURE 1

5-1-2Page 2

May 01/11


5-1-3 Typical Ramp Layout - Aircraft at an Open Apron

**ON A/C A319-100

Aircraft at an Open Apron

1. This section gives the typical servicing arrangement for pax version (Open Apron).

5-1-3Page 1

May 01/11


**ON A/C A319-100

6 12 180 0SCALE METERS

2 4 6SCALE FEETS

BULK

FUEL

LV

WV CB

CATPS

BULK

PS

AC

TOW

GPU

AS

CAT

CB

N_AC_050103_1_0010101_01_02

Aircraft at an Open ApronAircraft at an Open Apron (Bulk Loading)

FIGURE 1

5-1-3Page 2

May 01/11


**ON A/C A319-100

N_AC_050103_1_0050101_01_01

6 12 180 0SCALE METERS

2 4 6SCALE FEETS

LV

AS

GPU

FUEL

ULD

LD CL

LD CL

ULD

AC

WV

PS

TOW

CATPS

CAT

Aircraft at an Open ApronAircraft at an Open Apron (ULD Loading)

FIGURE 2

5-1-3Page 3

May 01/11


5-2-0 Terminal Operations - Full Servicing Turnaround

**ON A/C A319-100

Terminal Operations - Full Servicing Turnaround

1. This section provides a chart showing typical activities for full servicing turnaround.

These data are provided to show the general scope and type of activities involved in ramp operationsduring the turnaround of an aircraft.

Varying airline practices and operating circumstances may result in different sequences and differenttime intervals to do the activities shown.

5-2-0Page 1

May 01/11


5-2-1 Full Servicing Turnaround Charts

**ON A/C A319-100

Full Servicing Turnaround Charts

1. Assumptions for 41 minutes turnaround chart - Full Servicing.

Please note this turnaround time is an assumption regarding a given example.

A. Passenger handling: 124 pax / 1 bridge

(1) Deboarding- 1L:124- 2L:0- Deboarding rate: 22 pax / min per door.- No PRM

(2) Boarding- 1L:124- 2L:0- Boarding rate: 18 pax / min per door.- No PRM

B. Catering: R1 - R 2 / sequential- Galley M1: 4 FSTE- Galley M2: 4 FSTE

C. Cleaning: Time available

D. Security/Safety checks: Yes (3 min each)- Cabin crew change: Yes (3min)

E. Cargo- ULD only- 2 Cargo loaders- FWD compartment : 2 LD3- AFT compartment : 2 LD3

F. Refuel: 5.2 tons, 6624 (l), 2 hoses (1 side)

G. Water servicing: 100%

H. Toilet servicing: 100%

5-2-1Page 1

May 01/11


**ON A/C A319-100

SECURITY CHECK/SAFETY

CATERING AT DOOR R1

CATERING AT DOOR R2

CLEANING

CARGO FWD CC

CARGO AFT CC

BULK CC

REFUELLING

POTABLE WATERSERVICING

TOILET SERVICING

GSE POSITIONING

ACTIVITY

DEBOARDING/BOARDINGAFT DOOR

HEADCOUNTING

TASK NAMEELAPSED TIME IN MINUTES

DEBOARDING/BOARDINGFORWARD DOOR

ID

2

3

4

5

6

7

8

10

11

12

13

9

1

2 4 6 8 10 12 14 16 18 20 2224 26 28 30 32 3436 38 40 42 44 46 48

60

0to50

TRT: 41 min

AVAILABLE TIME

N_AC_050201_1_0030101_01_02

Turnaround StationsFull Servicing (41 Min.)

FIGURE 1

5-2-1Page 2

May 01/11


5-3-0 Terminal Operation - Minimum Servicing Turnaround

**ON A/C A319-100

Terminal Operation

1. This section provides a chart showing typical activities for minimum servicing turnaround.

These data are provided to show the general scope and type of activities involved in ramp operationsduring the turnaround of an aircraft.

Varying airline practices and operating circumstances may result in different sequences and differenttime intervals to do the activities shown.

5-3-0Page 1

May 01/11


5-3-1 Minimum Servicing Turnaround Chart

**ON A/C A319-100

Minimum Servicing Turnaround Chart

1. Assumptions for 21 minutes turnaround chart - Minimum servicing.

Please note this turnaround time is an assumption regarding a given example.

A. Passenger handling: 156 pax / 2 stairways

(1) Deboarding- 1L:78- 2L:78- Deboarding rate: 20 pax / min per door.- No PRM

(2) Boarding- 1L:78- 2L:78- Boarding rate: 15 pax / min per door.- No PRM

B. Catering: No- Galley M1:- Galley M2:

C. Cleaning: No

D. Security/Safety checks: Yes (3 min each)- Cabin crew change: No

E. Cargo- ULD only- 2 Cargo loaders- FWD compartment bulk: 2 LD3- AFT compartment bulk: 2 LD3

F. Refuel: 5.2 tons, 6624 (l), 2 hoses (1 side)

G. Water servicing: 0%:

H. Toilet servicing: 0%

5-3-1Page 1

May 01/11


**ON A/C A319-100

SECURITY CHECK/SAFETY

CATERING AT DOOR R1

CATERING AT DOOR R2

CLEANING

CARGO FWD CC

CARGO AFT CC

BULK CC

REFUELLING

POTABLE WATERSERVICING

TOILET SERVICING

DEBOARDING/BOARDINGAFT DOOR

HEADCOUNTING

DEBOARDING/BOARDINGFORWARD DOOR

2

3

4

5

6

7

8

10

11

12

13

9

1

TASK NAMEELAPSED TIME IN MINUTES

ID 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

30

0to25

GSE POSITIONING

ACTIVITY

TRT: 21 min

N_AC_050301_1_0020101_01_02

Turnaround StationsMinimum Servicing (21 Min.)

FIGURE 1

5-3-1Page 2

May 01/11


5-4-0 Ground Service Connections

**ON A/C A319-100

Ground Service Connections

1. Ground Service Connections.

5-4-0Page 1

May 01/11


5-4-1 Ground Service Connections Layout

**ON A/C A319-100

Ground Service Connections Layout

1. This section gives the ground service connections layout.

Ground Service Connections Layout

1 -- TOILET SERVICING2 -- WATER FILLING AND DRAINAGE3 -- GROUND ELECTRICAL POWER PANEL4 -- GROUND SERVICE CONDITIONED AIR CONNECTOR5 -- GROUND HP AIR CONDITIONING AND AIR START CONNECTOR

6 -- HYDRAULIC CONNECTORS (GROUND SERVICE PANELS)

7 -- IDG OIL FILLING CONNECTOR8 -- ENGINE OIL FILLING CONNECTOR

9 -- REFUEL/DEFUEL CONNECTOR

10 -- GRAVITY FILLING PANELS

11 -- REFUEL/DEFUEL PANEL

12 -- APU OIL FILLING CONNECTOR13 -- AIRCRAFT GROUNDING

5-4-1Page 1

May 01/11


**ON A/C A319-100

1213 67 − 823 13 1 − 21

3 1 2 4 57

8

9

11

8

7

9

10

1

26 12

10

N_AC_050401_1_0020101_01_00

Ground Service ConnectionsGround Service Connections Layout

FIGURE 1

5-4-1Page 2

May 01/11


5-4-2 Grounding Points

**ON A/C A319-100

Grounding Points

1. Grounding Points.

DISTANCE: Meters (ft)

FROM AIRPLANE CENTERLINEAFT OF NOSE

R SIDE L SIDE

MEAN HEIGHTFROM

GROUNDOn Nose Landing Gearleg:

5.07 m(16.63 ft) on centerline

0.94 m(3.08 ft)

On left Main LandingGear leg:

16.11 m(52.85 ft)

3.79 m(12.43 ft)

1.07 m(3.51 ft)

On right Main LandingGear leg:

16.11 m(52.85 ft)

3.79 m(12.43 ft)

1.07 m(3.51 ft)

A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).

B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for:- refuel/defuel operations,- maintenance operations,- bad weather conditions.

NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.

5-4-2Page 1

May 01/11


**ON A/C A319-100

(2)(1)

GROUND CABLE(OPTIONAL)

LANDINGGEAR

NOSE LANDING GEAR

MAIN LANDING GEAR

(1)

A

A

A

(1)

N_AC_050402_1_0030101_01_00

Ground Service ConnectionsGrounding Points

FIGURE 1

5-4-2Page 2

May 01/11


**ON A/C A319-100

NOTE: R SIDE SYMMETRICAL

A

RIB20

RIB19

B

FWD

A

A

FOR SPECIFICATIONS REFERTO FLIGHT MANUAL

BN_AC_050402_1_0040101_01_00

Ground Service ConnectionsGrounding Points

FIGURE 2

5-4-2Page 3

May 01/11


5-4-3 Hydraulic System

**ON A/C A319-100

Hydraulic System

1. Access.

POSITION FROM AIRCRAFTCENTERLINE

ACCESSAFT OF NOSE

m (ft) RH SIDEm (ft)

LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Green System:Access door 197CB

17.57(57.64)

1.27(4.17)

1.76(5.77)

Yellow System:Access door 198CB

17.57(57.64)

1.27(4.17)

1.76(5.77)

Blue System:Access door 197EB

18.92(60.07)

1.27(4.17)

1.76(5.77)

NOTE : Distances are approximate.

2. Reservoir Pressurization.On the air pressurization manifold:


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Access door 195AB14.05(46.1)

0.25(0.82)

1.74(5.71)

NOTE : Distances are approximate.- One 1/4 in. AEROQUIP AE 96994E self-sealing connection common to the 3 reservoirs.

3. Accumulator Charging.Four (MS28889-1) connections (one for each accumulator) for:


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Yellow Systemaccumulator:Access door 196BB

14.5(47.57)

0.25(0.82)

1.99(6.53)

5-4-3Page 1

May 01/11



ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Green Systemaccumulator:Left MLG door

15.67(51.41)

0.25(0.82)

3.2(10.5)

Blue Systemaccumulator:Access door 195BB

14.31(46.95)

0.25(0.82)

1.99(6.53)

Yellow System brakingaccumulator:Access door 196BB

14.5(47.57)

0.76(2.49)

1.74(5.71)


4. Reservoir Filling.On the Green system ground service panel:


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Access door 197CB17.57(57.64)

1.27(4.17)

1.76(5.77)

NOTE : Distances are approximate.One 1/4 in. AEROQUIP AE96993E self-sealing connection for pressurized supply.One handpump filling connection for unpressurized (suction) supply.

5. Reservoir Drain.On 3/8 in. self-sealing connection on reservoir for:


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Yellow System:Access door 196BB -198CB

14.5(47.57)

1.43(4.69)

1.90(6.23)

Green System:Left MLG door

15.67(51.41)

1.27(4.17)

2.61(8.56)

5-4-3Page 2

May 01/11



ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Blue System:Access door 197EB

18.92(62.07)

1.27(4.17)

1.76(5.77)

NOTE : Distances are approximate.On 3/8 in. self-sealing connection for the Blue system on:- Blue system ground service panel.

6. Ground Test.On each ground service panel:- One self-sealing connector AE80532N (suction).- One self-sealing connector AE80531K (delivery).

5-4-3Page 3

May 01/11


**ON A/C A319-100

RESERVOIR FILL SYSTEMHAND PUMP FILL CONNECTION

GROUND TESTPRESSURE

CONNECTION

GROUND TESTSUCTION

CONNECTIONRESERVOIR FILLCONNECTION

AE96993GM

GROUND SUPPLY

AE80531K AE80532N

1698GM

1008GM 1007GM 1006GM

197CB

A

AN_AC_050403_1_0040101_01_00

Hydraulic SystemGreen System Ground Service Panel

FIGURE 1

5-4-3Page 4

May 01/11


**ON A/C A319-100

GROUND CONNECTIONSUCTION

GROUNDCONNECTION

DELIVERY

AE80531K

AE80532N

2006GM

2008GM

A

Z197

A

N_AC_050403_1_0050101_01_00

Hydraulic SystemBlue System Ground Service Panel

FIGURE 2

5-4-3Page 5

May 01/11


**ON A/C A319-100

GROUND TESTPRESSURE CONNECTION

GROUND TESTSUCTION CONNECTION

AE80531K AE80532N

A

A

3008GM 3006GM

198CB

N_AC_050403_1_0060101_01_00

Hydraulic SystemYellow System Ground Service Panel

FIGURE 3

5-4-3Page 6

May 01/11


5-4-4 Electrical System

**ON A/C A319-100

Electrical System

1. Electrical System.This chapter gives data related to the location of the ground service connections.


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

A/C External Power:Access door 121AL

2.55(8.37) on centerline

2(6.56)


2. Technical SpecificationsThis chapter gives data related to the location of the ground service connections.

A. External Power Receptacle:- One MS90362-3 receptacle - 90 KVA.

B. Power Supply:- Three-phase, 400 Hz, 115/200V

C. Electrical connectors for servicing- AC outlets: Hubbel 5258- DC outlets: Hubbel 7472- Vacuum cleaner outlets: Hubbel 5258

5-4-4Page 1

May 01/11


**ON A/C A319-100

108VU

A

N_AC_050404_1_0010101_01_01

A

121AL

Ground Service ConnectionsExternal Power Receptacles

FIGURE 1

5-4-4Page 2

May 01/11


5-4-5 Oxygen System

**ON A/C A319-100

Oxygen System

1. Oxygen System.

DISTANCE: Meters (ft)

FROM AIRPLANE CENTERLINE

AFT OF NOSER SIDE L SIDE

MEANHEIGHTFROM

GROUNDOne service connection(external charging in theavionics compartment)MS22066 Std.

3.45 m(11.32 ft)

1.15 m(3.77 ft)

2.60 m(8.53 ft)

3/8” UNF × 24 TPI

Nominal pressure: 1850 psi (127.55 bar)

Max fill pressure: 2035 psi (140.31 bar)

NOTE : Internal charging connection provided.

5-4-5Page 1

May 01/11


5-4-6 Fuel System

**ON A/C A319-100

Fuel System

1. Refuel/Defuel Couplings.This chapter gives data related to the location of the ground service connections.


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

Refuel/DefuelIntegrated Panel:Access door 192MB

14.8(48.56)

1.8(5.91)

1.8(5.91)

Refuel/defuel coupling,LeftAccess Door 522HB(Optional)

15.6(51.18)

10(32.81)

3.5(11.48)

Refuel/defuel coupling,RightAccess Door 622HB

15.6(51.18)

10(32.81)

3.5(11.48)

Gravity Refuel Coupling17.4(57.09)

12.4(40.68)

12.4(40.68)

3.7(12.14)


2. Technical SpecificationsThis chapter gives data related to the specifications of the ground service connections.

A. Refuel/defuel couplings:- Right wing: one standard ISO R45, 2.5in.- Left wing: one optional standard ISO R45, 2.5 in.

B. Refuel pressure:- Maximum pressure: 3.45 bar (50 psi)

C. Refuel Flow:- 1400 l/minute (369.84 US gal/minute)

5-4-6Page 1

May 01/11


**ON A/C A319-100

REFUEL/DEFUELCONTROL PANEL

NOTE: STANDARD CONFIGURATION OF REFUEL/DEFUEL PANEL.

A

FUELkg x 1000

QTY

RIGHTCTRLEFT

LEFT CTR RIGHT

LVLHI

OPEN

NORM

SHUT

OPEN

NORM

SHUT

REFUEL VALVESOPEN

NORM

SHUT

BATT POWERTESTHI LVL ON

OPEN LTS NORM

MODE SELECTREFUEL

OFF

DEFUEL / XFR

kg x 1000

PRESELECTED

DEC INC

ACTUALREFUEL

CKPT END

A

N_AC_050406_1_0010101_01_00

Ground Service ConnectionsRefuel/Defuel Panel

FIGURE 1

5-4-6Page 2

May 01/11


**ON A/C A319-100

RIB15

RIB14

A

41QM

40QM

LEADINGEDGE

WING FRONTSPAR

A

N_AC_050406_1_0020101_01_00

Ground Service ConnectionsRefuel/Defuel Couplings

FIGURE 2

5-4-6Page 3

May 01/11


**ON A/C A319-100

RIB19

RIB20

A

ADAPTER(REF ONLY)

GROUND CONNECTION(REF ONLY)

44QM

(45QM)

AFWD

N_AC_050406_1_0030101_01_00

Ground Service ConnectionsGravity Refuel Couplings

FIGURE 3

5-4-6Page 4

May 01/11


5-4-7 Pneumatic System

**ON A/C A319-100

Pneumatic System

1. High Pressure Air Connectors.This chapter gives data related to the location of the ground service connections.


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

HP ConnectorAccess door 191DB

11.38(37.34)

0.84(2.76)

1.76(5.77)


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.


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM

GROUNDm (ft)

LP ConnectorAccess door 191CB

10.85(35.6)

1.11(3.64)

1.73(5.68)


A. Connector:- One standard 8 in. connection (SAE AS4262 type B) for cabin air preconditioning (LP)

installed on the left side of the belly fairing

5-4-7Page 1

May 01/11


5-4-8 Potable Water System

**ON A/C A319-100

Potable Water System

1. Potable Water Ground Service Panel.


ACCESSAFT OF NOSE


LH SIDEm (ft)

MEAN HEIGHTFROM GROUND

m (ft)

Potable WaterGround ServicePanel:Access door 171AL:

27.5(90.22)

0.3(0.98)

2.6(8.53)

NOTE : Distances are approximate

2. Potable Water Ground Drain Panel.


ACCESSAFT OF NOSE


LH SIDEm (ft)


m (ft)

Potable WaterGround ServicePanel:Access door 133AL:

11.8(38.71)

0.15(0.49)

1.75(5.74)


3. Technical Specifications

A. Connectors:

(1) On the potable ground service panel (Access Door 171AL)- Fill/Drain Nipple 3/4 in (ISO 17775).- One ground pressurization connector.

(2) On drain panel (Access Door 133AL)- Drain Nipple 3/4 in (ISO 17775)

B. Usable capacity:- Standard configuration - one tank:200 l (52.83 US gal)

C. Filling pressure:- 3.45 bar (50 psi).

5-4-8Page 1

May 01/11


D. Typical flow rate:- 50 l/min (13.21 US gal/min).

5-4-8Page 2

May 01/11


**ON A/C A319-100

DRAIN CONNECTION

FILL ANDDRAIN PORT

GROUND CONNECTION

PRESSURIZATION

Z133

Z171

A

B

B

A

N_AC_050408_1_0010101_01_00

Ground Service ConnectionsPotable Water Ground Service Panel

FIGURE 1

5-4-8Page 3

May 01/11


5-4-9 Oil System

**ON A/C A319-100

Oil System

1. Engine Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-9-991-001-A):One gravity filling cap and one pressure filling connection per engine.


