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@AIRBUS
A380
AIRPLANE CHARACTERISTICS
AC
The content of this document is the property of Airbus.It is supplied in confidence and commercial security on its contents must be maintained.It must not be used for any purpose other than that for which it is supplied, nor mayinformation contained in it be disclosed to unauthorized persons.It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorizedfor it must be addressed to Airbus.
© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.
Customer Services
Technical Data Support and Services
31707 Blagnac Cedex
FRANCE
Issue: Mar 30/05 Rev: Nov 01/08
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@A380 AIRPLANE CHARACTERISTICS
HIGHLIGHTS
Revision No. 7 - Nov 01/08
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 1
Section 1-2
Subject 1-2-0
Introduction R MINOR EDITORIAL CHANGES
Subject 1-2-1
Glossary R PART EFFECTIVITYADDED/REVISED/DELETED
CHAPTER 2
Section 2-1
Subject 2-1-1
General Airplane Characteristics data R Volume of cargo compartments updatedUsable Fuel Capacity updated - A380-800
ModelsVolume of Cockpit data incorporated -A380-800 ModelsVolume of Cargo Compartments updated -
A380-800 ModelsUsable Fuel Capacity updated - A380-800FModelsVolume of Cockpit data incorporated -
A380-800F ModelsPART EFFECTIVITYADDED/REVISED/DELETED
Section 2-2
Subject 2-2-0
FIGURE General Airplane Dimensions -
General Airplane Dimensions
R
Section 2-5
Subject 2-5-1
FIGURE Interior Arrangements - Cross-section - Typical Configuration - A380-800F Models All Decks
R
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Pneumatic System R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-8
Potable Water System - Pax R PART EFFECTIVITYADDED/REVISED/DELETED
Potable Water System - Freighter R MINOR EDITORIAL CHANGE.PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-9
Engine Oil Servicing R PART EFFECTIVITYADDED/REVISED/DELETED
VFG Oil Servicing R PART EFFECTIVITYADDED/REVISED/DELETED
Starter Oil Servicing R PART EFFECTIVITYADDED/REVISED/DELETED
APU Oil Servicing R PART EFFECTIVITYADDED/REVISED/DELETED
Subject 5-4-10
Vacuum Toilet System - Pax R PART EFFECTIVITYADDED/REVISED/DELETED
Vacuum Toilet System - Freighter R PART EFFECTIVITYADDED/REVISED/DELETED
Section 5-8
Subject 5-8-0
FIGURE Ground Towing Requirements -A380-800 Models
R REVISED ILLUSTRATION.
CHAPTER 6
Section 6-2
Subject 6-2-1Airport and Community Noise Data R REVISED PARAGRAPH, ADDITION OF
DESCRIPTION OF TEST CONDITION ANDMETEOROLOGICAL FOR GP7200ENGINES.
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Airport and Community NoiseData - TRENT 900 Engines
R REVISED ILLUSTRATION, N1PERCENTAGE DELETED.
FIGURE Airport and Community NoiseData - GP 7200 Engines
R
CHAPTER 7
Section 7-1
Subject 7-1-0
General Information R UPDATED DATAMinor correction in text descriptionPART EFFECTIVITYADDED/REVISED/DELETED
Section 7-2
Subject 7-2-0
Landing Gear Footprint - Pax R
FIGURE Landing Gear Footprint - MRW512 000 kg - A380-800 Models
N ILLUSTRATION ADDED
FIGURE Landing Gear Footprint - MRW562 000 kg - A380-800 Models
N ILLUSTRATION ADDED
FIGURE Landing Gear Footprint - MRW
571 000 kg - A380-800 Models
N ILLUSTRATION ADDED
Landing Gear Footprint - Freighter R
FIGURE Landing Gear Footprint - MRW592 000 kg - A380-800F Models
N ILLUSTRATION ADDED
FIGURE Landing Gear Footprint - MRW602 000 kg - A380-800F Models
N ILLUSTRATION ADDED
Section 7-3
Subject 7-3-0
Maximum Pavement Loads - Pax R
FIGURE Maximum Pavement Loads -MRW 512 000 kg - A380-800 Models
N ILLUSTRATION ADDED
FIGURE Maximum Pavement Loads -MRW 562 000 kg - A380-800 Models
R
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Maximum Pavement Loads -MRW 571 000 kg - A380-800 Models
R
FIGURE Maximum Pavement Loads -Freighter - MRW 592 000 kg - A380-800FModels
R
FIGURE Maximum Pavement Loads -MRW 602 000 kg- A380-800F Models
R
Section 7-4
Subject 7-4-0
Landing Gear Loading on Pavement R MINOR LAYOUT UPDATESADDED DATA WITH MRW 512000 KG
FOR A380-800.Subject 7-4-1
Landing Gear Loading on Pavement - Pax R
FIGURE Landing Gear Loading onPavement - MRW 512 000 kg - A380-800Models
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - MRW 562 000 kg - A380-800Models
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - MRW 571 000 kg - A380-800Models
N ILLUSTRATION ADDED
Landing Gear Loading on Pavement -Freighter
R
FIGURE Landing Gear Loading onPavement - MRW 592 000kg - A380-800FModels
N ILLUSTRATION ADDED
FIGURE Landing Gear Loading onPavement - MRW 602 000kg - A380-800FModels
N ILLUSTRATION ADDED
Subject 7-4-2
Wing Gear and Body Gear Loading onPavement
R MINOR LAYOUT UPDATESADDED INFORMATION FOR MRW 512000kg for A380-800
Subject 7-4-3
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Wing Gear and Body Gear Loading onPavement - Pax
R
FIGURE Wing Gear and Body Gear Loadson Pavement - MRW 512 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Wing Gear and Body Gear Loadson Pavement - MRW 562 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Wing Gear and Body Gear Loadson Pavement - MRW 571 000 kg -A380-800 Models
N ILLUSTRATION ADDED
Wing Gear and Body Gear Loading on
Pavement - Freighter
R
FIGURE Wing Gear and Body Gear Loadson Pavement - MRW 592 000 kg -A380-800F Models
N ILLUSTRATION ADDED
FIGURE Wing Gear and Body Gear Loadson Pavement - MRW 602 000 kg -A380-800F Models
N ILLUSTRATION ADDED
Section 7-5
Subject 7-5-0
Flexible Pavement Requirements - USArmy Corps of Engineers Design Method
R CHANGED MRW VALUE FROM 562000 KGTO 512000 KG AND FLEXIBLE PAVEMENTTHICKNESS FROM 58 CM TO 54 CM.
Subject 7-5-1
Flexible Pavement Requirements - USArmy Corps of Engineers Design Method -Pax
R
FIGURE Flexible Pavement Requirements-- 4 Wheel Bogie - MRW 512 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements-- 6 Wheel Bogie - MRW 512 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements-- 4 Wheel Bogie - MRW 562 000 kg -A380-800 Models
N ILLUSTRATION ADDED
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Flexible Pavement Requirements-- 6 Wheel Bogie - MRW 562 000 kg -
A380-800 Models
R
FIGURE Flexible Pavement Requirements-- 4 Wheel Bogie - MRW 571 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements-- 6 Wheel Bogie - MRW 571 000 kg -A380-800 Models
R
Flexible Pavement Requirements - USArmy Corps of Engineers Design Method -Freighter
R
FIGURE Flexible Pavement Requirements-- 4 Wheel Bogie - MRW 592 000 kg -A380-800F Models
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements-- 6 Wheel Bogie - MRW 592 000 kg -A380-800F Models
R
FIGURE Flexible Pavement Requirements-- 4 Wheel Bogie - MRW 602 000 kg -A380-800F Models
N ILLUSTRATION ADDED
FIGURE Flexible Pavement Requirements-- 6 Wheel Bogie - MRW 602 000 kg -A380-800F Models
R
Section 7-6
Subject 7-6-0
General R UPDATED MRW AND LCN VALUES
Subject 7-6-1
Flexible Pavement Requirements - LCNConversion - Pax
R
FIGURE Flex Pavement Requirements
LCN - 4 Wheel Bogie - MRW 512 000 kg- A380-800 Models
N ILLUSTRATION ADDED
FIGURE Flex Pavement RequirementsLCN - 6 Wheel Bogie - MRW 512 000 kg- A380-800 Models
N ILLUSTRATION ADDED
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Flex Pavement RequirementsLCN - 4 Wheel Bogie - MRW 562 000 kg
- A380-800 Models
R
FIGURE Flex Pavement RequirementsLCN - 6 Wheel Bogie - MRW 562 000 kg- A380-800 Models
R
FIGURE Flex Pavement RequirementsLCN - 4 Wheel Bogie - MRW 571 000 kg- A380-800 Models
R
FIGURE Flex Pavement RequirementsLCN - 6 Wheel Bogie - MRW 571 000 kg- A380-800 Models
R
FIGURE Flex Pavement RequirementsLCN - 4 Wheel Bogie - MRW 592 000 kg- A380-800F Models
R
FIGURE Flex Pavement RequirementsLCN - 6 Wheel Bogie - MRW 592 000 kg- A380-800F Models
R
FIGURE Flex Pavement RequirementsLCN - 4 Wheel Bogie - MRW 602 000 kg- A380-800F Models
R
FIGURE Flex Pavement Requirements
LCN - 6 Wheel Bogie - MRW 602 000 kg- A380-800F Models
R
Section 7-7
Subject 7-7-0
Rigid Pavement Requirements - PortlandCement Association Design Method
R UPDATED VALUES
Subject 7-7-1
Rigid Pavement Requirements - PortlandCement Association Design Method - Pax
R
FIGURE Rigid Pavement Requirements - 4Wheel Bogie - MRW 512 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements - 6Wheel Bogie - MRW 512 000 kg -A380-800 Models
N ILLUSTRATION ADDED
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Rigid Pavement Requirements - 4Wheel Bogie - MRW 562 000 kg -
A380-800 Models
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements - 6Wheel Bogie - MRW 562 000 kg -A380-800 Models
R
FIGURE Rigid Pavement Requirements - 4Wheel Bogie - MRW 571 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements - 6Wheel Bogie - MRW 571 000 kg -A380-800 Models
R
Rigid Pavement Requirements - PortlandCement Association Design Method -Freighter
R
FIGURE Rigid Pavement Requirements - 4Wheel Bogie - MRW 592 000 kg -A380-800F Models
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements - 6Wheel Bogie - MRW 592 000 kg -A380-800F Models
R
FIGURE Rigid Pavement Requirements - 4
Wheel Bogie - MRW 602 000 kg -A380-800F Models
N ILLUSTRATION ADDED
FIGURE Rigid Pavement Requirements - 6Wheel Bogie - MRW 602 000 kg -A380-800F Models
R
Section 7-8
Subject 7-8-0
Rigid Pavement Requirements - LCNConversion
R
Subject 7-8-2Rigid Pavement Requirements - LCNConversion - Pax
R
FIGURE Rigid Pavement RequirementsLCN - 4 Wheel Bogie - MRW 512 000 kg- A380-800 Models
N ILLUSTRATION ADDED
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Rigid Pavement RequirementsLCN - 6 Wheel Bogie - MRW 512 000 kg
