@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
DESCRIPTIONS OF CHANGE
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
FIGURE Landing Gear Footprint -Landing Gear Footprint
R ILLUSTRATION REVISED
FIGURE Landing Gear Footprint -Landing Gear Footprint
R ILLUSTRATION REVISED
FIGURE Landing Gear Footprint -Landing Gear Footprint
R ILLUSTRATION REVISED
FIGURE Landing Gear Footprint -Landing Gear Footprint
N NEW ILLUSTRATION ADDEDILLUSTRATION ADDED
FIGURE Landing Gear Footprint -Landing Gear Footprint
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
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
FIGURE Maximum Pavement Loads -Maximum Pavement Loads
N ILLUSTRATION ADDED
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
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
HIGHLIGHTSPage 4
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - Landing Gear Loading onPavement
N ILLUSTRATION ADDED
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
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- Flexible Pavement Requirements
N ILLUSTRATION ADDED
Section 7-6
Subject 7-6-0
Flexible Pavement Requirements - LCNConversion
R
Subject 7-6-1
Flexible Pavement Requirements - LCNConversion
R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
HIGHLIGHTSPage 7
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
HIGHLIGHTSPage 8
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements- LCN Conversion - Flexible PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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
R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
HIGHLIGHTSPage 10
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
HIGHLIGHTSPage 11
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements(PCA) - Rigid Pavement Requirements(PCA)
N ILLUSTRATION ADDED
Section 7-8
Subject 7-8-0
Rigid Pavement Requirements - LCNConversion
R
Subject 7-8-2
Rigid Pavement Requirements - LCNConversion
R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements -LCN Conversion - Rigid PavementRequirements - LCN Conversion
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
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)
R ILLUSTRATION REVISED
Section 7-9
Subject 7-9-0
ACN/PCN Reporting System R
Subject 7-9-1
Aircraft Classification Number - FlexiblePavement
R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Flexible Pavement - Aircraft ClassificationNumber -- Flexible Pavement
N ILLUSTRATION ADDED
Subject 7-9-2
Aircraft Classification Number - RigidPavement
R NOTE AMENDEDCROSS REFERENCED DOCUMENTARYUNIT ADDED/REVISED/DELETED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number --Rigid Pavement - Aircraft ClassificationNumber -- Rigid Pavement
N ILLUSTRATION ADDED
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
L.E.C.Page 1
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CONTENT CHGCODE
LAST REVISIONDATE
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
L.E.C.Page 2
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CONTENT CHGCODE
LAST REVISIONDATE
Main Landing Gear Doors Dec 01/07
FIGURE Doors Clearances - Main Landing Gear Doors Dec 01/07
Subject 2-7-8
Radome Dec 01/07
FIGURE Doors Clearances - Radome Dec 01/07
Subject 2-7-9
APU and Nose Landing Gear Doors Dec 01/07
FIGURE Doors Clearances - APU and Nose Landing Gear Doors Dec 01/07
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
ISA Conditions Dec 01/07
FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions --CFM56 series engine
Dec 01/07
FIGURE FAR / JAR Take-off Weight Limitation - ISA Conditions --IAE V2500 series engine
Dec 01/07
Subject 3-3-2
ISA +15˚C (+59˚F) Conditions Dec 01/07
FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C(+59˚F) Conditions -- CFM56 series engine
Dec 01/07
L.E.C.Page 3
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE FAR / JAR Take-off Weight Limitation - ISA +15˚C(+59˚F) Conditions -- IAE V2500 series engine
Dec 01/07
Subject 3-4-0
FAR / JAR Landing Field Length Dec 01/07
Subject 3-4-1
ISA Conditions Dec 01/07
FIGURE FAR / JAR Landing Field Length - CFM56-5A series engine Dec 01/07
FIGURE FAR / JAR Landing Field Length - IAE V2500 series engine Dec 01/07
Subject 3-5-0
Final Approach Speed Dec 01/07
FIGURE Final Approach Speed - CFM56-5A series engine Dec 01/07
FIGURE Final Approach Speed - IAE V2500 series engine Dec 01/07
CHAPTER 4
Subject 4-1-0
General Information Dec 01/07
Subject 4-2-0
Turning Radii Dec 01/07
FIGURE Turning Radii, no Slip Angle - 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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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
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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CONTENT CHGCODE
LAST REVISIONDATE
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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CONTENT CHGCODE
LAST REVISIONDATE
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
L.E.C.Page 7
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CONTENT CHGCODE
LAST REVISIONDATE
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
L.E.C.Page 8
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CONTENT CHGCODE
LAST REVISIONDATE
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
L.E.C.Page 9
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CONTENT CHGCODE
LAST REVISIONDATE
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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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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 R May 01/11
FIGURE Landing Gear Footprint - 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
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
L.E.C.Page 11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Maximum Pavement Loads - Maximum Pavement Loads N May 01/11
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
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
FIGURE Landing Gear Loading on Pavement - Landing Gear Loadingon Pavement
N May 01/11
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
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
FIGURE Flexible Pavement Requirements - Flexible PavementRequirements
N May 01/11
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
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
L.E.C.Page 16
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
FIGURE Flexible Pavement Requirements - LCN Conversion - FlexiblePavement Requirements - LCN Conversion
N May 01/11
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)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements (PCA) - Rigid PavementRequirements (PCA)
N May 01/11
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
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
FIGURE Rigid Pavement Requirements - LCN Conversion - RigidPavement Requirements - LCN Conversion
N May 01/11
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
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Flexible Pavement - AircraftClassification Number -- Flexible Pavement
N May 01/11
Subject 7-9-2
Aircraft Classification Number - Rigid Pavement R May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
L.E.C.Page 23
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
FIGURE Aircraft Classification Number -- Rigid Pavement - AircraftClassification Number -- Rigid Pavement
N May 01/11
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
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
3-3-1 ISA Conditions
3-3-2 ISA +15˚C (+59˚F) Conditions
3-4-0 FAR / JAR Landing Field Length
3-4-1 ISA Conditions
3-5-0 Final Approach Speed
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4 GROUND MANEUVERING
4-1-0 General Information
4-2-0 Turning Radii
4-3-0 Minimum Turning Radii
4-4-0 Visibility from Cockpit in Static Position
4-5-0 Runway and Taxiway Turn Paths
4-5-1 135˚ Turn - Runway to Taxiway
4-5-2 90˚ Turn - Runway to Taxiway
4-5-3 180˚ Turn on a Runway
4-5-6 180˚ 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
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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
7-1-0 General Information
7-2-0 Landing Gear Footprint
7-3-0 Maximum Pavement Loads
7-4-0 Landing Gear Loading on Pavement
7-4-1 Landing Gear Loading on Pavement
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
7-6-0 Flexible Pavement Requirements - LCN Conversion
7-6-1 Flexible Pavement Requirements - LCN Conversion
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
7-8-0 Rigid Pavement Requirements - LCN Conversion
7-8-1 Radius of Relative Stiffness
7-8-2 Rigid Pavement Requirements - LCN Conversion
7-8-3 Radius of Relative Stiffness (Other values of E and L)
7-8-4 Radius of Relative Stiffness
7-9-0 ACN/PCN Reporting System
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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,
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- 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.
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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.
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
Aircraft CharacteristicsWV005 WV006 WV007 WV008 WV009
Kilograms 70 400 73 900 75 900 64 400 66 400Maximum Ramp Weight(MRW)Maximum Taxi Weight(MTW)
Pounds155 205 162 922 167 331 141 978 146 387
Kilograms 70 000 73 500 75 500 64 000 66 000Maximum Takeoff Weight(MTOW) Pounds 154 324 162 040 166 449 141 096 145 505
Kilograms 62 500 62 500 61 000 62 500 62 500Maximum Landing Weight(MLW) Pounds 137 789 137 789 134 482 137 789 137 789
Kilograms 58 500 58 500 57 000 58 500 58 500Maximum Zero FuelWeight (MZFW) Pounds 128 970 128 970 125 663 128 970 128 970
CFM Engines 39 725 kg (87 579 lb)Estimated OperationalEmpty Weight (OEW) IAE Engines 39 826 kg (87 801 lb)
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
Aircraft CharacteristicsWV005 WV006 WV007 WV008 WV009
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
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-3-0 Ground Clearances
**ON A/C A319-100
Ground Clearances
1. This section gives the height of various points of the aircraft, above the ground, for different aircraftconfigurations.Dimensions in the tables are approximate and will vary with tire type, 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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-4-0 Interior Arrangements
**ON A/C A319-100
Interior Arrangements
1. This section gives the standard interior arrangements configuration.
2-4-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-4-1 Passenger Compartment Layout
**ON A/C A319-100
Typical Configuration
1. This section gives the typical interior configuration.
2-4-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
156
SE
AT
S A
LL T
OU
RIS
T C
LAS
S28
/30
in P
ITC
H. 6
AB
RE
AS
T. 3
.3
FW
D P
AS
SE
NG
ER
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
AF
T P
AS
SE
NG
ER
A A
A
A
G L
G L
A
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(2)
AA
TT
EN
DA
NT
SE
AT
(5)
N_AC_020401_1_0020101_01_02
Typical ConfigurationTypical Configuration Single-Class, High Density
FIGURE 1
2-4-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
8 S
UP
ER
FIR
ST
CLA
SS
PA
SS
EN
GE
R S
EA
TS
(12
4 T
OT
AL)
SE
AT
PIT
CH
ES
:
/CR
EW
DO
OR
EM
ER
GE
NC
Y E
XIT
AF
T P
AS
SE
NG
ER
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
116
EC
ON
OM
Y C
LAS
S
FIR
ST
36
inE
CO
NO
MY
32
in
AF
T P
AS
SE
NG
ER
EM
ER
GE
NC
Y E
XIT
/CR
EW
DO
OR
FW
D P
AS
SE
NG
ER
/CR
EW
DO
OR
N_AC_020401_1_0080101_01_00
G
A AL
LG
L
A
ITE
MD
ES
IGN
AT
ION
GG
ALL
EY
(2)
LLA
VA
TO
RY
(3)
AA
TT
EN
DA
NT
SE
AT
(3)
Typical ConfigurationTypical Configuration Two-Class
FIGURE 2
2-4-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-5-0 Passenger Compartment Cross Section
**ON A/C A319-100
Passenger Compartment Cross-section
1. This section gives the typical passenger compartment cross-section configuration.
2-5-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
3.95(155.51)
Cargo CompartmentFloor
CABINFLOOR
Top of cargoCompartment
AircraftDatum
Windows
2.64
(103.94)
2.13(83.86)
1.60(62.99)
1.24(48.82)
NOTE: DIMENSIONS m (in)
0.49(19.29)
0.52(20.47)
N_AC_020500_1_0010101_01_01
3.45(135.83)
3.68
(144.88)
1.42(55.91)
Passenger Compartment Cross-sectionFIGURE 1
2-5-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE: DIMENSIONS m (in)
1.24
(48.
9)2.
21(8
7)
6 ABREAST−WIDER AISLE
4.14
(163
)
3.95(155.5)
3.64(143)
1.50(59)
0.64(25)
1.50(59)
0.432(17)
N_AC_020500_1_0050101_01_00
Passenger Compartment Cross-sectionEconomy Class, 6 Abreast - Wider Aisle (Sheet 1 of 2)
FIGURE 2
2-5-0Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE: DIMENSIONS m (in)
6 ABREAST−WIDER SEAT
3.95(155.5)
3.64(143)
1.58(62)
0.48(19)
1.58(62)
1.24
(48.
9)2.
21(8
7)
4.14
(163
)
0.457(18)
N_AC_020500_1_0050102_01_02
Passenger Compartment Cross-sectionEconomy Class, 6 Abreast - Wider Seat (Sheet 2 of 2)
FIGURE 3
2-5-0Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE: DIMENSIONS m (in)
4 ABREAST−FIRST CLASS
3.95(155.5)
1.24
(48.
9)2.
21(8
7)
4.14
(163
)
3.59(141)
0.69(27)
1.45(57)
1.45(57)
(22.6)0.57
N_AC_020500_1_0060101_01_00
Passenger Compartment Cross-sectionPassenger Compartment Cross-section, First-class
FIGURE 4
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-1 Forward Passenger / Crew Doors
**ON A/C A319-100
Forward Passenger / Crew Doors
1. This section gives forward passenger / crew doors clearances.
2-7-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
CRITICAL
CLEARANCE LIMIT
0.61 m(2 ft)
0.48 m(1 ft 6.88 in)
2.54 m(8 ft 3.99 in)
5.02 m(16 ft 5.62 in)
1.8 m(5 ft 10.8 in) 0.81 m
(2 ft 7.8 in)
1.85 m(6 ft 0.82 in)
SEECHAPTER
2.375 m(7 ft 9.48 in)
2−3
0.03 m(1.18 in)
N_AC_020701_1_0020101_01_00
Doors ClearancesForward Passenger / Crew Doors
FIGURE 1
2-7-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-2 Emergency Exits
**ON A/C A319-100
Emergency Exits
1. This section gives emergency exits doors clearances.
2-7-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE: ESCAPE SLIDE COMPARTMENT DOOROPENS ON WING UPPER SURFACE.
(FROM NOSE)12.83 m
(42 ft 1.11 in)
0.5 m
0.47 m(1ft 6.49 in)
1.23 m(4 ft 0.42 in)
0.2 m(7.87 in)
FWD
0.9 m(2 ft 11.4 in)
0.495 m(1ft 7.48 in)
(TOP OF FLOOR)
0.12 m(4.72 in)
SEESECTION
2−3
A
A
B
B
CL
(1ft 7.68 in)
0.85 m(2 ft 9.45 in)
(FRAME 47)B BA A
OPTIONAL
N_AC_020702_1_0030101_01_00
Doors ClearancesEmergency Exits
FIGURE 1
2-7-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-3 Aft Passenger / Crew Doors
**ON A/C A319-100
Aft Passenger / Crew Doors
1. This section gives Aft passenger / crew doors clearances.
2-7-3Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1.79 m(5 ft 10.46 in)
0.81 m(2 ft 7.88 in)
0.58 m(1 ft 10.8 in)
CRITICALCLEARANCE
LIMIT
25.91 m(85 ft)
(FROM NOSE)
2.44 m(8 ft)
1.85 m(6 ft 0.82 in)
0.6 m(1 ft 11.6 in)
(1.18 in)0.03 m
FWD
SEE
2−3CHAPTER
A A
A
A
N_AC_020703_1_0020101_01_00
Doors ClearancesAft Passenger / Crew Doors
FIGURE 1
2-7-3Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-4 Forward Cargo Compartment Doors
**ON A/C A319-100
Forward Cargo Compartment Door
1. This section gives forward cargo compartment door clearances.
2-7-4Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
8.16 m(26 ft 9.25 in)
1.82 m(5 ft 11.65 in)
1.24 m(4 ft 0.81 in)
3.945 m(12 ft 11.3 in)
1.495 m(4 ft 10.84 in)
0.5 m(1 ft 7.68 in)
(FROM NOSE)
2−3
SEECHAPTER
A
A
FWD
A A
2.71 m(8 ft 10.69 in)
N_AC_020704_1_0020101_01_00
Doors ClearancesForward Cargo Compartment Door
FIGURE 1
2-7-4Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-5 Aft Cargo Compartment Doors
**ON A/C A319-100
Aft Cargo Compartment Door
1. This section gives Aft cargo compartment door clearances.
2-7-5Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
20.58 m
(67ft 6.22 in)
1.82 m(5 ft 11.65 in)
(FROM NOSE)
FWD
A
A
1.6 m5 ft 2.93 in)
1.23 m(4 ft 0.42 in)
3.945 m
(12 ft 11.3 in)
1.43 m(4 ft 8.29 in)
2−3
SEECHAPTER
A A
FWD
N_AC_020705_1_0020101_01_01
Doors ClearancesAft Cargo Compartment Door
FIGURE 1
2-7-5Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-7 Main Landing Gear Doors
**ON A/C A319-100
Main Landing Gear Doors
1. This section gives the main landing gear doors clearances.
2-7-7Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE: VALUE OF CG: 25% RC.
A
GROUND LINE
0.207 m(8.14 in)
0.485 m
(1 ft 7.09 in)
AIRCRAFT
1.23 m(4 ft 0.42 in)
0.14 m(5.51 in)
84°
1.942 m
(6 ft 4.45 in)
14.758 m(48 ft 5 in)
1.826 m(5 ft 11.88 in)
1.761 m(5 ft 9.32 in)
A
N_AC_020707_1_0020101_01_02
Doors ClearancesMain Landing Gear Doors
FIGURE 1
2-7-7Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-8 Radome
**ON A/C A319-100
Radome
1. This section gives the radome clearances.
2-7-8Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
0.63 m(2 ft 0.79 in)
STA 3500FR1
65°
(5 ft 0.62 in)1.54 m
N_AC_020708_1_0020101_01_00
Doors ClearancesRadome
FIGURE 1
2-7-8Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
2-7-9 APU and Nose Landing Gear Doors
**ON A/C A319-100
APU and Nose Landing Gear Doors
1. This section gives APU and Nose Landing Gear doors clearances.
2-7-9Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
3.23
m(1
0 ft
7.16
in)
3.86
m(1
2 ft
7.96
in)
NOTE: VALUE OF CG : 25% RC.
1.5
m(4
ft 1
1 in
)
1.4
m(4
ft 7
.11
in)
FR80
FR84
N_AC_020709_1_0020101_01_00
Doors ClearancesAPU and Nose Landing Gear Doors
FIGURE 1
2-7-9Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
AIRPLANE PERFORMANCE
3-1-0 General Information
**ON A/C A319-100
General Information
1. This section gives standard day temperatures.
Section 3-2 indicates payload range information at specific altitudes recommended for long rangecruise with a given fuel reserve condition.
Section 3-3 represents FAR take-off runway length requirements at ISA and ISA +15˚C (+59˚F) forCFM56-5A, CFM56-5B and IAE V2500 series engine conditions for FAA certification.