ACCESSAFT OF NOSE

m (ft) ENGINE 1 (LH)m (ft)

ENGINE 2 (RH)m (ft)


m (ft)

Engine Oil GravityFilling Cap:Access door: 437BL(LH),447BL (RH)

11.56(37.79)

6.63(21.75)

4.82(15.81)

1.46(4.79)

Engine Oil PressureFilling Port:

11.4(37.4)

6.49(21.29)

4.74(15.55)

1.42(4.66)


A. Tank capacity:- Full level: 19.6 l (5.18 US gal)- Usable: 9.46 l (2.50 US gal)

B. Maximum delivery pressure required: 25 psi (1.72 bar)Maximum delivery flow required: 180 l/h (47.55 US gal/h)

2. IDG Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-9-991-002-A):One pressure filling connection per engine: OMP 2506-18 plus one connection overflow: OMP2505-18.


ACCESSAFT OF NOSE


ENGINE 2 (RH)m (ft)


m (ft)

IDG Oil PressureFilling Connection:Access door 438DR(LH),448DR (RH)

10.6(34.77)

6.9(22.64)

5.52(18.11)

0.68(2.23)


5-4-9Page 1

May 01/11


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 5-4-9-991-003-A):One gravity filling cap per engine.


ACCESSAFT OF NOSE


ENGINE 2 (RH)m (ft)


m (ft)

Starter Oil FillingConnection:

11.04(37.4)

5.3(17.39)

6.2(20.34)

0.76(2.49)


A. Tank capacity: 0.8 l (0.21 US gal)

4. Engine Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-9-991-004-B):One gravity filling cap per engine.


ACCESSAFT OF NOSE


ENGINE 2 (RH)m (ft)


m (ft)

Engine Oil GravityFilling Cap:Access door 437BL(LH),447BL (RH)

10.64(34.9)

6.56(21.52)

4.92(16.14)

1.22(4)


A. Tank capacity:- Full level: 28 l (7.4 US gal)- Usable: 23.50 l (6.21 US gal)

1. IDG Oil Replenishment for IAE V2500 Series Engine:One pressure filling connection per engine: OMP 2506-2 plus one overflow connection: OMP 2505-2.

5-4-9Page 2

May 01/11



ACCESSAFT OF NOSE


ENGINE 2 (RH)m (ft)


m (ft)

IDG Oil PressureFilling Connection:

11.2(36.74)

5.42(17.78)

6.04(19.81)

0.8(2.62)



5. Starter Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-9-991-006-B):One gravity filling cap per engine.


ACCESSAFT OF NOSE


ENGINE 2 (RH)m (ft)


m (ft)

Starter Oil FillingConnection:

11.04(37.4)

5.3(17.39)

6.14(20.14)

0.75(2.46)



6. APU Oil System (See FIGURE 5-4-9-991-007-A):APU oil gravity filling cap.

AFT OF NOSEm (ft)

FROM AIRPLANECENTERLINE(LEFT HAND)

m (ft)

MEAN HEIGHT FROMGROUND

m (ft)

GTCP 36-30031.76(104.19)

0.3(0.98)

4.83(15.85)

APS 320031.76(104.19)

0.3(0.98)

4.78(15.68)

131-931.66(103.87)

0.35(1.15)

4.32(14.17)


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

May 01/11


- APU type 131-9: 6.25 l (1.65 US gal)

5-4-9Page 4

May 01/11


**ON A/C A319-100

ACCESS PANEL: 437BL (LEFT)447BL (RIGHT) OIL IN

VENT

OIL LEVELTRANSMITTER(OPTIONAL)

OIL CAP

SIGHT WINDOW

ANTI−SIPHONDEVICE

AIR PRESSURESWITCH NIPPLE

SELF−SEALING MAGNETICDRAIN PLUG

PRESSURE NIPPLE

OIL OUT

OIL/FUEL HEATEXCHANGER

SERVO FUELHEATER

A

A

B

FWD

B

N_AC_050409_1_0010101_01_00

Ground Service ConnectionsEngine Oil Tank -- CFM56 Series Engine

FIGURE 1

5-4-9Page 5

May 01/11


**ON A/C A319-100

C

A

B

SIGHT GLASS

NOTE: ATHE YELLOW BAND, OIL SERVICINGIS REQUIRED.

BTHE GREEN AND YELLOW BANDS,OIL SERVICING IS NOT REQUIRED.

CTHE GREEN BAND, OIL SERVICINGIS REQUIRED.

1 − PRESSURE FILL VALVE2 − CASE DRAIN PLUG3 − DUST CAP4 − DUST CAP5 − OVERFLOW DRAIN VALVE6 − OIL LEVEL INDICATOR

(SIGHT GLASS)

1

2

34

5

6

A B

A

B

OVERFULL

ADDOIL

ADDOIL

CFM−56

IF THE OIL LEVEL IS ABOVE

IF THE OIL LEVEL IS WITHIN

IF THE OIL LEVEL IS BELOW

N_AC_050409_1_0020101_01_01

Ground Service ConnectionsIDG Oil Tank -- CFM56 Series Engine

FIGURE 2

5-4-9Page 6

May 01/11


**ON A/C A319-100

DRAIN PORTAND MAGNETICPLUG

OVERFLOWPLUG

STARTER

OIL FILLERPLUG

A

A

N_AC_050409_1_0030101_01_02

Ground Service ConnectionsStarter Oil Tank -- CFM56 Series Engine

FIGURE 3

5-4-9Page 7

May 01/11


**ON A/C A319-100

’FULL’ LEVEL NOTCH27.3 LT29.0 US QTS6.0 IMP GAL(WITHIN 60 MIN FROM SHUTDOWN)

NOTCH ’3’20 LT22 US QTS4.5 IMP GAL

NOTCH ’1’26 LT27 US QTS5.7 IMP GALNOTCH ’2’

23 LT24 US QTS5.1 IMP GAL

FCOC

PRISMALITELEVEL INDICATOR

OIL TANK

GRAVITYFILLER CAP

ACCESS PANEL: 437BL (LEFT)447BL (RIGHT)

B

A

A

B

FWD

N_AC_050409_1_0040201_01_00

Ground Service ConnectionsEngine Oil Tank -- IAE V2500 Series Engine

FIGURE 4

5-4-9Page 8

May 01/11


**ON A/C A319-100

THE OIL LEVEL MUST NOT BE INTHE YELLOW BAND BUT IT CANBE IMMEDIATELY ABOVE THELOWER LIMIT OF THE YELLOWBAND BECAUSE OF THE AIRCRAFTRAMP ANGLE

DO THE IDG SERVICINGTO GET THE CORRECT IDGOIL LEVEL.

AFTER SERVICING ORENGINE SHUTDOWN

(COLD OIL/IDG)

INCORRECTLY FILLED IDG

THE OIL LEVEL MUST NOT BEIN THE RED BAND

PERFORM IDG OIL SERVICINGTO GET THE CORRECT IDG OIL LEVEL.DO NOT USE THE OVERFLOW DRAIN HOSETO GET THE CORRECT IDG OIL LEVEL.

AT ALL TIMES(HOT OR COLD OIL/IDG)

OIL LEVEL CAN BEIN THE GREEN BAND OR THEYELLOW BAND

AFTER ENGINESHUTDOWN

CORRECTLY FILLED IDG

OIL LEVELINDICATOR

DUST CAPPRESSUREFILL HOSE

OIL LEVEL MUST BE AT OR NEARTHE LINE BETWEEN THE YELLOW BANDAND THE GREEN BAND

(HOT OIL/IDG)

PRESSUREFILL VALVE

DUST CAP

OVER FLOWDRAIN VALVE

OVER FLOWDRAIN HOSE

AFTER SERVICING ORENGINE SHUTDOWN

(COLD OIL/IDG)

IDG

B

BB

A

B

A

B

OVER FULL

ADDOIL

ADDOIL

V2500

OVER FULL

ADDOIL

ADDOIL

V2500

OVER FULL

ADDOIL

ADDOIL

V2500

OVER FULL

ADDOIL

ADDOIL

V2500

OVER FULL

ADDOIL

ADDOIL

V2500

N_AC_050409_1_0050201_01_00

Ground Service ConnectionsIDG Oil Tank -- IAE V2500 Series Engine

FIGURE 5

5-4-9Page 9

May 01/11


**ON A/C A319-100

OIL OVERFLOWPOINT

SIGHT GLASS

EXTERNAL GEARBOX

OIL FILLING POINT

ADAPTER

B

A

B

THE STARTER IS FULL WHEN THE OIL LEVELSHOWS NOT LESS THAN 3/4 FULL

ON THE SIGHT GLASS

*

PNEUMATIC STARTERA

*

N_AC_050409_1_0060201_01_00

Ground Service ConnectionsStarter Oil Tank -- IAE V2500 Series Engine

FIGURE 6

5-4-9Page 10

May 01/11


**ON A/C A319-100

FR80

Z316Z315

FR84

GRAVITYOIL FILLER

PRESSUREFILL PORT

OVERFLOWDRAIN VALVE

A

A

OIL LEVELSIGHT GLASS

N_AC_050409_1_0070101_01_00

Ground Service ConnectionsAPU Oil Tank

FIGURE 7

5-4-9Page 11

May 01/11


5-4-10 Vacuum Toilet System

**ON A/C A319-100

Vacuum Toilet System

1. Vacuum Toilet System.


ACCESSAFT OF NOSE

m (ft) R SIDEm (ft)

L SIDEm (ft)


m (ft)

Waste WaterGround ServicePanel:Access door 172AR

27.5(90.22)

0.8(2.62)

2.8(9.18)


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

May 01/11


**ON A/C A319-100

FILL AND RINSECONNECTION

TOILET DRAINCONNECTION

FR66 FR65

A

Z172

A

N_AC_050410_1_0010101_01_00

Ground Service ConnectionsWaste Water Ground Service Panel

FIGURE 1

5-4-10Page 2

May 01/11


5-5-0 Engine Starting Pneumatic Requirements

**ON A/C A319-100

Engine Starting Pneumatic Requirements

1. Engine Starting Pneumatic Requirements.

5-5-0Page 1

May 01/11


5-5-1 Low Temperatures

**ON A/C A319-100

Low Temperature -40˚C (-40˚F)

1. This section provides the engine starting pneumatic requirements for a temperature of -40˚C(-40˚F).

5-5-1Page 1

May 01/11


**ON A/C A319-100

N_AC_050501_1_0030101_01_00

AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS

AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION

220°C

200°C

150°C

100°C

50°C

0°C

100

90

80

70

60

50

40

30 2

Z = 8000 ftSEA LEVEL

2.5

3

4

3.5

5

6

7

6.5

5.5

4.5

ESTIMATED STARTINGTIMES UP TO IDLE

30 40 50 60 70 80 90 100 110 120

AIR FLOW REQUIRED AT GROUND CONNECTION

kg/mn

MIN. PRESSUREAT GROUND CONNECTION: 33 PSIG

RECOMMENDED PRESSURE:38 PSIG ATGROUND CONNECTION

SEA LEVEL

Z = 8000 ft

Z = 8000 ft

MAXIMUM DUCT PRESSURE: 60 PSIG

SEA LEVEL

MAXIM

UM T

EMPERATURE L

IMIT

35s

40s

50s

60s70s

Engine Starting Pneumatic RequirementsTemperature -40˚C (-40˚F) -- CFM56 series engine

FIGURE 1

5-5-1Page 2

May 01/11


**ON A/C A319-100

AIR SUPPLY PRESSUREAT GROUND CONNECTION

kg/mn

PSIA ABSOLUTE BARS


TIMES UP TO IDLEESTIMATED STARTING

MAXIMUM T

EMPERATURE LIMIT

30

40

50

60

70

80

90

6

5

4

3

2

0°C

50°C

100°C

150°C

200°C220°C

40 50 60 70 80 90 100 110 120

MAXIMUM DUCT PRESSURE


70s

75s

60s

65s

N_AC_050501_1_0040101_01_00

Engine Starting Pneumatic RequirementsTemperature -40˚C (-40˚F) -- IAE V2500 series engine

FIGURE 2

5-5-1Page 3

May 01/11


5-5-2 Ambient Temperatures

**ON A/C A319-100

Ambient Temperature +15˚C (+59˚F)

1. This section provides the engine starting pneumatic requirements for a temperature of +15˚C(+59˚F).

5-5-2Page 1

May 01/11


**ON A/C A319-100

N_AC_050502_1_0030101_01_00


kg/mn

PRESSURE: 33 PSIG ATRECOMMENDED

GROUND CONNECTION:MIN PRESSURE AT

PSIA ABSOLUTE BARS


22 PSIG

GROUND CONNECTION


0°C

50°C

100°C

150°C

200°C

220°C

30

40

50

60

70

80

90

100

2

3

4

5

6

7

6.5

5.5

4.5

2.5

3.5

30 40 50 60 70 80 90 100 110 120

35s

40s

50s

60s

70s

Z = 8000 ft


SEA LEVEL

MAXIM

UM T

EMPERATURE L

IMIT


SEA LEVEL

Z = 8000 ft

Z = 8000 ft

SEA LEVEL

Engine Starting Pneumatic RequirementsTemperature +15˚C (+59˚F) -- CFM56 series engine

FIGURE 1

5-5-2Page 2

May 01/11


**ON A/C A319-100

AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA


220°C200°C

150°C

100°C

50°C

0°C

90

80

70

60

50

40

30 2

3

4

5

6

MAXIMUM DUCT PRESSUREMAXIM

UM TEMPERATURE LI

MIT

ESTIMATED STARTINGTIMES UP TO IDLE


40 50 60 70 80 100 110 12090 kg/mn

ABSOLUTE BARS

45s

50s

55s

60s

N_AC_050502_1_0040101_01_00

Engine Starting Pneumatic RequirementsTemperature +15˚C (+59˚F) -- IAE V2500 series engine

FIGURE 2

5-5-2Page 3

May 01/11


5-5-3 High Temperatures

**ON A/C A319-100

High Temperature +50˚C (+122˚F) and +55˚C (+131˚F)

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

May 01/11


**ON A/C A319-100

N_AC_050503_1_0030101_01_00


PSIA ABSOLUTE BARS

30

40

50

60

70

80

90

100

2

3

4

5

6

7

2.5

3.5

4.5

5.5

6.5

30 40 50 60 70 80 90 100 110 120 kg/mn

PRESSURE: 33 PSIG ATRECOMMENDED

GROUND CONNECTION:MIN PRESSURE AT


22 PSIG

GROUND CONNECTION


50°C

100°C

150°C

200°C220°C


Z = 8000 ft

SEA LEVEL


SEA LEVEL

Z = 8000 ft

Z = 8000 ft

SEA LEVEL

35s

40s

50s

60s

70s

MAXIM

UM T

EMPERATURE L

IMIT

Engine Starting Pneumatic RequirementsTemperature +55˚C (+131˚F) -- CFM56 series engine

FIGURE 1

5-5-3Page 2

May 01/11


**ON A/C A319-100

N_AC_050503_1_0040101_01_00


kg/mn

PSIA ABSOLUTE BARS


MAXIMUM T

EMPERATURE LIMIT

0°C

50°C

100°C

150°C

200°C220°C

MAXIMUM DUCT PRESSURE

30

40

50

2

3

4

570

60

80

90

6

40 50 60 70 80 90 100 110 120


45s

50s

55s

60s


Engine Starting Pneumatic RequirementsTemperature +50˚C (+122˚F) -- IAE V2500 series engine

FIGURE 2

5-5-3Page 3

May 01/11


5-6-0 Ground Pneumatic Power Requirements

**ON A/C A319-100

Ground Pneumatic Power Requirements

1. Ground Pneumatic Power Requirements.

FRESH AIRFLOW PULL UP PULL DOWNTOTAL CABIN TIME T TIME T

(kg/s) (lb/s) (kg/s) (lb/s) (min.) (min.)

0.5 1.10 0.429 0.946after 60 min.13.6˚C

--

0.6 1.32 0.515 1.135after 60 min.18.2˚C

--

0.7 1.54 0.600 1.323 56.5 --

0.8 1.76 0.686 1.512 47.5after 60 min.28˚C

0.9 1.98 0.772 1.702 40.5 52.51.0 2.20 0.858 1.892 35.5 38.51.1 2.43 0.944 2.081 31.0 29.51.2 2.65 1.030 2.271 27.5 23.51.3 2.87 1.115 2.458 24.0 18.51.4 3.09 1.201 2.648 21.5 15.01.5 3.31 1.287 2.837 19.5 12.0

NOTE : Data for unstabilized conditions see 5-6-1 and 5-6-2.

5-6-0Page 1

May 01/11


5-6-1 Heating

**ON A/C A319-100

Heating

1. This section provides the ground pneumatic power requirements heating.

5-6-1Page 1

May 01/11


**ON A/C A319-100

TOTAL AIRFLOW

(kg/

s)

TOTAL AIRFLOW

CABIN AIRFLOW

1.28

7

1.20

1

1.11

5

1.03

0.94

4

0.85

8

0.72

2

0.68

6

0.51

5

0.60

0.42

9

1.5

1.2

1.0

0.5

3040

50T

IME

(m

in)

MA

X A

LLO

WE

D T

OT

AL

AIR

FLO

W (

2 m

bar

CA

BIN

OV

ER

PR

ES

SU

RE

)

1.28

1.72

2.15

2.59

3.0

2.5

2.0

1.5

(lb/s

)

CABIN AIRFLOW

TIM

E T

O H

EA

T C

AB

IN T

O 2

1°C

(69

.8°

F O

N G

RO

UN

D)

INIT

IAL

CA

BIN

TE

MP

ER

AT

UR

E A

T −

23°

C (

−9.