- A380-800 Models
N ILLUSTRATION ADDED
FIGURE Rigid Pavement RequirementsLCN - 4 Wheel Bogie - MRW 562 000 kg- A380-800 Models
R
FIGURE Rigid Pavement RequirementsLCN - 6 Wheel Bogie - MRW 562 000 kg- A380-800 Models
R
FIGURE Rigid Pavement RequirementsLCN - 4 Wheel Bogie - MRW 571 000 kg- A380-800 Models
R
FIGURE Rigid Pavement RequirementsLCN - 6 Wheel Bogie - MRW 571 000 kg- A380-800 Models
R
FIGURE Rigid Pavement RequirementsLCN - 4 Wheel Bogie - MRW 592 000 kg- A380-800F Models
R
FIGURE Rigid Pavement RequirementsLCN - 6 Wheel Bogie - MRW 592 000 kg- A380-800F Models
R
FIGURE Rigid Pavement Requirements
LCN - 4 Wheel Bogie - MRW 602 000 kg- A380-800F Models
R
FIGURE Rigid Pavement RequirementsLCN - 6 Wheel Bogie - MRW 602 000 kg- A380-800F Models
R
Subject 7-8-3 R
Radius of Relative Stiffness (Other valuesof E and µ)
R DESCRIPTION TITLE UPDATED
Subject 7-8-4 R
Radius of Relative Stiffness (Other valuesof E and µ)
R DESCRIPTION TITLE UPDATED
Section 7-9
Subject 7-9-0
ACN/PCN Reporting System R
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Subject 7-9-1
Aircraft Classification Number - FlexiblePavement - Pax R
FIGURE Aircraft Classification Number -Flexible Pavement - MRW 512 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - MRW 562 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - MRW 571 000 kg -A380-800 Models
N ILLUSTRATION ADDED
Aircraft Classification Number - FlexiblePavement - Freighter
R
FIGURE Aircraft Classification Number -Flexible Pavement - MRW 592 000 kg -A380-800F Models
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Flexible Pavement - MRW 602 000 kg -A380-800F Models
N ILLUSTRATION ADDED
Subject 7-9-2
Aircraft Classification Number - RigidPavement - Pax
R
FIGURE Aircraft Classification Number -Rigid Pavement - MRW 512 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Rigid Pavement - MRW 562 000 kg -A380-800 Models
N ILLUSTRATION ADDED
FIGURE Aircraft Classification Number -Rigid Pavement - MRW 571 000 kg -
A380-800 Models
N ILLUSTRATION ADDED
Aircraft Classification Number - RigidPavement - Freighter
R
FIGURE Aircraft Classification Number -Rigid Pavement - MRW 592 000 kg -A380-800F Models
N ILLUSTRATION ADDED
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@A380 AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Aircraft Classification Number -Rigid Pavement - MRW 602 000 kg -
A380-800F Models
N ILLUSTRATION ADDED
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@A380 AIRPLANE CHARACTERISTICS
LIST OF EFFECTIVE CONTENT
Revision No. 7 - Nov 01/08
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 1
Subject 1-1-0
Purpose Jun 01/07
Subject 1-2-0
Introduction R Nov 01/08
Subject 1-2-1
Glossary R Nov 01/08
CHAPTER 2
Subject 2-1-0
General Airplane Characteristics Jun 01/07
Subject 2-1-1
General Airplane Characteristics data R Nov 01/08
Subject 2-2-0
General Airplane Dimensions Data Jun 01/07
FIGURE General Airplane Dimensions - General Airplane Dimensions R Nov 01/08Subject 2-3-0
Ground Clearances - Pax Jun 01/07
FIGURE Ground Clearances - A380-800 Models Jun 01/07
Ground Clearances - Freighter Jun 01/07
FIGURE Ground clearances - A380-800F Models Jun 01/07
Subject 2-4-0
Interior Arrangement - Plan View Jun 01/07
Subject 2-4-1
Standard Configuration - Pax Jun 01/07
FIGURE Interior Arrangements - Plan View - Standard Configuration- Upper Deck
Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Interior Arrangements - Plan View - Standard Configuration- Main Deck
Jun 01/07
Standard Configuration - Freighter Jun 01/07
FIGURE Interior Arrangements - Plan View - Standard Configuration Jun 01/07
Subject 2-5-0
Interior Arrangements - Cross Section Jun 01/07
Subject 2-5-1
Typical Configuration - Pax Jun 01/07
FIGURE Interior Arrangements - Cross-section - Typical Configuration- Upper Deck
Jun 01/07
FIGURE Interior Arrangements - Cross-section - Typical Configuration- Main Deck
Jun 01/07
Typical Configuration - Freighter Jun 01/07
FIGURE Interior Arrangements - Cross-section - Typical Configuration- A380- 800F Models All Decks
R Nov 01/08
Subject 2-6-0
Cargo Compartments Jun 01/07
Subject 2-6-1
Location and Dimensions - Pax Jun 01/07FIGURE Cargo Compartments - Location and Dimensions Jun 01/07
Location and Dimensions - Freighter Jun 01/07
FIGURE Cargo Compartments - Location and Dimensions (Sheet 1) Jun 01/07
FIGURE Cargo Compartments - Location and Dimensions (Sheet 2) Jun 01/07
Subject 2-6-2
Loading Combinations - Pax Jun 01/07
FIGURE Cargo Compartments - Loading Combinations Jun 01/07
Loading Combinations - Freighter Jun 01/07FIGURE Cargo Compartments - Loading Combinations (Sheet 1) Jun 01/07
FIGURE Cargo Compartments - Loading Combinations (Sheet 2) Jun 01/07
Subject 2-7-0
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Door Clearances - Pax Jun 01/07
FIGURE Door Clearances - Door Location (Sheet 1) - A380-800Models Jun 01/07
FIGURE Door Clearances - Door Location (Sheet 2) - A380-800Models
Jun 01/07
Door Clearances - Freighter Jun 01/07
FIGURE Door Clearances - Door Location (Sheet 1) - A380-800FModels
Jun 01/07
FIGURE Door Clearances - Door Location (Sheet 2) - A380-800FModels
Jun 01/07
Subject 2-7-1
Forward Doors Jun 01/07
FIGURE Door Clearances - Forward Doors Jun 01/07
Subject 2-7-2
Main and Upper Deck Doors - Pax Jun 01/07
FIGURE Door Clearances - Main and Upper Deck Doors - A380-800Models
Jun 01/07
Upper Deck Door - Freighter Jun 01/07
FIGURE Door Clearances - Upper Deck Door - A380-800F Models Jun 01/07
Subject 2-7-3
Aft Doors - Pax Jun 01/07
FIGURE Door Clearances - Aft Doors - A380-800 Models Jun 01/07
Aft Doors - Freighter Jun 01/07
FIGURE Door Clearances - Aft Doors - A380-800F Models Jun 01/07
Subject 2-7-4
Aft Cargo Compartment Doors - Pax Jun 01/07
FIGURE Door Clearances - Aft Cargo Compartment Doors -A380-800 Models
Jun 01/07
Aft Cargo Compartment Doors - Freighter Jun 01/07
FIGURE Door Clearances - Main Deck Cargo Door - A380-800FModels
Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Door Clearances - Lower Deck Aft Cargo Doors - A380-800FModels
Jun 01/07
Subject 2-7-5
Forward Cargo Compartment Doors - Pax Jun 01/07
FIGURE Door Clearances - Forward Cargo Compartment Doors -A380-800 Models
Jun 01/07
Forward Cargo Compartment Doors - Freighter Jun 01/07
FIGURE Door Clearances - Upper Deck Cargo Door - A380-800FModels
Jun 01/07
FIGURE Door Clearances - Lower Deck Forward Cargo Door -A380-800F Models
Jun 01/07
Subject 2-7-6
Nose Landing Gear Doors Jun 01/07
FIGURE Door Clearances - Forward Nose Landing Gear Doors Jun 01/07
FIGURE Door Clearances - Aft Nose Landing Gear Doors Jun 01/07
Subject 2-7-7
Wing Landing Gear Doors Jun 01/07
FIGURE Door Clearances - Wing Landing Gear Doors Jun 01/07
Subject 2-7-8
Body Landing Gear Doors Jun 01/07
FIGURE Door Clearances - Body Landing Gear Doors (Sheet 1) Jun 01/07
FIGURE Door Clearances - Body Landing Gear Doors (Sheet 2) Jun 01/07
Subject 2-7-9
APU Doors Jun 01/07
FIGURE Door Clearances - APU Doors Jun 01/07
CHAPTER 3
Subject 3-1-0
General Information R Nov 01/08
Subject 3-2-0
Payload /Range Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Subject 3-2-1
Payload/Range - Pax Jun 01/07FIGURE Payload/Range - ISA Conditions - TRENT 900 Engines Jun 01/07
FIGURE Payload/Range - ISA Conditions - GP 7200 Engines Jun 01/07
Payload/Range - Freighter Jun 01/07
FIGURE Payload/Range - ISA Conditions - TRENT 900 Engines Jun 01/07
FIGURE Payload/Range - ISA Conditions - GP 7200 Engines Jun 01/07
Subject 3-3-0
Take Off Weight Limitation Jun 01/07
Subject 3-3-1Take Off Weight Limitation - Pax Jun 01/07
FIGURE Take-Off Weight Limitation - ISA Conditions - TRENT 900Engines
Jun 01/07
FIGURE Take-Off Weight Limitation - ISA Conditions - GP 7200Engines
Jun 01/07
Take-Off Weight Limitation - Freighter Jun 01/07
FIGURE Take-Off Weight Limitation - ISA Conditions - TRENT 900Engines
Jun 01/07
FIGURE Take-Off Weight Limitation - ISA Conditions - GP 7200Engines
Jun 01/07
Subject 3-3-2
ISA + 15 ̊ C (59 ̊ F) - Pax Jun 01/07
FIGURE Take-Off Weight Limitation - ISA + 15 ˚C (59 ˚F) -TRENT 900 Engines
Jun 01/07
FIGURE Take-Off Weight Limitation - ISA + 15 ˚C (59 ˚F) - GP7200 Engines
Jun 01/07
ISA + 15 ̊ C (59 ̊ F) - Freighter Jun 01/07FIGURE Take-Off Weight Limitation - ISA + 15 ˚C (59 ˚F) -TRENT 900 Engines
Jun 01/07
FIGURE Take-Off Weight Limitation - ISA + 15 ˚C (59 ˚F) - GP7200 Engines
Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Subject 3-4-0
Landing Field Length Jun 01/07Subject 3-4-1
Landing Field Length - Pax Jun 01/07
FIGURE Landing Field Length - Landing Field Length - A380-800Models
Jun 01/07
Landing Field Length - Freighter Jun 01/07
FIGURE Landing Field Length - Landing Field Length - A380-800FModels
R Nov 01/08
Subject 3-5-0
Final Approach Speed Jun 01/07
Subject 3-5-1
Final Approach Speed - Pax Jun 01/07
FIGURE Final Approach Speed (CG=29%) - A380-800 Models Jun 01/07
Final Approach Speed - Freighter Jun 01/07
FIGURE Final Approach Speed (CG=29%) - A380-800F Models Jun 01/07
CHAPTER 4
Subject 4-1-0
General Jun 01/07
Subject 4-2-0
Turning Radii Jun 01/07
FIGURE Turning Radii - Turning Radii (Sheet 1) Jun 01/07
FIGURE Turning Radii - Turning Radii (Sheet 2) Jun 01/07
Subject 4-3-0
Minimum Turning Radii Jun 01/07
FIGURE Minimum Turning Radii - Minimum Turning Radii Jun 01/07Subject 4-4-0
Visibility from Cockpit in Static Position Jun 01/07
FIGURE Visibility from Cockpit in Static Position - Visibility fromCockpit in Static Position
Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Subject 4-5-0
Runway and Taxiway Turn Paths Jun 01/07Subject 4-5-1
135˚ Turn - Runway to Taxiway Jun 01/07
FIGURE 135˚ Turn -- Runway to Taxiway - 135˚ Turn -- Runway toTaxiway (Sheet 1)
Jun 01/07
FIGURE 135˚ Turn -- Runway to Taxiway - 135˚ Turn -- Runway toTaxiway (Sheet 2)
Jun 01/07
Subject 4-5-2
90˚ Turn - Runway to Taxiway Jun 01/07
FIGURE 90˚ Turn -- Runway to Taxiway - 90˚ Turn -- Runway toTaxiway (Sheet 1)
Jun 01/07
FIGURE 90˚ Turn -- Runway to Taxiway - 90˚ Turn -- Runway toTaxiway (Sheet 2)
Jun 01/07
Subject 4-5-3
180˚ Turn on a Runway Jun 01/07
FIGURE 180˚ Turn on a Runway - 180˚ Turn on a Runway Jun 01/07
Subject 4-5-4
90˚ Turn - Taxiway to Taxiway Jun 01/07
FIGURE 90˚ Turn -- Taxiway to Taxiway - 90˚ Turn -- Taxiway toTaxiway (Sheet 1)
Jun 01/07
FIGURE 90˚ Turn -- Taxiway to Taxiway - 90˚ Turn -- Taxiway toTaxiway (Sheet 2)
Jun 01/07
Subject 4-5-5
135˚ Turn - Taxiway to Taxiway Jun 01/07
FIGURE 135˚ Turn -- Taxiway to Taxiway - 135˚ Turn -- Taxiway toTaxiway (Sheet 1)
Jun 01/07
FIGURE 135˚ Turn -- Taxiway to Taxiway - 135˚ Turn -- Taxiway toTaxiway (Sheet 2)
Jun 01/07
Subject 4-6-0
Runway Holding Bay (Apron) Jun 01/07
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FIGURE Runway Holding Bay (Apron) - Runway Holding Bay(Apron)
Jun 01/07
Subject 4-7-0
Airplane Parking Jun 01/07
FIGURE Airplane Parking - Steering Geometry Jun 01/07
FIGURE Airplane Parking - Minimum Parking Space Requirements Jun 01/07
Subject 4-8-0
General Jun 01/07
FIGURE Airplane Mooring - Airplane Mooring Jun 01/07
CHAPTER 5Subject 5-1-0
Airplane Servicing Arrangements Jun 01/07
Subject 5-1-1
Typical Ramp Layout - Two Bridges - Standard Servicing Jun 01/07
FIGURE Baseline Ramp Layout -- Two Bridges - Servicing Via Mainand Upper Decks
Jun 01/07
Subject 5-1-2
Typical Ramp Layout - Two Bridges - Servicing Via Main Deck Jan 31/08FIGURE Typical Ramp Layout -- Two Bridges - Servicing Via MainDeck
Jun 01/07
Subject 5-1-3
Opportunities of Direct Upper Deck Access for Airport and Airlines Jan 31/08
FIGURE Opportunities of Direct Upper Deck Access - for Airport andAirlines
Jun 01/07
Subject 5-1-4
Baseline Ramp Layout Jun 01/07
FIGURE Baseline Ramp Layout - Baseline Ramp Layout Jun 01/07
Subject 5-2-0
Terminal Operation - Passenger Aircraft Jun 01/07
Subject 5-2-1
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CONTENT CHGCODE
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Typical Turn-Round Time - Two Bridges - Standard Servicing ViaMain Deck and Upper Decks
Jun 01/07
FIGURE Typical Turn-Round Time -- Two Bridges - Servicing ViaMain and Upper Decks
Jun 01/07
Subject 5-2-2
Typical Turn-Round Time - Two Bridges - Servicing Via Main Deck Jun 01/07
FIGURE Typical Turn-Round Time -- Two Bridges - Servicing ViaMain Deck
Jun 01/07
Subject 5-3-0
Terminal Operation - Cargo Aircraft Jun 01/07
Subject 5-3-1Typical Turn-Round Time Jun 01/07
Subject 5-4-0
Ground Service Connections Jan 31/08
Subject 5-4-1
Ground Service Connections Layout - Pax Jun 01/07
FIGURE Ground Service Connections - Ground Service ConnectionsLayout - A380-800 Models
Jun 01/07
Ground Service Connections Layout - Freighter Jun 01/07FIGURE Ground Service Connections - Ground Service ConnectionsLayout - A380-800F Models
Jun 01/07
Subject 5-4-2
Grounding Points R Nov 01/08
FIGURE Ground Points NLG - Ground Points NLG Jun 01/07
FIGURE Ground Point WLG - Ground Point WLG Jun 01/07
FIGURE Ground Points BLG - Ground Points BLG Jun 01/07
Subject 5-4-3Hydraulic System R Nov 01/08
FIGURE Ground Service Connections - Hydraulical Reservoir ServicingPanel
Jun 01/07
FIGURE Ground Service Connections - Hydraulic Ground Connections Jun 01/07
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CONTENT CHGCODE
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Subject 5-4-4
Electrical System - Pax R Nov 01/08FIGURE Ground Service Connections - Electrical Service Panel -A380-800 Models
Jun 01/07
Electrical System - Freighter R Nov 01/08
FIGURE Ground Service Connections - Electrical Service Panel -A380-800F Models
Jun 01/07
Subject 5-4-5
Oxygen System R Nov 01/08
FIGURE Ground Service Connections - Oxygen System Jun 01/07
Subject 5-4-6
Fuel System R Nov 01/08
FIGURE Ground Service Connections - Refuel/Defuel Control Panel Jun 01/07
FIGURE Ground Service Connections - Pressure Refuel Connections Jun 01/07
Subject 5-4-7
Pneumatic System R Nov 01/08
FIGURE Ground Service Connections - Low Pressure PreconditionedAir
Jun 01/07
FIGURE Ground Service Connections - High Pressure PreconditionedAir
Jun 01/07
Subject 5-4-8
Potable Water System - Pax R Nov 01/08
FIGURE Ground Service Connections - Potable Water Ground ServicePanel - A380-800 Models
Jun 01/07
FIGURE Ground Service Connections - Potable Water Drain Panel -A380-800 Models
Jun 01/07
Potable Water System - Freighter R Nov 01/08
FIGURE Ground Service Connections - Potable Water Ground ServicePanel - A380-800F Models
Jun 01/07
Subject 5-4-9
Engine Oil Servicing R Nov 01/08
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CONTENT CHGCODE
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FIGURE Ground Service Connections - Engine Oil Servicing - TRENT900 Engines
Jun 01/07
FIGURE Ground Service Connections - Engine Oil Servicing - GP7200 Engines
Jun 01/07
VFG Oil Servicing R Nov 01/08
FIGURE Ground Service Connections - VFG Oil Servicing - TRENT900 Engines
Jun 01/07
FIGURE Ground Service Connections - VFG Oil Servicing - GP 7200Engines
Jun 01/07
Starter Oil Servicing R Nov 01/08
FIGURE Ground Service Connections - Starter Oil Servicing - TRENT900 Engines
Jun 01/07
FIGURE Ground Service Connections - Starter Oil Servicing - GP7200 Engines
Jun 01/07
APU Oil Servicing R Nov 01/08
FIGURE Ground Service Connections - APU Oil Servicing Jun 01/07
Subject 5-4-10
Vacuum Toilet System - Pax R Nov 01/08
FIGURE Ground Service Connections - Vacuum Toilet System -A380-800 Models
Jun 01/07
Vacuum Toilet System - Freighter R Nov 01/08
FIGURE Ground Service Connections - Vacuum Toilet System -A380-800F Models
Jun 01/07
Subject 5-5-0
Engine Starting Pneumatic Requirements Jun 01/07
Subject 5-5-1
Outside Air Temperature = -40 ̊ C (-40 ̊ F) Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature -40 ˚C (-40 ˚F), sea level -TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature -40˚C (-40˚F), sea level - GP7200 Engines
Jun 01/07
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CONTENT CHGCODE
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FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature -40˚C (-40˚F), Sea
Level - TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature -40˚C (-40˚F), SeaLevel - GP 7200 Engines
Jun 01/07
Subject 5-5-2
Outside Air Temperature = 15 ̊ C (59 ̊ F) Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature +15˚C (+59˚F), Sea Level -TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature +15˚C (+59˚F), Sea Level -GP 7200 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature +15˚C (+59˚F), 5000FTLevel - TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature +15˚C (+59˚F), 5000FTLevel - GP 7200 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature +15˚C (+59˚F), SeaLevel - TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature +15˚C (+59˚F), SeaLevel - GP 7200 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature +15˚C (+59˚F),5000FT Level - TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (three high
pressure ground carts) - Ambient Temperature +15˚C (+59˚F),5000FT Level - GP 7200 Engines
Jun 01/07
Subject 5-5-3
Outside Air Temperature = 50˚C (122 ̊ F) Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature +55˚C (+131˚F), Sea Level -
TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (two high pressureground carts) - Ambient Temperature +55˚C (+131˚F), Sea Level -GP 7200 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature +55˚C (+131˚F),Sea Level - TRENT 900 Engines
Jun 01/07
FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature +55˚C (+131˚F),
Sea Level - GP 7200 Engines
Jun 01/07
Subject 5-6-0
Ground Pneumatic Power Requirements Jun 01/07
Subject 5-6-1
Heating Jun 01/07
FIGURE Ground Pneumatic Power Requirements Heating - GroundPneumatic Power Requirements Heating - A380-800 Models
Jun 01/07
FIGURE Ground Pneumatic Power Requirements Heating - GroundPneumatic Power Requirements Heating - A380-800F Models
Jun 01/07
Subject 5-6-2
Cooling Jun 01/07
FIGURE Ground Pneumatic Power Requirements Cooling - GroundPneumatic Power Requirements Cooling - A380-800 Models
Jun 01/07
FIGURE Ground Pneumatic Power Requirements Cooling - GroundPneumatic Power Requirements Cooling - A380-800F Models
Jun 01/07
Subject 5-7-0
Preconditioned Airflow Requirements Jun 01/07
FIGURE Preconditioned Airflow Requirements - PreconditionedAirflow Requirements - A380-800 Models
Jun 01/07
FIGURE Preconditioned Airflow Requirements - PreconditionedAirflow Requirements - A380-800F Models
Jun 01/07
Subject 5-8-0
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Ground Towing Requirements Jan 31/08
FIGURE Ground Towing Requirements - A380-800 Models R Nov 01/08
CHAPTER 6
Subject 6-1-0
Engine Exhaust Velocities and Temperatures Jun 01/07
Subject 6-1-1
Engine Exhaust Velocities - Ground Idle Power Jun 01/07
FIGURE Engine Exhaust Velocities - Ground Idle Power - TRENT 900Engines
Jun 01/07
FIGURE Engine Exhaust Velocities - Ground Idle Power - GP 7200Engines
Jun 01/07
Subject 6-1-2
Engine Exhaust Temperatures - Ground Idle Power Jun 01/07