Section 3-4 represents FAR landing runway length requirements for FAA certification.
Section 3-5 indicates final approach speeds.
Standard day temperatures for the altitudes shown are tabulated below:
Standard day temperatures for the altitude
Altitude Standard Day Temperature
FEET METERS ˚F ˚C0 0 59.0 15.02000 610 51.9 11.14000 1219 44.7 7.16000 1829 37.6 3.18000 2438 30.5 -0.8
3-1-0Page 1
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-2-0 Payload / Range
**ON A/C A319-100
Payload / Range
1. Payload / Range
3-2-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-2-1 ISA Conditions
**ON A/C A319-100
ISA Conditions
1. This section gives the payload / range at ISA conditions.
3-2-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
50 40 30 20 10 0
20 10 00
1000
2000
3000
4000
010
0020
0030
0040
0050
0060
0070
00
(100
0 lb
)(1
000
kg)
PA
YLO
AD
RA
NG
E(K
M)
RA
NG
E(N
M)
MA
X T
AK
E−
OF
F W
EIG
HT
145
504
lb(6
6 00
0 kg
)
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
124
PA
SS
EN
GE
RS
64t
75.5
t
70t
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
NO
TE
:
N_AC_030201_1_0030101_01_00
Payload / RangeCFM56-5A series engine
FIGURE 1
3-2-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
50 40 30 20 10 0
20 10 00
1000
2000
3000
4000
010
0020
0030
0040
0050
0060
0070
00
(100
0 lb
)(1
000
kg)
PA
YLO
AD
RA
NG
E(K
M)
RA
NG
E(N
M)
MA
X T
AK
E−
OF
F W
EIG
HT
145
504
lb(6
6 00
0 kg
)
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
124
PA
SS
EN
GE
RS
64t
75.5
t
70t
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
NO
TE
:
N_AC_030201_1_0040101_01_00
Payload / RangeCFM56-5B series engine
FIGURE 2
3-2-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
50 40 30 20 10 0
20 10 00
1000
2000
3000
4000
010
0020
0030
0040
0050
0060
0070
00
(100
0 lb
)(1
000
kg)
PA
YLO
AD
RA
NG
E(K
M)
RA
NG
E(N
M)
MA
X T
AK
E−
OF
F W
EIG
HT
145
504
lb(6
6 00
0 kg
)
200
NM
(37
0 K
M)
DIV
ER
SIO
N30
MIN
UT
ES
HO
LD A
T 1
500
ftA
PP
RO
AC
H A
ND
LA
ND
ING
CR
UIS
E C
ON
DIT
ION
SIS
A +
10°
M =
0.7
635
000
/39
000
ft
INT
ER
NA
TIO
NA
L R
ES
ER
VE
S :
EN
RO
UT
E 1
0% F
LIG
HT
TIM
EO
VE
RS
HO
OT
124
PA
SS
EN
GE
RS
64t
75.5
t
70t
TH
ES
E C
UR
VE
S A
RE
GIV
EN
FO
R IN
FO
RM
AT
ION
ON
LYT
HE
AP
PR
OV
ED
VA
LUE
AR
E S
TA
TE
D IN
TH
E "
OP
ER
AT
ING
MA
NU
ALS
" S
PE
CIF
IC T
O T
HE
AIR
LIN
E O
PE
RA
TIN
G T
HE
AIR
CR
AF
T.
NO
TE
:
N_AC_030201_1_0050101_01_00
Payload / RangeIAE V2500-A5 series engine
FIGURE 3
3-2-1Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-3-0 FAR / JAR Takeoff Weight Limitation
**ON A/C A319-100
FAR / JAR Take-off Weight Limitation
1. FAR / JAR Take-off Weight Limitation
3-3-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-3-1 ISA Conditions
**ON A/C A319-100
ISA Conditions
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
86420
N_AC_030301_1_0030101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA Conditions -- CFM56 series engine
FIGURE 1
3-3-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
0
86
24
N_AC_030301_1_0040101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA Conditions -- IAE V2500 series engine
FIGURE 2
3-3-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-3-2 ISA +15˚C (+59˚F) Conditions
**ON A/C A319-100
ISA +15˚C (+59˚F) Conditions
1. This section gives the take-off weight limitation at ISA +15˚C (+59˚F) conditions.
3-3-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
0
8642
N_AC_030302_1_0030101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- CFM56 series engine
FIGURE 1
3-3-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RUNWAY LENGTH
1000 ft
1000 m
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
AIR
PO
RT
PR
ES
SU
RE
ALT
ITU
DE
(10
00 ft
)
110
120
130
140
150
160
170
180
190
200
210
220
230
110
100
90
80
70
60
50
40
1 2 3
4 6 8 10 12 14
4 5
16
0
86
24
N_AC_030302_1_0040101_01_00
1000 kg
TA
KE
−O
FF
WE
IGH
T
1000 lb
FAR / JAR Take-off Weight LimitationISA +15˚C (+59˚F) Conditions -- IAE V2500 series engine
FIGURE 2
3-3-2Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-4-0 FAR / JAR Landing Field Length
**ON A/C A319-100
FAR / JAR Landing Field Length
1. FAR / JAR Landing Field Length
3-4-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-4-1 ISA Conditions
**ON A/C A319-100
ISA Conditions
1. This section gives the landing field length.
3-4-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
3.0
3.5
4.0
4.5
5.0
5.5
6.0
160140120100806040GROSS WEIGHT
(1000 lb)
F.A
.R L
AN
DIN
G L
EN
GT
H (
1000
ft)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
ISA CONDITIONSSLATS 27 DEG.FLAPS 35 DEG.
PRESSURE ALTITUDE(1000 ft)
10
6
SEA
4 2
8
LEVEL
N_AC_030401_1_0030101_01_00
FAR / JAR Landing Field LengthCFM56-5A series engine
FIGURE 1
3-4-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
5.5
5.0
4.5
4.0
3.5
3.0160
GROSS WEIGHT(1000 lb)140120100806040
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
10 8 6 4 2SEA
PRESSURE ALTITUDE(1000 ft)
ISA CONDITIONSSLATS 27 DEG.FLAPS 35 DEG.
LEVEL
N_AC_030401_1_0040101_01_00
F.A
.R L
AN
DIN
G L
EN
GT
H (
1000
ft)
FAR / JAR Landing Field LengthIAE V2500 series engine
FIGURE 2
3-4-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
3-5-0 Final Approach Speed
**ON A/C A319-100
Final Approach Speed
1. This section gives the final approach speed.
3-5-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
20018016014012010080100
110
120
130
140
150
160
170
C.A.S. (Kts)
GROSS WEIGHT(1000 lb)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 35DEG.
SEA LEVEL
N_AC_030500_1_0030101_01_00
Final Approach SpeedCFM56-5A series engine
FIGURE 1
3-5-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
20018016014012010080100
110
120
130
140
150
160
170
C.A.S. (Kts)
GROSS WEIGHT(1000 lb)
THESE CURVES ARE GIVEN FOR INFORMATION ONLYTHE APPROVED VALUES ARE STATED IN THE "OPERATINGMANUALS" SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
NOTE:
LANDING GEAR EXTENDEDSLATS 27 DEG.FLAPS 35 DEG.
SEA LEVEL
N_AC_030500_1_0040101_01_00
Final Approach SpeedIAE V2500 series engine
FIGURE 2
3-5-0Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A319-100
General Information
1. This section provides airplane turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.
In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the using airlines prior to layout planning.
4-1-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-3-0 Minimum Turning Radii
**ON A/C A319-100
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A319-100
Visibility from Cockpit in Static Position
1. This section gives the visibility from cockpit in static position.
4-4-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A319-100
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths.
4-5-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A319-100
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn - runway to taxiway.
4-5-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A319-100
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn - runway to taxiway.
4-5-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-5-3 180˚ Turn on a Runway
**ON A/C A319-100
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
4-6-0 Runway Holding Bay (Apron)
**ON A/C A319-100
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
4-6-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RUNWAY WIDTH 60.00 m
ED
GE
OF
RU
NW
AY
29.3
5 m
(REF)
18.3
1 m
END OF RUNWAY
NOTE:
3.05
m(R
EF
)
69° STEERING AND NO SLIP ON NLG TIRES.
(10.
0 ft)
(96
ft 3.
6 in
)
(60.
0 ft)
(196 ft 10.8 in)
3.05 m(10.0 ft)
N_AC_040700_1_0090101_01_01
Runway Length AlterationsLine Up Distances -- 90˚ Turn
FIGURE 1
4-7-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
END OF RUNWAY
EDGE OFRUNWAY
27.41 m(90.0 ft)
16.60 m(54 ft 6 in)
3.05 m(10.0 ft)(REF)3.05 m
(10.0 ft)
NOTES: 69° STEERING AND NO SLIP ON NLG TIRES.
32.62 m(107.0 ft)
21.58 m(70 ft 9.6 in)
(REF)
3.05 m(10.0 ft)(REF)
N_AC_040700_1_0100101_01_01
Runway Length AlterationsLine Up Distances -- 180˚ Turn
FIGURE 2
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
TERMINAL SERVICING
5-0-0 TERMINAL SERVICING
**ON A/C A319-100
Terminal Servicing
1. GeneralThis chapter provides typical ramp layouts, corresponding minimum turnaround time estimations,locations of ground service points and service requirements.The information given in this chapter reflects ideal conditions. Actual ramp layouts and servicerequirements may vary according to local regulations, airline procedures and the airplane condition.- Section 5.1 shows typical ramp layouts for passenger aircraft at the gate or on an open apron.- Section 5.2 shows the minimum turnaround schedules for full servicing arrangements.- Section 5.3 shows the minimum turnaround schedule for reduced servicing arrangements.- Section 5.4 gives the locations of ground service connections, the standard of connections used
and typical capacities and requirements.- Section 5.5 provides the engine starting pneumatic requirements for different engine types and
different ambient temperatures.- Section 5.6 provides the air conditioning requirements for heating and cooling (pull-down and
pull-up) using ground conditioned air for different ambient temperatures.- Section 5.7 provides the air conditioning requirements for heating and cooling to maintain a
constant cabin air temperature using low pressure conditioned air.- Section 5.8 shows the ground towing requirements taking into account different ground surface
and aircraft conditions.
5-0-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-1-1 Symbols Used on Servicing Diagrams
**ON A/C A319-100
Symbols Used on Servicing Diagrams
1. This table gives the symbols used on servicing diagrams.
Ground Support Equipment
AC AIR CONDITIONING UNITAS AIR STARTING UNITBULK BULK TRAINCAT CATERING TRUCKCB CONVEYOR BELTCLEAN CLEANING TRUCKFUEL FUEL HYDRANT DISPENSER or TANKERGPU GROUND POWER UNITLD CL LOWER DECK CARGO LOADERLV LAVATORY VEHICLEPBB PASSENGER BOARDING BRIDGEPS PASSENGER STAIRSTOW TOW TRACTORULD ULD TRAINWV POTABLE WATER VEHICLE
5-1-1Page 1
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
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May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-1 Ground Service Connections Layout
**ON A/C A319-100
Ground Service Connections Layout
1. This section gives the ground service connections layout.
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-2 Grounding Points
**ON A/C A319-100
Grounding Points
1. Grounding Points.
DISTANCE: Meters (ft)
FROM AIRPLANE CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM
GROUNDOn Nose Landing Gearleg:
5.07 m(16.63 ft) on centerline
0.94 m(3.08 ft)
On left Main LandingGear leg:
16.11 m(52.85 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
On right Main LandingGear leg:
16.11 m(52.85 ft)
3.79 m(12.43 ft)
1.07 m(3.51 ft)
A. The grounding stud on each landing gear leg is designed for use with a clip-on connector (suchas Appleton TGR).
B. The grounding studs are used to connect the aircraft to an approved ground connection on theramp or in the hangar for:- refuel/defuel operations,- maintenance operations,- bad weather conditions.
NOTE : In all other conditions, the electrostatic discharge through the tyre is sufficient.
5-4-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
(2)(1)
GROUND CABLE(OPTIONAL)
LANDINGGEAR
NOSE LANDING GEAR
MAIN LANDING GEAR
(1)
A
A
A
(1)
N_AC_050402_1_0030101_01_00
Ground Service ConnectionsGrounding Points
FIGURE 1
5-4-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE: R SIDE SYMMETRICAL
A
RIB20
RIB19
B
FWD
A
A
FOR SPECIFICATIONS REFERTO FLIGHT MANUAL
BN_AC_050402_1_0040101_01_00
Ground Service ConnectionsGrounding Points
FIGURE 2
5-4-2Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-3 Hydraulic System
**ON A/C A319-100
Hydraulic System
1. Access.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green System:Access door 197CB
17.57(57.64)
1.27(4.17)
1.76(5.77)
Yellow System:Access door 198CB
17.57(57.64)
1.27(4.17)
1.76(5.77)
Blue System:Access door 197EB
18.92(60.07)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.
2. Reservoir Pressurization.On the air pressurization manifold:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Access door 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:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Yellow Systemaccumulator:Access door 196BB
14.5(47.57)
0.25(0.82)
1.99(6.53)
5-4-3Page 1
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Green Systemaccumulator:Left MLG door
15.67(51.41)
0.25(0.82)
3.2(10.5)
Blue Systemaccumulator:Access door 195BB
14.31(46.95)
0.25(0.82)
1.99(6.53)
Yellow System brakingaccumulator:Access door 196BB
14.5(47.57)
0.76(2.49)
1.74(5.71)
NOTE : Distances are approximate.
4. Reservoir Filling.On the Green system ground service panel:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Access door 197CB17.57(57.64)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.One 1/4 in. AEROQUIP AE96993E self-sealing connection for pressurized supply.One handpump filling connection for unpressurized (suction) supply.
5. Reservoir Drain.On 3/8 in. self-sealing connection on reservoir for:
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Yellow System:Access door 196BB -198CB
14.5(47.57)
1.43(4.69)
1.90(6.23)
Green System:Left MLG door
15.67(51.41)
1.27(4.17)
2.61(8.56)
5-4-3Page 2
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Blue System:Access door 197EB
18.92(62.07)
1.27(4.17)
1.76(5.77)
NOTE : Distances are approximate.On 3/8 in. self-sealing connection for the Blue system on:- Blue system ground service panel.
6. Ground Test.On each ground service panel:- One self-sealing connector AE80532N (suction).- One self-sealing connector AE80531K (delivery).
5-4-3Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RESERVOIR FILL SYSTEMHAND PUMP FILL CONNECTION
GROUND TESTPRESSURE
CONNECTION
GROUND TESTSUCTION
CONNECTIONRESERVOIR FILLCONNECTION
AE96993GM
GROUND SUPPLY
AE80531K AE80532N
1698GM
1008GM 1007GM 1006GM
197CB
A
AN_AC_050403_1_0040101_01_00
Hydraulic SystemGreen System Ground Service Panel
FIGURE 1
5-4-3Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
GROUND CONNECTIONSUCTION
GROUNDCONNECTION
DELIVERY
AE80531K
AE80532N
2006GM
2008GM
A
Z197
A
N_AC_050403_1_0050101_01_00
Hydraulic SystemBlue System Ground Service Panel
FIGURE 2
5-4-3Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
GROUND TESTPRESSURE CONNECTION
GROUND TESTSUCTION CONNECTION
AE80531K AE80532N
A
A
3008GM 3006GM
198CB
N_AC_050403_1_0060101_01_00
Hydraulic SystemYellow System Ground Service Panel
FIGURE 3
5-4-3Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-4 Electrical System
**ON A/C A319-100
Electrical System
1. Electrical System.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
A/C External Power:Access door 121AL
2.55(8.37) on centerline
2(6.56)
NOTE : Distances are approximate.
2. Technical SpecificationsThis chapter gives data related to the location of the ground service connections.
A. External Power Receptacle:- One 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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-5 Oxygen System
**ON A/C A319-100
Oxygen System
1. Oxygen System.
DISTANCE: Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDOne service connection(external charging in theavionics compartment)MS22066 Std.
3.45 m(11.32 ft)
1.15 m(3.77 ft)
2.60 m(8.53 ft)
3/8” UNF × 24 TPI
Nominal pressure: 1850 psi (127.55 bar)
Max fill pressure: 2035 psi (140.31 bar)
NOTE : Internal charging connection provided.
5-4-5Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
Refuel/DefuelIntegrated Panel:Access door 192MB
14.8(48.56)
1.8(5.91)
1.8(5.91)
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)
NOTE : Distances are approximate.
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
REFUEL/DEFUELCONTROL PANEL
NOTE: STANDARD CONFIGURATION OF REFUEL/DEFUEL PANEL.
A
FUELkg x 1000
QTY
RIGHTCTRLEFT
LEFT CTR RIGHT
LVLHI
OPEN
NORM
SHUT
OPEN
NORM
SHUT
REFUEL VALVESOPEN
NORM
SHUT
BATT POWERTESTHI LVL ON
OPEN LTS NORM
MODE SELECTREFUEL
OFF
DEFUEL / XFR
kg x 1000
PRESELECTED
DEC INC
ACTUALREFUEL
CKPT END
A
N_AC_050406_1_0010101_01_00
Ground Service ConnectionsRefuel/Defuel Panel
FIGURE 1
5-4-6Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RIB15
RIB14
A
41QM
40QM
LEADINGEDGE
WING FRONTSPAR
A
N_AC_050406_1_0020101_01_00
Ground Service ConnectionsRefuel/Defuel Couplings
FIGURE 2
5-4-6Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
RIB19
RIB20
A
ADAPTER(REF ONLY)
GROUND CONNECTION(REF ONLY)
44QM
(45QM)
AFWD
N_AC_050406_1_0030101_01_00
Ground Service ConnectionsGravity Refuel Couplings
FIGURE 3
5-4-6Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-7 Pneumatic System
**ON A/C A319-100
Pneumatic System
1. High Pressure Air Connectors.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
HP ConnectorAccess door 191DB
11.38(37.34)
0.84(2.76)
1.76(5.77)
NOTE : Distances are approximate.