4°F

)T

EM

PE

RA

TU

RE

AT

GR

OU

ND

CO

NN

EC

TIO

N: 7

0°C

(15

8°F

)E

MP

TY

CA

BIN

ELE

CT

RIC

AL

LOA

D =

270

0 W

RE

CIR

CU

LAT

ION

: ON

NO

OT

HE

R H

EA

T L

OA

D

N_AC_050601_1_0020101_01_01

Ground Pneumatic Power RequirementsHeating

FIGURE 1

5-6-1Page 2

May 01/11


5-6-2 Cooling

**ON A/C A319-100

Cooling

1. This section provides the ground pneumatic power requirements cooling.

5-6-2Page 1

May 01/11


**ON A/C A319-100

1.28

7

1.20

1

1.11

5

1.03

0.94

4

0.85

8

0.72

2

0.68

6

0.51

5

0.60

0.42

9

1.5

1.2

1.0

0.5

TOTAL AIRFLOW

(kg/

s)

TOTAL AIRFLOW

CABIN AIRFLOW

2030

40

TIM

E T

O C

OO

L C

AB

IN T

O 2

7°C

(80

.6°

F O

N G

RO

UN

D)

TIM

E (

min

)

MA

X A

LLO

WE

D T

OT

AL

AIR

FLO

W (

2 m

bar

CA

BIN

OV

ER

PR

ES

SU

RE

)

1.28

1.72

2.15

2.59

3.0

2.5

2.0

1.5

(lb/s

)

INIT

IAL

CA

BIN

TE

MP

ER

AT

UR

E A

T 3

8°C

(10

0.4°

F)

TE

MP

ER

AT

UR

E A

T G

RO

UN

D C

ON

NE

CT

ION

: 1.5

°C

(34

.7°

F)

EM

PT

Y C

AB

INE

LEC

TR

ICA

L LO

AD

= 2

000

WS

UN

= 4

990

WR

EC

IRC

ULA

TIO

N: O

N

CABIN AIRFLOW

N_AC_050602_1_0020101_01_01

Ground Pneumatic Power RequirementsCooling

FIGURE 1

5-6-2Page 2

May 01/11


5-7-0 Preconditioned Airflow Requirements

**ON A/C A319-100

Preconditioned Airflow Requirements

1. This section gives the preconditioned airflow requirements for cabin air conditioning.

A. Preconditioned Airflow Requirements.

FRESH AIRFLOW CURVE 1TOTAL CABIN T FL

(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)

0.5 1.10 0.429 0.946 -40.4 -40.70.6 1.32 0.515 1.135 -28.5 -19.30.7 1.54 0.600 1.323 -20.1 -4.20.8 1.76 0.686 1.512 -13.9 7.00.9 1.98 0.772 1.702 -9.1 15.61.0 2.20 0.858 1.892 -5.3 22.51.1 2.43 0.944 2.081 -2.2 28.01.2 2.65 1.030 2.271 0.4 32.71.3 2.87 1.115 2.458 2.6 36.71.4 3.09 1.201 2.648 4.4 39.91.5 3.31 1.287 2.837 6.0 42.8

NOTE : Data for stabilized conditions see 5-7-0.

B. Preconditioned Airflow Requirements.


(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)

0.5 1.10 0.429 0.946 31.7 89.10.6 1.32 0.515 1.135 29.7 85.50.7 1.54 0.600 1.323 28.4 83.10.8 1.76 0.686 1.512 27.3 81.10.9 1.98 0.772 1.702 26.5 79.71.0 2.20 0.858 1.892 25.9 78.61.1 2.43 0.944 2.081 25.4 77.71.2 2.65 1.030 2.271 25.0 77.01.3 2.87 1.115 2.458 24.6 76.31.4 3.09 1.201 2.648 24.3 75.7

5-7-0Page 1

May 01/11



(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)

1.5 3.31 1.287 2.837 24.0 75.2


C. Preconditioned Airflow Requirements.


(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)

0.5 1.10 0.429 0.946 36.0 96.80.6 1.32 0.515 1.135 33.3 91.90.7 1.54 0.600 1.323 31.4 88.50.8 1.76 0.686 1.512 29.9 85.80.9 1.98 0.772 1.702 28.8 83.81.0 2.20 0.858 1.892 27.9 82.21.1 2.43 0.944 2.081 27.2 81.01.2 2.65 1.030 2.271 26.6 79.91.3 2.87 1.115 2.458 26.1 79.01.4 3.09 1.201 2.648 25.7 78.31.5 3.31 1.287 2.837 25.3 77.5


D. Preconditioned Airflow Requirements.


(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)

0.5 1.10 0.429 0.946 42.2 108.00.6 1.32 0.515 1.135 38.4 101.10.7 1.54 0.600 1.323 35.7 96.30.8 1.76 0.686 1.512 33.7 92.70.9 1.98 0.772 1.702 32.1 89.81.0 2.20 0.858 1.892 30.9 87.61.1 2.43 0.944 2.081 29.9 85.81.2 2.65 1.030 2.271 29.0 84.21.3 2.87 1.115 2.458 28.3 82.91.4 3.09 1.201 2.648 27.7 81.9

5-7-0Page 2

May 01/11



(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)

1.5 3.31 1.287 2.837 27.2 81.0


5-7-0Page 3

May 01/11


**ON A/C A319-100

TOTAL AIRFLOW

(kg/

s)

TOTAL AIRFLOW

CABIN AIRFLOW

1.28

7

1.20

1

1.11

5

1.03

0.94

4

0.85

8

0.72

2

0.68

6

0.51

5

0.60

1.28

1.72

2.15

2.59

3.0

2.5

2.0

1.5

(lb/s

)

0.42

9

CU

RV

E 2

, 3, 4

(°C

)IN

LET

FLO

WT

EM

PE

RA

TU

RE

(°F

)

NO

TE

:LP

GR

OU

ND

CO

NN

EC

TIO

N M

AX

IMU

M P

RE

SS

UR

E 4

0 m

b

0.5

1.0

1.2

1.5

−40

−30

−20

−10

010

2030

40

−40

−10

010

5010

0

OA

T =

−23

°C

(−

9.4°

F)

OA

T =

−30

°C

(−

22°

F)

OA

T =

−40

°C

(−

40°

F)

MA

X A

LLO

WE

D T

OT

AL

AIR

FLO

W (

2 m

bar

CA

BIN

OV

ER

PR

ES

SU

RE

)

CABIN AIRFLOW

CU

RV

E 1

: CA

BIN

AT

27°

C (

80.6

°F

)13

4 P

AS

SE

NG

ER

S, 4

CA

BIN

AT

TE

ND

AN

TS

, 3 C

RE

W M

EM

BE

RS

BR

IGH

T D

AY

SO

LAR

LO

AD

: 297

5 W

ELE

CT

RIC

AL

LOA

D =

620

0 W

RE

CIR

CU

LAT

ION

: ON

OA

T (

OU

TS

IDE

AIR

TE

MP

ER

AT

UR

E)

= 3

8°C

(10

0.4°

F)

CA

BIN

AT

21°

C (

69.8

°F

)

NO

OT

HE

R H

EA

T L

OA

D

ELE

CT

RIC

AL

LOA

D =

380

0 W

RE

CIR

CU

LAT

ION

: ON

NO

PA

SS

EN

GE

R O

R C

AB

INA

TT

EN

DA

NT

S

N_AC_050700_1_0020101_01_01

Preconditioned Airflow RequirementsFIGURE 1

5-7-0Page 4

May 01/11


5-8-0 Ground Towing Requirements

**ON A/C A319-100

Ground Towing Requirements

1. GeneralThis section provides information on aircraft towing.This aircraft is designed with means for conventional or towbarless towing.Information/procedures can be found for both in chapter 9 of the Aircraft Maintenance Manual.Status on towbarless towing equipment qualification can be found in SIL 09-002.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a tow bar attached to the nose gear leg (refer to AMM chap 9 for conditions andlimitations).One tow bar fitting is installed at the front of the leg.The main landing gears have attachment points for towing or debogging (for details, refer to chapter07 of the Aircraft Recovery Manual).

A. The first part of this section shows the chart to determine the draw bar pull and tow tractormass requirements as function of the following physical characteristics:- Aircraft weight- Number of engines at idle- Slope.The chart is based on the engine type with the highest idle thrust level.

B. The second part of this section supplies guidelines for the tow bar.The aircraft tow bar shall respect the following norms:- SAE AS 1614, ”Main Line Aircraft Tow Bar Attach Fitting Interface”- SAE ARP1915 Revision C, ”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/AS 1614 (issue C) cat. l.

NOTE : Information on aircraft towing procedures and corresponding aircraft limitations aregiven in chapter 9 on the Aircraft Maintenance Manual.

5-8-0Page 1

May 01/11


**ON A/C A319-100

70

404550556065

EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A319 AT 60 t, AT 1.5% SLOPE,1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:

− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (60 t)− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%)− FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL NO OF ENGINES AT IDLE = 2− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER OF ENGINES (1)− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5.0 t)− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS

THE RECOMMENDED MINIMUM TRACTOR WEIGHT (8.8 t)

10

0 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0

5

0

TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]

1 ENGINE ON1.5% SLOPE

60 tons

DRAWBAR PULL [ t ] A/C WEIGHT [ t ]

5.0

8.83

WE

T C

ON

CR

ET

E m

= 0

.57

HA

RD

SN

OW

m =

0.2

ICE m = 0.05

AT IDLE

DR

Y C

ON

CR

ET

E m

= 0

.8BREAKAWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 525 daN

N_AC_050800_1_0010201_01_03

Ground Towing RequirementsFIGURE 1

5-8-0Page 2

May 01/11


**ON A/C A319-100

D1

MF

M

LONGHOLE BLOCKINGLATERAL MOVEMENTS

HOLES FOR SPARE SHEAR PINS

MF

LOCKING/UNLOCKING HANDLE

SHEAR PIND1

L

F F

Fshear

F

Mshear

Fshear

Lshear

M = Fshear

x L

Mshear

= Fshear

x Lshear

Mshear

= F x D1 (Mshear

< M)

D1 = (M/L) x Lshear

/ F

Fshear

= M / L

Mshear

= (M/L) x Lshear

D1 = (M x Lshear

/ (F x L)

A

A

N_AC_050800_1_0020101_01_03

Ground Towing RequirementsTypical Tow Bar Configuration 1

FIGURE 2

5-8-0Page 3

May 01/11


**ON A/C A319-100

MF

D2

OVERSIZED HOLEWRT RETENTION BOLT

M

L

F

F/2

F/2

D2

D2 = (2 x Mshear

) / F D2 = (2 x M x Lshear

) / (F x L)

F M D1 D2

9425 826 78.9 168.3

[daN] [m.daN] [mm] [mm]

RESULTS FOR A TOWBAR LENGTH OF Lshear

/L = 0.90

Fshear

Fshear

Lshear

Mshear

M = Fshear

x L

Mshear

= Fshear

x Lshear

Mshear

= F/2 x D2 (Mshear

< M)

Fshear

= M / L

Mshear

= (M / L) x Lshear

A

AN_AC_050800_1_0030101_01_01

Ground Towing RequirementsTypical Tow Bar Configuration 2

FIGURE 3

5-8-0Page 4

May 01/11


OPERATING CONDITIONS

6-1-0 Engine Exhaust Velocities and Temperatures

**ON A/C A319-100

Engine Exhaust Velocities and Temperatures

1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway, Maximum Takeoff conditions.

6-1-0Page 1

May 01/11


6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power

**ON A/C A319-100

Engine Exhaust Velocities Contours - Ground Idle Power

1. This section gives engine exhaust velocities contours at ground idle power.

6-1-1Page 1

May 01/11


**ON A/C A319-100

ELE

VA

TIO

N

FE

ET

050

100

150

200

250

300

350

400

015

3045

6075

9010

512

0

40 30 20 10 0036912

mft

PLA

NA

IRP

LAN

E

V (

m/s

)

GR

OU

ND

PLA

NE

ME

TE

RS

40 30 20 10 0036912

mft

4525

2015

10

4530

2520

1510

30

N_AC_060101_1_0030101_01_00

Engine Exhaust VelocitiesGround Idle Power -- CFM56 series engine

FIGURE 1

6-1-1Page 2

May 01/11


**ON A/C A319-100

ME

TE

RS

015

3045

60

250

300

ELE

VA

TIO

N

VE

LOC

ITY

= ft

/s (

m/s

)

FE

ET

050

100

150

200

7590

ftm

PLA

N

ftm

100

(30)

50 (15)

30 (9)

100

(30)

50 (15)

30 (9)

15 10 5 0

60 40 20 0

15 10 5 0

60 40 20 0

N_AC_060101_1_0040101_01_00

Engine Exhaust VelocitiesGround Idle Power -- IAE V2500 series engine

FIGURE 2

6-1-1Page 3

May 01/11


6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power

**ON A/C A319-100

Engine Exhaust Temperatures Contours - Ground Idle Power

1. This section gives engine exhaust temperatures contours at ground idle power.

6-1-2Page 1

May 01/11


**ON A/C A319-100

ELE

VA

TIO

N

FE

ET

050

100

150

200

250

300

350

400

015

3045

6075

9010

512

0

40 30 20 10 0036912

mft

PLA

NA

IRP

LAN

E

GR

OU

ND

PLA

NE

ME

TE

RS

40 30 20 10 0036912

mft

400

350

325

300

400

350

325

300

T (

°K

)

N_AC_060102_1_0030101_01_00

Engine Exhaust TemperaturesGround Idle Power -- CFM56 series engine

FIGURE 1

6-1-2Page 2

May 01/11


**ON A/C A319-100

ME

TE

RS

015

3045

60

250

300

ELE

VA

TIO

N

TE

MP

ER

AT

UR

E =

°K

FE

ET

050

100

150

200

7590

ftm

PLA

N

ftm

32531

830

830

0

325

318

300

308

15 10 5 0

60 40 20 0

15 10 5 0

60 40 20 0

N_AC_060102_1_0040101_01_00

Engine Exhaust TemperaturesGround Idle Power -- IAE V2500 series engine

FIGURE 2

6-1-2Page 3

May 01/11


6-1-5 Engine Exhaust Velocities Contours - Takeoff Power

**ON A/C A319-100

Engine Exhaust Velocities Contours - Takeoff Power

1. This section gives engine exhaust velocities contours at takeoff power.

6-1-5Page 1

May 01/11


**ON A/C A319-100

420

390

360

330

300

270

240

210

180

150

120

9060

3000

100

200

300

400

500

700

600

800

900

1000

1100

1200

1300

1400

ME

TE

RS

FE

ET

ftm

ft

V =

40

m/s

V =

20

m/s

V =

12

m/s

V =

40

m/s

V =

20

m/s

V =

12

m/s

PLA

NA

IRP

LAN

E

ELE

VA

TIO

NG

RO

UN

D P

LAN

E

TA

KE

OF

F P

OW

ER

INC

LUD

ES

(W

OR

ST

CA

SE

)G

RO

UN

D P

LAN

EH

EA

DW

IND

(20

KT

S.)

m

42 36 30 24 18 12 6 0

140

120

100 80 60 40 200

140

120

100 80 60 40 200

42 36 30 24 18 12 6 0

N_AC_060105_1_0030101_01_00

Engine Exhaust VelocitiesTakeoff Power -- CFM56 series engine

FIGURE 1

6-1-5Page 2

May 01/11


**ON A/C A319-100

ME

TE

RS

015

3045

60

250

300

ELE

VA

TIO

N

MA

XIM

UM

TA

KE

OF

F T

HR

US

T

FE

ET

050

100

150

200

7590

ftm

PLA

N

ftm

136

MP

H10

2 M

PH

68 M

PH

34 M

PH

20 M

PH

TO

990

ft (

301

m)

TO

575

ft (

175

m)

60

15 10 5 0

40 20 0 60

15 10 5 0

40 20 0

N_AC_060105_1_0040101_01_00

Engine Exhaust VelocitiesTakeoff Power -- IAE V2500 series engine

FIGURE 2

6-1-5Page 3

May 01/11


6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power

**ON A/C A319-100

Engine Exhaust Temperatures Contours - Takeoff Power

1. This section gives engine exhaust temperatures contours at takeoff power.

6-1-6Page 1

May 01/11


**ON A/C A319-100

60 40 20 0

ftm

18 12 6 0E

LEV

AT

ION

GR

OU

ND

PLA

NE

2040

6080

100

120

140

160

TA

KE

OF

F P

OW

ER

INC

LUD

ES

(W

OR

ST

CA

SE

):G

RO

UN

D P

LAN

EH

EA

DW

IND

(20

KT

S.)

FE

ET

ME

TE

RS

PLA

N

T =

425

°K

T =

370

°K

T =

315

°K

T =

425

°K

T =

370

°K

T =

315

°K

AIR

PLA

NE

1020

3040

500

ftm

60 40 20 0

18 12 6 0

N_AC_060106_1_0030101_01_00

Engine Exhaust TemperaturesTakeoff Power -- CFM56 series engine

FIGURE 1

6-1-6Page 2

May 01/11


**ON A/C A319-100

ME

TE

RS

1530

4560

250

300

ELE

VA

TIO

N

FE

ET

5010

015

020

0

7590

ftm

PLA

N

ftm

00

65°

C55

°C

45°

C35

°C

25°

C

60

15 10 5 0

40 20 060

15 10 5 0

40 20 0

N_AC_060106_1_0040101_01_00

Engine Exhaust TemperaturesTakeoff Power -- IAE V2500 series engine

FIGURE 2

6-1-6Page 3

May 01/11


6-2-0 Airport and Community Noise

**ON A/C A319-100

Airport and Community Noise

1. Airport and Community Noise Data

This section gives data concerning engine maintenance run-up noise to permit evaluation of possibleattenuation requirements.

6-2-0Page 1

May 01/11


6-2-1 Noise Data

**ON A/C A319-100

Noise Data

1. Noise Data for CFM56-5A series engine

A. Description of test conditions:

The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.

B. Engine parameters: 2 engines running

C. Meteorological data:

The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 3˚C (37˚F)- Relative humidity: 66%- Atmospheric pressure: 1016 hPa- Wind speed: Negligible- No rain

2. Noise Data for CFM56-5B series engine






3. Noise Data for IAE V2500 series engine


6-2-1Page 1

May 01/11






6-2-1Page 2

May 01/11


**ON A/C A319-100

112110108106104102

98969492908886848280

100

150°

135°

120°

105°

90°

75°

60°

45°

30°

15°

0°

345°

330°

315°

300°

285°

270°

255°

240°

225°

210°

GROUND IDLE

N1

CURVE

MAX THRUST POSSIBLEON BRAKES

20.8% 90%

NOISE REFERENCEPOINT

78

N_AC_060201_1_0040101_01_00

Airport and Community NoiseCFM56-5A series engine

FIGURE 1

6-2-1Page 3

May 01/11


**ON A/C A319-100

8082

8486

8890

9294

96

0°10°

20°

30°

40°

50°

60°

70°

80°

90°

100°

110°

120°

130°

140°

150°

98100

102104

106108

110112

350°340°

330°

320°

310°

300°

290°

280°

270°

250°

240°

230°

220°

210°


GROUND IDLE

N1

CURVE


87%18.9%

260°

N_AC_060201_1_0050101_01_00

78

Airport and Community NoiseCFM56-5B series engine

FIGURE 2

6-2-1Page 4

May 01/11


**ON A/C A319-100

11811611411211010810610410210098969492908886848280

GROUND IDLE

N1

CURVE


25.2% 94.4%


E.P.R 1.012 1.564

150°

140°

130°

120°

110°

100°

90°

80°

70°

60°

50°

40°

30°

20°10°

0°350°

340°

330°

320°

310°

300°

290°

280°

270°

210°

220°

230°

240°

250°

260°78

N_AC_060201_1_0060101_01_00

Airport and Community NoiseIAE V2500 series engine

FIGURE 3

6-2-1Page 5

May 01/11


6-3-0 Danger Areas of Engines

**ON A/C A319-100

Danger Areas of Engines

1. Danger Areas of the Engines.

6-3-0Page 1

May 01/11


6-3-1 Ground Idle Power

**ON A/C A319-100

Ground Idle Power

1. This section gives danger areas of the engines at ground idle power conditions.

6-3-1Page 1

May 01/11


**ON A/C A319-100

AREA

A

B

C

D65−20

E < 20 (32)

NOT TO SCALE

POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV. 1951

A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.