FIGURE Engine Exhaust Temperatures - Ground Idle Power - TRENT900 Engines
Jun 01/07
FIGURE Engine Exhaust Temperatures - Ground Idle Power - GP7200 Engines
Jun 01/07
Subject 6-1-3
Engine Exhaust Velocities - Breakaway Power Jun 01/07
FIGURE Engine Exhaust Velocities - Breakaway Power - TRENT 900Engines
Jun 01/07
FIGURE Engine Exhaust Velocities - Breakaway Power - GP 7200Engines
Jun 01/07
Subject 6-1-4
Engine Exhaust Temperatures - Breakaway Power Jun 01/07
FIGURE Engine Exhaust Temperatures - Breakaway Power - TRENT
900 Engines
Jun 01/07
FIGURE Engine Exhaust Temperatures - Breakaway Power - GP 7200Engines
Jun 01/07
Subject 6-1-5
Engine Exhaust Velocities - Max Take-off Power Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Exhaust Velocities - Max. Take-Off Power - TRENT900 Engines
Jun 01/07
FIGURE Engine Exhaust Velocities - Max. Take-Off Power - GP 7200Engines
Jun 01/07
Subject 6-1-6
Engine Exhaust Temperatures - Max Take-off Power Jun 01/07
FIGURE Engine Exhaust Temperatures - Max Take-Off Power -TRENT 900 Engines
Jun 01/07
FIGURE Engine Exhaust Temperatures - Max Take-Off Power - GP7200 Engines
Jun 01/07
Subject 6-2-0Airport and Community Noise Data Jun 01/07
Subject 6-2-1
Airport and Community Noise Data R Nov 01/08
FIGURE Airport and Community Noise Data - TRENT 900 Engines R Nov 01/08
FIGURE Airport and Community Noise Data - GP 7200 Engines R Nov 01/08
Subject 6-3-0
Danger Areas of the Engines Jun 01/07
Subject 6-3-1Danger Areas of the Engines - Ground Idle Power Jun 01/07
FIGURE Danger Areas of the Engines - Ground Idle Power - TRENT900 Engines
Jun 01/07
FIGURE Danger Areas of the Engines - Ground Idle Power - GP 7200Engines
Jun 01/07
Subject 6-3-2
Danger Areas of the Engines - Max. Take-Off Power Jun 01/07
FIGURE Danger Areas of the Engines - Max Take-Off Power -TRENT 900 Engines Jun 01/07
FIGURE Danger Areas of the Engines - Max Take-Off Power - GP7200 Engines
Jun 01/07
Subject 6-3-3
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CONTENT CHGCODE
LAST REVISIONDATE
Danger Areas of the Engines - Breakaway Power Jun 01/07
FIGURE Danger Areas of the Engines - Breakaway Power - TRENT900 Engines Jun 01/07
FIGURE Danger Areas of the Engines - Breakaway Power - GP 7200Engines
Jun 01/07
Subject 6-4-0
APU Exhaust Velocities and Temperatures Jun 01/07
Subject 6-4-1
APU Exhaust Velocities and Temperatures Jun 01/07
FIGURE APU Exhaust Velocities and Temperatures - Max. ECS
Conditions
Jun 01/07
Subject 6-4-2
APU Exhaust Velocities and Temperatures - MES Conditions Jun 01/07
FIGURE APU Exhaust Velocities and Temperatures - MES Conditions Jun 01/07
CHAPTER 7
Subject 7-1-0
General Information R Nov 01/08
Subject 7-2-0
Landing Gear Footprint - Pax R Nov 01/08
FIGURE Landing Gear Footprint - MRW 512 000 kg - A380-800Models
N Nov 01/08
FIGURE Landing Gear Footprint - MRW 562 000 kg - A380-800Models
N Nov 01/08
FIGURE Landing Gear Footprint - MRW 571 000 kg - A380-800Models
N Nov 01/08
Landing Gear Footprint - Freighter R Nov 01/08
FIGURE Landing Gear Footprint - MRW 592 000 kg - A380-800FModels
N Nov 01/08
FIGURE Landing Gear Footprint - MRW 602 000 kg - A380-800FModels
N Nov 01/08
Subject 7-3-0
Maximum Pavement Loads - Pax R Nov 01/08
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CONTENT CHGCODE
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FIGURE Maximum Pavement Loads - MRW 512 000 kg - A380-800Models
N Nov 01/08
FIGURE Maximum Pavement Loads - MRW 562 000 kg - A380-800Models
R Nov 01/08
FIGURE Maximum Pavement Loads - MRW 571 000 kg - A380-800Models
R Nov 01/08
Maximum Pavement Loads - Freighter Jun 01/07
FIGURE Maximum Pavement Loads - Freighter - MRW 592 000 kg -A380-800F Models
R Nov 01/08
FIGURE Maximum Pavement Loads - MRW 602 000 kg- A380-800FModels
R Nov 01/08
Subject 7-4-0Landing Gear Loading on Pavement R Nov 01/08
Subject 7-4-1
Landing Gear Loading on Pavement - Pax R Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 512 000 kg -A380-800 Models
N Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 562 000 kg -A380-800 Models
N Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 571 000 kg -
A380-800 Models
N Nov 01/08
Landing Gear Loading on Pavement - Freighter R Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 592 000kg -A380-800F Models
N Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 602 000kg -A380-800F Models
N Nov 01/08
Subject 7-4-2
Wing Gear and Body Gear Loading on Pavement R Nov 01/08
Subject 7-4-3
Wing Gear and Body Gear Loading on Pavement - Pax R Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 512000 kg - A380-800 Models
N Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 562000 kg - A380-800 Models
N Nov 01/08
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 571000 kg - A380-800 Models
N Nov 01/08
Wing Gear and Body Gear Loading on Pavement - Freighter R Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 592000 kg - A380-800F Models
N Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 602000 kg - A380-800F Models
N Nov 01/08
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method
R Nov 01/08
Subject 7-5-1Flexible Pavement Requirements - US Army Corps of EngineersDesign Method - Pax
R Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW512 000 kg - A380-800 Models
N Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW512 000 kg - A380-800 Models
N Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW562 000 kg - A380-800 Models
N Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW562 000 kg - A380-800 Models
R Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW571 000 kg - A380-800 Models
N Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW571 000 kg - A380-800 Models
R Nov 01/08
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method - Freighter
R Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW
592 000 kg - A380-800F Models
N Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW592 000 kg - A380-800F Models
R Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW602 000 kg - A380-800F Models
N Nov 01/08
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW602 000 kg - A380-800F Models
R Nov 01/08
Subject 7-6-0
General R Nov 01/08
Subject 7-6-1
Flexible Pavement Requirements - LCN Conversion - Pax R Nov 01/08
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW512 000 kg - A380-800 Models
N Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW512 000 kg - A380-800 Models
N Nov 01/08
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW562 000 kg - A380-800 Models
R Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW562 000 kg - A380-800 Models
R Nov 01/08
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW571 000 kg - A380-800 Models
R Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW571 000 kg - A380-800 Models
R Nov 01/08
For A380-800F ModelsFlexible Pavement Requirements - LCN
Conversion - Freighter
Jun 01/07
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW592 000 kg - A380-800F Models
R Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW592 000 kg - A380-800F Models
R Nov 01/08
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW602 000 kg - A380-800F Models
R Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW602 000 kg - A380-800F Models
R Nov 01/08
Subject 7-7-0Rigid Pavement Requirements - Portland Cement Association DesignMethod
R Nov 01/08
Subject 7-7-1
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Rigid Pavement Requirements - Portland Cement Association DesignMethod - Pax
R Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 512000 kg - A380-800 Models
N Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 512000 kg - A380-800 Models
N Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 562000 kg - A380-800 Models
N Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 562000 kg - A380-800 Models
R Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 571
000 kg - A380-800 Models
N Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 571000 kg - A380-800 Models
R Nov 01/08
Rigid Pavement Requirements - Portland Cement Association DesignMethod - Freighter
R Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 592000 kg - A380-800F Models
N Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 592000 kg - A380-800F Models
R Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 602000 kg - A380-800F Models
N Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 602000 kg - A380-800F Models
R Nov 01/08
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion R Nov 01/08
Subject 7-8-1
Radius of Relative Stiffness Jun 01/07
FIGURE Radius of Relative Stiffness - Radius of Relative Stiffness Jun 01/07Subject 7-8-2
Rigid Pavement Requirements - LCN Conversion - Pax R Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW512 000 kg - A380-800 Models
N Nov 01/08
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW512 000 kg - A380-800 Models
N Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW562 000 kg - A380-800 Models
R Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW562 000 kg - A380-800 Models
R Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW571 000 kg - A380-800 Models
R Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW571 000 kg - A380-800 Models
R Nov 01/08
Rigid Pavement Requirements - LCN Conversion - Freighter Jun 01/07
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW592 000 kg - A380-800F Models
R Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW592 000 kg - A380-800F Models
R Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW602 000 kg - A380-800F Models
R Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW602 000 kg - A380-800F Models
R Nov 01/08
Subject 7-8-3Radius of Relative Stiffness (Other values of E and µ) R Nov 01/08
Subject 7-8-4
Radius of Relative Stiffness (Other values of E and µ) R Nov 01/08
FIGURE Radius of Relative Stiffness - Radius of Relative Stiffness Jun 01/07
Subject 7-9-0
ACN/PCN Reporting System R Nov 01/08
Subject 7-9-1
Aircraft Classification Number - Flexible Pavement - Pax R Nov 01/08FIGURE Aircraft Classification Number - Flexible Pavement - MRW512 000 kg - A380-800 Models
N Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW562 000 kg - A380-800 Models
N Nov 01/08
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@A380 AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Aircraft Classification Number - Flexible Pavement - MRW571 000 kg - A380-800 Models
N Nov 01/08
Aircraft Classification Number - Flexible Pavement - Freighter R Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW592 000 kg - A380-800F Models
N Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW602 000 kg - A380-800F Models
N Nov 01/08
Subject 7-9-2
Aircraft Classification Number - Rigid Pavement - Pax R Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 512
000 kg - A380-800 Models
N Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 562000 kg - A380-800 Models
N Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 571000 kg - A380-800 Models
N Nov 01/08
Aircraft Classification Number - Rigid Pavement - Freighter R Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 592000 kg - A380-800F Models
N Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 602
000 kg - A380-800F Models
N Nov 01/08
CHAPTER 8
Subject 8-1-0
Possible Future Derivative Airplanes Jun 01/07
CHAPTER 9
Subject 9-1-0
Scaled Drawing - 1 cm. = 500 cm. Jun 01/07
FIGURE Scaled Drawing -- 1 cm = 500 cm - A380-800 Models Jun 01/07FIGURE Scaled Drawing -- 1 cm = 500 cm - A380-800F Models Jun 01/07
FIGURE Scaled Drawing -- 1 cm = 500 cm - A380-800 Models Jun 01/07
FIGURE Scaled Drawing -- 1 cm = 500 cm - A380-800F Models Jun 01/07
Subject 9-2-0
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CONTENT CHGCODE
LAST REVISIONDATE
Scaled Drawing - 1 in. = 50 ft. Jun 01/07
FIGURE Scaled Drawing -- 1 in = 50 ft - A380-800 Models Jun 01/07FIGURE Scaled Drawing -- 1 in = 50 ft - A380-800F Models Jun 01/07
FIGURE Scaled Drawing -- 1 in = 50 ft - A380-800 Models Jun 01/07
FIGURE Scaled Drawing -- 1 in = 50 ft - A380-800F Models Jun 01/07
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@A380 AIRPLANE CHARACTERISTICS
TABLE OF CONTENTS
1 SCOPE
1-1-0 Purpose
1-2-0 Introduction
1-2-1 Glossary
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 Arrangement - Plan View2-4-1 Standard Configuration
2-5-0 Interior Arrangements - Cross Section
2-5-1 Typical Configuration
2-6-0 Cargo Compartments
2-6-1 Location and Dimensions
2-6-2 Loading Combinations
2-7-0 Door Clearances
2-7-1 Forward Doors
2-7-2 Main and Upper Deck Doors2-7-3 Aft Doors
2-7-4 Aft Cargo Compartment Doors
2-7-5 Forward Cargo Compartment Doors
2-7-6 Nose Landing Gear Doors
2-7-7 Wing Landing Gear Doors
2-7-8 Body Landing Gear Doors
2-7-9 APU Doors
3 AIRPLANE PERFORMANCE
3-1-0 General Information3-2-0 Payload / Range
3-2-1 ISA Conditions
3-3-0 Take Off Weight Limitation
3-3-1 ISA Conditions
3-3-2 ISA + 15 ˚C (59 ˚F)
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3-4-0 Landing Field Length
3-4-1 Landing Field Length
3-5-0 Final Approach Speed
3-5-1 Final Approach Speed
4 GROUND MANEUVERING
4-1-0 General Information
4-2-0 Turning Radii
4-3-0 Minimum Turning Radii
4-4-0 Visibility from Cockpit in Static Position
4-5-0 Runway and Taxiway Turn Paths
4-5-1 135˚ Turn - Runway to Taxiway
4-5-2 90˚ Turn - Runway to Taxiway
4-5-3 180˚ Turn on a Runway4-5-4 90˚ Turn - Taxiway to Taxiway
4-5-5 135˚ Turn - Taxiway to Taxiway
4-6-0 Runway Holding Bay (Apron)
4-7-0 Airplane Parking
4-8-0 Airplane Mooring
5 TERMINAL SERVICING
5-1-0 Airplane Servicing Arrangements
5-1-1 Typical Ramp Layout - Two Bridges - Standard Servicing Via Main Deck and Upper Deck
5-1-2 Typical Ramp Layout - Two Bridges - Servicing Via Main Deck
5-1-3 Opportunities of Direct Upper Deck Access for Airport and Airlines
5-1-4 Baseline Ramp Layout
5-2-0 Terminal Operation - Passenger Aircraft
5-2-1 Typical Turn-Round Time - Two Bridges - Standard Servicing Via Main Deck and UpperDeck
5-2-2 Typical Turn-Round Time - Two Bridges - Servicing Via Main Deck
5-3-0 Terminal Operation - Cargo Aircraft
5-3-1 Typical Turn-Round Time
5-4-0 Ground Service Connections5-4-1 Ground Service Connections Layout
5-4-2 Grounding Points
5-4-3 Hydraulic System
5-4-4 Electrical System
5-4-5 Oxygen System
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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 Outside Air Temperature = -40 ˚C (-40 ˚F)
5-5-2 Outside Air Temperature = 15 ˚C (59 ˚F)
5-5-3 Outside Air Temperature = 50˚C (122 ˚F)
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 - Ground Idle Power
6-1-2 Engine Exhaust Temperatures - Ground Idle Power
6-1-3 Engine Exhaust Velocities - Breakaway Power
6-1-4 Engine Exhaust Temperatures - Breakaway Power
6-1-5 Engine Exhaust Velocities - Max Take-off Power
6-1-6 Engine Exhaust Temperatures - Max Take-off Power
6-2-0 Airport and Community Noise Data
6-2-1 Airport and Community Noise Data
6-3-0 Danger Areas of the Engines
6-3-1 Danger Areas of the Engines - Ground Idle Power
6-3-2 Danger Areas of the Engines - Max. Take-Off Power
6-3-3 Danger Areas of the Engines - Breakaway Power
6-4-0 APU Exhaust Velocities and Temperatures
6-4-1 APU Exhaust Velocities and Temperatures
6-4-2 APU Exhaust Velocities and Temperatures - MES Conditions
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
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7-4-1 Landing Gear Loading on Pavement
7-4-2 Wing Gear and Body Gear Loading on Pavement
7-4-3 Wing Gear and Body Gear Loading on Pavement
7-5-0 Flexible Pavement Requirements - US Army Corps of Engineers Design Method
7-5-1 Flexible Pavement Requirements - US Army Corps of Engineers Design Method S-77-1
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 µ)
7-8-4 Radius of Relative Stiffness (Other values of E and µ)7-9-0 ACN/PCN Reporting System
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 Airplanes
9 SCALED DRAWINGS
9-1-0 Scaled Drawing - 1 cm. = 500 cm.
9-2-0 Scaled Drawing - 1 in. = 50 ft.
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SCOPE
1-1-0 Purpose
**ON A/C A380-800 Models A380-800F ModelsPurpose
1. GeneralThis A380 AIRPLANE CHARACTERISTICS (AC) manual is issued for the A380-800 and A380-800Fseries aircraft to provide necessary data to airport operators and airlines for airport facilities planning.
The A380-800 is a subsonic, very long range, very high capacity, civil transport aircraft.
There are two models in the A380-800 series :
- A380-841 model equipped with Rolls-Royce Trent 970 engine,- A380-861 model equipped with Engine Alliance GP 7270 engine.
The A380-800F is a subsonic, very long range, civil freighter aircraft.
There are two models in the A380-800F series :
- A380-843F model equipped with Rolls-Royce Trent 977 engine,- A380-863F model equipped with Engine Alliance GP 7277 engine.
In this manual, effectivity is managed as follows :
- by default, the data is effective for all A380-800 and A380-800F models,- ″ A380-800/800F models″ indicates that the related data or page is effective for all A380-800 and
A380-800F models,- ″ A380-800 models″ restricts the effectivity of the related data or page to the A380-841 and
A380-861 models,- ″ A380-800F models″ restricts the effectivity of the related data or page to the A380-843F and
A380-863F models,- the mention of a specific model (e.g. A380-841 model, A380-863F model, etc.) restricts the
effectivity of the related data or page to that specific model.
This document conforms to NAS 3601.
1-1-0
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@A380 AIRPLANE CHARACTERISTICS
CORRESPONDENCECorrespondence concerning this publication should be directed to :
AIRBUS S.A.S.
Technical Data Support and Services1 Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0
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1-2-0 Introduction
**ON A/C A380-800 Models A380-800F Models
Introduction
1. GeneralThis manual comprises 9 chapters with a List of Effective Content (L.E.C.) and a Table Of Contents(TOC) at the beginning of the manual.
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 arrangements.
CHAPTER 3 : AIRPLANE PERFORMANCE
This chapter indicates the aircraft performance.
It covers :- payload/range,- take-off 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 equipment.
It covers :- location and connections of ground servicing equipment,- engines starting pneumatic and preconditioned airflow requirements.
1-2-0
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CHAPTER 6 : OPERATING CONDITIONS
This chapter contains data and safety/environmental precautions related to engine and APU
operation on the ground.
It includes :- engine and APU exhaust velocities and temperatures data,- engine noise data.
CHAPTER 7 : PAVEMENT DATA
This chapter contains the pavements 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 a possible new version with the associated size change.
CHAPTER 9 : SCALED DRAWINGS
This chapter contains different A380-800 and A380-800F scaled drawings.