A. Connector- One standard 3 in. ISO TC20 connection (MS33740) for engine starting and cabin air
preconditioning (HP) installed on the left side of the belly fairing
2. Low Pressure Air Connectors.This chapter gives data related to the location of the ground service connections.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM
GROUNDm (ft)
LP ConnectorAccess door 191CB
10.85(35.6)
1.11(3.64)
1.73(5.68)
NOTE : Distances are approximate.
A. Connector:- One standard 8 in. connection (SAE AS4262 type B) for cabin air preconditioning (LP)
installed on the left side of the belly fairing
5-4-7Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-8 Potable Water System
**ON A/C A319-100
Potable Water System
1. Potable Water Ground Service Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Potable WaterGround ServicePanel:Access door 171AL:
27.5(90.22)
0.3(0.98)
2.6(8.53)
NOTE : Distances are approximate
2. Potable Water Ground Drain Panel.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) RH SIDEm (ft)
LH SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Potable WaterGround ServicePanel:Access door 133AL:
11.8(38.71)
0.15(0.49)
1.75(5.74)
NOTE : Distances are approximate
3. Technical Specifications
A. Connectors:
(1) On the potable ground service panel (Access Door 171AL)- Fill/Drain Nipple 3/4 in (ISO 17775).- One ground pressurization connector.
(2) On drain panel (Access Door 133AL)- Drain Nipple 3/4 in (ISO 17775)
B. Usable capacity:- Standard configuration - one tank:200 l (52.83 US gal)
C. Filling pressure:- 3.45 bar (50 psi).
5-4-8Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
D. Typical flow rate:- 50 l/min (13.21 US gal/min).
5-4-8Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
DRAIN CONNECTION
FILL ANDDRAIN PORT
GROUND CONNECTION
PRESSURIZATION
Z133
Z171
A
B
B
A
N_AC_050408_1_0010101_01_00
Ground Service ConnectionsPotable Water Ground Service Panel
FIGURE 1
5-4-8Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Engine Oil GravityFilling Cap:Access door: 437BL(LH),447BL (RH)
11.56(37.79)
6.63(21.75)
4.82(15.81)
1.46(4.79)
Engine Oil PressureFilling Port:
11.4(37.4)
6.49(21.29)
4.74(15.55)
1.42(4.66)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 19.6 l (5.18 US gal)- Usable: 9.46 l (2.50 US gal)
B. Maximum delivery pressure required: 25 psi (1.72 bar)Maximum delivery flow required: 180 l/h (47.55 US gal/h)
2. IDG Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-9-991-002-A):One pressure filling connection per engine: OMP 2506-18 plus one connection overflow: OMP2505-18.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
IDG Oil PressureFilling Connection:Access door 438DR(LH),448DR (RH)
10.6(34.77)
6.9(22.64)
5.52(18.11)
0.68(2.23)
NOTE : Distances are approximate
5-4-9Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
A. Tank capacity: 5 l (1.32 US gal)
B. Delivery pressure required: 5 to 40 psi (0.34 to 2.76 bar) at the IDG inlet.
3. Starter Oil Replenishment for CFM56 Series Engine (See FIGURE 5-4-9-991-003-A):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Starter Oil FillingConnection:
11.04(37.4)
5.3(17.39)
6.2(20.34)
0.76(2.49)
NOTE : Distances are approximate
A. Tank capacity: 0.8 l (0.21 US gal)
4. Engine Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-9-991-004-B):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Engine Oil GravityFilling Cap:Access door 437BL(LH),447BL (RH)
10.64(34.9)
6.56(21.52)
4.92(16.14)
1.22(4)
NOTE : Distances are approximate
A. Tank capacity:- Full level: 28 l (7.4 US gal)- Usable: 23.50 l (6.21 US gal)
1. IDG Oil Replenishment for IAE V2500 Series Engine:One pressure filling connection per engine: OMP 2506-2 plus one overflow connection: OMP 2505-2.
5-4-9Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
IDG Oil PressureFilling Connection:
11.2(36.74)
5.42(17.78)
6.04(19.81)
0.8(2.62)
NOTE : Distances are approximate
A. Tank capacity: 4.1 l (1.08 US gal)
5. Starter Oil Replenishment for IAE V2500 Series Engine (See FIGURE 5-4-9-991-006-B):One gravity filling cap per engine.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) ENGINE 1 (LH)m (ft)
ENGINE 2 (RH)m (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Starter Oil FillingConnection:
11.04(37.4)
5.3(17.39)
6.14(20.14)
0.75(2.46)
NOTE : Distances are approximate
A. Tank capacity: 0.35 l (0.09 US gal)
6. APU Oil System (See FIGURE 5-4-9-991-007-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)
NOTE : Distances are approximate
A. Tank capacity (usable):- APU type GTCP 36-300: 6.20 l (1.64 US gal)- APU type APS 3200: 5.40 l (1.43 US gal)
5-4-9Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
- APU type 131-9: 6.25 l (1.65 US gal)
5-4-9Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
ACCESS PANEL: 437BL (LEFT)447BL (RIGHT) OIL IN
VENT
OIL LEVELTRANSMITTER(OPTIONAL)
OIL CAP
SIGHT WINDOW
ANTI−SIPHONDEVICE
AIR PRESSURESWITCH NIPPLE
SELF−SEALING MAGNETICDRAIN PLUG
PRESSURE NIPPLE
OIL OUT
OIL/FUEL HEATEXCHANGER
SERVO FUELHEATER
A
A
B
FWD
B
N_AC_050409_1_0010101_01_00
Ground Service ConnectionsEngine Oil Tank -- CFM56 Series Engine
FIGURE 1
5-4-9Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
C
A
B
SIGHT GLASS
NOTE: ATHE YELLOW BAND, OIL SERVICINGIS REQUIRED.
BTHE GREEN AND YELLOW BANDS,OIL SERVICING IS NOT REQUIRED.
CTHE GREEN BAND, OIL SERVICINGIS REQUIRED.
1 − PRESSURE FILL VALVE2 − CASE DRAIN PLUG3 − DUST CAP4 − DUST CAP5 − OVERFLOW DRAIN VALVE6 − OIL LEVEL INDICATOR
(SIGHT GLASS)
1
2
34
5
6
A B
A
B
OVERFULL
ADDOIL
ADDOIL
CFM−56
IF THE OIL LEVEL IS ABOVE
IF THE OIL LEVEL IS WITHIN
IF THE OIL LEVEL IS BELOW
N_AC_050409_1_0020101_01_01
Ground Service ConnectionsIDG Oil Tank -- CFM56 Series Engine
FIGURE 2
5-4-9Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
DRAIN PORTAND MAGNETICPLUG
OVERFLOWPLUG
STARTER
OIL FILLERPLUG
A
A
N_AC_050409_1_0030101_01_02
Ground Service ConnectionsStarter Oil Tank -- CFM56 Series Engine
FIGURE 3
5-4-9Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
’FULL’ LEVEL NOTCH27.3 LT29.0 US QTS6.0 IMP GAL(WITHIN 60 MIN FROM SHUTDOWN)
NOTCH ’3’20 LT22 US QTS4.5 IMP GAL
NOTCH ’1’26 LT27 US QTS5.7 IMP GALNOTCH ’2’
23 LT24 US QTS5.1 IMP GAL
FCOC
PRISMALITELEVEL INDICATOR
OIL TANK
GRAVITYFILLER CAP
ACCESS PANEL: 437BL (LEFT)447BL (RIGHT)
B
A
A
B
FWD
N_AC_050409_1_0040201_01_00
Ground Service ConnectionsEngine Oil Tank -- IAE V2500 Series Engine
FIGURE 4
5-4-9Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
THE OIL LEVEL MUST NOT BE INTHE YELLOW BAND BUT IT CANBE IMMEDIATELY ABOVE THELOWER LIMIT OF THE YELLOWBAND BECAUSE OF THE AIRCRAFTRAMP ANGLE
DO THE IDG SERVICINGTO GET THE CORRECT IDGOIL LEVEL.
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
INCORRECTLY FILLED IDG
THE OIL LEVEL MUST NOT BEIN THE RED BAND
PERFORM IDG OIL SERVICINGTO GET THE CORRECT IDG OIL LEVEL.DO NOT USE THE OVERFLOW DRAIN HOSETO GET THE CORRECT IDG OIL LEVEL.
AT ALL TIMES(HOT OR COLD OIL/IDG)
OIL LEVEL CAN BEIN THE GREEN BAND OR THEYELLOW BAND
AFTER ENGINESHUTDOWN
CORRECTLY FILLED IDG
OIL LEVELINDICATOR
DUST CAPPRESSUREFILL HOSE
OIL LEVEL MUST BE AT OR NEARTHE LINE BETWEEN THE YELLOW BANDAND THE GREEN BAND
(HOT OIL/IDG)
PRESSUREFILL VALVE
DUST CAP
OVER FLOWDRAIN VALVE
OVER FLOWDRAIN HOSE
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
IDG
B
BB
A
B
A
B
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
OVER FULL
ADDOIL
ADDOIL
V2500
N_AC_050409_1_0050201_01_00
Ground Service ConnectionsIDG Oil Tank -- IAE V2500 Series Engine
FIGURE 5
5-4-9Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
OIL OVERFLOWPOINT
SIGHT GLASS
EXTERNAL GEARBOX
OIL FILLING POINT
ADAPTER
B
A
B
THE STARTER IS FULL WHEN THE OIL LEVELSHOWS NOT LESS THAN 3/4 FULL
ON THE SIGHT GLASS
*
PNEUMATIC STARTERA
*
N_AC_050409_1_0060201_01_00
Ground Service ConnectionsStarter Oil Tank -- IAE V2500 Series Engine
FIGURE 6
5-4-9Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
FR80
Z316Z315
FR84
GRAVITYOIL FILLER
PRESSUREFILL PORT
OVERFLOWDRAIN VALVE
A
A
OIL LEVELSIGHT GLASS
N_AC_050409_1_0070101_01_00
Ground Service ConnectionsAPU Oil Tank
FIGURE 7
5-4-9Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-4-10 Vacuum Toilet System
**ON A/C A319-100
Vacuum Toilet System
1. Vacuum Toilet System.
POSITION FROM AIRCRAFTCENTERLINE
ACCESSAFT OF NOSE
m (ft) R SIDEm (ft)
L SIDEm (ft)
MEAN HEIGHTFROM GROUND
m (ft)
Waste WaterGround ServicePanel:Access door 172AR
27.5(90.22)
0.8(2.62)
2.8(9.18)
NOTE : Distances are approximate
2. Technical Specifications
A. Connectors:- Draining: 4 in (ISO 17775).- Flushing and filling: 1 in (ISO 17775).
B. Usable waste tank capacity:- Standard configuration - on tank: 177 l (30.91 US gal).
C. Waste tank - Rinsing:- Operating pressure: 3.45 bar (50 psi).
D. Waste tank - Precharge:- 10 l (2.64 US gal).
5-4-10Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
FILL AND RINSECONNECTION
TOILET DRAINCONNECTION
FR66 FR65
A
Z172
A
N_AC_050410_1_0010101_01_00
Ground Service ConnectionsWaste Water Ground Service Panel
FIGURE 1
5-4-10Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
N_AC_050501_1_0030101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
220°C
200°C
150°C
100°C
50°C
0°C
100
90
80
70
60
50
40
30 2
Z = 8000 ftSEA LEVEL
2.5
3
4
3.5
5
6
7
6.5
5.5
4.5
ESTIMATED STARTINGTIMES UP TO IDLE
30 40 50 60 70 80 90 100 110 120
AIR FLOW REQUIRED AT GROUND CONNECTION
kg/mn
MIN. PRESSUREAT GROUND CONNECTION: 33 PSIG
RECOMMENDED PRESSURE:38 PSIG ATGROUND CONNECTION
SEA LEVEL
Z = 8000 ft
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
MAXIM
UM T
EMPERATURE L
IMIT
35s
40s
50s
60s70s
Engine Starting Pneumatic RequirementsTemperature -40˚C (-40˚F) -- CFM56 series engine
FIGURE 1
5-5-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
TIMES UP TO IDLEESTIMATED STARTING
MAXIMUM T
EMPERATURE LIMIT
30
40
50
60
70
80
90
6
5
4
3
2
0°C
50°C
100°C
150°C
200°C220°C
40 50 60 70 80 90 100 110 120
MAXIMUM DUCT PRESSURE
AIR FLOW REQUIRED AT GROUND CONNECTION
70s
75s
60s
65s
N_AC_050501_1_0040101_01_00
Engine Starting Pneumatic RequirementsTemperature -40˚C (-40˚F) -- IAE V2500 series engine
FIGURE 2
5-5-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
N_AC_050502_1_0030101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
PRESSURE: 33 PSIG ATRECOMMENDED
GROUND CONNECTION:MIN PRESSURE AT
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
22 PSIG
GROUND CONNECTION
TIMES UP TO IDLEESTIMATED STARTING
0°C
50°C
100°C
150°C
200°C
220°C
30
40
50
60
70
80
90
100
2
3
4
5
6
7
6.5
5.5
4.5
2.5
3.5
30 40 50 60 70 80 90 100 110 120
35s
40s
50s
60s
70s
Z = 8000 ft
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
MAXIM
UM T
EMPERATURE L
IMIT
AIR FLOW REQUIRED AT GROUND CONNECTION
SEA LEVEL
Z = 8000 ft
Z = 8000 ft
SEA LEVEL
Engine Starting Pneumatic RequirementsTemperature +15˚C (+59˚F) -- CFM56 series engine
FIGURE 1
5-5-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR SUPPLY PRESSUREAT GROUND CONNECTIONPSIA
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
220°C200°C
150°C
100°C
50°C
0°C
90
80
70
60
50
40
30 2
3
4
5
6
MAXIMUM DUCT PRESSUREMAXIM
UM TEMPERATURE LI
MIT
ESTIMATED STARTINGTIMES UP TO IDLE
AIR FLOW REQUIRED AT GROUND CONNECTION
40 50 60 70 80 100 110 12090 kg/mn
ABSOLUTE BARS
45s
50s
55s
60s
N_AC_050502_1_0040101_01_00
Engine Starting Pneumatic RequirementsTemperature +15˚C (+59˚F) -- IAE V2500 series engine
FIGURE 2
5-5-2Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
N_AC_050503_1_0030101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTION
PSIA ABSOLUTE BARS
30
40
50
60
70
80
90
100
2
3
4
5
6
7
2.5
3.5
4.5
5.5
6.5
30 40 50 60 70 80 90 100 110 120 kg/mn
PRESSURE: 33 PSIG ATRECOMMENDED
GROUND CONNECTION:MIN PRESSURE AT
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
22 PSIG
GROUND CONNECTION
TIMES UP TO IDLEESTIMATED STARTING
50°C
100°C
150°C
200°C220°C
AIR FLOW REQUIRED AT GROUND CONNECTION
Z = 8000 ft
SEA LEVEL
MAXIMUM DUCT PRESSURE: 60 PSIG
SEA LEVEL
Z = 8000 ft
Z = 8000 ft
SEA LEVEL
35s
40s
50s
60s
70s
MAXIM
UM T
EMPERATURE L
IMIT
Engine Starting Pneumatic RequirementsTemperature +55˚C (+131˚F) -- CFM56 series engine
FIGURE 1
5-5-3Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
N_AC_050503_1_0040101_01_00
AIR SUPPLY PRESSUREAT GROUND CONNECTION
kg/mn
PSIA ABSOLUTE BARS
AIR SUPPLY TEMPERATUREAT FUSELAGE CONNECTION
MAXIMUM T
EMPERATURE LIMIT
0°C
50°C
100°C
150°C
200°C220°C
MAXIMUM DUCT PRESSURE
30
40
50
2
3
4
570
60
80
90
6
40 50 60 70 80 90 100 110 120
AIR FLOW REQUIRED AT GROUND CONNECTION
45s
50s
55s
60s
TIMES UP TO IDLEESTIMATED STARTING
Engine Starting Pneumatic RequirementsTemperature +50˚C (+122˚F) -- IAE V2500 series engine
FIGURE 2
5-5-3Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-6-1 Heating
**ON A/C A319-100
Heating
1. This section provides the ground pneumatic power requirements heating.
5-6-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
1.28
7
1.20
1
1.11
5
1.03
0.94
4
0.85
8
0.72
2
0.68
6
0.51
5
0.60
0.42
9
1.5
1.2
1.0
0.5
3040
50T
IME
(m
in)
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
1.28
1.72
2.15
2.59
3.0
2.5
2.0
1.5
(lb/s
)
CABIN AIRFLOW
TIM
E T
O H
EA
T C
AB
IN T
O 2
1°C
(69
.8°
F O
N G
RO
UN
D)
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T −
23°
C (
−9.
4°F
)T
EM
PE
RA
TU
RE
AT
GR
OU
ND
CO
NN
EC
TIO
N: 7
0°C
(15
8°F
)E
MP
TY
CA
BIN
ELE
CT
RIC
AL
LOA
D =
270
0 W
RE
CIR
CU
LAT
ION
: ON
NO
OT
HE
R H
EA
T L
OA
D
N_AC_050601_1_0020101_01_01
Ground Pneumatic Power RequirementsHeating
FIGURE 1
5-6-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-6-2 Cooling
**ON A/C A319-100
Cooling
1. This section provides the ground pneumatic power requirements cooling.
5-6-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1.28
7
1.20
1
1.11
5
1.03
0.94
4
0.85
8
0.72
2
0.68
6
0.51
5
0.60
0.42
9
1.5
1.2
1.0
0.5
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
2030
40
TIM
E T
O C
OO
L C
AB
IN T
O 2
7°C
(80
.6°
F O
N G
RO
UN
D)
TIM
E (
min
)
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
1.28
1.72
2.15
2.59
3.0
2.5
2.0
1.5
(lb/s
)
INIT
IAL
CA
BIN
TE
MP
ER
AT
UR
E A
T 3
8°C
(10
0.4°
F)
TE
MP
ER
AT
UR
E A
T G
RO
UN
D C
ON
NE
CT
ION
: 1.5
°C
(34
.7°
F)
EM
PT
Y C
AB
INE
LEC
TR
ICA
L LO
AD
= 2
000
WS
UN
= 4
990
WR
EC
IRC
ULA
TIO
N: O
N
CABIN AIRFLOW
N_AC_050602_1_0020101_01_01
Ground Pneumatic Power RequirementsCooling
FIGURE 1
5-6-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-7-0 Preconditioned Airflow Requirements
**ON A/C A319-100
Preconditioned Airflow Requirements
1. This section gives the preconditioned airflow requirements for cabin air conditioning.
A. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 1TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 -40.4 -40.70.6 1.32 0.515 1.135 -28.5 -19.30.7 1.54 0.600 1.323 -20.1 -4.20.8 1.76 0.686 1.512 -13.9 7.00.9 1.98 0.772 1.702 -9.1 15.61.0 2.20 0.858 1.892 -5.3 22.51.1 2.43 0.944 2.081 -2.2 28.01.2 2.65 1.030 2.271 0.4 32.71.3 2.87 1.115 2.458 2.6 36.71.4 3.09 1.201 2.648 4.4 39.91.5 3.31 1.287 2.837 6.0 42.8
NOTE : Data for stabilized conditions see 5-7-0.
B. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 2TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 31.7 89.10.6 1.32 0.515 1.135 29.7 85.50.7 1.54 0.600 1.323 28.4 83.10.8 1.76 0.686 1.512 27.3 81.10.9 1.98 0.772 1.702 26.5 79.71.0 2.20 0.858 1.892 25.9 78.61.1 2.43 0.944 2.081 25.4 77.71.2 2.65 1.030 2.271 25.0 77.01.3 2.87 1.115 2.458 24.6 76.31.4 3.09 1.201 2.648 24.3 75.7
5-7-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
FRESH AIRFLOW CURVE 2TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
1.5 3.31 1.287 2.837 24.0 75.2
NOTE : Data for stabilized conditions see 5-7-0.
C. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 3TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 36.0 96.80.6 1.32 0.515 1.135 33.3 91.90.7 1.54 0.600 1.323 31.4 88.50.8 1.76 0.686 1.512 29.9 85.80.9 1.98 0.772 1.702 28.8 83.81.0 2.20 0.858 1.892 27.9 82.21.1 2.43 0.944 2.081 27.2 81.01.2 2.65 1.030 2.271 26.6 79.91.3 2.87 1.115 2.458 26.1 79.01.4 3.09 1.201 2.648 25.7 78.31.5 3.31 1.287 2.837 25.3 77.5
NOTE : Data for stabilized conditions see 5-7-0.
D. Preconditioned Airflow Requirements.
FRESH AIRFLOW CURVE 4TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
0.5 1.10 0.429 0.946 42.2 108.00.6 1.32 0.515 1.135 38.4 101.10.7 1.54 0.600 1.323 35.7 96.30.8 1.76 0.686 1.512 33.7 92.70.9 1.98 0.772 1.702 32.1 89.81.0 2.20 0.858 1.892 30.9 87.61.1 2.43 0.944 2.081 29.9 85.81.2 2.65 1.030 2.271 29.0 84.21.3 2.87 1.115 2.458 28.3 82.91.4 3.09 1.201 2.648 27.7 81.9
5-7-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
FRESH AIRFLOW CURVE 4TOTAL CABIN T FL
(kg/s) (lb/s) (kg/s) (lb/s) (˚C) (˚F)
1.5 3.31 1.287 2.837 27.2 81.0
NOTE : Data for stabilized conditions see 5-7-0.
5-7-0Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
TOTAL AIRFLOW
(kg/
s)
TOTAL AIRFLOW
CABIN AIRFLOW
1.28
7
1.20
1
1.11
5
1.03
0.94
4
0.85
8
0.72
2
0.68
6
0.51
5
0.60
1.28
1.72
2.15
2.59
3.0
2.5
2.0
1.5
(lb/s
)
0.42
9
CU
RV
E 2
, 3, 4
(°C
)IN
LET
FLO
WT
EM
PE
RA
TU
RE
(°F
)
NO
TE
:LP
GR
OU
ND
CO
NN
EC
TIO
N M
AX
IMU
M P
RE
SS
UR
E 4
0 m
b
0.5
1.0
1.2
1.5
−40
−30
−20
−10
010
2030
40
−40
−10
010
5010
0
OA
T =
−23
°C
(−
9.4°
F)
OA
T =
−30
°C
(−
22°
F)
OA
T =
−40
°C
(−
40°
F)
MA
X A
LLO
WE
D T
OT
AL
AIR
FLO
W (
2 m
bar
CA
BIN
OV
ER
PR
ES
SU
RE
)
CABIN AIRFLOW
CU
RV
E 1
: CA
BIN
AT
27°
C (
80.6
°F
)13
4 P
AS
SE
NG
ER
S, 4
CA
BIN
AT
TE
ND
AN
TS
, 3 C
RE
W M
EM
BE
RS
BR
IGH
T D
AY
SO
LAR
LO
AD
: 297
5 W
ELE
CT
RIC
AL
LOA
D =
620
0 W
RE
CIR
CU
LAT
ION
: ON
OA
T (
OU
TS
IDE
AIR
TE
MP
ER
AT
UR
E)
= 3
8°C
(10
0.4°
F)
CA
BIN
AT
21°
C (
69.8
°F
)
NO
OT
HE
R H
EA
T L
OA
D
ELE
CT
RIC
AL
LOA
D =
380
0 W
RE
CIR
CU
LAT
ION
: ON
NO
PA
SS
EN
GE
R O
R C
AB
INA
TT
EN
DA
NT
S
N_AC_050700_1_0020101_01_01
Preconditioned Airflow RequirementsFIGURE 1
5-7-0Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
5-8-0 Ground Towing Requirements
**ON A/C A319-100
Ground Towing Requirements
1. GeneralThis section provides information on aircraft towing.This aircraft is designed with means for conventional or towbarless towing.Information/procedures can be found for both in chapter 9 of the Aircraft Maintenance Manual.Status on towbarless towing equipment qualification can be found in SIL 09-002.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a tow bar attached to the nose gear leg (refer to AMM chap 9 for conditions andlimitations).One tow bar fitting is installed at the front of the leg.The main landing gears have attachment points for towing or debogging (for details, refer to chapter07 of the Aircraft Recovery Manual).
A. The first part of this section shows the chart to determine the draw bar pull and tow tractormass requirements as function of the following physical characteristics:- Aircraft weight- Number of engines at idle- Slope.The chart is based on the engine type with the highest idle thrust level.
B. The second part of this section supplies guidelines for the tow bar.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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
70
404550556065
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A319 AT 60 t, AT 1.5% SLOPE,1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (60 t)− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%)− FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL NO OF ENGINES AT IDLE = 2− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER OF ENGINES (1)− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5.0 t)− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE. THE OBTAINED X−COORDINATE IS
THE RECOMMENDED MINIMUM TRACTOR WEIGHT (8.8 t)
10
0 10 20 30 40 50 60 70 80 0 1 2 0 0.5 1.0 1.5 2.0
5
0
TOTAL TRACTION WHEEL LOAD [ t ] NO OF ENGINES SLOPE [ % ]
1 ENGINE ON1.5% SLOPE
60 tons
DRAWBAR PULL [ t ] A/C WEIGHT [ t ]
5.0
8.83
WE
T C
ON
CR
ET
E m
= 0
.57
HA
RD
SN
OW
m =
0.2
ICE m = 0.05
AT IDLE
DR
Y C
ON
CR
ET
E m
= 0
.8BREAKAWAY RESISTANCE 6%# OF ENGINES ON FOR PB: 1ENGINE THRUST 525 daN
N_AC_050800_1_0010201_01_03
Ground Towing RequirementsFIGURE 1
5-8-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A319-100
Engine Exhaust Velocities and Temperatures
1. GeneralThis section shows the estimated engine exhaust efflux velocities and temperatures contours forGround Idle, Breakaway, Maximum Takeoff conditions.
6-1-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-1 Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A319-100
Engine Exhaust Velocities Contours - Ground Idle Power
1. This section gives engine exhaust velocities contours at ground idle power.
6-1-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
40 30 20 10 0036912
mft
PLA
NA
IRP
LAN
E
V (
m/s
)
GR
OU
ND
PLA
NE
ME
TE
RS
40 30 20 10 0036912
mft
4525
2015
10
4530
2520
1510
30
N_AC_060101_1_0030101_01_00
Engine Exhaust VelocitiesGround Idle Power -- CFM56 series engine
FIGURE 1
6-1-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
VE
LOC
ITY
= ft
/s (
m/s
)
FE
ET
050
100
150
200
7590
ftm
PLA
N
ftm
100
(30)
50 (15)
30 (9)
100
(30)
50 (15)
30 (9)
15 10 5 0
60 40 20 0
15 10 5 0
60 40 20 0
N_AC_060101_1_0040101_01_00
Engine Exhaust VelocitiesGround Idle Power -- IAE V2500 series engine
FIGURE 2
6-1-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-2 Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A319-100
Engine Exhaust Temperatures Contours - Ground Idle Power
1. This section gives engine exhaust temperatures contours at ground idle power.
6-1-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
ELE
VA
TIO
N
FE
ET
050
100
150
200
250
300
350
400
015
3045
6075
9010
512
0
40 30 20 10 0036912
mft
PLA
NA
IRP
LAN
E
GR
OU
ND
PLA
NE
ME
TE
RS
40 30 20 10 0036912
mft
400
350
325
300
400
350
325
300
T (
°K
)
N_AC_060102_1_0030101_01_00
Engine Exhaust TemperaturesGround Idle Power -- CFM56 series engine
FIGURE 1
6-1-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
TE
MP
ER
AT
UR
E =
°K
FE
ET
050
100
150
200
7590
ftm
PLA
N
ftm
32531
830
830
0
325
318
300
308
15 10 5 0
60 40 20 0
15 10 5 0
60 40 20 0
N_AC_060102_1_0040101_01_00
Engine Exhaust TemperaturesGround Idle Power -- IAE V2500 series engine
FIGURE 2
6-1-2Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-5 Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A319-100
Engine Exhaust Velocities Contours - Takeoff Power
1. This section gives engine exhaust velocities contours at takeoff power.
6-1-5Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
420
390
360
330
300
270
240
210
180
150
120
9060
3000
100
200
300
400
500
700
600
800
900
1000
1100
1200
1300
1400
ME
TE
RS
FE
ET
ftm
ft
V =
40
m/s
V =
20
m/s
V =
12
m/s
V =
40
m/s
V =
20
m/s
V =
12
m/s
PLA
NA
IRP
LAN
E
ELE
VA
TIO
NG
RO
UN
D P
LAN
E
TA
KE
OF
F P
OW
ER
INC
LUD
ES
(W
OR
ST
CA
SE
)G
RO
UN
D P
LAN
EH
EA
DW
IND
(20
KT
S.)
m
42 36 30 24 18 12 6 0
140
120
100 80 60 40 200
140
120
100 80 60 40 200
42 36 30 24 18 12 6 0
N_AC_060105_1_0030101_01_00
Engine Exhaust VelocitiesTakeoff Power -- CFM56 series engine
FIGURE 1
6-1-5Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
ME
TE
RS
015
3045
60
250
300
ELE
VA
TIO
N
MA
XIM
UM
TA
KE
OF
F T
HR
US
T
FE
ET
050
100
150
200
7590
ftm
PLA
N
ftm
136
MP
H10
2 M
PH
68 M
PH
34 M
PH
20 M
PH
TO
990
ft (
301
m)
TO
575
ft (
175
m)
60
15 10 5 0
40 20 0 60
15 10 5 0
40 20 0
N_AC_060105_1_0040101_01_00
Engine Exhaust VelocitiesTakeoff Power -- IAE V2500 series engine
FIGURE 2
6-1-5Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-1-6 Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A319-100
Engine Exhaust Temperatures Contours - Takeoff Power
1. This section gives engine exhaust temperatures contours at takeoff power.
6-1-6Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
60 40 20 0
ftm
18 12 6 0E
LEV
AT
ION
GR
OU
ND
PLA
NE
2040
6080
100
120
140
160
TA
KE
OF
F P
OW
ER
INC
LUD
ES
(W
OR
ST
CA
SE
):G
RO
UN
D P
LAN
EH
EA
DW
IND
(20
KT
S.)
FE
ET
ME
TE
RS
PLA
N
T =
425
°K
T =
370
°K
T =
315
°K
T =
425
°K
T =
370
°K
T =
315
°K
AIR
PLA
NE
1020
3040
500
ftm
60 40 20 0
18 12 6 0
N_AC_060106_1_0030101_01_00
Engine Exhaust TemperaturesTakeoff Power -- CFM56 series engine
FIGURE 1
6-1-6Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
ME
TE
RS
1530
4560
250
300
ELE
VA
TIO
N
FE
ET
5010
015
020
0
7590
ftm
PLA
N
ftm
00
65°
C55
°C
45°
C35
°C
25°
C
60
15 10 5 0
40 20 060
15 10 5 0
40 20 0
N_AC_060106_1_0040101_01_00
Engine Exhaust TemperaturesTakeoff Power -- IAE V2500 series engine
FIGURE 2
6-1-6Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-2-0 Airport and Community Noise
**ON A/C A319-100
Airport and Community Noise
1. Airport and Community Noise Data
This section gives data concerning engine maintenance run-up noise to permit evaluation of possibleattenuation requirements.
6-2-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-2-1 Noise Data
**ON A/C A319-100
Noise Data
1. Noise Data for CFM56-5A series engine
A. Description of test conditions:
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 3˚C (37˚F)- Relative humidity: 66%- Atmospheric pressure: 1016 hPa- Wind speed: Negligible- No rain
2. Noise Data for CFM56-5B series engine
A. Description of test conditions:
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 22˚C (72˚F)- Relative humidity: 42%- Atmospheric pressure: 1003 hPa- Wind speed: Negligible- No rain
3. Noise Data for IAE V2500 series engine
A. Description of test conditions:
6-2-1Page 1
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@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
The arc of circle (radius = 60 m (196.85 ft)), with microphones 1.2 m (3.94 ft) high, iscentered on the position of the noise reference point.A.P.U.: off; E.C.S.: Packs off.
B. Engine parameters: 2 engines running
C. Meteorological data:
The meteorological parameters measured 1.6 m (5.25 ft) from the ground on the day of testwere as follows:- Temperature: 27˚C (81˚F)- Relative humidity: 40%- Atmospheric pressure: 1000 hPa- Wind speed: Negligible- No rain
6-2-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
112110108106104102
98969492908886848280
100
150°
135°
120°
105°
90°
75°
60°
45°
30°
15°
0°
345°
330°
315°
300°
285°
270°
255°
240°
225°
210°
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
20.8% 90%
NOISE REFERENCEPOINT
78
N_AC_060201_1_0040101_01_00
Airport and Community NoiseCFM56-5A series engine
FIGURE 1
6-2-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
8082
8486
8890
9294
96
0°10°
20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°
98100
102104
106108
110112
350°340°
330°
320°
310°
300°
290°
280°
270°
250°
240°
230°
220°
210°
NOISE REFERENCEPOINT
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
87%18.9%
260°
N_AC_060201_1_0050101_01_00
78
Airport and Community NoiseCFM56-5B series engine
FIGURE 2
6-2-1Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
11811611411211010810610410210098969492908886848280
GROUND IDLE
N1
CURVE
MAX THRUST POSSIBLEON BRAKES
25.2% 94.4%
NOISE REFERENCEPOINT
E.P.R 1.012 1.564
150°
140°
130°
120°
110°
100°
90°
80°
70°
60°
50°
40°
30°
20°10°
0°350°
340°
330°
320°
310°
300°
290°
280°
270°
210°
220°
230°
240°
250°
260°78
N_AC_060201_1_0060101_01_00
Airport and Community NoiseIAE V2500 series engine
FIGURE 3
6-2-1Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-3-0 Danger Areas of Engines
**ON A/C A319-100
Danger Areas of Engines
1. Danger Areas of the Engines.
6-3-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-3-1 Ground Idle Power
**ON A/C A319-100
Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions.
6-3-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AREA
A
B
C
D65−20
E < 20 (32)
NOT TO SCALE
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV. 1951
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPEAIRCRAFT.
LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT
BEYOND DANGER AREA
APPROX. WINDVELOCITYMPH (km/h)
210−145(338−233)
145−105(233−169)
105−65(169−105)
EXHAUST DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET HAZARDDIMENSIONS CALCULATEDON 40 ft/sec (12 m/sec)CRITICAL VELOCITYWITH A 3 ft (0.9 m)ADJUSTMENT FOR SAFETY
WIDTH72 ft (22 m)
RADIUS = 7.2 ft (2.2 m)
NO ENTRY 82 ft (25 m)AFT OF NOZZLE EXIT
3.4 ft (1 m)
TO 199 ft (61 m)
45°CLOSE ENTRY CORRIDORFOR WIND DIRECTION
B
C
D
> 90°
E
ENTRY CORRIDOREXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
INLET SUCTIONDANGER AREA
(105−32)
N_AC_060301_1_0030101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE 1
6-3-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
0.91 m(3 ft)
R = 5.79 m(19ft)
30°
TO 59 m (195 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA
EXHAUST DANGER AREA
ENTRY CORRIDOR
N_AC_060301_1_0040101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE 2
6-3-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-3-2 Takeoff Power
**ON A/C A319-100
Takeoff Power
1. This section gives danger areas of the engines at max takeoff conditions.
6-3-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AREA
A
B
C
D65−20
E < 20 (32)
NOT TO SCALE
POSSIBLE EFFECTS WITHIN DANGER ZONE BASED ON"RADIOLOGICAL DEFENSE" VOL. II, ARMED FORCES SPECIALWEAPONS PROJECT, NOV. 1951
A MAN STANDING WILL BE PICKED UP AND THROWN; AIRCRAFT WILL BECOMPLETELY DESTROYED OR DAMAGED BEYOND ECONOMICAL REPAIR:COMPLETE DESTRUCTION OF FRAME OR BRICK HOMES.