A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPEAIRCRAFT.

LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT

BEYOND DANGER AREA

APPROX. WINDVELOCITYMPH (km/h)

210−145(338−233)

145−105(233−169)

105−65(169−105)

EXHAUST DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)

INLET DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)

INLET HAZARDDIMENSIONS CALCULATEDON 40 ft/sec (12 m/sec)CRITICAL VELOCITYWITH A 3 ft (0.9 m)ADJUSTMENT FOR SAFETY

WIDTH72 ft (22 m)

RADIUS = 7.2 ft (2.2 m)

NO ENTRY 82 ft (25 m)AFT OF NOZZLE EXIT

3.4 ft (1 m)

TO 199 ft (61 m)

45°CLOSE ENTRY CORRIDORFOR WIND DIRECTION

B

C

D

> 90°

E

ENTRY CORRIDOREXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER

EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS

INLET SUCTIONDANGER AREA

(105−32)

N_AC_060301_1_0030101_01_01

Danger Areas of EnginesCFM56 series engine

FIGURE 1

6-3-1Page 2

May 01/11


**ON A/C A319-100

0.91 m(3 ft)

R = 5.79 m(19ft)

30°

TO 59 m (195 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)

INTAKE SUCTION DANGER AREA

EXHAUST DANGER AREA

ENTRY CORRIDOR

N_AC_060301_1_0040101_01_00

Danger Areas of EnginesIAE V2500 series engine

FIGURE 2

6-3-1Page 3

May 01/11


6-3-2 Takeoff Power

**ON A/C A319-100

Takeoff Power

1. This section gives danger areas of the engines at max takeoff conditions.

6-3-2Page 1

May 01/11


**ON A/C A319-100

AREA

A

B

C

D65−20

E < 20 (32)

NOT TO SCALE

POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV. 1951

A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.

A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPEAIRCRAFT.

LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT

BEYOND DANGER AREA

APPROX. WINDVELOCITYMPH (km/h)

210−145(338−233)

145−105(233−169)

105−65(169−105)

INLET SUCTIONDANGER AREA

EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER

EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS

EXHAUST DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)

INLET DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)

INLET HAZARD DIMENSIONSBASED ON 40 ft/sec (12 m/sec)CRITICAL VELOCITY WITH A3 ft (0.9 m) ADJUSTMENTFOR SAFETY

WIDTH195 ft (59 m)

RADIUS = 19.5 ft (5.9 m)

NO ENTRY 684 ft (208 m)AFT OF NOZZLE EXIT

A

B

C

D

ETO 1160 ft (354 m)

(105−32)

N_AC_060302_1_0030101_01_01

Danger Areas of EnginesCFM56 series engine

FIGURE 1

6-3-2Page 2

May 01/11


**ON A/C A319-100

1.68 m(5.5 ft)

R = 5.79 m(19ft)

30°TO 348 m (1150 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)

INTAKE SUCTION DANGER AREA

EXHAUST DANGER AREA

ENTRY CORRIDOR

N_AC_060302_1_0040101_01_00

Danger Areas of EnginesIAE V2500 series engine

FIGURE 2

6-3-2Page 3

May 01/11


6-4-0 APU Exhaust Velocities and Temperatures

**ON A/C A319-100

APU Exhaust Velocities and Temperatures

1. APU Exhaust Velocities and Temperatures.

6-4-0Page 1

May 01/11


6-4-1 APU

**ON A/C A319-100

APU - APIC & GARRETT

1. This section gives APU exhaust velocities and temperatures.

6-4-1Page 1

May 01/11


**ON A/C A319-100

0 PLAN 5 10 15 2520

0 16.404 32.808 49.212 65.616 82.02

0

0

FEET

0

5

ELEVATION

10

0

16.404

32.808

80°C176°F

100°C212°F

120°C248°F

150°C302°F

200°C392°F

300°C572°F

METERS

HEIGHT

m ft

FEET

METERS

45 m/s147 ft/s

30 m/s98 ft/s

20 m/s65 ft/s

10 m/s32 ft/s

5 m/s16 ft/s

5 10 15 20

16.404 32.808 49.212 65.616

N_AC_060401_1_0020101_01_00

Exhaust Velocities and TemperaturesAPU -- APIC & GARRETT

FIGURE 1

6-4-1Page 2

May 01/11


PAVEMENT DATA


**ON A/C A319-100

General Information

1. General Information

This brief description of the pavement charts that follow will help in their use for airport planning.

To aid in the interpolation between the discrete values shown, each airplane configuration is shownwith a minimum range of five loads on the main landing gear.

All curves on the charts represent data at a constant specified tire pressure with:- The airplane loaded to the maximum ramp weight.- The Center of Gravity (CG) at its maximum permissible aft position.

Pavement requirements for commercial airplanes are derived from the static analysis of loads imposedon the main landing gear struts.

The A/C codes are used for configuration management of chapter 07 only. There is no relationbetween these A/C codes and the ICAO A/C codes used for determining the airplane wing span andouter main gear wheel span as described in ICAO-Annex 14 Volume 1, Aerodrome Design andOperation Chapter 1.4, Table 1-1.

Section 7-2-0 presents basic data on the landing gear footprint configuration, maximum ramp weightsand tire sizes and pressures.

Section 7-3-0 shows maximum vertical and horizontal pavement loads for certain critical conditions atthe tire-ground interfaces.

Section 7-4-1 contain charts to find these loads throughout the stability limits of the airplane at reston the pavement.

These main landing gear loads are used as the point of entry to the pavement design charts whichfollow, interpolating load values where necessary.

Section 7-5-1 uses procedures in Instruction Report No S-77-1 ”Procedures for Development of CBRDesign Curves”, dated June 1977 and as modified according to the methods described in ICAOAerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCNMethod), and utilizing the alpha factors approved by ICAO in October 2007.

7-1-0Page 1

May 01/11


The report was prepared by the U.S. Army Corps Engineers Waterways Experiment Station, Soils andPavement Laboratory, Vicksburg, Mississippi.

The line showing 10 000 coverages is used to calculate Aircraft Classification Number (ACN).

The procedure that follows is used to develop flexible pavement design curves such as shown inSection 7-5-1.- With the scale for pavement thickness at the bottom and the scale for CBR at the top, an

arbitrary line is drawn representing 10 000 coverages.- Incremental values of the weight on the main landing gear are then plotted.- Annual departure lines are drawn based on the load lines of the weight on the main landing gear

that is shown on the graph.

Section 7-7-1 gives the rigid pavement design curves that have been prepared with the use of theWestergaard Equation. This is in general accordance with the procedures outlined in the PortlandCement Association publications, ”Design of Concrete Airport Pavement”, 1973 and ”ComputerProgram for Airport Pavement Design”, (Program PDILB), 1967 both by Robert G. Packard.

The procedure that follows is used to develop rigid pavement design curves such as shown in Section7-7-1.- With the scale for pavement thickness on the left and the scale for allowable working stress on

the right, an arbitrary load line is drawn. This represents the maximum weight to be shown forthe main landing gear .

- All values of the subgrade modulus (k values) are then plotted.- Additional load lines for the incremental values of weight on the main landing gear are drawn on

the basis of the curve for k = 300 already shown on the graph.

All Load Classification Number (LCN) curves shown in Section 7-6-1 and Section 7-8-2 have beendeveloped from a computer program based on data provided in International Civil AviationOrganisation (ICAO) document 7920-AN/865/2, Aerodrome Manual, Part 2, ”Aerodrome PhysicalCharacteristics”, Second Edition, 1965.

The flexible pavement charts in Section 7-6-1 show LCN against equivalent single wheel load andequivalent single wheel load against pavement thickness.

The rigid pavement charts in Section 7-8-2 show LCN against equivalent single wheel load andequivalent single wheel load against radius of relative stiffness.

Section 7-9-0 gives ACN data prepared in accordance to the ACN/PCN system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 Fourth Edition July 2004, incorporating Amendments 1 to 6.

The ACN/PCN system gives a standardized international airplane/pavement rating system replacingthe various S, T, TT, LCN, AUW, ISWL, etc..., rating systems used throughout the world.

7-1-0Page 2

May 01/11


The ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.

An aircraft having an ACN equal to or less than the PCN can operate without restriction on thepavement.

Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.The derived single wheel is defined as the load on a single tire inflated to 1.25 Mpa (181 psi) thatwould have the same pavement requirements as the aircraft.

Computationally, the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1for flexible pavements to calculate ACN values.The Airport Authority must decide on the method of pavement analysis and the results of theirevaluation shown as follows:

PCNPAVEMENT

TYPESUBGRADECATEGORY

TIRE PRESSURE CATEGORY EVALUATION METHOD

R -- Rigid A -- High W -- No Limit T -- Technical

F -- Flexible B -- Medium X -- To 1.5 Mpa (217 psi) U -- Using Aircraft

C -- Low Y -- To 1.0 Mpa (145 psi)

D -- Ultra Low Z -- To 0.5 Mpa (73 psi)

Section 7-9-1 shows the aircraft ACN values for flexible pavements.

The four subgrade categories are:- A. High Strength CBR 15- B. Medium Strength CBR 10- C. Low Strength CBR 6- D. Ultra Low Strength CBR 3

Section 7-9-2 shows the aircraft ACN values for rigid pavements.

The four subgrade categories are:- A. High Strength Subgrade k = 150 MN/m3 (550 pci)- B. Medium Strength Subgrade k = 80 MN/m3 (300 pci)- C. Low Strength Subgrade k = 40 MN/m3 (150 pci)- D. Ultra Low Strength Subgrade k = 20 MN/m3 (75 pci)

7-1-0Page 3

May 01/11


**ON A/C A319-100

MODELA319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−133A319−115A319−111A319−112A319−113A319−114A319−131A319−132A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132

WV1212121212121212000000000000000008080808080808081111111111111111090909090909090903030303030303030404040404040404

AIRCRAFT CODECCCCCCDDEEFFFFFFGGGGGGHHIIIIIIJJKKKKKKLLMMNNNNNNOOPPPPPP

MODELA319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132

A319−112−CJA319−114−CJA319−115−CJA319−132−CJA319−133−CJ

A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132

A319−112−CJA319−114−CJA319−115−CJA319−132−CJA319−133−CJ

A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132

A319−111−CJA319−112−CJA319−113−CJA319−114−CJA319−131−CJA319−132−CJ

WV0101010101010101050505050505050505050505050606060606060606070707070707070702020202020202020202020202101010101010

AIRCRAFT CODEQQRRRRRRSSSSSTTUUUUUUVVVVVVWWXXYYYYYYZZZZZ

AAAAABABABABABABACACACACACAC

NOTE: FOR WEIGHT VARIANT DEFINITION, REFER TO CHAPTER 02−01−01.

NOTE: THE A/C CODES ARE USED FOR CONFIGURATION MANAGEMENT OFCHAPTER 07 ONLY.THERE IS NO RELATION BETWEEN THESE A/C CODES AND THE ICAO A/C CODES USED FOR DETERMINING THE AIRPLANE WING SPAN ANDOUTER MAIN GEAR WHEEL SPAN AS DESCRIBED IN ICAO−ANNEX 14 VOLUME 1,AERODROME DESIGN AND OPERATION CHAPTER 1.4, TABLE 1−1. N_AC_070100_1_0020101_01_00

Aircraft CodesFIGURE 1

7-1-0Page 4

May 01/11


7-2-0 Landing Gear Footprint

**ON A/C A319-100

Landing Gear Footprint

1. This section gives Landing Gear Footprint.

NOTE : For A/C Code definition, refer to chapter 7-1-0.

7-2-0Page 1

May 01/11


**ON A/C A319-100

500 mm(19.7 in)

11 039 mm

(36 ft 2.6 in)

7 590 mm(24 ft 10.8 in)

927 mm(36.5 in)

30 x 8.8 R15 (30 x 8.8 − 15)

11.4 bar (165 psi)

46 x 17 R20 (46 x 16 − 20)

11.9 bar (173 psi)

NOSE GEAR TIRE SIZE

NOSE GEAR TIRE PRESSURE

MAIN GEAR TIRE SIZE

MAIN GEAR TIRE PRESSURE

PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP

C − D − E − F − G − H

SEE SECTION 7−4−1

A/C CODE

N_AC_070200_1_0040101_01_01

Landing Gear FootprintLanding Gear Footprint

FIGURE 1

7-2-0Page 2

May 01/11


**ON A/C A319-100

11 039 mm

500 mm(19.7 in)

(36 ft 2.6 in)

927 mm(36.5 in)

7 590 mm(24 ft 10.8 in)

30 x 8.8 R15 (30 x 8.8 − 15)

12.1 bar (175 psi)

46 x 17 R20 (46 x 16 − 20)

12.5 bar (181 psi)

NOSE GEAR TIRE SIZE


MAIN GEAR TIRE SIZE



I − J − K − L − M − N − O − P


A/C CODE

N_AC_070200_1_0050101_01_01


FIGURE 2

7-2-0Page 3

May 01/11


**ON A/C A319-100

30 x 8.8 R15 (30 x 8.8 − 15)

12.5 bar (181 psi)

46 x 17 R20 (46 x 16 − 20)

12.9 bar (187 psi)

NOSE GEAR TIRE SIZE


MAIN GEAR TIRE SIZE



500 mm(19.7 in)

11 039 mm

(36 ft 2.6 in)

7 590 mm(24 ft 10.8 in)

927 mm(36.5 in)

Q − R − T − U


A/C CODE

N_AC_070200_1_0060101_01_01


FIGURE 3

7-2-0Page 4

May 01/11


**ON A/C A319-100

11 039 mm

500 mm(19.7 in)

(36 ft 2.6 in)

927 mm(36.5 in)

7 590 mm(24 ft 10.8 in)

30 x 8.8 R15 (30 x 8.8 − 15)

13.5 bar (196 psi)

46 x 17 R20 (46 x 16 − 20)

13.4 bar (194 psi)

NOSE GEAR TIRE SIZE


MAIN GEAR TIRE SIZE



V − W


A/C CODE

N_AC_070200_1_0070101_01_01


FIGURE 4

7-2-0Page 5

May 01/11


**ON A/C A319-100

30 x 8.8 R15 (30 x 8.8 − 15)

13.9 bar (202 psi)

46 x 17 R20 (46 x 16 − 20)

13.8 bar (200 psi)

NOSE GEAR TIRE SIZE


MAIN GEAR TIRE SIZE



500 mm(19.7 in)

11 039 mm

(36 ft 2.6 in)

7 590 mm(24 ft 10.8 in)

927 mm(36.5 in)

S − Z − AC


A/C CODE

N_AC_070200_1_0250101_01_00

Landing Gear FootprintFIGURE 5

7-2-0Page 6

May 01/11


**ON A/C A319-100

11 039 mm

500 mm(19.7 in)

(36 ft 2.6 in)

927 mm(36.5 in)

7 590 mm(24 ft 10.8 in)

30 x 8.8 R15 (30 x 8.8 − 15)

13.2 bar (191 psi)

46 x 17 R20 (46 x 16 − 20)

13.8 bar (200 psi)

NOSE GEAR TIRE SIZE


MAIN GEAR TIRE SIZE



X − Y − AA − AB


A/C CODE

N_AC_070200_1_0260101_01_00

Landing Gear FootprintFIGURE 6

7-2-0Page 7

May 01/11


7-3-0 Maximum Pavement Loads

**ON A/C A319-100

Maximum Pavement Loads

1. This section gives Maximum Pavement Loads.

NOTE : For A/C code definition, refer to chapter 7-1-0.