1-2-0
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1-2-1 Glossary
**ON A/C A380-800 Models A380-800F Models
Glossary
1. List of Abbreviations
A/C Aircraft
ACN Aircraft Classification NumberAPU Auxiliary Power Unit
BLG Body Landing Gear
CAS Calibrated Air Speed
CBR California Bearing Ratio
CG Center of Gravity
C/L Center Line
E Young’s ModulusFAA Federal Aviation AdministrationFDL Fuselage Datum Line
FR FrameFSTE Full Size Trolley Equivalent
FWD ForwardGPU Ground Power UnitGSE Ground Support Equipment
ICAO International Civil Aviation Organisation
ISA International Standard Atmosphere
L LeftL Radius of relative stiffnessLCN Load Classification NumberLPS Last Pax Seating
MAC Mean Aerodynamic Chord
MAX MaximumMIN MinimumMLW Maximum Design Landing Weight
MRW Maximum Design Ramp Weight
MTOW Maximum Design Take-Off WeightMTW Maximum Design Taxi Weight
MZFW Maximum Design Zero Fuel Weight
NLG Nose Landing Gear
OAT Outside Air Temperature
OEW Operational Empty Weight
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PAX Passenger
PB/D Passenger Boarding/Deboarding
PCN Pavement Classification NumberR Right
SLS Sea Level Static conditionTBD To Be DeterminedTBIL To Be Issued LaterULD Unit Load DeviceUS United StatesVF Variable Frequency
Vref Landing reference speed
WLG Wing Landing Gear
2. Units of Measurement˚ degree (angle)
% percent
˚C degree Celsius
˚F degree Fahrenheit
bar barcm centimeterdeg degree (angle)
ft foot
ft/s foot per second
ft/s2 foot per second squared
ft2 square foot
ft3 cubic footin inchkg kilogram
kg/l kilogram per liter
km/h kilometer per hour
kt knotkVA kiloVolt Ampere
l literlb poundm meter
m/s meter per second
m2 square meter
m3 cubic meter
1-2-1
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min minutemm millimeterMN/m3 MegaNewton per cubic meter
MPa MegaPascal
nm nautical milepci pound-force per cubic inch
psi pound-force per square incht tonneUS gal United States gallon
3. Design Weight Terminology- Maximum Design Ramp Weight (MRW) :Maximum weight for ground maneuver (including weight of taxi and runup fuel) as limited by aircraftstrength and airworthiness requirements. It is also called Maximum Design Taxi Weight (MTW).- Maximum Design Landing Weight (MLW) :
Maximum weight for landing as limited by aircraft strength and airworthiness requirements.- Maximum Design Takeoff Weight (MTOW) :
Maximum weight for takeoff as limited by aircraft strength and airworthiness requirements. (Thisis the maximum weight at start of the take-off run).
- Maximum Design Zero Fuel Weight (MZFW) :Maximum permissible weight of the aircraft less 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
are the flight and cabin crew and their baggage, unusable fuel, engine oil, emergency equipment,toilet chemical and fluids, galley structure, catering equipment, seats, documents, etc.
- Maximum Payload :Maximum Design Zero Fuel Weight (MZFW) minus Operating Weight Empty (OWE).
- 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.
1-2-1
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AIRPLANE DESCRIPTION
2-1-0 General Airplane Characteristics
**ON A/C A380-800 Models A380-800F ModelsGeneral Airplane Characteristics
1. General Airplane Characteristics
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2-1-1 General Airplane Characteristics Data
**ON A/C A380-800 Models A380-800F Models
General Airplane Characteristics data
1. The following table provides characteristics of A380-800 Models:
Aircraft CharacteristicsAirplane Model A380-841 A380-861
Engines TRENT 970 GP 7270
kilograms 562 000 562 000Maximum Design RampWeight (MRW) pounds 1 238 998 1 238 998
kilograms 560 000 560 000Maximum Design Take Off Weight (MTOW) pounds 1 234 588 1 234 588
kilograms 386 000 386 000Maximum Design Landing
Weight (MLW) pounds 850 984 850 984kilograms 361 000 361 000Maximum Design Zero Fuel
Weight (MZFW) pounds 795 869 795 869
kilograms 270 015 270 281Operating Empty Weight(OEW) -- Typical pounds 595 281 595 868
kilograms 90 985 90 718Maximum Payload
pounds 200 587 199 999
Standard Seating Capacity Three-Class 555 <1> 555 <1>
liters 310 000 310 000
US gallons 81 893 81 893kilograms (density =
0.785 kg/l)
243 350 243 350Usable Fuel Capacity
pound 536 494 536 494
cubic meters 175.30 175.30Volume of CargoCompartments <2> cubic feet 6191 6191
cubic meters 12.60 12.60Volume of Cockpit
cubic feet 444.96 444.96
<1> 555 pax :
- main deck : First Class 22 and Tourist Class 334- upper deck : Business Class 96 and Tourist Class 103<2> Volume of cargo compartments :- lower deck forward cargo compartment
(usable containerised volume) : 89.4 m3 (3157 ft3)- lower deck aft cargo compartment
(usable containerised volume) : 71.5 m3 (2525 ft3)
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- lower bulk cargo compartment(usable volume) : 14.4 m3 (505 ft3)
2. The following table provides characteristics of A380-800F Models.
Aircraft CharacteristicsAirplane Model A380-843F A380-863F
Engines TRENT 977 GP 7277
kilograms 592 000 592 000Maximum Design RampWeight (MRW) pounds 1 305 136 1 305 136
kilograms 590 000 590 000Maximum Design Take Off Weight (MTOW) pounds 1 300 727 1 300 727
kilograms 427 000 427 000Maximum Design LandingWeight (MLW) pounds 941 374 941 374
kilograms 402 000 402 000Maximum Design Zero Fuel
Weight (MZFW) pounds 886 258 886 258kilograms 250 560 250 826Operating Empty Weight
(OEW) -- Typical pounds 552 390 552 976
kilograms 151 440 151 174Maximum Payload
pounds 333 868 333 281
liters 310 000 <2> 310 000 <2>US gallons 81 893 81 893
kilograms (density =0.785 kg/l)
243 350 243 350Usable Fuel Capacity
pounds 536 494 536 494cubic meters 938.4 938.4Volume of Cargo
Compartments <1> cubic feet 33 139 33 139
cubic meters 12.60 12.60Volume of Cockpit
cubic feet 444.96 444.96
<1> Volume of cargo compartments :- lower deck forward cargo compartment
(usable containerised volume) : 90 m3 (3 157 ft3)- lower deck aft cargo compartment
(usable containerised volume) : 72 m3 (2 525 ft3)- lower bulk cargo compartment
(usable volume) : 18.4 m3 (650 ft3)- main deck cargo compartment
(usable palletized volume) : 508 m3 (18 222 ft3)- upper deck cargo compartment
(usable palletized volume) : 250 m3 (9 075 ft3)
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<2> Usable fuel capacity with center tank : 355 850 l (94 005 US gal)
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2-2-0 General Airplane Dimensions
**ON A/C A380-800 Models A380-800F Models
General Airplane Dimensions Data
1. This section provides General Airplane Dimensions.
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2-3-0 Ground Clearances
**ON A/C A380-800 Models
Ground Clearances - Pax
1. This section gives ground clearances of A380-800 Models.
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**ON A/C A380-800 Models
NOTE: MAXIMUM JACKING WEIGHT = 333 700 kg L_AC_020300_1_0010101_01_01
D
C1F1
E1
F3F2C2
E2
H G
K2 K1
L2
L3 L4 L5 L6 J2 J1
M1M2M3M5 M4 U1U2U3
C3
m ft m ft m ft m ft
MRWAFT CG
290tMID CG
A/C JACKEDFDL = 7.2 m
(23.6 ft)
ft
MRW (562t)FWD CG
10.010.3
23.435.335.67.77.55.4
30.2
79.324.817.33.56.210.113.4
3.113.10
7.2110.8110.802.402.241.669.11
24.087.505.221.081.903.074.08
3.113.10
7.2110.8110.802.402.241.669.11
24.087.505.221.081.903.074.08
10.210.2
23.735.535.47.97.45.5
29.9
79.024.617.13.56.210.113.4
3.303.23
7.42
2.592.381.829.20
24.178.225.941.302.273.264.31
4.2
10.810.6
24.336.135.98.57.86.0
30.2
79.3
19.5
7.410.714.1 4.34
1.25
3.193.32
7.2510.9011.032.492.461.829.43
24.408.336.05
2.273.27
4.1
10.510.9
23.835.836.28.28.16.0
30.9
80.127.319.8
7.510.714.2
5.125.12
9.2212.8212.824.414.273.6811.14
26.1110.12
3.147.84
4.135.126.18
16.816.8
30.242.142.114.514.012.136.6
85.733.225.710.313.516.820.3
300tAFT CG
11.0010.93
27.0
10.7 3.22 10.6 3.36 11.0 3.43 11.3 5.24 17.2
16.716.816.917.025.8
25.926.0
5.145.135.135.127.89
7.887.88
5.145.135.135.127.89
7.887.88
16.916.816.816.825.9
25.925.8
5.325.295.265.258.06
8.038.01
17.517.317.317.226.5
26.326.3
5.235.295.345.378.00
8.078.11
17.217.417.517.626.3
26.526.6
7.157.157.15
9.90
9.909.90
23.523.523.523.532.5
32.532.5
7.15
15.316.417.116.6
4.654.995.185.14
4.654.995.185.14
15.316.417.016.9
4.935.345.615.34
16.217.518.417.5
4.985.405.675.19
16.417.718.617.0
6.817.227.507.15
22.423.724.623.5
CONFIGURATIONA/C
mC1C2
DE1E2F1F2F3G
HJ1J2K1K2L2L3
1.05
3.053.14
7.1310.7610.842.352.271.669.21
24.187.555.27
1.903.084.10
C3 3.27
M2M3M4M5U1
U2U3
5.095.135.165.187.85
7.907.92
L4L5L6M1
4.675.015.215.07
Ground ClearancesA380-800 Models
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**ON A/C A380-800F Models
Ground Clearances - Freighter
1. This section gives ground clearances of A380-800F models.
2-3-0
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2-4-0 Interior Arrangement - Plan View
**ON A/C A380-800 Models A380-800F Models
Interior Arrangement - Plan View
1. Interior Arrangement - Plan View
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2-4-1 Standard Configuration
**ON A/C A380-800 Models
Standard Configuration - Pax
1. This section gives the standard configuration of A380-800 models
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**ON A/C A380-800 Models
STOWAGES 1
PASSENGER SEATS UPPER DECK (199 TOTAL)
BUSINESS CLASS 96 SEATS
TOURIST CLASS 103 SEATS
ATTENDANT SEATS 8
COAT STOWAGE 6
GALLEYS 8
LIFT 2
UPPER DECK
LAVATORIES 7
STAIRS 2
CREW REST BUNKS 5
L_AC_020401_1_0010101_01_00
Interior Arrangements - Plan ViewStandard Configuration - Upper Deck
2-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
PASSENGER SEATS MAIN DECK (356 TOTAL)
FIRST CLASS 22 SEATS
TOURIST CLASS 334 SEATS
COAT STOWAGE 1
STOWAGES 1
GALLEYS 9
MAIN DECK
LAVATORIES 10
ATTENDANT SEATS 12
LIFT 2
STAIRS 2
L_AC_020401_1_0020101_01_00
Interior Arrangements - Plan ViewStandard Configuration - Main Deck
2-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Standard Configuration - Freighter