A MAN STANDING FACE−ON WILL BE PICKED UP AND THROWN; DAMAGENEARING TOTAL DESTRUCTION TO LIGHT INDUSTRIAL BUILDINGS OR RIGIDSTEEL FRAMING: CORRUGATED STEEL STRUCTURES LESS SEVERELY.MODERATE DAMAGE TO LIGHT INDUSTRIAL BUILDINGS AND TRANSPORT−TYPEAIRCRAFT.
LIGHT TO MODERATE DAMAGE TO TRANSPORT−TYPE AIRCRAFT
BEYOND DANGER AREA
APPROX. WINDVELOCITYMPH (km/h)
210−145(338−233)
145−105(233−169)
105−65(169−105)
INLET SUCTIONDANGER AREA
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR GREATER
EXHAUST WAKE DANGERAREA 65 MPH (105 km/h)OR LESS
EXHAUST DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET DANGER AREASINCLUDE (WORST CASE)GROUND PLANEHEADWIND (20 KTS)
INLET HAZARD DIMENSIONSBASED ON 40 ft/sec (12 m/sec)CRITICAL VELOCITY WITH A3 ft (0.9 m) ADJUSTMENTFOR SAFETY
WIDTH195 ft (59 m)
RADIUS = 19.5 ft (5.9 m)
NO ENTRY 684 ft (208 m)AFT OF NOZZLE EXIT
A
B
C
D
ETO 1160 ft (354 m)
(105−32)
N_AC_060302_1_0030101_01_01
Danger Areas of EnginesCFM56 series engine
FIGURE 1
6-3-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1.68 m(5.5 ft)
R = 5.79 m(19ft)
30°TO 348 m (1150 ft) AFT COMMON NOZZLE ASSEMBLY (CNA)
INTAKE SUCTION DANGER AREA
EXHAUST DANGER AREA
ENTRY CORRIDOR
N_AC_060302_1_0040101_01_00
Danger Areas of EnginesIAE V2500 series engine
FIGURE 2
6-3-2Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A319-100
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures.
6-4-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
6-4-1 APU
**ON A/C A319-100
APU - APIC & GARRETT
1. This section gives APU exhaust velocities and temperatures.
6-4-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
0 PLAN 5 10 15 2520
0 16.404 32.808 49.212 65.616 82.02
0
0
FEET
0
5
ELEVATION
10
0
16.404
32.808
80°C176°F
100°C212°F
120°C248°F
150°C302°F
200°C392°F
300°C572°F
METERS
HEIGHT
m ft
FEET
METERS
45 m/s147 ft/s
30 m/s98 ft/s
20 m/s65 ft/s
10 m/s32 ft/s
5 m/s16 ft/s
5 10 15 20
16.404 32.808 49.212 65.616
N_AC_060401_1_0020101_01_00
Exhaust Velocities and TemperaturesAPU -- APIC & GARRETT
FIGURE 1
6-4-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
PAVEMENT DATA
7-1-0 General Information
**ON A/C A319-100
General Information
1. General Information
This brief description of the pavement charts that follow will help in their use for airport planning.
To aid in the interpolation between the discrete values shown, each airplane configuration is shownwith a minimum range of five loads on the main landing gear.
All curves on the charts represent data at a constant specified tire pressure with:- The airplane loaded to the maximum ramp weight.- The Center of Gravity (CG) at its maximum permissible aft position.
Pavement requirements for commercial airplanes are derived from the static analysis of loads imposedon the main landing gear struts.
The A/C codes are used for configuration management of chapter 07 only. There is no relationbetween these A/C codes and the ICAO A/C codes used for determining the airplane wing span andouter main gear wheel span as described in ICAO-Annex 14 Volume 1, Aerodrome Design andOperation Chapter 1.4, Table 1-1.
Section 7-2-0 presents basic data on the landing gear footprint configuration, maximum ramp weightsand tire sizes and pressures.
Section 7-3-0 shows maximum vertical and horizontal pavement loads for certain critical conditions atthe tire-ground interfaces.
Section 7-4-1 contain charts to find these loads throughout the stability limits of the airplane at reston the pavement.
These main landing gear loads are used as the point of entry to the pavement design charts whichfollow, interpolating load values where necessary.
Section 7-5-1 uses procedures in Instruction Report No S-77-1 ”Procedures for Development of CBRDesign Curves”, dated June 1977 and as modified according to the methods described in ICAOAerodrome Design Manual, Part 3. Pavements, 2nd Edition, 1983, Section 1.1 (The ACN-PCNMethod), and utilizing the alpha factors approved by ICAO in October 2007.
7-1-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
The report was prepared by the U.S. Army Corps Engineers Waterways Experiment Station, Soils andPavement Laboratory, Vicksburg, Mississippi.
The line showing 10 000 coverages is used to calculate Aircraft Classification Number (ACN).
The procedure that follows is used to develop flexible pavement design curves such as shown inSection 7-5-1.- With the scale for pavement thickness at the bottom and the scale for CBR at the top, an
arbitrary line is drawn representing 10 000 coverages.- Incremental values of the weight on the main landing gear are then plotted.- Annual departure lines are drawn based on the load lines of the weight on the main landing gear
that is shown on the graph.
Section 7-7-1 gives the rigid pavement design curves that have been prepared with the use of theWestergaard Equation. This is in general accordance with the procedures outlined in the PortlandCement Association publications, ”Design of Concrete Airport Pavement”, 1973 and ”ComputerProgram for Airport Pavement Design”, (Program PDILB), 1967 both by Robert G. Packard.
The procedure that follows is used to develop rigid pavement design curves such as shown in Section7-7-1.- With the scale for pavement thickness on the left and the scale for allowable working stress on
the right, an arbitrary load line is drawn. This represents the maximum weight to be shown forthe main landing gear .
- All values of the subgrade modulus (k values) are then plotted.- Additional load lines for the incremental values of weight on the main landing gear are drawn on
the basis of the curve for k = 300 already shown on the graph.
All Load Classification Number (LCN) curves shown in Section 7-6-1 and Section 7-8-2 have beendeveloped from a computer program based on data provided in International Civil AviationOrganisation (ICAO) document 7920-AN/865/2, Aerodrome Manual, Part 2, ”Aerodrome PhysicalCharacteristics”, Second Edition, 1965.
The flexible pavement charts in Section 7-6-1 show LCN against equivalent single wheel load andequivalent single wheel load against pavement thickness.
The rigid pavement charts in Section 7-8-2 show LCN against equivalent single wheel load andequivalent single wheel load against radius of relative stiffness.
Section 7-9-0 gives ACN data prepared in accordance to the ACN/PCN system as referenced in ICAOAnnex 14, ”Aerodromes”, Volume 1 Fourth Edition July 2004, incorporating Amendments 1 to 6.
The ACN/PCN system gives a standardized international airplane/pavement rating system replacingthe various S, T, TT, LCN, AUW, ISWL, etc..., rating systems used throughout the world.
7-1-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
The ACN is the Aircraft Classification Number and PCN is the corresponding Pavement ClassificationNumber.
An aircraft having an ACN equal to or less than the PCN can operate without restriction on thepavement.
Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms.The derived single wheel is defined as the load on a single tire inflated to 1.25 Mpa (181 psi) thatwould have the same pavement requirements as the aircraft.
Computationally, the ACN/PCN system uses PCA program PDILB for rigid pavements and S-77-1for flexible pavements to calculate ACN values.The Airport Authority must decide on the method of pavement analysis and the results of theirevaluation shown as follows:
PCNPAVEMENT
TYPESUBGRADECATEGORY
TIRE PRESSURE CATEGORY EVALUATION METHOD
R -- Rigid A -- High W -- No Limit T -- Technical
F -- Flexible B -- Medium X -- To 1.5 Mpa (217 psi) U -- Using Aircraft
C -- Low Y -- To 1.0 Mpa (145 psi)
D -- Ultra Low Z -- To 0.5 Mpa (73 psi)
Section 7-9-1 shows the aircraft ACN values for flexible pavements.
The four subgrade categories are:- A. High Strength CBR 15- B. Medium Strength CBR 10- C. Low Strength CBR 6- D. Ultra Low Strength CBR 3
Section 7-9-2 shows the aircraft ACN values for rigid pavements.
The four subgrade categories are:- A. High Strength Subgrade k = 150 MN/m3 (550 pci)- B. Medium Strength Subgrade k = 80 MN/m3 (300 pci)- C. Low Strength Subgrade k = 40 MN/m3 (150 pci)- D. Ultra Low Strength Subgrade k = 20 MN/m3 (75 pci)
7-1-0Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
MODELA319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−133A319−115A319−111A319−112A319−113A319−114A319−131A319−132A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
WV1212121212121212000000000000000008080808080808081111111111111111090909090909090903030303030303030404040404040404
AIRCRAFT CODECCCCCCDDEEFFFFFFGGGGGGHHIIIIIIJJKKKKKKLLMMNNNNNNOOPPPPPP
MODELA319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
A319−112−CJA319−114−CJA319−115−CJA319−132−CJA319−133−CJ
A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132A319−111A319−112A319−113A319−114A319−131A319−132A319−115A319−133A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
A319−112−CJA319−114−CJA319−115−CJA319−132−CJA319−133−CJ
A319−115A319−133A319−111A319−112A319−113A319−114A319−131A319−132
A319−111−CJA319−112−CJA319−113−CJA319−114−CJA319−131−CJA319−132−CJ
WV0101010101010101050505050505050505050505050606060606060606070707070707070702020202020202020202020202101010101010
AIRCRAFT CODEQQRRRRRRSSSSSTTUUUUUUVVVVVVWWXXYYYYYYZZZZZ
AAAAABABABABABABACACACACACAC
NOTE: FOR WEIGHT VARIANT DEFINITION, REFER TO CHAPTER 02−01−01.
NOTE: THE A/C CODES ARE USED FOR CONFIGURATION MANAGEMENT OFCHAPTER 07 ONLY.THERE IS NO RELATION BETWEEN THESE A/C CODES AND THE ICAO A/C CODES USED FOR DETERMINING THE AIRPLANE WING SPAN ANDOUTER MAIN GEAR WHEEL SPAN AS DESCRIBED IN ICAO−ANNEX 14 VOLUME 1,AERODROME DESIGN AND OPERATION CHAPTER 1.4, TABLE 1−1. N_AC_070100_1_0020101_01_00
Aircraft CodesFIGURE 1
7-1-0Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-2-0 Landing Gear Footprint
**ON A/C A319-100
Landing Gear Footprint
1. This section gives Landing Gear Footprint.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-2-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
500 mm(19.7 in)
11 039 mm
(36 ft 2.6 in)
7 590 mm(24 ft 10.8 in)
927 mm(36.5 in)
30 x 8.8 R15 (30 x 8.8 − 15)
11.4 bar (165 psi)
46 x 17 R20 (46 x 16 − 20)
11.9 bar (173 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
C − D − E − F − G − H
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0040101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE 1
7-2-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
11 039 mm
500 mm(19.7 in)
(36 ft 2.6 in)
927 mm(36.5 in)
7 590 mm(24 ft 10.8 in)
30 x 8.8 R15 (30 x 8.8 − 15)
12.1 bar (175 psi)
46 x 17 R20 (46 x 16 − 20)
12.5 bar (181 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
I − J − K − L − M − N − O − P
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0050101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE 2
7-2-0Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
30 x 8.8 R15 (30 x 8.8 − 15)
12.5 bar (181 psi)
46 x 17 R20 (46 x 16 − 20)
12.9 bar (187 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
500 mm(19.7 in)
11 039 mm
(36 ft 2.6 in)
7 590 mm(24 ft 10.8 in)
927 mm(36.5 in)
Q − R − T − U
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0060101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE 3
7-2-0Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
11 039 mm
500 mm(19.7 in)
(36 ft 2.6 in)
927 mm(36.5 in)
7 590 mm(24 ft 10.8 in)
30 x 8.8 R15 (30 x 8.8 − 15)
13.5 bar (196 psi)
46 x 17 R20 (46 x 16 − 20)
13.4 bar (194 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
V − W
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0070101_01_01
Landing Gear FootprintLanding Gear Footprint
FIGURE 4
7-2-0Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
30 x 8.8 R15 (30 x 8.8 − 15)
13.9 bar (202 psi)
46 x 17 R20 (46 x 16 − 20)
13.8 bar (200 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
500 mm(19.7 in)
11 039 mm
(36 ft 2.6 in)
7 590 mm(24 ft 10.8 in)
927 mm(36.5 in)
S − Z − AC
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0250101_01_00
Landing Gear FootprintFIGURE 5
7-2-0Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
11 039 mm
500 mm(19.7 in)
(36 ft 2.6 in)
927 mm(36.5 in)
7 590 mm(24 ft 10.8 in)
30 x 8.8 R15 (30 x 8.8 − 15)
13.2 bar (191 psi)
46 x 17 R20 (46 x 16 − 20)
13.8 bar (200 psi)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
MAIN GEAR TIRE SIZE
MAIN GEAR TIRE PRESSURE
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
X − Y − AA − AB
SEE SECTION 7−4−1
A/C CODE
N_AC_070200_1_0260101_01_00
Landing Gear FootprintFIGURE 6
7-2-0Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-3-0 Maximum Pavement Loads
**ON A/C A319-100
Maximum Pavement Loads
1. This section gives Maximum Pavement Loads.
NOTE : For A/C code definition, refer to chapter 7-1-0.
7-3-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
C62
400
VM
G (
PE
R S
TR
UT
)V
NG
137
575
23 6
2510
720
36 5
0016
550
63 7
2528
900
21 3
759
700
50 9
7523
120
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
62
400
kgM
RW
= 6
2 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
14
% M
AC
AT
A/C
WE
IGH
T =
62
400
kgF
WD
CG
= 2
0.4
% M
AC
AT
A/C
WE
IGH
T =
62
400
kg
D E64
925
29 4
5022
075
10 0
1051
925
23 5
60
A/C
CO
DE
C DM
RW
= 6
4 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgE
(2)
MR
W =
62
400
kgM
RW
= 6
2 40
0 kg
AF
T C
G =
39
% M
AC
AT
A/C
WE
IGH
T =
62
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 6
2 40
0 kg
C DM
RW
= 6
4 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgE
62 4
0013
7 57
520
200
9 17
033
075
15 0
0062
900
28 5
3021
375
9 70
050
325
22 8
20
64 4
0014
1 97
520
500
9 30
033
750
15 3
10
N_AC_070300_1_0230101_01_00
Maximum Pavement LoadsFIGURE 1
7-3-0Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
F64
400
VM
G (
PE
R S
TR
UT
)V
NG
141
975
20 5
009
300
33 7
5015
310
65 7
7529
830
22 0
7510
010
52 6
2523
860
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
64
400
kgM
RW
= 6
4 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
4 40
0 kg
G H64
925
29 4
5022
075
10 0
1051
925
23 5
60
A/C
CO
DE
F GM
RW
= 6
4 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgH
(2)
MR
W =
64
400
kgM
RW
= 6
4 40
0 kg
AF
T C
G =
39
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgA
FT
CG
= 3
9 %
MA
C A
T A
/C W
EIG
HT
= 6
4 40
0 kg
F GM
RW
= 6
4 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
64
400
kgH
64 4
0014
1 97
520
500
9 30
033
750
15 3
10
64 4
0014
1 97
520
500
9 30
033
750
15 3
1065
775
29 8
3022
075
10 0
1052
625
23 8
60
N_AC_070300_1_0240101_01_00
Maximum Pavement LoadsFIGURE 2
7-3-0Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
I66
400
VM
G (
PE
R S
TR
UT
)V
NG
146
375
21 1
259
580
34 8
0015
780
67 7
5030
730
22 7
5010
320
54 2
0024
590
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
66
400
kgM
RW
= 6
6 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
6 40
0 kg
J K67
750
30 7
3022
750
10 3
2054
200
24 5
90
A/C
CO
DE
I JM
RW
= 6
6 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgK
(2)
MR
W =
66
400
kgM
RW
= 6
6 40
0 kg
AF
T C
G =
38.
8 %
MA
C A
T A
/C W
EIG
HT
= 6
6 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgI J
MR
W =
66
400
kgA
FT
CG
= 3
8.8
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgK
66 4
0014
6 37
521
125
9 58
034
800
15 7
8066
950
30 3
6022
750
10 3
2053
550
24 2
90
66 4
0014
6 37
521
125
9 58
034
800
15 7
80
N_AC_070300_1_0250101_01_00
Maximum Pavement LoadsFIGURE 3
7-3-0Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
L66
400
VM
G (
PE
R S
TR
UT
)V
NG
146
375
21 1
259
580
34 8
0015
780
66 9
5030
360
22 7
5010
320
53 5
5024
290
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
66
400
kgM
RW
= 6
8 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
M N68
400
150
800
21 7
509
860
35 7
7516
230
69 6
0031
570
23 4
2510
630
55 6
7525
250
A/C
CO
DE
L MM
RW
= 6
8 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgN
(2)
MR
W =
66
400
kgM
RW
= 6
8 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
66
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
L MM
RW
= 6
8 40
0 kg
AF
T C
G =
38.