7-3-0Page 1

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GS

TA

TIC

BR

AK

ING

DE

CE

LER

AT

ION

@ 1

0 ft/

sS

TE

AD

Y B

RA

KIN

G

DE

CE

LER

AT

ION

@ 1

0 ft/

sA

T IN

ST

AN

TA

NE

OU

SB

RA

KIN

GC

OE

FF

ICIE

NT

= 0

.8

23

45

6H

(P

ER

ST

RU

T)

MA

XIM

UM

RA

MP

WE

IGH

T

lbkg

lbkg

lbkg

lbkg

lbkg

lbkg

C62

400

VM

G (

PE

R S

TR

UT

)V

NG

137

575

23 6

2510

720

36 5

0016

550

63 7

2528

900

21 3

759

700

50 9

7523

120

V(N

G)

MA

XIM

UM

VE

RT

ICA

L N

OS

E G

EA

R G

RO

UN

D L

OA

D A

T M

OS

T F

OR

WA

RD

CG

V(M

G)

MA

XIM

UM

VE

RT

ICA

L M

AIN

GE

AR

GR

OU

ND

LO

AD

AT

MO

ST

AF

T C

G

HM

AX

IMU

M H

OR

IZO

NT

AL

GR

OU

ND

LO

AD

FR

OM

BR

AK

ING

(1)

MR

W =

62

400

kgM

RW

= 6

2 40

0 kg

NO

TE

:A

LL L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

PLA

NE

MA

XIM

UM

RA

MP

WE

IGH

T

22

V(N

G)

V(M

G)

H

A/C

CO

DE

(1)

(2)

FW

D C

G =

14

% M

AC

AT

A/C

WE

IGH

T =

62

400

kgF

WD

CG

= 2

0.4

% M

AC

AT

A/C

WE

IGH

T =

62

400

kg

D E64

925

29 4

5022

075

10 0

1051

925

23 5

60

A/C

CO

DE

C DM

RW

= 6

4 40

0 kg

FW

D C

G =

21

% M

AC

AT

A/C

WE

IGH

T =

64

400

kgE

(2)

MR

W =

62

400

kgM

RW

= 6

2 40

0 kg

AF

T C

G =

39

% M

AC

AT

A/C

WE

IGH

T =

62

400

kgA

FT

CG

= 3

6 %

MA

C A

T A

/C W

EIG

HT

= 6

2 40

0 kg

C DM

RW

= 6

4 40

0 kg

AF

T C

G =

36

% M

AC

AT

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IGH

T =

64

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62 4

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N_AC_070300_1_0230101_01_00

Maximum Pavement LoadsFIGURE 1

7-3-0Page 2

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GS

TA

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BR

AK

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@ 1

0 ft/

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ER

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lbkg

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NO

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US

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T =

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T =

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MR

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AF

T C

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T =

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FT

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9 %

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C A

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F GM

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AF

T C

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% M

AC

AT

A/C

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IGH

T =

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64 4

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1 97

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N_AC_070300_1_0240101_01_00


7-3-0Page 3

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

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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

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DE

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LER

AT

ION

@ 1

0 ft/

sS

TE

AD

Y B

RA

KIN

G

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0 ft/

sA

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= 0

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23

45

6H

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ST

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IGH

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lbkg

lbkg

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MR

W =

66

400

kgM

RW

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6 40

0 kg

NO

TE

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LL L

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US

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AF

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AF

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AC

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T =

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MR

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66 4

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N_AC_070300_1_0250101_01_00


7-3-0Page 4

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GS

TA

TIC

BR

AK

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DE

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LER

AT

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@ 1

0 ft/

sS

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AD

Y B

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KIN

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ST

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TA

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OU

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RA

KIN

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= 0

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45

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IGH

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lbkg

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L66

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0 kg

NO

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US

ING

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AF

T C

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T =

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AF

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N_AC_070300_1_0260101_01_00


7-3-0Page 5

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GS

TA

TIC

BR

AK

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DE

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LER

AT

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@ 1

0 ft/

sS

TE

AD

Y B

RA

KIN

G

DE

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@ 1

0 ft/

sA

T IN

ST

AN

TA

NE

OU

SB

RA

KIN

GC

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= 0

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23

45

6H

(P

ER

ST

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MA

XIM

UM

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MP

WE

IGH

T

lbkg

lbkg

lbkg

lbkg

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NO

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AF

T C

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N_AC_070300_1_0270101_01_00


7-3-0Page 6

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GS

TA

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AK

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@ 1

0 ft/

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AD

Y B

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KIN

G

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= 0

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45

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WE

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lbkg

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NO

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AF

T C

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AC

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T =

70

400

kgR T

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N_AC_070300_1_0280101_01_00


7-3-0Page 7

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

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AK

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KIN

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NO

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AC

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FW

D C

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(2)

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0 kg

AF

T C

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AF

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MA

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V WM

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AF

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N_AC_070300_1_0290101_01_00


7-3-0Page 8

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GS

TA

TIC

BR

AK

ING

DE

CE

LER

AT

ION

@ 1

0 ft/

sS

TE

AD

Y B

RA

KIN

G

DE

CE

LER

AT

ION

@ 1

0 ft/

sA

T IN

ST

AN

TA

NE

OU

SB

RA

KIN

GC

OE

FF

ICIE

NT

= 0

.8

23

45

6H

(P

ER

ST

RU

T)

MA

XIM

UM

RA

MP

WE

IGH

T

lbkg

lbkg

lbkg

lbkg

lbkg

lbkg

Y75

900

VM

G (

PE

R S

TR

UT

)V

NG

167

325

23 6

2510

720

39 4

0017

870

76 6

0034

750

26 0

0011

800

61 2

7527

800

V(N

G)

MA

XIM

UM

VE

RT

ICA

L N

OS

E G

EA

R G

RO

UN

D L

OA

D A

T M

OS

T F

OR

WA

RD

CG

V(M

G)

MA

XIM

UM

VE

RT

ICA

L M

AIN

GE

AR

GR

OU

ND

LO

AD

AT

MO

ST

AF

T C

G

HM

AX

IMU

M H

OR

IZO

NT

AL

GR

OU

ND

LO

AD

FR

OM

BR

AK

ING

(1)

MR

W =

75

900

kgM

RW

= 7

5 90

0 kg

NO

TE

:A

LL L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

PLA

NE

MA

XIM

UM

RA

MP

WE

IGH

T

22

V(N

G)

V(M

G)

H

A/C

CO

DE

(1)

(2)

FW

D C

G =

21

% M

AC

AT

A/C

WE

IGH

T =

74

500

kgF

WD

CG

= 2

1 %

MA

C A

T A

/C W

EIG

HT

= 7

4 50

0 kg

AA

75 9

0016

7 32

523

625

AB

75 9

0016

7 32

523

500

10 7

2039

400

17 8

7076

600

34 7

5026

000

11 8

0061

275

27 8

00

10 6

6039

100

17 7

4076

675

34 7

8026

000

11 8

0061

350

27 8

30

A/C

CO

DE

Y AA

MR

W =

75

900

kgF

WD

CG

= 2

1 %

MA

C A

T A

/C W

EIG

HT

= 7

4 50

0 kg

AB

(2)

MR

W =

75

900

kgM

RW

= 7

5 90

0 kg

AF

T C

G =

36

% M

AC

AT

A/C

WE

IGH

T =

75

900

kgA

FT

CG

= 3

6 %

MA

C A

T A

/C W

EIG

HT

= 7

5 90

0 kg

Y AA

MR

W =

75

900

kgA

FT

CG

= 3

6 %

MA

C A

T A

/C W

EIG

HT

= 7

5 90

0 kg

AB

N_AC_070300_1_0300101_01_00


7-3-0Page 9

May 01/11


**ON A/C A319-100

1

ST

AT

IC L

OA

D A

TM

OS

T F

WD

CG

ST

AT

IC L

OA

D A

TM

AX

AF

T C

GS

TA

TIC

BR

AK

ING

DE

CE

LER

AT

ION

@ 1

0 ft/

sS

TE

AD

Y B

RA

KIN

G

DE

CE

LER

AT

ION

@ 1

0 ft/

sA

T IN

ST

AN

TA

NE

OU

SB

RA

KIN

GC

OE

FF

ICIE

NT

= 0

.8

23

45

6H

(P

ER

ST

RU

T)

MA

XIM

UM

RA

MP

WE

IGH

T

lbkg

lbkg

lbkg

lbkg

lbkg

lbkg

S70

400

VM

G (

PE

R S

TR

UT

)V

NG

155

200

25 4

5011

550

39 6

5017

990

71 1

0032

250

24 1

2510

940

56 8

7525

800

V(N

G)

MA

XIM

UM

VE

RT

ICA

L N

OS

E G

EA

R G

RO

UN

D L

OA

D A

T M

OS

T F

OR

WA

RD

CG

V(M

G)

MA

XIM

UM

VE

RT

ICA

L M

AIN

GE

AR

GR

OU

ND

LO

AD

AT

MO

ST

AF

T C

G

HM

AX

IMU

M H

OR

IZO

NT

AL

GR

OU

ND

LO

AD

FR

OM

BR

AK

ING

(1)

MR

W =

70

400

kgM

RW

= 7

5 90

0 kg

NO

TE

:A

LL L

OA

DS

CA

LCU

LAT

ED

US

ING

AIR

PLA

NE

MA

XIM

UM

RA

MP

WE

IGH

T

22

V(N

G)

V(M

G)

H

A/C

CO

DE

(1)

(2)

FW

D C

G =

14

% M

AC

AT

A/C

WE

IGH

T =

67

500

kgF

WD

CG

= 2

1 %

MA

C A

T A

/C W

EIG

HT

= 7

4 50

0 kg

Z AC

77 7

0035

240

26 3

5011

950

62 1

5028

190

A/C

CO

DE

S ZM

RW

= 7

6 90

0 kg

FW

D C

G =

21

% M

AC

AT

A/C

WE

IGH

T =

74

500

kgA

C

(2)

MR

W =

70

400

kgM

RW

= 7

5 90

0 kg

AF

T C

G =

36

% M

AC

AT

A/C

WE

IGH

T =

70

400

kgA

FT

CG

= 3

6 %

MA

C A

T A

/C W

EIG

HT

= 7

5 90

0 kg

S ZM

RW

= 7

6 90

0 kg

AF

T C

G =

36

% M

AC

AT

A/C

WE

IGH

T =

76

900

kgA

C

76 9

0016

9 52

523

500

10 6

6039

100

17 7

30

75 9

0016

7 52

523

500

10 6

6039

100

17 7

4076

675

34 7

8026

000

11 8

0061

350

27 8

30

N_AC_070300_1_0310101_01_00


7-3-0Page 10

May 01/11



**ON A/C A319-100

Landing Gear Loading on Pavement

1. General

In the example shown in Section 7-4-1 Landing Gear Loading on Pavement, A/C Code C, the GrossAircraft Weight is 48 000 kg (105 825 lb) and the percentage of weight on the Main Landing Gear is92.6 %.

For these conditions the total weight on the Main Landing Gear is 44 470 kg (98 025 lb).

7-4-0Page 1

May 01/11



**ON A/C A319-100

Landing Gear Loading on Pavement

1. This section gives Landing Gear Loading on Pavement.


7-4-1Page 1

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)

PERCENTAGE OF WEIGHT ON MAIN GEAR

50

55

60

65

50

55

60

65

35

40

45

35

40

45

80 82 84 86 88 90 92 94 96 98 100

CG FOR ACNCALCULATIONS

PERCENTAGE MAC

10 20 30 40 50

A/C CODE C

LANDING

TAKE OFF

MZFW = 57 000 kg

MLW = 61 000 kg

MTOW = 62 000 kg

N_AC_070401_1_0380101_01_00

Landing Gear Loading on PavementFIGURE 1

7-4-1Page 2

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


50

55

60

65

50

55

60

65

35

40

45

35

40

45

80 82 84 86 88 90 92 94 96 98 100

MZFW = 57 000 kg

MLW = 61 000 kg

MTOW = 62 000 kg


PERCENTAGE MAC

10 20 30 40 50

A/C CODE D

LANDING

TAKE OFF

N_AC_070401_1_0390101_01_00

LANDING


7-4-1Page 3

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


50

55

60

65

50

55

60

65

35

40

45

35

40

45

80 82 84 86 88 90 92 94 96 98 100

PERCENTAGE MAC

10 20 30 40 50

A/C CODE E

MLW = 61 000 kg

MZFW = 57 000 kg

LANDING

TAKE OFF


MTOW = 64 000 kg

N_AC_070401_1_0400101_01_00

LANDING


7-4-1Page 4

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


50

55

60

65

50

55

60

65

35

40

45

35

40

45

80 82 84 86 88 90 92 94 96 98 100

MTOW = 64 000 kg


LANDING

TAKE OFF

PERCENTAGE MAC

10 20 30 40 50

MLW = 61 000 kg

A/C CODE F

N_AC_070401_1_0410101_01_00

MZFW = 57 000 kg


7-4-1Page 5

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


50

55

60

65

50

55

60

65

35

40

45

35

40

45

80 82 84 86 88 90 92 94 96 98 100

MLW = 62 500 kg

MTOW = 64 000 kg

MZFW = 58 500 kg

TAKE OFF

LANDING

PERCENTAGE MAC

10 20 30 40 50

N_AC_070401_1_0420101_01_00


A/C CODE G


7-4-1Page 6

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


50

55

60

65

50

55

60

65

35

40

45

35

40

45

80 82 84 86 88 90 92 94 96 98 100

MLW = 62 500 kg

MTOW = 64 000 kg

MZFW = 58 500 kg


PERCENTAGE MAC

10 20 30 40 50

A/C CODE H

N_AC_070401_1_0430101_01_00

LANDING

TAKE OFF


7-4-1Page 7

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098


PERCENTAGE MAC

10 20 30 40 50

A/C CODE I

N_AC_070401_1_0440101_01_00

MZFW = 57 000 kg

MLW = 61 000 kg

MTOW = 66 000 kg

LANDING

TAKE OFF

LANDING

Landing Gear Loading on PavementLanding Gear Loading on Pavement

FIGURE 7

7-4-1Page 8

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098

MTOW = 66 000 kg

MZFW = 57 000 kg

PERCENTAGE MAC

10 20 30 40 50

TAKE OFF

LANDING

A/C CODE J

MLW = 61 000 kg


LANDING

N_AC_070401_1_0450101_01_00


7-4-1Page 9

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098

MTOW = 66 000 kg

MZFW = 58 500 kg

PERCENTAGE MAC

10 20 30 40 50

A/C CODE K

TAKE OFF

MLW = 62 500 kg

N_AC_070401_1_0460101_01_00

LANDINGLANDING



7-4-1Page 10

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098

MZFW = 58 500 kg

MTOW = 66 000 kg

TAKE OFF


MLW = 62 500 kg

LANDING

PERCENTAGE MAC

10 20 30 40 50

A/C CODE L

N_AC_070401_1_0470101_01_00

LANDING


7-4-1Page 11

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098

MZFW = 57 000 kg


MLW = 61 000 kg

PERCENTAGE MAC

10 20 30 40 50

A/C CODE M

MTOW = 68 000 kg

LANDING

TAKE OFF

N_AC_070401_1_0480101_01_00

LANDING


7-4-1Page 12

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098

MZFW = 57 000 kg

MTOW = 68 000 kg


PERCENTAGE MAC

10 20 30 40 50

A/C CODE N

MLW = 61 000 kg

LANDING

TAKE OFF

N_AC_070401_1_0490101_01_00

LANDING


7-4-1Page 13

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098

MZFW = 58 500 kg

TAKE OFF


MTOW = 68 000 kg

MLW = 62 500 kg

LANDING

PERCENTAGE MAC

10 20 30 40 50

A/C CODE O

N_AC_070401_1_0500101_01_00

LANDING


7-4-1Page 14

May 01/11


**ON A/C A319-100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


3580

40

45

50

55

60

65

70 70

35

40

45

50

55

60

65

82 84 86 88 90 92 94 96 10098

MTOW = 68 000 kg


PERCENTAGE MAC

10 20 30 40 50

A/C CODE P

MZFW = 58 500 kg

MLW = 62 500 kg

LANDING

TAKE OFF

N_AC_070401_1_0510101_01_00

LANDING


7-4-1Page 15

May 01/11


**ON A/C A319-100

55

60

65

70

55

60

65

7010 20 30 40 50

35

40

45

50

35

40

45

50

80 82 84 86 88 90 92 94 96 98 100

A/C CODE Q

PERCENTAGE MAC

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)



LANDING

TAKE OFF

MZFW = 57 000 kg

MLW = 61 000 kg

MTOW = 70 000 kg

N_AC_070401_1_0520101_01_00


7-4-1Page 16

May 01/11


**ON A/C A319-100

55

60

65

70

55

60

65

7010 20 30 40 50

35

40

45

50

35

40

45

50

80 82 84 86 88 90 92 94 96 98 100

PERCENTAGE MAC

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


A/C CODE R


LANDING

TAKE OFF

MZFW = 57 000 kg

MLW = 61 000 kg

MTOW = 70 000 kg

N_AC_070401_1_0530101_01_00


FIGURE 16

7-4-1Page 17

May 01/11


**ON A/C A319-100

55

60

65

70

55

60

65

7010 20 30 40 50

35

40

45

50

35

40

45

50

80 82 84 86 88 90 92 94 96 98 100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


A/C CODE S


LANDING

TAKE OFF

MZFW = 58 500 kg

MLW = 62 500 kg

MTOW = 70 000 kg

PERCENTAGE MAC

N_AC_070401_1_0540101_01_00


FIGURE 17

7-4-1Page 18

May 01/11


**ON A/C A319-100

55

60

65

70

55

60

65

7010 20 30 40 50

35

40

45

50

35

40

45

50

80 82 84 86 88 90 92 94 96 98 100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


LANDING

TAKE OFF


MLW = 62 500 kg

MTOW = 70 000 kg

MZFW = 58 500 kg

A/C CODE T

PERCENTAGE MAC

N_AC_070401_1_0550101_01_00


7-4-1Page 19

May 01/11


**ON A/C A319-100

55

60

65

70

55

60

65

7010 20 30 40 50

35

40

45

50

35

40

45

50

80 82 84 86 88 90 92 94 96 98 100

PERCENTAGE MAC

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


A/C CODE U

LANDING

TAKE OFF

MZFW = 58 500 kg

MLW = 62 500 kg

MTOW = 70 000 kg


N_AC_070401_1_0560101_01_00


7-4-1Page 20

May 01/11


**ON A/C A319-100

55

60

65

70

10 20 30 40 50

35

40

45

50

3580 82 84 86 88 90 92 94 96 98 100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)

75

55

60

65

70

40

45

50

75

PERCENTAGE MAC


A/C CODE V

MZFW = 58 500 kg


MLW = 62 500 kg

MTOW = 73 500 kg

TAKE OFF

LANDING

N_AC_070401_1_0570101_01_00


7-4-1Page 21

May 01/11


**ON A/C A319-100

55

60

65

70

10 20 30 40 50

35

40

45

50

3580 82 84 86 88 90 92 94 96 98 100

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)

75

55

60

65

70

40

45

50

75


MTOW = 73 500 kg

A/C CODE W

MLW = 62 500 kg

MZFW = 58 500 kg


LANDING

TAKE OFF

PERCENTAGE MAC

N_AC_070401_1_0580101_01_00


7-4-1Page 22

May 01/11


**ON A/C A319-100

55

60

65

70

10 20 30 40 50

35

40

45

50

3580 82 84 86 88 90 92 94 96 98 100

75

55

60

65

70

40

45

50

75

8080

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)


A/C CODE X

LANDING

TAKE OFF

MTOW = 75 500 kg

MLW = 61 000 kg

MZFW = 57 000 kg


PERCENTAGE MAC

N_AC_070401_1_0590101_01_00


7-4-1Page 23

May 01/11


**ON A/C A319-100

55

60

65

70

10 20 30 40 50

35

40

45

50

3580 82 84 86 88 90 92 94 96 98 100

75

55

60

65

70

40

45

50

75

8080

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)

PERCENTAGE MAC


A/C CODE Y

MLW = 61 000 kg

MZFW = 57 000 kg

MTOW = 75 500 kg


LANDING

TAKE OFF

N_AC_070401_1_0600101_01_00


7-4-1Page 24

May 01/11


**ON A/C A319-100

55

60

65

70

10 20 30 40 50

35

40

45

50

3580 82 84 86 88 90 92 94 96 98 100

75

55

60

65

70

40

45

50

75

8080

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)

PERCENTAGE MAC


A/C CODE Z

MZFW = 58 500 kg

MLW = 62 500 kg

MTOW = 75 500 kg

LANDING

TAKE OFF CG FOR ACNCALCULATIONS

N_AC_070401_1_0610101_01_00


7-4-1Page 25

May 01/11


**ON A/C A319-100

55

60

65

70

35

40

45

50

35

75

55

60

65

70

40

45

50

75

80

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)

MLW = 62 500 kg

MTOW = 75 500 kg

TAKE OFF

MZFW = 58 500 kg

LANDING


10 20 30 40 5080

PERCENTAGE MAC

A/C CODE AA

N_AC_070401_1_0620101_01_00

80 82 84 86 88 90 92 94 96 98 100



7-4-1Page 26

May 01/11


**ON A/C A319-100

55

60

65

70

35

40

45

50

35

75

55

60

65

70

40

45

50

75

8080

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)

MLW = 62 500 kg

MTOW = 75 500 kg

MZFW = 58 500 kg


LANDING

10 20 30 40 50

PERCENTAGE MAC

A/C CODE AB

TAKE OFF

80 82 84 86 88 90 92 94 96 98 100


N_AC_070401_1_0630101_01_00


7-4-1Page 27

May 01/11


**ON A/C A319-100

55

60

65

70

35

40

45

50

3580 82 84 86 88 90 92 94 96 98 100

75

55

60

65

70

40

45

50

75

8080

AIR

CR

AF

T G

RO

SS

WE

IGH

T −

(x

1 00

0 kg

)

WE

IGH

T O

N M

AIN

LA

ND

ING

GE

AR

− (

x 1

000

kg)



LANDING

MTOW = 76 500 kg

TAKE OFF

10 20 30 40 50

PERCENTAGE MAC

A/C CODE AC

MZFW = 58 500 kg

MLW = 62 500 kg

N_AC_070401_1_0640101_01_00


7-4-1Page 28

May 01/11



**ON A/C A319-100

Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method

1. General

In order to determine a particular Flexible Pavement Thickness, the Subgrade Strength (CBR), theAnnual Departure Level and the weight on one Main Landing Gear must be known.