1. This section gives the standard configuration of A380-800F models.
2-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
MAIN DECK SERVICE AREA
UPPER DECK COURIER AREA
UPPER DECKCARGOCOMPARTMENT
STAIR
COURIER AREA
BARRIER
BARRIERSTAIR
12 SEATS B/C
MAIN DECKCARGOCOMPARTMENT
STOWAGES 1
ATTENDANT SEATS 2
GALLEYS 1
LAVATORIES 1
L_AC_020401_1_0030101_01_00
Interior Arrangements - Plan ViewStandard Configuration
2-4-1
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@A380 AIRPLANE CHARACTERISTICS
2-5-0 Interior Arrangements - Cross Section
**ON A/C A380-800 Models A380-800F Models
Interior Arrangements - Cross Section
1. Interior Arrangements - Cross Section
2-5-0
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@A380 AIRPLANE CHARACTERISTICS
2-5-1 Typical Configuration
**ON A/C A380-800 Models
Typical Configuration - Pax
1. This section gives the typical configuration of A380-800 models.
2-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
UPPER DECKBUSINESS CLASS 6 ABREAST
UPPER DECK
TOURIST CLASS 8 ABREAST
1.07 m 1.07 m
(42 in)
1.07 m
(42 in)
1.07 m
(42 in)
1.37 m
(54 in)
1.37 m
(54 in)
1.37 m
(54 in)
0.58 m
(23 in)
0.51 m(20 in)
(42 in)
L_AC_020501_1_0010101_01_00
Interior Arrangements - Cross-sectionTypical Configuration - Upper Deck
2-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
MAIN DECKTOURIST CLASS 10 ABREAST
MAIN DECKFIRST CLASS 6 ABREAST
(62 in)
1.07 m
(42 in)
0.51 m(20 in)
1.57 m 1.07 m
(42 in) (62 in)
1.57 m
(38 in)
0.97 m
1.45 m
(57 in)
1.45 m
(57 in)
1.45 m
(57 in)
L_AC_020501_1_0020101_01_00
Interior Arrangements - Cross-sectionTypical Configuration - Main Deck
2-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Typical Configuration - Freighter
1. This section gives the typical configuration of A380-800F models.
2-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
UPPER DECKCARGO COMPARTMENT
MAIN DECKCARGO COMPARTMENT
LOWER DECKCARGO COMPARTMENT
UPPER DECKCOURIER AREA
L_AC_020501_1_0030101_01_00
Interior Arrangements - Cross-sectionTypical Configuration - A380- 800F Models All Decks
2-5-1
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@A380 AIRPLANE CHARACTERISTICS
2-6-0 Cargo Compartments
**ON A/C A380-800 Models A380-800F Models
Cargo Compartments
1. Cargo Compartments
2-6-0
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@A380 AIRPLANE CHARACTERISTICS
2-6-1 Location and Dimensions
**ON A/C A380-800 Models
Location and Dimensions - Pax
1. This section gives the cargo compartments location and dimensions of A380-800 models.
2-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
F O R W A R D A F T C A R G O
C O M P A R T M E N T )
L O W E R D E C K
F O R W A R D C A R G O
C O M P A R T M E N T
L O W E R D E C K
F O R W A R D A F T C A R G O
C O M P A R T M E N T
( T − S H A P E D
L O W E
R D E C K
R E A R A
F T C A R G O
C O M P A R T M E N T
L O W E R D E C K
B U L K C A R G O
C O M P A R T M E N T
2.8 m
(110.2 in)
(110.2 in)
9.7 m
(381.9 in)
1.1 m
(43.3 in)
3.1 m
(122.8 in)
8.2 m
(322.8 in)
F R 1 7
F R 4 4
F R 5 7
F R 9 0
F R 8 6
F R 1 7
F R 4 4
F R 5 7
F R 9 0
F R 8 6
2.8 m
17.4 m
(685.04 in)
L_AC_020601_1_0010101_01_00
Cargo CompartmentsLocation and Dimensions
2-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Location and Dimensions - Freighter
1. This section gives the cargo compartments location and dimensions of A380-800F models.
2-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L O W E R D E C K
F O R W A R D C A R G O
C O M P A R T M E N T
L O W E R D E C K
F O R W A R D A F T C A R G O
C O M P A R T M E N T
( T − S H A P E D
C O M P A R T M E N T )
R E A R A F T C A R
G O
C O M P A R T M E N T
L O W E R D E C K
B U L K C A R G O
C O M P A R T M E N T
U P P E R D E C K
C A R G O C O M P A R T M E N T
M A
I N D E C K
C A R G O C
O M P A R T M E N T
L O W E R D E C K
A F T C A R G O
C O M P A R T M E N T
L O W E R D E C K
F O R W A R D C A R G O
C O M P A R T M E N T
L O W E R D E C K
F O R W A R D A F T C A R G O
C O M P A R T M E N T
( T − S H A P E D
C O M P A R T M E N T )
L O W E R D E C K
R E A R A F T C A R
G O
C O M P A R T M E N T
L O W E R D E C K
B U L K C A R G O
C O M P A R T M E N T
U P P E R D E C K
C A R G O C O M P A R T M E N T
M A
I N D E C K
C A R G O C
O M P A R T M E N T
L O W E R D E C K
A F T C A R G O
C O M P A R T M E N T
F R 9 5
F R 2 7
F R 2 1
F R 1 7
F R 9 0
L_AC_020601_1_0020101_01_00
Cargo CompartmentsLocation and Dimensions (Sheet 1)
2-6-1
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@A380 AIRPLANE CHARACTERISTICS
2-6-2 Loading Combinations
**ON A/C A380-800 Models
Loading Combinations - Pax
1. This section gives cargo compartments loading combinations.
2-6-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Loading Combinations - Freighter
1. This section gives cargo compartments loading combinations.
2-6-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
U P P E R D E C K L O A D I N G 5 3 A Y Y
M A I N D E C K L O A D I N G 3 3 A M J
U P P E R D E C K L O A D I N G 5 3 A Y Y
M A I N D E C K L O A D I N G 3 3 A M J
L_AC_020602_1_0030101_01_00
Cargo CompartmentsLoading Combinations (Sheet 2)
2-6-2
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@A380 AIRPLANE CHARACTERISTICS
2-7-0 Door Clearances
**ON A/C A380-800 Models
Door Clearances - Pax
1. This section gives Door Clearances.
2-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
FORWARDCARGO DOOR
AFTCARGO DOOR
BULKDOOR
DOORM2L
DOORM1L
DOORU1L
DOORU2L
DOORU3L
DOORM4L
DOORM5L
EMERGENCYEXIT DOOR
M3L
DOORU1R
DOORU2R
DOORU3R
DOORM5R
DOORM4R
DOORM2R
DOORM1R
EMERGENCYEXIT DOOR
M3R
L_AC_020700_1_0010101_01_00
Door ClearancesDoor Location (Sheet 1) - A380-800 Models
2-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
11.74 m
(462.20 in)
48.08 m
(1892.91 in)
51.10 m
(2011.80 in)
53.64 m
(2111.81 in)
48.22 m
(1898.42 in)
44.77 m
(1762.59 in)
40.33 m
(1587.79 in)
32.71 m
(1287.79 in)
20.97 m
(825.59 in)
16.32 m
(642.52 in)
6.33 m
(249.21 in)
L_AC_020700_1_0020101_01_00
Door ClearancesDoor Location (Sheet 2) - A380-800 Models
2-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Door Clearances - Freighter
1. This section gives door clearances.
2-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
LOWER DECK AFTCARGO DOOR
MAIN DECKCARGO DOOR
UPPER DECKCARGO DOOR
LOWER DECK FORWARDCARGO DOOR
BULK DOOR
DOOR M1L DOOR M2L
HATCH U1R
HATCH U1L
DOOR M1R
L_AC_020700_1_0030101_01_00
Door ClearancesDoor Location (Sheet 1) - A380-800F Models
2-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6.33 m
(249.21 in)
51.01 m
(2008.26 in)
16.02 m
(630.71 in)
48.24 m
(1899.21 in)
53.64 m
(2111.81 in)
11.74 m
(462.20 in)
48.08 m
(1892.91 in)
11.10 m
(437.01 in)
6.33 m
(249.21 in)
11.10 m
(437.01 in)
L_AC_020700_1_0040101_01_00
Door ClearancesDoor Location (Sheet 2) - A380-800F Models
2-7-0
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@A380 AIRPLANE CHARACTERISTICS
2-7-1 Forward Doors
**ON A/C A380-800 Models A380-800F Models
Forward Doors
1. This section gives forward doors clearances.
2-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
SEECHAPTER
2−3
1067 mm
(42 in)
(96.5 in)
859 mm
(33.8 in)
2451 mm
MAIN DECK DOORM1L, M1R
1891 mm
(74.45 in)
45 mm
(1.77 in)
MEASURED FROM THE EXTERNAL POINT OFTHE SCUFF PLATE AND THE MOSTEXTERNAL POINT OF THE DOOR SKIN
2137 mm
(84.1 in)2128 mm
(83.8 in)
1262 mm
(49.7 in)
FREE AISLE
720 mm
(28.3 in)
01
NOTE:
FREE AISLE
01
01
L_AC_020701_1_0010101_01_00
Door ClearancesForward Doors
2-7-1
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@A380 AIRPLANE CHARACTERISTICS
2-7-2 Main and Upper Deck Doors
**ON A/C A380-800 Models
Main and Upper Deck Doors - Pax
1. This section gives main and upper deck doors clearances.
2-7-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
UPPER DECK DOORU1L, U2L, U3L, U1R, U2R, U3R
MAIN DECK DOORM2L, M3L, M4L, M2R, M3R, M4R
FWD
45 mm
(1.77 in)
SEECHAPTER
2−3MEASURED FROM THE EXTERNAL POINT OF THE SCUFF PLATEAND THE MOST EXTERNAL POINT OF THE DOOR SKIN
01
NOTE:
02 ON DOOR M3L/M3R MEASURED FROM THE EXTERNAL POINTOF THE CUTOUT IN THE BELLY FAIRING AND THE MOSTEXTERNAL POINT OF THE BELLY FAIRING FROM THE DOOR
2134 mm
(84 in)
SEECHAPTER
2−3
1883 mm(74.1in)FREEAISLE
2124 mm(83.6 in)
1916 mm(75.4 in)
FREEAISLE 2087 mm
(82.2 in)2088 mm(82.2 in)
84 mm(3.31 in)
2453 mm(96.6 in)
1067 mm
(42 in)
FREE AISLE
891 mm
(35.1 in)ON M3L/M3R702 mm(27.6 in)
2434 mm(95.8 in)
1067 mm(42 in)
FREE AISLE
719 mm(28.3 in)
518 mm(20.4 in)
01
01
1022 mm(40.2 in)ON M3L/M3R840 mm(33.1 in)
01
02
01
02
L_AC_020702_1_0010101_01_00
Door ClearancesMain and Upper Deck Doors - A380-800 Models
2-7-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Upper Deck Door - Freighter