1 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
N
68 4
0015
0 80
021
750
9 86
035
775
16 2
3068
975
31 2
8023
425
10 6
3055
175
25 0
20
N_AC_070300_1_0260101_01_00
Maximum Pavement LoadsFIGURE 4
7-3-0Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
O68
400
VM
G (
PE
R S
TR
UT
)V
NG
150
800
21 7
509
860
35 8
0016
240
68 9
7531
280
23 4
2510
630
55 1
7525
020
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
68
400
kgM
RW
= 6
8 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 6
8 40
0 kg
P Q70
400
155
200
22 3
2510
120
36 7
5016
660
71 0
2532
210
24 1
2510
940
56 8
0025
770
A/C
CO
DE
O PM
RW
= 7
0 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgQ
(2)
MR
W =
68
400
kgM
RW
= 6
8 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgA
FT
CG
= 3
8.1
% M
AC
AT
A/C
WE
IGH
T =
68
400
kgO P
MR
W =
70
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
0 40
0 kg
Q
68 4
0015
0 80
021
700
9 84
035
725
16 2
1069
625
31 5
8023
425
10 6
3055
700
25 2
60
N_AC_070300_1_0270101_01_00
Maximum Pavement LoadsFIGURE 5
7-3-0Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
R70
400
VM
G (
PE
R S
TR
UT
)V
NG
155
200
22 3
2510
120
36 7
2516
660
71 4
7532
420
24 1
2510
940
57 1
7525
940
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
70
400
kgM
RW
= 7
0 40
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
0 40
0 kg
T U70
400
155
200
22 3
2510
120
36 7
2516
660
71 4
7532
420
24 1
2510
940
57 1
7525
940
A/C
CO
DE
R TM
RW
= 7
0 40
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgU
(2)
MR
W =
70
400
kgM
RW
= 7
0 40
0 kg
AF
T C
G =
37.
5 %
MA
C A
T A
/C W
EIG
HT
= 7
0 40
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgR T
MR
W =
70
400
kgA
FT
CG
= 3
7.5
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgU
70 4
0015
5 20
022
325
10 1
2036
750
16 6
6071
025
32 2
1024
125
10 9
4056
800
25 7
70
N_AC_070300_1_0280101_01_00
Maximum Pavement LoadsFIGURE 6
7-3-0Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
V73
900
VM
G (
PE
R S
TR
UT
)V
NG
162
925
23 4
0010
610
38 5
0017
460
74 7
2533
890
25 3
2511
480
59 7
7527
110
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
73
900
kgM
RW
= 7
3 90
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
73
900
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
3 90
0 kg
W X75
900
167
325
23 6
2510
720
39 4
0017
870
76 6
0034
750
26 0
0011
800
61 2
7527
800
A/C
CO
DE
V WM
RW
= 7
5 90
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
74
500
kgX
(2)
MR
W =
73
900
kgM
RW
= 7
3 90
0 kg
AF
T C
G =
36.
5 %
MA
C A
T A
/C W
EIG
HT
= 7
3 90
0 kg
AF
T C
G =
36.
5 %
MA
C A
T A
/C W
EIG
HT
= 7
3 90
0 kg
V WM
RW
= 7
5 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
75
900
kgX
73 9
0016
2 92
523
400
10 6
1038
500
17 4
6074
725
33 8
9025
325
11 4
8059
775
27 1
10
N_AC_070300_1_0290101_01_00
Maximum Pavement LoadsFIGURE 7
7-3-0Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
Y75
900
VM
G (
PE
R S
TR
UT
)V
NG
167
325
23 6
2510
720
39 4
0017
870
76 6
0034
750
26 0
0011
800
61 2
7527
800
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
75
900
kgM
RW
= 7
5 90
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
74
500
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
4 50
0 kg
AA
75 9
0016
7 32
523
625
AB
75 9
0016
7 32
523
500
10 7
2039
400
17 8
7076
600
34 7
5026
000
11 8
0061
275
27 8
00
10 6
6039
100
17 7
4076
675
34 7
8026
000
11 8
0061
350
27 8
30
A/C
CO
DE
Y AA
MR
W =
75
900
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
4 50
0 kg
AB
(2)
MR
W =
75
900
kgM
RW
= 7
5 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
75
900
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
5 90
0 kg
Y AA
MR
W =
75
900
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
5 90
0 kg
AB
N_AC_070300_1_0300101_01_00
Maximum Pavement LoadsFIGURE 8
7-3-0Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1
ST
AT
IC L
OA
D A
TM
OS
T F
WD
CG
ST
AT
IC L
OA
D A
TM
AX
AF
T C
GS
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
@ 1
0 ft/
sS
TE
AD
Y B
RA
KIN
G
DE
CE
LER
AT
ION
@ 1
0 ft/
sA
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
23
45
6H
(P
ER
ST
RU
T)
MA
XIM
UM
RA
MP
WE
IGH
T
lbkg
lbkg
lbkg
lbkg
lbkg
lbkg
S70
400
VM
G (
PE
R S
TR
UT
)V
NG
155
200
25 4
5011
550
39 6
5017
990
71 1
0032
250
24 1
2510
940
56 8
7525
800
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(M
G)
MA
XIM
UM
VE
RT
ICA
L M
AIN
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
MR
W =
70
400
kgM
RW
= 7
5 90
0 kg
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
22
V(N
G)
V(M
G)
H
A/C
CO
DE
(1)
(2)
FW
D C
G =
14
% M
AC
AT
A/C
WE
IGH
T =
67
500
kgF
WD
CG
= 2
1 %
MA
C A
T A
/C W
EIG
HT
= 7
4 50
0 kg
Z AC
77 7
0035
240
26 3
5011
950
62 1
5028
190
A/C
CO
DE
S ZM
RW
= 7
6 90
0 kg
FW
D C
G =
21
% M
AC
AT
A/C
WE
IGH
T =
74
500
kgA
C
(2)
MR
W =
70
400
kgM
RW
= 7
5 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
70
400
kgA
FT
CG
= 3
6 %
MA
C A
T A
/C W
EIG
HT
= 7
5 90
0 kg
S ZM
RW
= 7
6 90
0 kg
AF
T C
G =
36
% M
AC
AT
A/C
WE
IGH
T =
76
900
kgA
C
76 9
0016
9 52
523
500
10 6
6039
100
17 7
30
75 9
0016
7 52
523
500
10 6
6039
100
17 7
4076
675
34 7
8026
000
11 8
0061
350
27 8
30
N_AC_070300_1_0310101_01_00
Maximum Pavement LoadsFIGURE 9
7-3-0Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-4-0 Landing Gear Loading on Pavement
**ON A/C A319-100
Landing Gear Loading on Pavement
1. General
In the example shown in Section 7-4-1 Landing Gear Loading on Pavement, A/C Code C, the GrossAircraft Weight is 48 000 kg (105 825 lb) and the percentage of weight on the Main Landing Gear is92.6 %.
For these conditions the total weight on the Main Landing Gear is 44 470 kg (98 025 lb).
7-4-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-4-1 Landing Gear Loading on Pavement
**ON A/C A319-100
Landing Gear Loading on Pavement
1. This section gives Landing Gear Loading on Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-4-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE C
LANDING
TAKE OFF
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 62 000 kg
N_AC_070401_1_0380101_01_00
Landing Gear Loading on PavementFIGURE 1
7-4-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 62 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE D
LANDING
TAKE OFF
N_AC_070401_1_0390101_01_00
LANDING
Landing Gear Loading on PavementFIGURE 2
7-4-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE MAC
10 20 30 40 50
A/C CODE E
MLW = 61 000 kg
MZFW = 57 000 kg
LANDING
TAKE OFF
CG FOR ACNCALCULATIONS
MTOW = 64 000 kg
N_AC_070401_1_0400101_01_00
LANDING
Landing Gear Loading on PavementFIGURE 3
7-4-1Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MTOW = 64 000 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
PERCENTAGE MAC
10 20 30 40 50
MLW = 61 000 kg
A/C CODE F
N_AC_070401_1_0410101_01_00
MZFW = 57 000 kg
Landing Gear Loading on PavementFIGURE 4
7-4-1Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MLW = 62 500 kg
MTOW = 64 000 kg
MZFW = 58 500 kg
TAKE OFF
LANDING
PERCENTAGE MAC
10 20 30 40 50
N_AC_070401_1_0420101_01_00
CG FOR ACNCALCULATIONS
A/C CODE G
Landing Gear Loading on PavementFIGURE 5
7-4-1Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
50
55
60
65
50
55
60
65
35
40
45
35
40
45
80 82 84 86 88 90 92 94 96 98 100
MLW = 62 500 kg
MTOW = 64 000 kg
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE H
N_AC_070401_1_0430101_01_00
LANDING
TAKE OFF
Landing Gear Loading on PavementFIGURE 6
7-4-1Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE I
N_AC_070401_1_0440101_01_00
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 66 000 kg
LANDING
TAKE OFF
LANDING
Landing Gear Loading on PavementLanding Gear Loading on Pavement
FIGURE 7
7-4-1Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MTOW = 66 000 kg
MZFW = 57 000 kg
PERCENTAGE MAC
10 20 30 40 50
TAKE OFF
LANDING
A/C CODE J
MLW = 61 000 kg
CG FOR ACNCALCULATIONS
LANDING
N_AC_070401_1_0450101_01_00
Landing Gear Loading on PavementFIGURE 8
7-4-1Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MTOW = 66 000 kg
MZFW = 58 500 kg
PERCENTAGE MAC
10 20 30 40 50
A/C CODE K
TAKE OFF
MLW = 62 500 kg
N_AC_070401_1_0460101_01_00
LANDINGLANDING
CG FOR ACNCALCULATIONS
Landing Gear Loading on PavementFIGURE 9
7-4-1Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 58 500 kg
MTOW = 66 000 kg
TAKE OFF
CG FOR ACNCALCULATIONS
MLW = 62 500 kg
LANDING
PERCENTAGE MAC
10 20 30 40 50
A/C CODE L
N_AC_070401_1_0470101_01_00
LANDING
Landing Gear Loading on PavementFIGURE 10
7-4-1Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 57 000 kg
CG FOR ACNCALCULATIONS
MLW = 61 000 kg
PERCENTAGE MAC
10 20 30 40 50
A/C CODE M
MTOW = 68 000 kg
LANDING
TAKE OFF
N_AC_070401_1_0480101_01_00
LANDING
Landing Gear Loading on PavementFIGURE 11
7-4-1Page 12
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 57 000 kg
MTOW = 68 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE N
MLW = 61 000 kg
LANDING
TAKE OFF
N_AC_070401_1_0490101_01_00
LANDING
Landing Gear Loading on PavementFIGURE 12
7-4-1Page 13
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MZFW = 58 500 kg
TAKE OFF
CG FOR ACNCALCULATIONS
MTOW = 68 000 kg
MLW = 62 500 kg
LANDING
PERCENTAGE MAC
10 20 30 40 50
A/C CODE O
N_AC_070401_1_0500101_01_00
LANDING
Landing Gear Loading on PavementFIGURE 13
7-4-1Page 14
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
3580
40
45
50
55
60
65
70 70
35
40
45
50
55
60
65
82 84 86 88 90 92 94 96 10098
MTOW = 68 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
10 20 30 40 50
A/C CODE P
MZFW = 58 500 kg
MLW = 62 500 kg
LANDING
TAKE OFF
N_AC_070401_1_0510101_01_00
LANDING
Landing Gear Loading on PavementFIGURE 14
7-4-1Page 15
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
A/C CODE Q
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 70 000 kg
N_AC_070401_1_0520101_01_00
Landing Gear Loading on PavementFIGURE 15
7-4-1Page 16
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE R
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
MZFW = 57 000 kg
MLW = 61 000 kg
MTOW = 70 000 kg
N_AC_070401_1_0530101_01_00
Landing Gear Loading on PavementLanding Gear Loading on Pavement
FIGURE 16
7-4-1Page 17
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE S
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
MZFW = 58 500 kg
MLW = 62 500 kg
MTOW = 70 000 kg
PERCENTAGE MAC
N_AC_070401_1_0540101_01_00
Landing Gear Loading on PavementLanding Gear Loading on Pavement
FIGURE 17
7-4-1Page 18
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
LANDING
TAKE OFF
CG FOR ACNCALCULATIONS
MLW = 62 500 kg
MTOW = 70 000 kg
MZFW = 58 500 kg
A/C CODE T
PERCENTAGE MAC
N_AC_070401_1_0550101_01_00
Landing Gear Loading on PavementFIGURE 18
7-4-1Page 19
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
55
60
65
7010 20 30 40 50
35
40
45
50
35
40
45
50
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE U
LANDING
TAKE OFF
MZFW = 58 500 kg
MLW = 62 500 kg
MTOW = 70 000 kg
CG FOR ACNCALCULATIONS
N_AC_070401_1_0560101_01_00
Landing Gear Loading on PavementFIGURE 19
7-4-1Page 20
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
75
55
60
65
70
40
45
50
75
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE V
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
MLW = 62 500 kg
MTOW = 73 500 kg
TAKE OFF
LANDING
N_AC_070401_1_0570101_01_00
Landing Gear Loading on PavementFIGURE 20
7-4-1Page 21
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
75
55
60
65
70
40
45
50
75
PERCENTAGE OF WEIGHT ON MAIN GEAR
MTOW = 73 500 kg
A/C CODE W
MLW = 62 500 kg
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
PERCENTAGE MAC
N_AC_070401_1_0580101_01_00
Landing Gear Loading on PavementFIGURE 21
7-4-1Page 22
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE X
LANDING
TAKE OFF
MTOW = 75 500 kg
MLW = 61 000 kg
MZFW = 57 000 kg
CG FOR ACNCALCULATIONS
PERCENTAGE MAC
N_AC_070401_1_0590101_01_00
Landing Gear Loading on PavementFIGURE 22
7-4-1Page 23
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE Y
MLW = 61 000 kg
MZFW = 57 000 kg
MTOW = 75 500 kg
CG FOR ACNCALCULATIONS
LANDING
TAKE OFF
N_AC_070401_1_0600101_01_00
Landing Gear Loading on PavementFIGURE 23
7-4-1Page 24
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
10 20 30 40 50
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE MAC
PERCENTAGE OF WEIGHT ON MAIN GEAR
A/C CODE Z
MZFW = 58 500 kg
MLW = 62 500 kg
MTOW = 75 500 kg
LANDING
TAKE OFF CG FOR ACNCALCULATIONS
N_AC_070401_1_0610101_01_00
Landing Gear Loading on PavementFIGURE 24
7-4-1Page 25
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
35
40
45
50
35
75
55
60
65
70
40
45
50
75
80
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
MLW = 62 500 kg
MTOW = 75 500 kg
TAKE OFF
MZFW = 58 500 kg
LANDING
CG FOR ACNCALCULATIONS
10 20 30 40 5080
PERCENTAGE MAC
A/C CODE AA
N_AC_070401_1_0620101_01_00
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
Landing Gear Loading on PavementFIGURE 25
7-4-1Page 26
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
35
40
45
50
35
75
55
60
65
70
40
45
50
75
8080
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
MLW = 62 500 kg
MTOW = 75 500 kg
MZFW = 58 500 kg
CG FOR ACNCALCULATIONS
LANDING
10 20 30 40 50
PERCENTAGE MAC
A/C CODE AB
TAKE OFF
80 82 84 86 88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR
N_AC_070401_1_0630101_01_00
Landing Gear Loading on PavementFIGURE 26
7-4-1Page 27
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
55
60
65
70
35
40
45
50
3580 82 84 86 88 90 92 94 96 98 100
75
55
60
65
70
40
45
50
75
8080
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
(x
1 00
0 kg
)
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
− (
x 1
000
kg)
PERCENTAGE OF WEIGHT ON MAIN GEAR
CG FOR ACNCALCULATIONS
LANDING
MTOW = 76 500 kg
TAKE OFF
10 20 30 40 50
PERCENTAGE MAC
A/C CODE AC
MZFW = 58 500 kg
MLW = 62 500 kg
N_AC_070401_1_0640101_01_00
Landing Gear Loading on PavementFIGURE 27
7-4-1Page 28
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-5-0 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A319-100
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
1. General
In order to determine a particular Flexible Pavement Thickness, the Subgrade Strength (CBR), theAnnual Departure Level and the weight on one Main Landing Gear must be known.
In the example shown in Section 7-5-1 Flexible Pavement Requirements, A/C Code C for:- a CBR value of 10- an Annual Departure Level of 25 000- the Load on one MLG of 20 000 kg (44 100 lb).
For these conditions, the Flexible Pavement Thickness is 41.4 cm (16.3 in).
The line showing 10 000 Coverages is used to calculate the Aircraft Classification Number (ACN).