In the example shown in Section 7-5-1 Flexible Pavement Requirements, A/C Code C for:- a CBR value of 10- an Annual Departure Level of 25 000- the Load on one MLG of 20 000 kg (44 100 lb).

For these conditions, the Flexible Pavement Thickness is 41.4 cm (16.3 in).

The line showing 10 000 Coverages is used to calculate the Aircraft Classification Number (ACN).

7-5-0Page 1

May 01/11



**ON A/C A319-100

Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method

1. This section gives Flexible Pavement Requirements.


7-5-1Page 1

May 01/11


**ON A/C A319-100

SUBGRADE STRENGTH − CBR

806050403020151063

[CENTIMETERS]

FLEXIBLE PAVEMENT THICKNESS

46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)

806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*

*20 YEAR PAVEMENT LIFE

1 2003 0006 00015 00025 000

MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG

WEIGHT ON ONE MAIN LANDING GEAR28 900 kg (63 725 lb)

20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE C ALPHA FACTOR = 0.9

FOR ACN CALCULATIONS10 000 COVERAGES USED

N_AC_070501_1_0380101_01_00

Flexible Pavement RequirementsFIGURE 1

7-5-1Page 2

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE D ALPHA FACTOR = 0.9

N_AC_070501_1_0390101_01_00



7-5-1Page 3

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE E ALPHA FACTOR = 0.9


N_AC_070501_1_0400101_01_00


7-5-1Page 4

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE F ALPHA FACTOR = 0.9


N_AC_070501_1_0410101_01_00


7-5-1Page 5

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE G ALPHA FACTOR = 0.9


N_AC_070501_1_0420101_01_00


7-5-1Page 6

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE H ALPHA FACTOR = 0.9


N_AC_070501_1_0430101_01_00


7-5-1Page 7

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE I ALPHA FACTOR = 0.9

N_AC_070501_1_0440101_01_00



7-5-1Page 8

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE J ALPHA FACTOR = 0.9


N_AC_070501_1_0450101_01_00


7-5-1Page 9

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE K ALPHA FACTOR = 0.9


N_AC_070501_1_0460101_01_00


7-5-1Page 10

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE L ALPHA FACTOR = 0.9


N_AC_070501_1_0470101_01_00


7-5-1Page 11

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE M ALPHA FACTOR = 0.9


N_AC_070501_1_0480101_01_00


7-5-1Page 12

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE N ALPHA FACTOR = 0.9


N_AC_070501_1_0490101_01_00


7-5-1Page 13

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE O ALPHA FACTOR = 0.9


N_AC_070501_1_0500101_01_00


7-5-1Page 14

May 01/11


**ON A/C A319-100


806050403020151063

[CENTIMETERS]



806050403020151063

10 15 20 30 40 60 80 100 120 150 180

[INCHES]

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

A/C CODE P ALPHA FACTOR = 0.9


N_AC_070501_1_0510101_01_00


7-5-1Page 15

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50

N_AC_070501_1_0520101_01_00

WEIGHT ON ONE MAIN LANDING GEAR

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000


USED FOR ACN10 000 COVERAGES

CALCULATIONS

A/C CODE Q

32 210 kg (71 025 lb)

20 000 kg (44 100 lb)15 000 kg (33 075 lb)

25 000 kg (55 125 lb)

10 000 kg (22 050 lb)

ALPHA FACTOR = 0.9


7-5-1Page 16

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50

N_AC_070501_1_0530101_01_00


ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE R ALPHA FACTOR = 0.9

32 420 kg (71 475 lb)

20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)


7-5-1Page 17

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE S ALPHA FACTOR = 0.9

N_AC_070501_1_0540101_01_00


7-5-1Page 18

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE T ALPHA FACTOR = 0.9

N_AC_070501_1_0550101_01_00


7-5-1Page 19

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE U ALPHA FACTOR = 0.9

N_AC_070501_1_0560101_01_00


7-5-1Page 20

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE V ALPHA FACTOR = 0.9

N_AC_070501_1_0570101_01_00


7-5-1Page 21

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

25 000 kg (55 125 lb)

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE W ALPHA FACTOR = 0.9

N_AC_070501_1_0580101_01_00


7-5-1Page 22

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50

WEIGHT ON ONE MAIN LANDING GEAR34 750 kg (76 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)

ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE X

10 000 kg (22 050 lb)

ALPHA FACTOR = 0.9

N_AC_070501_1_0590101_01_00


7-5-1Page 23

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE Y

10 000 kg (22 050 lb)

ALPHA FACTOR = 0.9

N_AC_070501_1_0600101_01_00


7-5-1Page 24

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE Z

10 000 kg (22 050 lb)

ALPHA FACTOR = 0.9

N_AC_070501_1_0610101_01_00


7-5-1Page 25

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE AA

10 000 kg (22 050 lb)

ALPHA FACTOR = 0.9

N_AC_070501_1_0620101_01_00


7-5-1Page 26

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE AB

10 000 kg (22 050 lb)

ALPHA FACTOR = 0.9

N_AC_070501_1_0630101_01_00


7-5-1Page 27

May 01/11


**ON A/C A319-100

10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]



[INCHES]


8060403020151063

806050403020151063

50


ANNUAL DEPARTURES*


1 2003 0006 00015 00025 000



CALCULATIONS

A/C CODE AC

10 000 kg (22 050 lb)

ALPHA FACTOR = 0.9

N_AC_070501_1_0640101_01_00


7-5-1Page 28

May 01/11



**ON A/C A319-100

Flexible Pavement Requirements - LCN Conversion

1. General

In order to determine the airplane weight that can be accommodated on a particular FlexiblePavement, both the LCN of the pavement and the thickness (h) must be known.

In the example shown in Section 7-6-1 Flexible Pavement Requirements - LCN Conversion, A/C CodeC for:The thickness (h) is shown at 20 inches with an LCN of 52.3.

For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).

7-6-0Page 1

May 01/11



**ON A/C A319-100

Flexible Pavement Requirements - LCN Conversion

1. This section gives Flexible Pavement Requirements - LCN Conversion.


7-6-1Page 1

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

1.9

bar

(173

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20

EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]

10

EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]

1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

28 9

00 k

g

(63

725

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

C

N_AC_070601_1_0410101_01_00

Flexible Pavement Requirements - LCN ConversionFIGURE 1

7-6-1Page 2

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

1.9

bar

(173

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

N_AC_070601_1_0420101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

28 5

30 k

g

(62

900

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

D


7-6-1Page 3

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

1.9

bar

(173

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

20

WE

IGH

T O

N O

NE

MA

IN

29 4

50 k

g

(64

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

A/C

CO

DE

E

N_AC_070601_1_0430101_01_00


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UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

1.9

bar

(173

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

20

WE

IGH

T O

N O

NE

MA

IN

29 8

30 k

g

(65

775

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

A/C

CO

DE

F

N_AC_070601_1_0440101_01_00


7-6-1Page 5

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NO

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:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

1.9

bar

(173

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

N_AC_070601_1_0450101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

29 8

30 k

g

(65

775

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

G


7-6-1Page 6

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NO

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:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

1.9

bar

(173

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

20

WE

IGH

T O

N O

NE

MA

IN

29 4

50 k

g

(64

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

A/C

CO

DE

H

N_AC_070601_1_0460101_01_00


7-6-1Page 7

May 01/11


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NO

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:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

20

WE

IGH

T O

N O

NE

MA

IN

30 7

30 k

g

(67

750

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

A/C

CO

DE

I

N_AC_070601_1_0470101_01_00


7-6-1Page 8

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

N_AC_070601_1_0480101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

30 3

60 k

g

(66

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

J


7-6-1Page 9

May 01/11


**ON A/C A319-100

NO

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:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

N_AC_070601_1_0490101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

30 7

30 k

g

(67

750

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

K


7-6-1Page 10

May 01/11


**ON A/C A319-100

NO

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:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

20

WE

IGH

T O

N O

NE

MA

IN

30 3

60 k

g

(66

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

A/C

CO

DE

L

N_AC_070601_1_0500101_01_00


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:IC

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AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

N_AC_070601_1_0510101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

31 2

80 k

g

(68

950

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

M

Flexible Pavement Requirements - LCN ConversionFlexible Pavement Requirements - LCN Conversion

FIGURE 11

7-6-1Page 12

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:IC

AO

AE

RO

DR

OM

E M

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UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

31 5

70 k

g

(69

600

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

N

N_AC_070601_1_0520101_01_00


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NO

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:IC

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AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

N_AC_070601_1_0530101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

31 2

80 k

g

(68

950

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

O


7-6-1Page 14

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:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

N_AC_070601_1_0540101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

WE

IGH

T O

N O

NE

MA

IN

31 5

80 k

g

(69

625

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

A/C

CO

DE

P


7-6-1Page 15

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NO

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:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.9

bar

(187

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

32 2

10 k

g

(71

000

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

Q

N_AC_070601_1_0550101_01_00


7-6-1Page 16

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.9

bar

(187

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

32 4

20 k

g

(71

475

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

R

N_AC_070601_1_0560101_01_00


7-6-1Page 17

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.8

bar

(200

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

32 2

50 k

g

(71

100

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

S

N_AC_070601_1_0570101_01_00


7-6-1Page 18

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.9

bar

(187

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

32 2

10 k

g

(71

000

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

T

N_AC_070601_1_0580101_01_00


7-6-1Page 19

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.9

bar

(187

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

32 4

20 k

g

(71

475

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

U

N_AC_070601_1_0590101_01_00


7-6-1Page 20

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.4

bar

(194

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

33 8

90 k

g

(74

725

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

V

N_AC_070601_1_0600101_01_00


7-6-1Page 21

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.4

bar

(194

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

33 8

90 k

g

(74

725

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

W

N_AC_070601_1_0610101_01_00


7-6-1Page 22

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.8

bar

(200

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

34 7

50 k

g

(76

600

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

X

N_AC_070601_1_0620101_01_00


7-6-1Page 23

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.8

bar

(200

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

34 7

50 k

g

(76

600

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

Y

N_AC_070601_1_0630101_01_00


7-6-1Page 24

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.8

bar

(200

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

34 7

80 k

g

(76

675

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

Z

N_AC_070601_1_0640101_01_00


7-6-1Page 25

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.8

bar

(200

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

34 7

50 k

g

(76

600

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

AA

N_AC_070601_1_0650101_01_00


7-6-1Page 26

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.8

bar

(200

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

34 7

80 k

g

(76

675

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

AB

N_AC_070601_1_0660101_01_00


7-6-1Page 27

May 01/11


**ON A/C A319-100

NO

TE

:IC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

Sec

ond

Edi

tion

1965

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

IN

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

3.8

bar

(200

psi

)46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

35 30 25 20 15 10 5 080

100

6050

4030

20


10


1020304050607080

8070

6050

4030

100

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S [I

NC

HE

S]

WE

IGH

T O

N O

NE

MA

IN

35 2

40 k

g

(77

700

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

LAN

DIN

G G

EA

RM

AX

IMU

M R

AM

P W

EIG

HT

AN

D A

FT

CG

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

T

20

FLE

XIB

LE P

AV

EM

EN

T T

HIC

KN

ES

S (

mm

)

25 0

00 k

g

(55

125

lb)

A/C

CO

DE

AC

N_AC_070601_1_0670101_01_00

Flexible Pavement Requirements - LCN ConversionFlexible Pavement Requirements - LCN Conversion

FIGURE 27

7-6-1Page 28

May 01/11



**ON A/C A319-100

Rigid Pavement Requirements - Portland Cement Association Design Method

1. General

In order to determine a particular Rigid Pavement Thickness, the Subgrade Modulus (k), theallowable working stress and the weight on one Main Landing Gear must be known.

In the example shown in Section 7-7-1 Rigid Pavement Requirements (PCA), A/C Code C for:- a ”k” value of 150 MN/m3 (550 lbf/in3)- an allowable working stress of 31.6 kgf/cm2 (450 lbf/in2)- the load on one MLG of 20 000 kg (44 100 lb).For these conditions, the Rigid Pavement Thickness is 18.9 cm (7.4 in).

7-7-0Page 1

May 01/11



**ON A/C A319-100

Rigid Pavement Requirements - Portland Cement Association Design Method

1. This section gives Rigid Pavement Requirements.


7-7-1Page 1

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

WEIGHT ON ONE MAIN LANDING GEAR28 905 kg (63 725 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

A/C CODE C

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20

NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,

SLIGHTLY FOR ANY OTHER

THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE

VALUES OF K

REFERENCE:

AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION

"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13

14

N_AC_070701_1_0380101_01_00

Rigid Pavement Requirements (PCA)FIGURE 1

7-7-1Page 2

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


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


K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE D

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13

14


N_AC_070701_1_0390101_01_00


7-7-1Page 3

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


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


K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE E

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13

14


N_AC_070701_1_0400101_01_00


7-7-1Page 4

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


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


K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE F

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13

14


N_AC_070701_1_0410101_01_00


7-7-1Page 5

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


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


K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE G

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13

14


N_AC_070701_1_0420101_01_00


7-7-1Page 6

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


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


K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE H

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13

14


N_AC_070701_1_0430101_01_00


7-7-1Page 7

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE I

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0440101_01_00


7-7-1Page 8

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE J

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0450101_01_00


7-7-1Page 9

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE K

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0460101_01_00


7-7-1Page 10

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE L

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0470101_01_00


7-7-1Page 11

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE M

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0480101_01_00


7-7-1Page 12

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE N

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0490101_01_00


7-7-1Page 13

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE O

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0500101_01_00


7-7-1Page 14

May 01/11


**ON A/C A319-100

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

200

300

400

500

600

700

800

900

1000

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

A/C CODE P

34

32

30

28

26

24

22

20

18

16

70

58

52

45

39

33

27

20




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

6

7

8

9

10

11

12

13



N_AC_070701_1_0510101_01_00

10 000 kg (22 050 lb)


7-7-1Page 15

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S

6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE QRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]


K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

N_AC_070701_1_0520101_01_00



25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)

32 210 kg (71 025 lb)


7-7-1Page 16

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20



32 420 kg (71 475 lb)

A/C CODE R

N_AC_070701_1_0530101_01_00

RIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³ [lb/in

²]

[kg/

cm²]



7-7-1Page 17

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20


A/C CODE SRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³



32 245 kg (71 100 lb)

[lb/in

²]

[kg/

cm²]

N_AC_070701_1_0540101_01_00


7-7-1Page 18

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S

6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20




32 210 kg (71 025 lb)

A/C CODE TRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]


K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

N_AC_070701_1_0550101_01_00

[lb/in

²]

[kg/

cm²]


7-7-1Page 19

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20




32 420 kg (71 475 lb)

A/C CODE URIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

N_AC_070701_1_0560101_01_00

[lb/in

²]

[kg/

cm²]


7-7-1Page 20

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE VRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³



33 895 kg (74 725 lb)

[lb/in

²]

[kg/

cm²]

N_AC_070701_1_0570101_01_00



7-7-1Page 21

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE WRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³



33 895 kg (74 725 lb)


N_AC_070701_1_0580101_01_00


7-7-1Page 22

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE XRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

N_AC_070701_1_0590101_01_00



34 745 kg (76 600 lb)



7-7-1Page 23

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE YRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³



34 745 kg (76 600 lb)

N_AC_070701_1_0600101_01_00



7-7-1Page 24

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE ZRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³



34 780 kg (76 675 lb)

N_AC_070701_1_0610101_01_00



7-7-1Page 25

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE AARIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³



34 745 kg (76 600 lb)

N_AC_070701_1_0620101_01_00



7-7-1Page 26

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE ABRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³



34 780 kg (76 675 lb)

N_AC_070701_1_0630101_01_00



7-7-1Page 27

May 01/11


**ON A/C A319-100




VALUES OF K

REFERENCE:


"DESIGN OF CONCRETE

[INC

HE

S]

[lb/in

²]

[kg/

cm²]

ALL

OW

AB

LE W

OR

KIN

G S

TR

ES

S


6

7

8

9

10

11

12

13

14

34

32

30

28

26

24

22

20

18

16

200

300

400

500

600

700

800

900

1000 70

58

52

45

39

33

27

20

A/C CODE ACRIG

ID P

AV

EM

EN

T T

HIC

KN

ES

S[C

EN

TIM

ET

ER

S]

K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³

K = 20 MN/m³

N_AC_070701_1_0640101_01_00


35 240 kg (77 700 lb)




7-7-1Page 28

May 01/11



**ON A/C A319-100

Rigid Pavement Requirements - LCN Conversion

1. General

In 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 Section 7-8-2 Rigid Pavement Requirements - LCN Conversion, A/C Code Cfor:The Radius of Relative Stiffness is shown at 30 inches with an LCN of 56.For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).

7-8-0Page 1

May 01/11



**ON A/C A319-100

Radius of Relative Stiffness

1. This section gives Radius of Relative Stiffness.

7-8-1Page 1

May 01/11


**ON A/C A319-100

d6.06.57.07.5

K=75 K=100 K=150 K=200 K=250 K=300 K=350 K=400 K=550

8.08.59.09.5

10.010.511.011.512.012.513.013.514.014.515.015.516.016.517.017.518.019.020.021.022.023.024.025.0

31.4833.4335.3437.2239.0640.8842.6744.4346.1847.9049.6051.2852.9454.5956.2257.8359.4361.0262.5964.1565.6967.2368.7570.2671.7674.7377.6680.5583.4186.2489.0491.81

29.3031.1132.8934.6336.3538.0439.7141.3542.9744.5746.1647.7249.2750.8052.3253.8255.3156.7858.2559.7061.1362.5663.9865.3866.7869.5472.2774.9677.6380.2682.8685.44

26.4728.1129.7231.2932.8534.3735.8837.3638.8340.2841.7143.1244.5245.9047.2748.6349.9851.3152.6353.9455.2456.5357.8159.0860.3462.8465.3067.7470.1472.5274.8777.20

24.6326.1627.6529.1230.5731.9933.3934.7736.1437.4838.8140.1341.4342.7243.9945.2646.5147.7548.9850.2051.4152.6153.8054.9856.1558.4860.7763.0465.2867.4969.6871.84

23.3024.7426.1527.5428.9130.2531.5832.8934.1735.4536.7137.9539.1840.4041.6142.8043.9845.1646.3247.4748.6249.7550.8852.0053.1155.3157.4759.6261.7363.8365.9067.95

22.2623.6424.9926.3227.6228.9130.1731.4232.6533.8735.0736.2637.4438.6039.7540.8942.0243.1544.2645.3646.4547.5448.6149.6850.7452.8454.9156.9658.9860.9862.9664.92

21.4222.7424.0425.3226.5827.8129.0330.2331.4232.5933.7534.8936.0237.1438.2539.3540.4441.5142.5843.6444.7045.7446.7747.8048.8250.8452.8454.8156.7558.6860.5862.46

20.7222.0023.2524.4925.7026.9028.0829.2430.3931.5232.6433.7434.8435.9236.9938.0639.1140.1541.1942.2143.2344.2445.2446.2347.2249.1751.1053.0154.8956.7558.5960.41

19.1320.3121.4722.6123.7424.8425.9327.0028.0629.1130.1432.1632.1733.1734.1635.1436.1237.0838.0338.9839.9240.8541.7842.7043.6145.4147.1948.9550.6952.4154.1155.79

RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES

L =

E = Young’s Modulus = 4 x 10 psi

k = Subgrade Modulus, lbf/in

d = Rigid Pavement Thickness, inches

= Poisson’s Ratio = 0.15

Ed12 (1 − ) k = 24.1652

dk

WHERE

43

2

4

6

3

3

N_AC_070801_1_0020101_01_01

Radius of Relative Stiffness(Reference: Portland Cement Association)

FIGURE 1

7-8-1Page 2

May 01/11



**ON A/C A319-100

Rigid Pavement Requirements - LCN Conversion

1. This section gives Rigid Pavement Requirements - LCN Conversion.


7-8-2Page 1

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S [I

NC

HE

S]

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

A/C

CO

DE

C

508

762

1 01

61

270

1 77

82

540

RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

WE

IGH

T O

N O

NE

MA

IN

28 9

00 k

g

(63

725

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0410101_01_00

Rigid Pavement Requirements - LCN ConversionFIGURE 1

7-8-2Page 2

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S [I

NC

HE

S]

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


A/C

CO

DE

D

508

762

1 01

61

270

1 77

82

540

RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

WE

IGH

T O

N O

NE

MA

IN

28 5

30 k

g

(62

900

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0420101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT


7-8-2Page 3

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S [I

NC

HE

S]

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


A/C

CO

DE

E

508

762

1 01

61

270

1 77

82

540

RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

WE

IGH

T O

N O

NE

MA

IN

29 4

50 k

g

(64

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0430101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT


7-8-2Page 4

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S [I

NC

HE

S]

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


A/C

CO

DE

F

508

762

1 01

61

270

1 77

82

540

RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

WE

IGH

T O

N O

NE

MA

IN

29 8

30 k

g

(65

775

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0440101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT


7-8-2Page 5

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S [I

NC

HE

S]

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


A/C

CO

DE

G

508

762

1 01

61

270

1 77

82

540

RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

WE

IGH

T O

N O

NE

MA

IN

29 8

30 k

g

(65

775

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0450101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT


7-8-2Page 6

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)


RA

DIU

S O

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TIF

FN

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S [I

NC

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S]

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N N

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BE

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NT

SIN

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WH

EE

L LO

AD

S A

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DE

RIV

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BY

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INIC

AO

AE

RO

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F R

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TIV

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TIF

FN

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S (

mm

)

WE

IGH

T O

N O

NE

MA

IN

29 4

50 k

g

(64

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

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R

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0460101_01_00

MA

XIM

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T A

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T C

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2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)


RA

DIU

S O

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TIV

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TIF

FN

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S [I

NC

HE

S]

LOA

D C

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N N

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R (

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NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

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ED

BY

ME

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S S

HO

WN

INIC

AO

AE

RO

DR

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E M

AN

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L P

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T 2

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d E

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n 19

65N

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E:


A/C

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508

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F R

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TIF

FN

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S (

mm

)

WE

IGH

T O

N O

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MA

IN

30 7

30 k

g

(67

750

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

EA

R

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0470101_01_00

MA

XIM

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T A

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AF

T C

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AT


7-8-2Page 8

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2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)


RA

DIU

S O

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TIF

FN

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S [I

NC

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S]

LOA

D C

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N N

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NT

SIN

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WH

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L LO

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S A

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BY

ME

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INIC

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AE

RO

DR

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E M

AN

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L P

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T 2

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d E

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65N

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E:


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FN

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S (

mm

)

WE

IGH

T O

N O

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IN

30 3

60 k

g

(66

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

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10 0

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(22

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N_AC_070802_1_0480101_01_00

MA

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T A

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T C

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AT


7-8-2Page 9

May 01/11


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2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

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12.

5 ba

r (1

81 p

si)


RA

DIU

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TIF

FN

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S [I

NC

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S]

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D C

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N N

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R (

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NT

SIN

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WH

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L LO

AD

S A

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BY

ME

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S S

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INIC

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AE

RO

DR

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E M

AN

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L P

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T 2

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65N

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S (

mm

)

WE

IGH

T O

N O

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IN

30 7

30 k

g

(67

750

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

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10 0

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(22

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N_AC_070802_1_0490101_01_00

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7-8-2Page 10

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

8090

7060

5040

3005101520253035

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)


RA

DIU

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TIF

FN

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S [I

NC

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S]

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N N

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NT

SIN

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WH

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L LO

AD

S A

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ED

BY

ME

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OD

S S

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WN

INIC

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AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

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65N

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T O

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IN

30 3

60 k

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(66

925

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

LAN

DIN

G G

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(22

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N_AC_070802_1_0500101_01_00

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7-8-2Page 11

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)


RA

DIU

S O

F R

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FN

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S [I

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S]

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NT

SIN

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WH

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L LO

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S A

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BY

ME

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S S

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WN

INIC

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AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

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R 4

.1.3

S

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d E

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n 19

65N

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E:


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7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R31

280

kg

(6

8 95

0 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

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MA

XIM

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T A

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(22

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N_AC_070802_1_0510101_01_00


7-8-2Page 12

May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

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12.

5 ba

r (1

81 p

si)


RA

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S O

F R

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S [I

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S]

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WH

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S A

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BY

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S S

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INIC

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AE

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E M

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L P

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65N

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T O

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IN L

AN

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G G

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R31

570

kg

(6

9 60

0 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)

N_AC_070802_1_0520101_01_00

MA

XIM

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10 0

00 k

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(22

050

lb)


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May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

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12.

5 ba

r (1

81 p

si)


RA

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S O

F R

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S [I

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WH

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BY

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INIC

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AE

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L P

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65N

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AN

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G G

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280

kg

(6

8 95

0 lb

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000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)

N_AC_070802_1_0530101_01_00

MA

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10 0

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(22

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May 01/11


**ON A/C A319-100

2030

4050

100

8070

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46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

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12.

5 ba

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81 p

si)


RA

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F R

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S [I

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WH

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L LO

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INIC

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AE

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(5

5 12

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(4

4 10

0 lb

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3 07

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MA

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10 0

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(22

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May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

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PR

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BY

ME

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INIC

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AE

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E M

AN

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L P

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AN

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G G

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210

kg

(7

1 00

0 lb

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000

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(5

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(4

4 10

0 lb

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000

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(3

3 07

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N_AC_070802_1_0550101_01_00

MA

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AD

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10 0

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(22

050

lb)


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May 01/11


**ON A/C A319-100

2030

4050

100

8070

6001020304050607080

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

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12.

9 ba

r (1

87 p

si)


RA

DIU

S O

F R

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TIV

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FN

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S [I

NC

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S]

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D C

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N N

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BE

R (

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EQ

UIV

ALE

NT

SIN

GLE

WH

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L LO

AD

S A

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BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

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L P

AR

T 2

PA

R 4

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d E

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65N

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5040

3005101520253035

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R32

420

kg

(7

1 47

5 lb

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000

kg

(5

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000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

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(2

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N_AC_070802_1_0560101_01_00

MA

XIM

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May 01/11


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4050

100

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46 x

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x 1

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ST

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PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S [I

NC

HE

S]

LOA

D C

LAS

SIF

ICA

TIO

N N

UM

BE

R (

LCN

)

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

A/C

CO

DE

S

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R32

250

kg

(7

1 10

0 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)

N_AC_070802_1_0570101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT

10 0

00 k

g

(22

050

lb)


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NT

AT

12.

9 ba

r (1

87 p

si)


RA

DIU

S O

F R

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D C

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SIF

ICA

TIO

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R (

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)

EQ

UIV

ALE

NT

SIN

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WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

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S (

mm

)

A/C

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DE

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508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R32

210

kg

(7

1 00

0 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)

N_AC_070802_1_0580101_01_00

10 0

00 k

g

(22

050

lb)

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

AD

AT


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12.

9 ba

r (1

87 p

si)


RA

DIU

S O

F R

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EQ

UIV

ALE

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SIN

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WH

EE

L LO

AD

S A

RE

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RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

A/C

CO

DE

U

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R32

420

kg

(7

1 47

5 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)

N_AC_070802_1_0590101_01_00

10 0

00 k

g

(22

050

lb)

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

LE M

AIN

GE

AR

LO

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AT


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x 1

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) T

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SU

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CO

NS

TA

NT

AT

13.

4 ba

r (1

94 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

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D C

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SIF

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R (

LCN

)

EQ

UIV

ALE

NT

SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INIC

AO

AE

RO

DR

OM

E M

AN

UA

L P

AR

T 2

PA

R 4

.1.3

S

econ

d E

ditio

n 19

65N

OT

E:


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

A/C

CO

DE

V

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

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IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

33 8

90 k

g

(74

725

lb)

N_AC_070802_1_0600101_01_00

10 0

00 k

g

(22

050

lb)

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

OS

SIB

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AIN

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x 1

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NT

AT

13.

4 ba

r (1

94 p

si)


RA

DIU

S O

F R

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EQ

UIV

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SIN

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WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

WN

INN

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E:

ICA

O A

ER

OD

RO

ME

MA

NU

AL

PA

RT

2 P

AR

4.1

.3

Sec

ond

Edi

tion

1965


RA

DIU

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F R

ELA

TIV

E S

TIF

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mm

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82

540

8090

7060

5040

3005101520253035

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IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R33

890

kg

(7

4 72

5 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)10

000

kg

(2

2 05

0 lb

)

MA

XIM

UM

RA

MP

WE

IGH

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T C

GM

AX

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M P

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N_AC_070802_1_0610101_01_00


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13.

8 ba

r (2

00 p

si)


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DIU

S O

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EQ

UIV

ALE

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SIN

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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

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ME

MA

NU

AL

PA

RT

2 P

AR

4.1

.3

Sec

ond

Edi

tion

1965


RA

DIU

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F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

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CO

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X

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R34

750

kg

(7

6 60

0 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)10

000

kg

(2

2 05

0 lb

)

N_AC_070802_1_0620101_01_00

MA

XIM

UM

RA

MP

WE

IGH

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13.

8 ba

r (2

00 p

si)


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DIU

S O

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SIN

GLE

WH

EE

L LO

AD

S A

RE

DE

RIV

ED

BY

ME

TH

OD

S S

HO

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INN

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ICA

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1965


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508

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1 01

61

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1 77

82

540

8090

7060

5040

3005101520253035

MA

XIM

UM

PO

SS

IBLE

MA

IN G

EA

R L

OA

D A

TW

EIG

HT

ON

ON

E M

AIN

LA

ND

ING

GE

AR

34 7

50 k

g

(76

600

lb)

25 0

00 k

g

(55

125

lb)

20 0

00 k

g

(44

100

lb)

15 0

00 k

g

(33

075

lb)

10 0

00 k

g

(22

050

lb)

N_AC_070802_1_0630101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

G


7-8-2Page 24

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x 1

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13.

8 ba

r (2

00 p

si)


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S O

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UIV

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WH

EE

L LO

AD

S A

RE

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RIV

ED

BY

ME

TH

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Z

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R34

780

kg

(7

6 67

5 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)10

000

kg

(2

2 05

0 lb

)

N_AC_070802_1_0640101_01_00

MA

XIM

UM

RA

MP

WE

IGH

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ND

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T C

GM

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x 1

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13.

8 ba

r (2

00 p

si)


RA

DIU

S O

F R

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SIF

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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

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PA

RT

2 P

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4.1

.3

Sec

ond

Edi

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1965


RA

DIU

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ELA

TIV

E S

TIF

FN

ES

S (

mm

)

A/C

CO

DE

AA

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R34

750

kg

(7

6 60

0 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)10

000

kg

(2

2 05

0 lb

)

N_AC_070802_1_0650101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

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T C

GM

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M P

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100

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46 x

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x 1

6−20

) T

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ST

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PR

ES

SU

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CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

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HE

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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


RA

DIU

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F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

A/C

CO

DE

AB

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R34

780

kg

(7

6 67

5 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)10

000

kg

(2

2 05

0 lb

)

N_AC_070802_1_0660101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

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AIN

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100

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x 1

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) T

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ST

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CO

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NT

AT

13.

8 ba

r (2

00 p

si)


RA

DIU

S O

F R

ELA

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E S

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FN

ES

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NC

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D C

LAS

SIF

ICA

TIO

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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


RA

DIU

S O

F R

ELA

TIV

E S

TIF

FN

ES

S (

mm

)

A/C

CO

DE

AC

508

762

1 01

61

270

1 77

82

540

8090

7060

5040

3005101520253035

WE

IGH

T O

N O

NE

MA

IN L

AN

DIN

G G

EA

R35

240

kg

(7

7 70

0 lb

)25

000

kg

(5

5 12

5 lb

)20

000

kg

(4

4 10

0 lb

)15

000

kg

(3

3 07

5 lb

)10

000

kg

(2

2 05

0 lb

)

N_AC_070802_1_0670101_01_00

MA

XIM

UM

RA

MP

WE

IGH

T A

ND

AF

T C

GM

AX

IMU

M P

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AIN

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7-8-2Page 28

May 01/11


7-8-3 Radius of Relative Stiffness (Other values of E and L)

**ON A/C A319-100

Radius of Relative Stiffness (Other values of ”E” and ”L”)

1. General

The table of Section 7-8-1, Radius of Relative Stiffness, presents ”L” values based on Young’sModulus (E) of 4 000 000 psi and Poisson’s Ratio (µ) of 0.15.

To find ”L” values based on other values of ”E” and ”µ”, see Section 7-8-4.

For example, to find an ”L” value based on an ”E” of 3 000 000 psi, the ”E” factor of 0.931 ismultiplied by the ”L” value found in the table of Section 7-8-1.

The effect of variations of ”µ” on the ”L” value is treated in a similar manner.

7-8-3Page 1

May 01/11



**ON A/C A319-100

Radius of Relative Stiffness

1. This section gives Radius of Relative Stiffness.

7-8-4Page 1

May 01/11


**ON A/C A319-100

0.80

0.85

0.90

0.95

1.00

1.05

1.10

0 1 2 3 4 5

0.995

1.000

1.005

1.010

1.015

0.00 0.05 0.10 0.15 0.25

E F

AC

TO

R

BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF TABLE 7−8−1

EFFECT OF ON L VALUES

E, Young’s Modulus (10 , PSI)

EFFECT OF E ON L VALUES

, Poisson’s Ratio

FA

CT

OR

NOTE:

0.20

N_AC_070804_1_0020101_01_02

Radius of Relative Stiffness(Effect E and µ on ”L” values)

FIGURE 1

7-8-4Page 2

May 01/11


7-9-0 ACN/PCN Reporting System

**ON A/C A319-100

ACN/PCN Reporting System

1. General

To determine the ACN of an aircraft on flexible or rigid pavement, both the aircraft gross weight andthe subgrade strength must be known.

In the example shown in Section 7-9-1 Aircraft Classification Number -- Flexible Pavement, A/C CodeC, for an aircraft gross weight of 55 000 kg (121 250 lb) and low subgrade strength (code C), theACN for the flexible pavement is 29.9.

In the example shown in Section 7-9-2 Aircraft Classification Number -- Rigid Pavement, A/C CodeC, for an aircraft gross weight of 55 000 kg (121 250 lb) and medium subgrade strength (code B),the ACN for the rigid pavement is 30.8.

NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref.: ICAO Aerodrome Design Manual Part 3, Chapter 1, Second Edition 1983).

7-9-0Page 1

May 01/11


7-9-1 Aircraft Classification Number - Flexible Pavement

**ON A/C A319-100

Aircraft Classification Number - Flexible Pavement

1. This section gives the Aircraft Classification Number - Flexible Pavement.


7-9-1Page 1

May 01/11


**ON A/C A319-100

15202530354045

65

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

9 %

MA

C.

ON

PA

VE

ME

NT

− A

/C C

OD

E C

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

AIRCRAFT CLASSIFICATION NUMBER (ACN)

6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

N_AC_070901_1_0510101_01_00

A/C

CO

DE

C

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

Aircraft Classification Number -- Flexible PavementFIGURE 1

7-9-1Page 2

May 01/11


**ON A/C A319-100

15202530354045

65

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

ON

PA

VE

ME

NT

− A

/C C

OD

E D

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)


SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

D

N_AC_070901_1_0520101_01_00


7-9-1Page 3

May 01/11


**ON A/C A319-100

15202530354045

65

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

E

ON

PA

VE

ME

NT

− A

/C C

OD

E E

N_AC_070901_1_0530101_01_00


7-9-1Page 4

May 01/11


**ON A/C A319-100

15202530354045

65

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

9 %

MA

C.


SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

A/C

CO

DE

F

ALP

HA

FA

CT

OR

= 0

.9

N_AC_070901_1_0540101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E F


7-9-1Page 5

May 01/11


**ON A/C A319-100

15202530354045

65

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

9 %

MA

C.


SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

A/C

CO

DE

G

ALP

HA

FA

CT

OR

= 0

.9

N_AC_070901_1_0550101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E G


7-9-1Page 6

May 01/11


**ON A/C A319-100

15202530354045

65

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

A/C

CO

DE

H

ALP

HA

FA

CT

OR

= 0

.9

N_AC_070901_1_0560101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E H


7-9-1Page 7

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

8.8

% M

AC

.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

I

65

148

152

N_AC_070901_1_0570101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E I


7-9-1Page 8

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

J

65

148

152

N_AC_070901_1_0580101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E J


7-9-1Page 9

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

8.8

% M

AC

.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

K

65

148

152

N_AC_070901_1_0590101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E K


7-9-1Page 10

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

L

65

148

152

N_AC_070901_1_0600101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E L


7-9-1Page 11

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

M

65

148

152

N_AC_070901_1_0610101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E M


7-9-1Page 12

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

8.1

% M

AC

.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

152

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

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= 0

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A/C

CO

DE

N

50

N_AC_070901_1_0620101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E N


7-9-1Page 13

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

152

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

O

50

N_AC_070901_1_0630101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E O


7-9-1Page 14

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

8.1

% M

AC

.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

152

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

P

50

N_AC_070901_1_0640101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E P


7-9-1Page 15

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

50

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

157

161

165

152 A

/C C

OD

E Q

75

N_AC_070901_1_0650101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E Q


7-9-1Page 16

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

7.5

% M

AC

.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

50

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

157

161

165

152 A

/C C

OD

E R

75

N_AC_070901_1_0660101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E R


7-9-1Page 17

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

50

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

157

161

165

152 A

/C C

OD

E S

75

N_AC_070901_1_0670101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E S


7-9-1Page 18

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

50

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R 3

(U

LTR

A L

OW

)C

− C

BR

6 (

LOW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

.9

157

161

165

152 A

/C C

OD

E T

75

N_AC_070901_1_0680101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E T


7-9-1Page 19

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

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CG

US

ED

FO

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CN

CA

LCU

LAT

ION

S: 3

7.5

% M

AC

.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

50

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

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(U

LTR

A L

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− C

BR

6 (

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− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

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157

161

165

152 A

/C C

OD

E U

75

N_AC_070901_1_0690101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E U


7-9-1Page 20

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

4 ba

r (1

94 p

si)

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

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US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6.52

% M

AC

.


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

50

SU

BG

RA

DE

ST

RE

NG

TH

D −

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− C

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6 (

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10

(ME

DIU

M)

A −

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R 1

5 (H

IGH

)

ALP

HA

FA

CT

OR

= 0

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157

161

165

152 A

/C C

OD

E V

75

N_AC_070901_1_0700101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E V


7-9-1Page 21

May 01/11


**ON A/C A319-100

7065

6055

5045

4035

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

751520253035404550


46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

4 ba

r (1

94 p

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AC

N W

AS

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INE

D A

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CE

D IN

ICA

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DIN

G G

EA

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DIN

G

7782

8690

9599

104

108

112

(x 1

000

lb)

C −

CB

R

6 (L

OW

)B

− C

BR

10

(ME

DIU

M)

A −

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R 1

5 (H

IGH

)

SU

BG

RA

DE

ST

RE

NG

TH

D −

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R

3 (U

LTR

A L

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)

ALP

HA

FA

CT

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= 0

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117

121

126

130

134

139

143

148

152

157

161

165

N_AC_070901_1_0710101_01_00

A/C

CO

DE

W

ON

PA

VE

ME

NT

− A

/C C

OD

E W


7-9-1Page 22

May 01/11


**ON A/C A319-100

1520253035404550


46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

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OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

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R 1

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CO

ND

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ITIO

N 1

983.

CG

US

ED

FO

R A

CN

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LCU

LAT

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S: 3

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SE

E S

EC

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N 7

−4−

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7782

8690

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104

108

112

(x 1

000

lb)

117

121

126

130

134

139

143

148

152

157

161

165

7065

6055

5045

4035

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

75

55

80

170

174

ALP

HA

FA

CT

OR

= 0

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A/C

CO

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X

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R

6 (L

OW

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− C

BR

10

(ME

DIU

M)

A −

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R 1

5 (H

IGH

)

SU

BG

RA

DE

ST

RE

NG

TH

D −

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R

3 (U

LTR

A L

OW

)

ON

PA

VE

ME

NT

− A

/C C

OD

E X

N_AC_070901_1_0720101_01_00


7-9-1Page 23

May 01/11


**ON A/C A319-100

1520253035404550


46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

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ME

DE

SIG

N M

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983.

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FO

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CN

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E S

EC

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N 7

−4−

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ING

GE

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LO

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7782

8690

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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

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kg)

75

55

80

170

174

ALP

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N_AC_070901_1_0730101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E Y


7-9-1Page 24

May 01/11


**ON A/C A319-100

1520253035404550


46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

7782

8690

9599

104

108

112

(x 1

000

lb)

117

121

126

130

134

139

143

148

152

157

161

165

7065

6055

5045

4035

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

75

55

80

170

174

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

Z

C −

CB

R

6 (L

OW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R

3 (U

LTR

A L

OW

)

N_AC_070901_1_0740101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E Z


7-9-1Page 25

May 01/11


**ON A/C A319-100

1520253035404550


46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

7782

8690

9599

104

108

112

(x 1

000

lb)

117

121

126

130

134

139

143

148

152

157

161

165

7065

6055

5045

4035

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

75

55

80

170

174

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

AA

C −

CB

R

6 (L

OW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R

3 (U

LTR

A L

OW

)

N_AC_070901_1_0750101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E A

A


7-9-1Page 26

May 01/11


**ON A/C A319-100

1520253035404550


46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

7782

8690

9599

104

108

112

(x 1

000

lb)

117

121

126

130

134

139

143

148

152

157

161

165

7065

6055

5045

4035

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

75

55

80

170

174

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

AB

C −

CB

R

6 (L

OW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R

3 (U

LTR

A L

OW

)

N_AC_070901_1_0760101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E A

B


7-9-1Page 27

May 01/11


**ON A/C A319-100

1520253035404550


46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

7782

8690

9599

104

108

112

(x 1

000

lb)

117

121

126

130

134

139

143

148

152

157

161

165

7065

6055

5045

4035

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

75

55

80

170

174

ALP

HA

FA

CT

OR

= 0

.9

A/C

CO

DE

AC

C −

CB

R

6 (L

OW

)B

− C

BR

10

(ME

DIU

M)

A −

CB

R 1

5 (H

IGH

)

SU

BG

RA

DE

ST

RE

NG

TH

D −

CB

R

3 (U

LTR

A L

OW

)

N_AC_070901_1_0770101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E A

C


7-9-1Page 28

May 01/11


7-9-2 Aircraft Classification Number - Rigid Pavement

**ON A/C A319-100

Aircraft Classification Number - Rigid Pavement

1. This section gives the Aircraft Classification Number - Rigid Pavement.


7-9-2Page 1

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

9 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

A/C

CO

DE

C

N_AC_070902_1_0500101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E C

Aircraft Classification Number -- Rigid PavementFIGURE 1

7-9-2Page 2

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

A/C

CO

DE

D

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0510101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E D


7-9-2Page 3

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

A/C

CO

DE

E

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0520101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E E


7-9-2Page 4

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

9 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

A/C

CO

DE

F

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0530101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E F


7-9-2Page 5

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

9 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

A/C

CO

DE

G

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0540101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E G


7-9-2Page 6

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

11.

9 ba

r (1

73 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

A/C

CO

DE

H

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

ON

PA

VE

ME

NT

− A

/C C

OD

E H

N_AC_070902_1_0550101_01_00


7-9-2Page 7

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

8.8

% M

AC

.S

EE

SE

CT

ION

7−

4−1

LAN

DIN

G G

EA

R L

OA

DIN

G46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152 70

A/C

CO

DE

I

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0560101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E I


7-9-2Page 8

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152 70

A/C

CO

DE

J

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0570101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E J


7-9-2Page 9

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

8.8

% M

AC

.S

EE

SE

CT

ION

7−

4−1

LAN

DIN

G G

EA

R L

OA

DIN

G46

x 1

7 R

20 (

46 x

16−

20)

TIR

ES

TIR

E P

RE

SS

UR

E C

ON

ST

AN

T A

T 1

2.5

bar

(181

psi

)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152 70

A/C

CO

DE

K

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0580101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E K


7-9-2Page 10

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

ICA

O A

ER

OD

RO

ME

DE

SIG

N M

AN

UA

L P

AR

T 3

CH

AP

TE

R 1

SE

CO

ND

ED

ITIO

N 1

983.

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

25 20 1535


AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

kg)

(x 1

000

lb)

3035

77

4045

5055

6065

404582

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152 70

A/C

CO

DE

L

C −

K =

40

MN

/m³

(LO

W)

B −

K =

80

MN

/m³

(M

ED

IUM

)A

− K

= 1

50 M

N/m

³ (

HIG

H)

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)S

UB

GR

AD

E S

TR

EN

GT

H

N_AC_070902_1_0590101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E L


7-9-2Page 11

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E M


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3 A/C

CO

DE

M

65

148

152

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)

N_AC_070902_1_0600101_01_00

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 36

% M

AC

.


7-9-2Page 12

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3 A/C

CO

DE

N

65

148

152

N_AC_070902_1_0610101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E N

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 38.

1 %

MA

C.

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)


7-9-2Page 13

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3 A/C

CO

DE

O

65

148

152

N_AC_070902_1_0620101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E O

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 36

% M

AC

.

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)


7-9-2Page 14

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3 A/C

CO

DE

P

65

148

152

N_AC_070902_1_0630101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

5 ba

r (1

81 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E P

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 38.

1 %

MA

C.

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)


7-9-2Page 15

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

5015

716

116

515

2 A/C

CO

DE

Q

75

N_AC_070902_1_0640101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E Q

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 36

% M

AC

.


7-9-2Page 16

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

5015

716

116

515

2 A/C

CO

DE

R

75

N_AC_070902_1_0650101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E R

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 37.

5 %

MA

C.


7-9-2Page 17

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

5015

716

116

515

2 A/C

CO

DE

S

75

N_AC_070902_1_0660101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E S

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 36

% M

AC

.


7-9-2Page 18

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

5015

716

116

515

2 A/C

CO

DE

T

75

N_AC_070902_1_0670101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E T

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 36

% M

AC

.


7-9-2Page 19

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

5015

716

116

515

2 A/C

CO

DE

U

75

N_AC_070902_1_0680101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

12.

9 ba

r (1

87 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E U

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 37.

5 %

MA

C.


7-9-2Page 20

May 01/11


**ON A/C A319-100

15202530354045

70

(x 1

000

kg)

AIR

CR

AF

T G

RO

SS

WE

IGH

T

(x 1

000

lb)


6055

5045

403577

8286

9095

9910

410

811

211

712

112

613

013

413

914

3

65

148

5015

716

116

515

2 A/C

CO

DE

V

75

N_AC_070902_1_0690101_01_00

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

4 ba

r (1

94 p

si)

ON

PA

VE

ME

NT

− A

/C C

OD

E V

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m³

(U

LTR

A L

OW

)C

− K

=

40 M

N/m

³ (

LOW

)B

− K

=

80 M

N/m

³ (

ME

DIU

M)

A −

K =

150

MN

/m³

(H

IGH

)

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.C

G U

SE

D F

OR

AC

N C

ALC

ULA

TIO

NS

: 36.

52 %

MA

C.


7-9-2Page 21

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6.52

% M

AC

.

1520253035404550

3540

4550

5560

6570

75

AIR

CR

AF

T G

RO

SS

WE

IGH

T

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

4 ba

r (1

94 p

si)

(x 1

000

kg)

(x 1

000

lb)


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)

7782

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152

157

161

165

A/C

CO

DE

W

N_AC_070902_1_0700101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E W


7-9-2Page 22

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

1520253035404550

3540

4550

5560

6570

75

AIR

CR

AF

T G

RO

SS

WE

IGH

T

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

(x 1

000

kg)

(x 1

000

lb)


7782

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152

157

161

174

165

170

A/C

CO

DE

X

55

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m

(ULT

RA

LO

W)

A −

K =

150

MN

/m

(HIG

H)

B −

K =

80

MN

/m

(ME

DIU

M)

C −

K =

40

MN

/m

(LO

W)

80

N_AC_070902_1_0710101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E X


7-9-2Page 23

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

1520253035404550

3540

4550

5560

6570

75

AIR

CR

AF

T G

RO

SS

WE

IGH

T

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

(x 1

000

kg)

(x 1

000

lb)


7782

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152

157

161

174

165

170

A/C

CO

DE

Y

55

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m

(ULT

RA

LO

W)

A −

K =

150

MN

/m

(HIG

H)

B −

K =

80

MN

/m

(ME

DIU

M)

C −

K =

40

MN

/m

(LO

W)

80

N_AC_070902_1_0720101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E Y


7-9-2Page 24

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

1520253035404550

3540

4550

5560

6570

75

AIR

CR

AF

T G

RO

SS

WE

IGH

T

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

(x 1

000

kg)

(x 1

000

lb)


7782

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152

157

161

174

165

170

A/C

CO

DE

Z

55

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m

(ULT

RA

LO

W)

A −

K =

150

MN

/m

(HIG

H)

B −

K =

80

MN

/m

(ME

DIU

M)

C −

K =

40

MN

/m

(LO

W)

80

N_AC_070902_1_0730101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E Z


7-9-2Page 25

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

1520253035404550

3540

4550

5560

6570

75

AIR

CR

AF

T G

RO

SS

WE

IGH

T

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

(x 1

000

kg)

(x 1

000

lb)


7782

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152

157

161

174

165

170

A/C

CO

DE

AA

55

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m

(ULT

RA

LO

W)

A −

K =

150

MN

/m

(HIG

H)

B −

K =

80

MN

/m

(ME

DIU

M)

C −

K =

40

MN

/m

(LO

W)

80

N_AC_070902_1_0740101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E A

A


7-9-2Page 26

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

1520253035404550

3540

4550

5560

6570

75

AIR

CR

AF

T G

RO

SS

WE

IGH

T

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

(x 1

000

kg)

(x 1

000

lb)


7782

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152

157

161

174

165

170

A/C

CO

DE

AB

55

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m

(ULT

RA

LO

W)

A −

K =

150

MN

/m

(HIG

H)

B −

K =

80

MN

/m

(ME

DIU

M)

C −

K =

40

MN

/m

(LO

W)

80

N_AC_070902_1_0750101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E A

B


7-9-2Page 27

May 01/11


**ON A/C A319-100

AC

N W

AS

DE

TE

RM

INE

D A

S R

EF

ER

EN

CE

D IN

IC

AO

AE

RO

DR

OM

E D

ES

IGN

MA

NU

AL

PA

RT

3C

HA

PT

ER

1 S

EC

ON

D E

DIT

ION

198

3.

SE

E S

EC

TIO

N 7

−4−

1 LA

ND

ING

GE

AR

LO

AD

ING

CG

US

ED

FO

R A

CN

CA

LCU

LAT

ION

S: 3

6 %

MA

C.

1520253035404550

3540

4550

5560

6570

75

AIR

CR

AF

T G

RO

SS

WE

IGH

T

46 x

17

R20

(46

x 1

6−20

) T

IRE

ST

IRE

PR

ES

SU

RE

CO

NS

TA

NT

AT

13.

8 ba

r (2

00 p

si)

(x 1

000

kg)

(x 1

000

lb)


7782

8690

9599

104

108

112

117

121

126

130

134

139

143

148

152

157

161

174

165

170

A/C

CO

DE

AC

55

SU

BG

RA

DE

ST

RE

NG

TH

D −

K =

20

MN

/m

(ULT

RA

LO

W)

A −

K =

150

MN

/m

(HIG

H)

B −

K =

80

MN

/m

(ME

DIU

M)

C −

K =

40

MN

/m

(LO

W)

80

N_AC_070902_1_0770101_01_00

ON

PA

VE

ME

NT

− A

/C C

OD

E A

C


7-9-2Page 28

May 01/11


DERIVATIVE AIRPLANES

8-1-0 Possible Future Derivative Airplane

**ON A/C A319-100

Possible Future Derivative Airplane

1. General

Derivative versions of the A319 are planned. All product line airplanes are studied for possible sizechanges that might be required for fulfilling future airline needs. History has proved that derivativeairplanes of a given model can encompass both increases and decreases in linear dimensions andweight.

8-1-0Page 1

May 01/11


SCALED DRAWINGS

9-1-0 Scaled Drawings

**ON A/C A319-100

Scaled Drawings

1. This section gives scaled drawings of the aircraft.

9-1-0Page 1

May 01/11


**ON A/C A319-100

WHEN PRINTING, MAKE SURE TO ADJUST FOR PROPER SCALING.NOTE:

N_AC_090100_1_0030101_01_03

0 10 20 30 40 50FEET

0 5 10 15METERS

010

2030

4050

FE

ET

05

1015

ME

TE

RS H²O

X

P

X

CMLG

F1

NLG

X

E

C

X

A

L

H²O

MLG

AIR CONDITIONINGA

CARGO COMPT DOORC

ELECTRICAL

LAVATORY

MAIN LANDING GEARMLG

PNEUMATICP

PASSENGER/CREW DOORX

E

L

FUEL (COUPLING)F1 NOSE LANDING GEARNLG

LEGEND:

FUEL (GRAVITY)

POTABLE WATER

F2

H²O

F1

F2F2

Scaled DrawingFIGURE 1

9-1-0Page 2

May 01/11


**ON A/C A319-100

WHEN PRINTING, MAKE SURE TO ADJUST FOR PROPER SCALING.NOTE:

0 10 20 30 40 50FEET

0 5 10 15METERS

010

2030

4050

FE

ET

05

1015

ME

TE

RS

N_AC_090100_1_0040101_01_03

Scaled DrawingFIGURE 2

9-1-0Page 3

May 01/11

Airbus a319 airplane characteristics for airport planning

Documents

landing gear footprintrnote

a319 airplane characteristics

illustration addedrnote

property of airbus

r dchapter

r dsubject

airport planningacthe

blagnac cedex franceissue