7-5-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-5-1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
**ON A/C A319-100
Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method
1. This section gives Flexible Pavement Requirements.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-5-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR28 900 kg (63 725 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE C ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0380101_01_00
Flexible Pavement RequirementsFIGURE 1
7-5-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR28 530 kg (62 900 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE D ALPHA FACTOR = 0.9
N_AC_070501_1_0390101_01_00
FOR ACN CALCULATIONS10 000 COVERAGES USED
Flexible Pavement RequirementsFIGURE 2
7-5-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 450 kg (64 925 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE E ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0400101_01_00
Flexible Pavement RequirementsFIGURE 3
7-5-1Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE F ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0410101_01_00
Flexible Pavement RequirementsFIGURE 4
7-5-1Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE G ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0420101_01_00
Flexible Pavement RequirementsFIGURE 5
7-5-1Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR29 450 kg (64 925 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE H ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0430101_01_00
Flexible Pavement RequirementsFIGURE 6
7-5-1Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 730 kg (67 750 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE I ALPHA FACTOR = 0.9
N_AC_070501_1_0440101_01_00
FOR ACN CALCULATIONS10 000 COVERAGES USED
Flexible Pavement RequirementsFIGURE 7
7-5-1Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 360 kg (66 950 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE J ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0450101_01_00
Flexible Pavement RequirementsFIGURE 8
7-5-1Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 730 kg (67 750 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE K ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0460101_01_00
Flexible Pavement RequirementsFIGURE 9
7-5-1Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 360 kg (66 950 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE L ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0470101_01_00
Flexible Pavement RequirementsFIGURE 10
7-5-1Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE M ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0480101_01_00
Flexible Pavement RequirementsFIGURE 11
7-5-1Page 12
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 570 kg (69 600 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE N ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0490101_01_00
Flexible Pavement RequirementsFIGURE 12
7-5-1Page 13
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE O ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0500101_01_00
Flexible Pavement RequirementsFIGURE 13
7-5-1Page 14
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
SUBGRADE STRENGTH − CBR
806050403020151063
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
806050403020151063
10 15 20 30 40 60 80 100 120 150 180
[INCHES]
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 580 kg (69 625 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
A/C CODE P ALPHA FACTOR = 0.9
FOR ACN CALCULATIONS10 000 COVERAGES USED
N_AC_070501_1_0510101_01_00
Flexible Pavement RequirementsFIGURE 14
7-5-1Page 15
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
N_AC_070501_1_0520101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE Q
32 210 kg (71 025 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)
25 000 kg (55 125 lb)
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
Flexible Pavement RequirementsFIGURE 15
7-5-1Page 16
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
N_AC_070501_1_0530101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE R ALPHA FACTOR = 0.9
32 420 kg (71 475 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
Flexible Pavement RequirementsFIGURE 16
7-5-1Page 17
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR32 250 kg (71 100 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE S ALPHA FACTOR = 0.9
N_AC_070501_1_0540101_01_00
Flexible Pavement RequirementsFIGURE 17
7-5-1Page 18
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR32 210 kg (71 025 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE T ALPHA FACTOR = 0.9
N_AC_070501_1_0550101_01_00
Flexible Pavement RequirementsFIGURE 18
7-5-1Page 19
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR32 420 kg (71 475 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE U ALPHA FACTOR = 0.9
N_AC_070501_1_0560101_01_00
Flexible Pavement RequirementsFIGURE 19
7-5-1Page 20
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR33 890 kg (74 725 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE V ALPHA FACTOR = 0.9
N_AC_070501_1_0570101_01_00
Flexible Pavement RequirementsFIGURE 20
7-5-1Page 21
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR33 890 kg (74 725 lb)
20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
25 000 kg (55 125 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE W ALPHA FACTOR = 0.9
N_AC_070501_1_0580101_01_00
Flexible Pavement RequirementsFIGURE 21
7-5-1Page 22
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 750 kg (76 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE X
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0590101_01_00
Flexible Pavement RequirementsFIGURE 22
7-5-1Page 23
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 750 kg (76 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE Y
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0600101_01_00
Flexible Pavement RequirementsFIGURE 23
7-5-1Page 24
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 780 kg (76 675 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE Z
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0610101_01_00
Flexible Pavement RequirementsFIGURE 24
7-5-1Page 25
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 750 kg (76 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE AA
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0620101_01_00
Flexible Pavement RequirementsFIGURE 25
7-5-1Page 26
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR34 780 kg (76 675 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE AB
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0630101_01_00
Flexible Pavement RequirementsFIGURE 26
7-5-1Page 27
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
10 15 20 30 40 60 80 100 120 150 180[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
[INCHES]
SUBGRADE STRENGTH − CBR
8060403020151063
806050403020151063
50
WEIGHT ON ONE MAIN LANDING GEAR35 240 kg (77 700 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
ANNUAL DEPARTURES*
*20 YEAR PAVEMENT LIFE
1 2003 0006 00015 00025 000
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
USED FOR ACN10 000 COVERAGES
CALCULATIONS
A/C CODE AC
10 000 kg (22 050 lb)
ALPHA FACTOR = 0.9
N_AC_070501_1_0640101_01_00
Flexible Pavement RequirementsFIGURE 27
7-5-1Page 28
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A319-100
Flexible Pavement Requirements - LCN Conversion
1. General
In order to determine the airplane weight that can be accommodated on a particular FlexiblePavement, both the LCN of the pavement and the thickness (h) must be known.
In the example shown in Section 7-6-1 Flexible Pavement Requirements - LCN Conversion, A/C CodeC for:The thickness (h) is shown at 20 inches with an LCN of 52.3.
For these conditions, the weight on one Main Landing Gear is 25 000 kg (55 125 lb).
7-6-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-6-1 Flexible Pavement Requirements - LCN Conversion
**ON A/C A319-100
Flexible Pavement Requirements - LCN Conversion
1. This section gives Flexible Pavement Requirements - LCN Conversion.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-6-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.9
bar
(173
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
28 9
00 k
g
(63
725
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
C
N_AC_070601_1_0410101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 1
7-6-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.9
bar
(173
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0420101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
28 5
30 k
g
(62
900
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
D
Flexible Pavement Requirements - LCN ConversionFIGURE 2
7-6-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.9
bar
(173
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
E
N_AC_070601_1_0430101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 3
7-6-1Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.9
bar
(173
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
F
N_AC_070601_1_0440101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 4
7-6-1Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.9
bar
(173
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0450101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
G
Flexible Pavement Requirements - LCN ConversionFIGURE 5
7-6-1Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
1.9
bar
(173
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
H
N_AC_070601_1_0460101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 6
7-6-1Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
750
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
I
N_AC_070601_1_0470101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 7
7-6-1Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0480101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
J
Flexible Pavement Requirements - LCN ConversionFIGURE 8
7-6-1Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0490101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
750
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
K
Flexible Pavement Requirements - LCN ConversionFIGURE 9
7-6-1Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
20
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
A/C
CO
DE
L
N_AC_070601_1_0500101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 10
7-6-1Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0510101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
31 2
80 k
g
(68
950
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
M
Flexible Pavement Requirements - LCN ConversionFlexible Pavement Requirements - LCN Conversion
FIGURE 11
7-6-1Page 12
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
31 5
70 k
g
(69
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
N
N_AC_070601_1_0520101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 12
7-6-1Page 13
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0530101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
31 2
80 k
g
(68
950
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
O
Flexible Pavement Requirements - LCN ConversionFIGURE 13
7-6-1Page 14
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
N_AC_070601_1_0540101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
WE
IGH
T O
N O
NE
MA
IN
31 5
80 k
g
(69
625
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
A/C
CO
DE
P
Flexible Pavement Requirements - LCN ConversionFIGURE 14
7-6-1Page 15
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.9
bar
(187
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
32 2
10 k
g
(71
000
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
Q
N_AC_070601_1_0550101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 15
7-6-1Page 16
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.9
bar
(187
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
32 4
20 k
g
(71
475
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
R
N_AC_070601_1_0560101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 16
7-6-1Page 17
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
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
Flexible Pavement Requirements - LCN ConversionFIGURE 17
7-6-1Page 18
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.9
bar
(187
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
32 2
10 k
g
(71
000
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
T
N_AC_070601_1_0580101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 18
7-6-1Page 19
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.9
bar
(187
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
32 4
20 k
g
(71
475
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
U
N_AC_070601_1_0590101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 19
7-6-1Page 20
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.4
bar
(194
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
33 8
90 k
g
(74
725
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
V
N_AC_070601_1_0600101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 20
7-6-1Page 21
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.4
bar
(194
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
33 8
90 k
g
(74
725
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
W
N_AC_070601_1_0610101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 21
7-6-1Page 22
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
34 7
50 k
g
(76
600
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
X
N_AC_070601_1_0620101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 22
7-6-1Page 23
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
34 7
50 k
g
(76
600
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
Y
N_AC_070601_1_0630101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 23
7-6-1Page 24
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
34 7
80 k
g
(76
675
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
Z
N_AC_070601_1_0640101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 24
7-6-1Page 25
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
34 7
50 k
g
(76
600
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
AA
N_AC_070601_1_0650101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 25
7-6-1Page 26
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
34 7
80 k
g
(76
675
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
AB
N_AC_070601_1_0660101_01_00
Flexible Pavement Requirements - LCN ConversionFIGURE 26
7-6-1Page 27
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NO
TE
:IC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
Sec
ond
Edi
tion
1965
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
3.8
bar
(200
psi
)46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
35 30 25 20 15 10 5 080
100
6050
4030
20
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
10
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
1020304050607080
8070
6050
4030
100
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
WE
IGH
T O
N O
NE
MA
IN
35 2
40 k
g
(77
700
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
LAN
DIN
G G
EA
RM
AX
IMU
M R
AM
P W
EIG
HT
AN
D A
FT
CG
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
T
20
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
25 0
00 k
g
(55
125
lb)
A/C
CO
DE
AC
N_AC_070601_1_0670101_01_00
Flexible Pavement Requirements - LCN ConversionFlexible Pavement Requirements - LCN Conversion
FIGURE 27
7-6-1Page 28
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A319-100
Rigid Pavement Requirements - Portland Cement Association Design Method
1. General
In order to determine a particular Rigid Pavement Thickness, the Subgrade Modulus (k), theallowable working stress and the weight on one Main Landing Gear must be known.
In the example shown in Section 7-7-1 Rigid Pavement Requirements (PCA), A/C Code C for:- a ”k” value of 150 MN/m3 (550 lbf/in3)- an allowable working stress of 31.6 kgf/cm2 (450 lbf/in2)- the load on one MLG of 20 000 kg (44 100 lb).For these conditions, the Rigid Pavement Thickness is 18.9 cm (7.4 in).
7-7-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A319-100
Rigid Pavement Requirements - Portland Cement Association Design Method
1. This section gives Rigid Pavement Requirements.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-7-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR28 905 kg (63 725 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
A/C CODE C
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14
N_AC_070701_1_0380101_01_00
Rigid Pavement Requirements (PCA)FIGURE 1
7-7-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE D
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR28 530 kg (62 900 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0390101_01_00
Rigid Pavement Requirements (PCA)FIGURE 2
7-7-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE E
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 445 kg (64 925 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0400101_01_00
Rigid Pavement Requirements (PCA)FIGURE 3
7-7-1Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE F
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0410101_01_00
Rigid Pavement Requirements (PCA)FIGURE 4
7-7-1Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE G
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 830 kg (65 775 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0420101_01_00
Rigid Pavement Requirements (PCA)FIGURE 5
7-7-1Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 11.9 bar (173 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE H
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14
WEIGHT ON ONE MAIN LANDING GEAR29 445 kg (64 925 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0430101_01_00
Rigid Pavement Requirements (PCA)FIGURE 6
7-7-1Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE I
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 735 kg (67 750 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0440101_01_00
Rigid Pavement Requirements (PCA)FIGURE 7
7-7-1Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE J
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 365 kg (66 950 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0450101_01_00
Rigid Pavement Requirements (PCA)FIGURE 8
7-7-1Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE K
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 735 kg (67 750 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0460101_01_00
Rigid Pavement Requirements (PCA)FIGURE 9
7-7-1Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE L
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR30 365 kg (66 950 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0470101_01_00
Rigid Pavement Requirements (PCA)FIGURE 10
7-7-1Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE M
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0480101_01_00
Rigid Pavement Requirements (PCA)FIGURE 11
7-7-1Page 12
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE N
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 565 kg (69 600 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0490101_01_00
Rigid Pavement Requirements (PCA)FIGURE 12
7-7-1Page 13
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE O
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 280 kg (68 975 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
N_AC_070701_1_0500101_01_00
Rigid Pavement Requirements (PCA)FIGURE 13
7-7-1Page 14
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.5 bar (181 psi)
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
200
300
400
500
600
700
800
900
1000
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
A/C CODE P
34
32
30
28
26
24
22
20
18
16
70
58
52
45
39
33
27
20
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
6
7
8
9
10
11
12
13
14MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR31 580 kg (69 625 lb)25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)
N_AC_070701_1_0510101_01_00
10 000 kg (22 050 lb)
Rigid Pavement Requirements (PCA)FIGURE 14
7-7-1Page 15
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE QRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0520101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
32 210 kg (71 025 lb)
Rigid Pavement Requirements (PCA)FIGURE 15
7-7-1Page 16
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
32 420 kg (71 475 lb)
A/C CODE R
N_AC_070701_1_0530101_01_00
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³ [lb/in
²]
[kg/
cm²]
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 16
7-7-1Page 17
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
A/C CODE SRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
32 245 kg (71 100 lb)
[lb/in
²]
[kg/
cm²]
N_AC_070701_1_0540101_01_00
Rigid Pavement Requirements (PCA)FIGURE 17
7-7-1Page 18
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
32 210 kg (71 025 lb)
A/C CODE TRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0550101_01_00
[lb/in
²]
[kg/
cm²]
Rigid Pavement Requirements (PCA)FIGURE 18
7-7-1Page 19
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 12.9 bar (187 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
32 420 kg (71 475 lb)
A/C CODE URIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0560101_01_00
[lb/in
²]
[kg/
cm²]
Rigid Pavement Requirements (PCA)FIGURE 19
7-7-1Page 20
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE VRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
33 895 kg (74 725 lb)
[lb/in
²]
[kg/
cm²]
N_AC_070701_1_0570101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 20
7-7-1Page 21
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.4 bar (194 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
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
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
33 895 kg (74 725 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
N_AC_070701_1_0580101_01_00
Rigid Pavement Requirements (PCA)FIGURE 21
7-7-1Page 22
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE XRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0590101_01_00
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
34 745 kg (76 600 lb)
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 22
7-7-1Page 23
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE YRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
34 745 kg (76 600 lb)
N_AC_070701_1_0600101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 23
7-7-1Page 24
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE ZRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
34 780 kg (76 675 lb)
N_AC_070701_1_0610101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 24
7-7-1Page 25
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE AARIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
34 745 kg (76 600 lb)
N_AC_070701_1_0620101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 25
7-7-1Page 26
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE ABRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
WEIGHT ON ONE MAIN LANDING GEAR
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
34 780 kg (76 675 lb)
N_AC_070701_1_0630101_01_00
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 26
7-7-1Page 27
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
NOTE:THE VALUES OBTAINED BY USING THE MAXIMUM LOAD REFERENCE LINE AND ANY VALUES FOR K ARE EXACT. FOR LOADS LESS THAN MAXIMUM,
SLIGHTLY FOR ANY OTHER
THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
VALUES OF K
REFERENCE:
AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
"DESIGN OF CONCRETE
[INC
HE
S]
[lb/in
²]
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
46 x 17 R20 (46 x 16−20) TIRESTIRE PRESSURE CONSTANT AT 13.8 bar (200 psi)
6
7
8
9
10
11
12
13
14
34
32
30
28
26
24
22
20
18
16
200
300
400
500
600
700
800
900
1000 70
58
52
45
39
33
27
20
A/C CODE ACRIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
K = 40 MN/m³K = 80 MN/m³K = 150 MN/m³
K = 20 MN/m³
N_AC_070701_1_0640101_01_00
25 000 kg (55 125 lb)20 000 kg (44 100 lb)15 000 kg (33 075 lb)10 000 kg (22 050 lb)
35 240 kg (77 700 lb)
WEIGHT ON ONE MAIN LANDING GEAR
MAXIMUM POSSIBLE MAIN GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
Rigid Pavement Requirements (PCA)FIGURE 27
7-7-1Page 28
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-0 Rigid Pavement Requirements - LCN Conversion
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-1 Radius of Relative Stiffness
**ON A/C A319-100
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
d6.06.57.07.5
K=75 K=100 K=150 K=200 K=250 K=300 K=350 K=400 K=550
8.08.59.09.5
10.010.511.011.512.012.513.013.514.014.515.015.516.016.517.017.518.019.020.021.022.023.024.025.0
31.4833.4335.3437.2239.0640.8842.6744.4346.1847.9049.6051.2852.9454.5956.2257.8359.4361.0262.5964.1565.6967.2368.7570.2671.7674.7377.6680.5583.4186.2489.0491.81
29.3031.1132.8934.6336.3538.0439.7141.3542.9744.5746.1647.7249.2750.8052.3253.8255.3156.7858.2559.7061.1362.5663.9865.3866.7869.5472.2774.9677.6380.2682.8685.44
26.4728.1129.7231.2932.8534.3735.8837.3638.8340.2841.7143.1244.5245.9047.2748.6349.9851.3152.6353.9455.2456.5357.8159.0860.3462.8465.3067.7470.1472.5274.8777.20
24.6326.1627.6529.1230.5731.9933.3934.7736.1437.4838.8140.1341.4342.7243.9945.2646.5147.7548.9850.2051.4152.6153.8054.9856.1558.4860.7763.0465.2867.4969.6871.84
23.3024.7426.1527.5428.9130.2531.5832.8934.1735.4536.7137.9539.1840.4041.6142.8043.9845.1646.3247.4748.6249.7550.8852.0053.1155.3157.4759.6261.7363.8365.9067.95
22.2623.6424.9926.3227.6228.9130.1731.4232.6533.8735.0736.2637.4438.6039.7540.8942.0243.1544.2645.3646.4547.5448.6149.6850.7452.8454.9156.9658.9860.9862.9664.92
21.4222.7424.0425.3226.5827.8129.0330.2331.4232.5933.7534.8936.0237.1438.2539.3540.4441.5142.5843.6444.7045.7446.7747.8048.8250.8452.8454.8156.7558.6860.5862.46
20.7222.0023.2524.4925.7026.9028.0829.2430.3931.5232.6433.7434.8435.9236.9938.0639.1140.1541.1942.2143.2344.2445.2446.2347.2249.1751.1053.0154.8956.7558.5960.41
19.1320.3121.4722.6123.7424.8425.9327.0028.0629.1130.1432.1632.1733.1734.1635.1436.1237.0838.0338.9839.9240.8541.7842.7043.6145.4147.1948.9550.6952.4154.1155.79
RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES
L =
E = Young’s Modulus = 4 x 10 psi
k = Subgrade Modulus, 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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-2 Rigid Pavement Requirements - LCN Conversion
**ON A/C A319-100
Rigid Pavement Requirements - LCN Conversion
1. This section gives Rigid Pavement Requirements - LCN Conversion.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-8-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
A/C
CO
DE
C
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
28 9
00 k
g
(63
725
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0410101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE 1
7-8-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
D
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
28 5
30 k
g
(62
900
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0420101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 2
7-8-2Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
E
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0430101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 3
7-8-2Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
F
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0440101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 4
7-8-2Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
G
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 8
30 k
g
(65
775
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0450101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 5
7-8-2Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
H
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
29 4
50 k
g
(64
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0460101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 6
7-8-2Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
I
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
750
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0470101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 7
7-8-2Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
J
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0480101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 8
7-8-2Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
K
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 7
30 k
g
(67
750
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0490101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 9
7-8-2Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
8090
7060
5040
3005101520253035
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
A/C
CO
DE
L
508
762
1 01
61
270
1 77
82
540
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
WE
IGH
T O
N O
NE
MA
IN
30 3
60 k
g
(66
925
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
LAN
DIN
G G
EA
R
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0500101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 10
7-8-2Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
M
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
280
kg
(6
8 95
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0510101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE 11
7-8-2Page 12
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
N
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
570
kg
(6
9 60
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0520101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE 12
7-8-2Page 13
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
O
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
280
kg
(6
8 95
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0530101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE 13
7-8-2Page 14
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
N_AC_070802_1_0540101_01_00
A/C
CO
DE
P
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R31
580
kg
(6
9 62
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE 14
7-8-2Page 15
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
Q
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
210
kg
(7
1 00
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0550101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE 15
7-8-2Page 16
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
R
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
420
kg
(7
1 47
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
N_AC_070802_1_0560101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 16
7-8-2Page 17
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
S
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
250
kg
(7
1 10
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0570101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
10 0
00 k
g
(22
050
lb)
Rigid Pavement Requirements - LCN ConversionFIGURE 17
7-8-2Page 18
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
T
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
210
kg
(7
1 00
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0580101_01_00
10 0
00 k
g
(22
050
lb)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 18
7-8-2Page 19
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
U
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R32
420
kg
(7
1 47
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)
N_AC_070802_1_0590101_01_00
10 0
00 k
g
(22
050
lb)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 19
7-8-2Page 20
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65N
OT
E:
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
V
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
33 8
90 k
g
(74
725
lb)
N_AC_070802_1_0600101_01_00
10 0
00 k
g
(22
050
lb)
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 20
7-8-2Page 21
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
W
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
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
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
N_AC_070802_1_0610101_01_00
Rigid Pavement Requirements - LCN ConversionFIGURE 21
7-8-2Page 22
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
X
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
750
kg
(7
6 60
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
N_AC_070802_1_0620101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 22
7-8-2Page 23
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
Y
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
MA
XIM
UM
PO
SS
IBLE
MA
IN G
EA
R L
OA
D A
TW
EIG
HT
ON
ON
E M
AIN
LA
ND
ING
GE
AR
34 7
50 k
g
(76
600
lb)
25 0
00 k
g
(55
125
lb)
20 0
00 k
g
(44
100
lb)
15 0
00 k
g
(33
075
lb)
10 0
00 k
g
(22
050
lb)
N_AC_070802_1_0630101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
G
Rigid Pavement Requirements - LCN ConversionFIGURE 23
7-8-2Page 24
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
Z
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
780
kg
(7
6 67
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
N_AC_070802_1_0640101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 24
7-8-2Page 25
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
AA
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
750
kg
(7
6 60
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
N_AC_070802_1_0650101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 25
7-8-2Page 26
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
AB
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R34
780
kg
(7
6 67
5 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
N_AC_070802_1_0660101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 26
7-8-2Page 27
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
2030
4050
100
8070
6001020304050607080
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
EQUIVALENT SINGLE WHEEL LOAD [1 000 lb]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INN
OT
E:
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
EQUIVALENT SINGLE WHEEL LOAD [1 000 kg]
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
A/C
CO
DE
AC
508
762
1 01
61
270
1 77
82
540
8090
7060
5040
3005101520253035
WE
IGH
T O
N O
NE
MA
IN L
AN
DIN
G G
EA
R35
240
kg
(7
7 70
0 lb
)25
000
kg
(5
5 12
5 lb
)20
000
kg
(4
4 10
0 lb
)15
000
kg
(3
3 07
5 lb
)10
000
kg
(2
2 05
0 lb
)
N_AC_070802_1_0670101_01_00
MA
XIM
UM
RA
MP
WE
IGH
T A
ND
AF
T C
GM
AX
IMU
M P
OS
SIB
LE M
AIN
GE
AR
LO
AD
AT
Rigid Pavement Requirements - LCN ConversionFIGURE 27
7-8-2Page 28
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-3 Radius of Relative Stiffness (Other values of E and L)
**ON A/C A319-100
Radius of Relative Stiffness (Other values of ”E” and ”L”)
1. General
The table of Section 7-8-1, Radius of Relative Stiffness, presents ”L” values based on Young’sModulus (E) of 4 000 000 psi and Poisson’s Ratio (µ) of 0.15.
To find ”L” values based on other values of ”E” and ”µ”, see Section 7-8-4.
For example, to find an ”L” value based on an ”E” of 3 000 000 psi, the ”E” factor of 0.931 ismultiplied by the ”L” value found in the table of Section 7-8-1.
The effect of variations of ”µ” on the ”L” value is treated in a similar manner.
7-8-3Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-8-4 Radius of Relative Stiffness
**ON A/C A319-100
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-4Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
0.80
0.85
0.90
0.95
1.00
1.05
1.10
0 1 2 3 4 5
0.995
1.000
1.005
1.010
1.015
0.00 0.05 0.10 0.15 0.25
E F
AC
TO
R
BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF TABLE 7−8−1
EFFECT OF ON L VALUES
E, Young’s Modulus (10 , PSI)
EFFECT OF E ON L VALUES
, Poisson’s Ratio
FA
CT
OR
NOTE:
0.20
N_AC_070804_1_0020101_01_02
Radius of Relative Stiffness(Effect E and µ on ”L” values)
FIGURE 1
7-8-4Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-9-0 ACN/PCN Reporting System
**ON A/C A319-100
ACN/PCN Reporting System
1. General
To determine the ACN of an aircraft on flexible or rigid pavement, both the aircraft gross weight andthe subgrade strength must be known.
In the example shown in Section 7-9-1 Aircraft Classification Number -- Flexible Pavement, A/C CodeC, for an aircraft gross weight of 55 000 kg (121 250 lb) and low subgrade strength (code C), theACN for the flexible pavement is 29.9.
In the example shown in Section 7-9-2 Aircraft Classification Number -- Rigid Pavement, A/C CodeC, for an aircraft gross weight of 55 000 kg (121 250 lb) and medium subgrade strength (code B),the ACN for the rigid pavement is 30.8.
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to any limitation on the tire pressure.(Ref.: ICAO Aerodrome Design Manual Part 3, Chapter 1, Second Edition 1983).
7-9-0Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-9-1 Aircraft Classification Number - Flexible Pavement
**ON A/C A319-100
Aircraft Classification Number - Flexible Pavement
1. This section gives the Aircraft Classification Number - Flexible Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-9-1Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9 %
MA
C.
ON
PA
VE
ME
NT
− A
/C C
OD
E C
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
N_AC_070901_1_0510101_01_00
A/C
CO
DE
C
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
Aircraft Classification Number -- Flexible PavementFIGURE 1
7-9-1Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
ON
PA
VE
ME
NT
− A
/C C
OD
E D
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
D
N_AC_070901_1_0520101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE 2
7-9-1Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
E
ON
PA
VE
ME
NT
− A
/C C
OD
E E
N_AC_070901_1_0530101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE 3
7-9-1Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
A/C
CO
DE
F
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0540101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Flexible PavementFIGURE 4
7-9-1Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
A/C
CO
DE
G
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0550101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Flexible PavementFIGURE 5
7-9-1Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
65
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
A/C
CO
DE
H
ALP
HA
FA
CT
OR
= 0
.9
N_AC_070901_1_0560101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E H
Aircraft Classification Number -- Flexible PavementFIGURE 6
7-9-1Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.8
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
I
65
148
152
N_AC_070901_1_0570101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E I
Aircraft Classification Number -- Flexible PavementFIGURE 7
7-9-1Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
J
65
148
152
N_AC_070901_1_0580101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
Aircraft Classification Number -- Flexible PavementFIGURE 8
7-9-1Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.8
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
K
65
148
152
N_AC_070901_1_0590101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E K
Aircraft Classification Number -- Flexible PavementFIGURE 9
7-9-1Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
L
65
148
152
N_AC_070901_1_0600101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
Aircraft Classification Number -- Flexible PavementFIGURE 10
7-9-1Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
M
65
148
152
N_AC_070901_1_0610101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E M
Aircraft Classification Number -- Flexible PavementFIGURE 11
7-9-1Page 12
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.1
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
N
50
N_AC_070901_1_0620101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E N
Aircraft Classification Number -- Flexible PavementFIGURE 12
7-9-1Page 13
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
O
50
N_AC_070901_1_0630101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E O
Aircraft Classification Number -- Flexible PavementFIGURE 13
7-9-1Page 14
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.1
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
P
50
N_AC_070901_1_0640101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E P
Aircraft Classification Number -- Flexible PavementFIGURE 14
7-9-1Page 15
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E Q
75
N_AC_070901_1_0650101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Q
Aircraft Classification Number -- Flexible PavementFIGURE 15
7-9-1Page 16
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E R
75
N_AC_070901_1_0660101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E R
Aircraft Classification Number -- Flexible PavementFIGURE 16
7-9-1Page 17
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E S
75
N_AC_070901_1_0670101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E S
Aircraft Classification Number -- Flexible PavementFIGURE 17
7-9-1Page 18
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E T
75
N_AC_070901_1_0680101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E T
Aircraft Classification Number -- Flexible PavementFIGURE 18
7-9-1Page 19
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
7.5
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E U
75
N_AC_070901_1_0690101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E U
Aircraft Classification Number -- Flexible PavementFIGURE 19
7-9-1Page 20
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.52
% M
AC
.
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
50
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.9
157
161
165
152 A
/C C
OD
E V
75
N_AC_070901_1_0700101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E V
Aircraft Classification Number -- Flexible PavementFIGURE 20
7-9-1Page 21
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
751520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.52
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G
7782
8690
9599
104
108
112
(x 1
000
lb)
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ALP
HA
FA
CT
OR
= 0
.9
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
Aircraft Classification Number -- Flexible PavementFIGURE 21
7-9-1Page 22
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
X
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
ON
PA
VE
ME
NT
− A
/C C
OD
E X
N_AC_070901_1_0720101_01_00
Aircraft Classification Number -- Flexible PavementFIGURE 22
7-9-1Page 23
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
Y
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
N_AC_070901_1_0730101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Y
Aircraft Classification Number -- Flexible PavementFIGURE 23
7-9-1Page 24
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
Z
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
N_AC_070901_1_0740101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Z
Aircraft Classification Number -- Flexible PavementFIGURE 24
7-9-1Page 25
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
AA
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
N_AC_070901_1_0750101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
A
Aircraft Classification Number -- Flexible PavementFIGURE 25
7-9-1Page 26
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
AB
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
N_AC_070901_1_0760101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
B
Aircraft Classification Number -- Flexible PavementFIGURE 26
7-9-1Page 27
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
1520253035404550
AIRCRAFT CLASSIFICATION NUMBER (ACN)
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
7782
8690
9599
104
108
112
(x 1
000
lb)
117
121
126
130
134
139
143
148
152
157
161
165
7065
6055
5045
4035
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
75
55
80
170
174
ALP
HA
FA
CT
OR
= 0
.9
A/C
CO
DE
AC
C −
CB
R
6 (L
OW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R
3 (U
LTR
A L
OW
)
N_AC_070901_1_0770101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
C
Aircraft Classification Number -- Flexible PavementFIGURE 27
7-9-1Page 28
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
7-9-2 Aircraft Classification Number - Rigid Pavement
**ON A/C A319-100
Aircraft Classification Number - Rigid Pavement
1. This section gives the Aircraft Classification Number - Rigid Pavement.
NOTE : For A/C Code definition, refer to chapter 7-1-0.
7-9-2Page 1
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
C
N_AC_070902_1_0500101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E C
Aircraft Classification Number -- Rigid PavementFIGURE 1
7-9-2Page 2
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
D
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0510101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E D
Aircraft Classification Number -- Rigid PavementFIGURE 2
7-9-2Page 3
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
E
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0520101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E E
Aircraft Classification Number -- Rigid PavementFIGURE 3
7-9-2Page 4
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
F
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0530101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E F
Aircraft Classification Number -- Rigid PavementFIGURE 4
7-9-2Page 5
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
9 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
G
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0540101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E G
Aircraft Classification Number -- Rigid PavementFIGURE 5
7-9-2Page 6
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
11.
9 ba
r (1
73 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
A/C
CO
DE
H
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
ON
PA
VE
ME
NT
− A
/C C
OD
E H
N_AC_070902_1_0550101_01_00
Aircraft Classification Number -- Rigid PavementFIGURE 6
7-9-2Page 7
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.8
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
I
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0560101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E I
Aircraft Classification Number -- Rigid PavementFIGURE 7
7-9-2Page 8
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
J
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0570101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E J
Aircraft Classification Number -- Rigid PavementFIGURE 8
7-9-2Page 9
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
8.8
% M
AC
.S
EE
SE
CT
ION
7−
4−1
LAN
DIN
G G
EA
R L
OA
DIN
G46
x 1
7 R
20 (
46 x
16−
20)
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
2.5
bar
(181
psi
)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
K
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0580101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E K
Aircraft Classification Number -- Rigid PavementFIGURE 9
7-9-2Page 10
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
ICA
O A
ER
OD
RO
ME
DE
SIG
N M
AN
UA
L P
AR
T 3
CH
AP
TE
R 1
SE
CO
ND
ED
ITIO
N 1
983.
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
25 20 1535
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
kg)
(x 1
000
lb)
3035
77
4045
5055
6065
404582
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152 70
A/C
CO
DE
L
C −
K =
40
MN
/m³
(LO
W)
B −
K =
80
MN
/m³
(M
ED
IUM
)A
− K
= 1
50 M
N/m
³ (
HIG
H)
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)S
UB
GR
AD
E S
TR
EN
GT
H
N_AC_070902_1_0590101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E L
Aircraft Classification Number -- Rigid PavementFIGURE 10
7-9-2Page 11
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E M
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
M
65
148
152
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
N_AC_070902_1_0600101_01_00
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE 11
7-9-2Page 12
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
N
65
148
152
N_AC_070902_1_0610101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E N
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 38.
1 %
MA
C.
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
Aircraft Classification Number -- Rigid PavementFIGURE 12
7-9-2Page 13
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
O
65
148
152
N_AC_070902_1_0620101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E O
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
Aircraft Classification Number -- Rigid PavementFIGURE 13
7-9-2Page 14
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3 A/C
CO
DE
P
65
148
152
N_AC_070902_1_0630101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
5 ba
r (1
81 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E P
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 38.
1 %
MA
C.
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
Aircraft Classification Number -- Rigid PavementFIGURE 14
7-9-2Page 15
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
Q
75
N_AC_070902_1_0640101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E Q
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE 15
7-9-2Page 16
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
R
75
N_AC_070902_1_0650101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E R
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 37.
5 %
MA
C.
Aircraft Classification Number -- Rigid PavementFIGURE 16
7-9-2Page 17
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
S
75
N_AC_070902_1_0660101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E S
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE 17
7-9-2Page 18
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
T
75
N_AC_070902_1_0670101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E T
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36
% M
AC
.
Aircraft Classification Number -- Rigid PavementFIGURE 18
7-9-2Page 19
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
U
75
N_AC_070902_1_0680101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
12.
9 ba
r (1
87 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E U
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 37.
5 %
MA
C.
Aircraft Classification Number -- Rigid PavementFIGURE 19
7-9-2Page 20
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
15202530354045
70
(x 1
000
kg)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
6055
5045
403577
8286
9095
9910
410
811
211
712
112
613
013
413
914
3
65
148
5015
716
116
515
2 A/C
CO
DE
V
75
N_AC_070902_1_0690101_01_00
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
4 ba
r (1
94 p
si)
ON
PA
VE
ME
NT
− A
/C C
OD
E V
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m³
(U
LTR
A L
OW
)C
− K
=
40 M
N/m
³ (
LOW
)B
− K
=
80 M
N/m
³ (
ME
DIU
M)
A −
K =
150
MN
/m³
(H
IGH
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 36.
52 %
MA
C.
Aircraft Classification Number -- Rigid PavementFIGURE 20
7-9-2Page 21
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6.52
% 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)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
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
Aircraft Classification Number -- Rigid PavementFIGURE 21
7-9-2Page 22
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
X
55
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
80
N_AC_070902_1_0710101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E X
Aircraft Classification Number -- Rigid PavementFIGURE 22
7-9-2Page 23
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
Y
55
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
80
N_AC_070902_1_0720101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Y
Aircraft Classification Number -- Rigid PavementFIGURE 23
7-9-2Page 24
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
Z
55
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
80
N_AC_070902_1_0730101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E Z
Aircraft Classification Number -- Rigid PavementFIGURE 24
7-9-2Page 25
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
AA
55
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
80
N_AC_070902_1_0740101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
A
Aircraft Classification Number -- Rigid PavementFIGURE 25
7-9-2Page 26
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
AB
55
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
80
N_AC_070902_1_0750101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
B
Aircraft Classification Number -- Rigid PavementFIGURE 26
7-9-2Page 27
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**ON A/C A319-100
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.
SE
E S
EC
TIO
N 7
−4−
1 LA
ND
ING
GE
AR
LO
AD
ING
CG
US
ED
FO
R A
CN
CA
LCU
LAT
ION
S: 3
6 %
MA
C.
1520253035404550
3540
4550
5560
6570
75
AIR
CR
AF
T G
RO
SS
WE
IGH
T
46 x
17
R20
(46
x 1
6−20
) T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
13.
8 ba
r (2
00 p
si)
(x 1
000
kg)
(x 1
000
lb)
AIRCRAFT CLASSIFICATION NUMBER (ACN)
7782
8690
9599
104
108
112
117
121
126
130
134
139
143
148
152
157
161
174
165
170
A/C
CO
DE
AC
55
SU
BG
RA
DE
ST
RE
NG
TH
D −
K =
20
MN
/m
(ULT
RA
LO
W)
A −
K =
150
MN
/m
(HIG
H)
B −
K =
80
MN
/m
(ME
DIU
M)
C −
K =
40
MN
/m
(LO
W)
80
N_AC_070902_1_0770101_01_00
ON
PA
VE
ME
NT
− A
/C C
OD
E A
C
Aircraft Classification Number -- Rigid PavementFIGURE 27
7-9-2Page 28
May 01/11
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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
@A319AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING
**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