1. This section gives upper deck door clearances.
2-7-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
A−A
SEECHAPTER
2−3
UPPER DECK DOORU1R
FWD
A
A
545 mm
(214.57 in)
1080 mm
(425.20 in)
L_AC_020702_1_0020101_01_00
Door ClearancesUpper Deck Door - A380-800F Models
2-7-2
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@A380 AIRPLANE CHARACTERISTICS
2-7-3 Aft Doors
**ON A/C A380-800 Models
Aft Doors - Pax
1. This section gives aft doors clearances.
2-7-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
SEECHAPTER
2−3
1067 mm
2453 mm
1091 mm
(96.6 in)
(42 in)
(43 in)
FWD
45 mm
(1.77 in)
MEASURED FROM THE EXTERNAL POINT OF
THE SCUFF PLATE AND THE MOSTEXTERNAL POINT OF THE DOOR SKIN
01
NOTE:
MAIN DECK DOORM5L, M5R
FREE AISLE
955 mm(37.6 in)
01
01
1262 mm
(49.7 in)
2138 mm
(84.2 in)
1883 mm(74.1 in)
FREE AISLE
2124 mm
(83.6 in)
L_AC_020703_1_0010101_01_00
Door ClearancesAft Doors - A380-800 Models
2-7-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aft Doors - Freighter
1. This section gives aft doors clearances.
2-7-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
SEECHAPTER
2−3
1067 mm
2453 mm
1091 mm
(96.6 in)
(42 in)
(43 in)
FWD
45 mm
(1.77 in)
MEASURED FROM THE EXTERNAL POINT OF
THE SCUFF PLATE AND THE MOSTEXTERNAL POINT OF THE DOOR SKIN
01
NOTE:
MAIN DECK DOORM5L
FREE AISLE01
2138 mm
(84.2 in)
1883 mm(74.1 in)
FREE AISLE
2124 mm
(83.6 in)
955 mm(37.6 in)
01
1262 mm
(49.7 in)
L_AC_020703_1_0020101_01_00
Door ClearancesAft Doors - A380-800F Models
2-7-3
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@A380 AIRPLANE CHARACTERISTICS
2-7-4 Aft Cargo Compartment Doors
**ON A/C A380-800 Models
Aft Cargo Compartment Doors - Pax
1. This section gives aft cargo compartment doors clearances.
2-7-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
SEECHAPTER
2−3
SEECHAPTER
2−3
1752 mm(68.98 in)
2090 mm(82.28 in)
6420 mm
(252.76 in) 991 mm
(39.02 in)
1402 mm
(55 in)
3071 mm AT FR81A
2945 mm AT FR85(121 in) AT FR81A(116 in) AT FR85
FWD
1130 mm
(44.49 in)
2794 mm
(110 in)
GROUND LINE
2008 mm
(79.05 in)
L_AC_020704_1_0010101_01_01
A
A
B
B
A AB B
Door ClearancesAft Cargo Compartment Doors - A380-800 Models
2-7-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aft Cargo Compartment Doors - Freighter
1. This section gives aft cargo compartment doors clearances.
2-7-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
SEECHAPTER
2−3
A
A−A
3086 mm
6385 mm
(251.38 in)
(121.50 in)
3038 mm(120 in)
A
4318 mm
(170 in)
2540 mm
(100 in)
FWD
L_AC_020704_1_0020101_01_00
Door ClearancesMain Deck Cargo Door - A380-800F Models
2-7-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_020704_1_0030101_01_01
SEECHAPTER
2−3
SEECHAPTER
2−3
1752 mm(68.98 in)
2090 mm(82.28 in)
6420 mm
(252.76 in)991 mm
(39.02 in)
1402 mm
(55 in)
3071 mm AT FR81A
2945 mm AT FR85(121 in) AT FR81A(116 in) AT FR85
FWD
1130 mm
(44.49 in)
2794 mm
(110 in)
GROUND LINE
2008 mm
(79.05 in)
A
A
B
B
A AB B
Door ClearancesLower Deck Aft Cargo Doors - A380-800F Models
2-7-4
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@A380 AIRPLANE CHARACTERISTICS
2-7-5 Forward Cargo Compartment Doors
**ON A/C A380-800 Models
Forward Cargo Compartment Doors - Pax
1. This section gives forward cargo compartment doors clearances.
2-7-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
SEECHAPTER
2−3
1752 mm(68.98 in)
6335 mm
(249.41 in)
2118 mm(83.39 in)
(118 in)
2986 mm
3111 mm
(122.48 in)
FWD
L_AC_020705_1_0010101_01_01
GROUND LINE
2091 mm
(82.32 in)
A
A
A A
Door ClearancesForward Cargo Compartment Doors - A380-800 Models
2-7-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Forward Cargo Compartment Doors - Freighter
1. This section gives forward cargo compartment doors clearances.
2-7-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
SEECHAPTER
2−3
1752 mm(68.98 in)
6335 mm
(249.41 in)
2118 mm(83.39 in)
(118 in)
2986 mm
3111 mm
(122.48 in)
FWD
GROUND LINE
2091 mm
(82.32 in)
A
A
A AL_AC_020705_1_0030101_01_01
Door ClearancesLower Deck Forward Cargo Door - A380-800F Models
2-7-5
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@A380 AIRPLANE CHARACTERISTICS
2-7-6 Nose Landing Gear Doors
**ON A/C A380-800 Models A380-800F Models
Nose Landing Gear Doors
1. This section gives nose landing gear doors clearances.
2-7-6
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A I R C R A F T C / L
GROUND LINE
A
62°
2.50 m
(8.20 ft)
1.36 m
(4.46 ft)A
(3.08 ft)
0.94 m
1.89 m
(6.20 ft)
L_AC_020706_1_0010101_01_00
Door ClearancesForward Nose Landing Gear Doors
2-7-6
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
0.75 m (2.46 ft)
A
A
A I R C R A F T C / L
69.2°
0.50 m (1.64 ft)
1.89 m (6.20 ft)
L_AC_020706_1_0020101_01_00
Door ClearancesAft Nose Landing Gear Doors
2-7-6
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND LINE
A
I R C R A F T C / L
* DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT
38.23 m(123.48 ft)
4.28 m
(5.61 ft)1.71 m
*(10.59 ft)
(15.04 ft)3.95 m
MAX 0.25 m (0.82 ft)MIN 0.10 m (0.32 ft)
A
A
3.23 m
(14.03 ft)
2.30 m(7.54 ft)
MAX 79°
L_AC_020707_1_0010101_01_00
Door ClearancesWing Landing Gear Doors
2-7-7
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@A380 AIRPLANE CHARACTERISTICS
2-7-8 Body Landing Gear Doors
**ON A/C A380-800 Models A380-800F Models
Body Landing Gear Doors
1. This section gives body landing gear doors clearances.
2-7-8
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND LINE
A
I R C R A F T C / L
* DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT
5.02 m(16.46 ft)
4.72 m(15.48 ft)
* MAX 0.35 m (1.41 ft)MIN 0.25 m (0.82 ft)
43.00 m(141.04 ft)
5.17 m(16.95 ft)
A
A
2.25 m(7.38 ft)
MAX 99° 2.90 m(9.51 ft)
L_AC_020708_1_0010101_01_00
Door ClearancesBody Landing Gear Doors (Sheet 1)
2-7-8
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND LINE
A I R C R A F T C / L
* DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT
*
2.25 m
1.18 m(3.87 ft)
1.23 m(4.03 ft)
MAX 0.95 m (3.11 ft)MIN 0.70 m (2.29 ft)
43.00 m(141.04 ft)
5.17 m(16.95 ft)
A
A
(7.38 ft)
MAX 94°
1.32 m(4.32 ft)
L_AC_020708_1_0020101_01_00
Door ClearancesBody Landing Gear Doors (Sheet 2)
2-7-8
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@A380 AIRPLANE CHARACTERISTICS
2-7-9 APU Doors
**ON A/C A380-800 Models A380-800F Models
APU Doors
1. This section gives APU doors clearances.
2-7-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND LINE
* DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT
**
FUSELAGE DATUM LINE
MAX 5.52 m (18.10 ft)MIN 5.49 m (18.00 ft)
MAX 6.66 m (21.84 ft)MIN 6.63 m (21.74 ft)
FR112 FR117
L_AC_020709_1_0010101_01_00
Door ClearancesAPU Doors
2-7-9
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@A380 AIRPLANE CHARACTERISTICS
AIRPLANE PERFORMANCE
3-1-0 General Information
**ON A/C A380-800 Models A380-800F ModelsGeneral Information
1. Standard day temperatures for the altitudes shown are tabulated below :
Standard day temperatures for the altitudes
Altitude Standard Day Temperature
FEET METERS ˚F ˚C0 0 59.0 15.0
2000 610 51.9 11.64000 1220 44.7 7.16000 1830 37.6 3.18000 2440 30.5 -0.8
3-1-0
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@A380 AIRPLANE CHARACTERISTICS
3-2-0 Payload / Range
**ON A/C A380-800 Models A380-800F Models
Payload /Range
1. Payload / Range
3-2-0
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@A380 AIRPLANE CHARACTERISTICS
3-2-1 ISA Conditions
**ON A/C A380-800 Models
Payload/Range - Pax
1. This section gives the payload/range at ISA conditions.
3-2-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
0
10
20
30
40
50
60
70
80
90
4000 4500 5000 5500 6000 6500 7000 7500 8000 8500 9000 9500 100000
20
40
60
80
140
160
180
2007400 8400 9400 10400 11400 12400 13400 14400 15400 16400 17400 18400
MAXIMUM PASSENGER PAYLOAD
MAXIMUM STRUCTURAL PAYLOAD
RANGE (km)
P A Y L O A D ( t )
RANGE (nm)
ISA / NO WIND
TYPICAL INTERNATIONAL FLIGHT PROFILE
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.
THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
100
120
P A Y L O A D ( x 1 0 0 0 l b )
200 nm DIVERSION5% TRIP FUEL ALLOWANCE, 30 min HOLDING
L_AC_030201_1_0010101_01_00
Payload/RangeISA Conditions - TRENT 900 Engines
3-2-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
0
10
20
30
40
50
60
70
80
90
4000 4500 5000 5500 6000 6500 7000 7500 8000 8500 9000 9500 100000
20
40
60
80
100
120
140
160
180
2007400 8400 9400 10400 11400 12400 13400 14400 15400 16400 17400 18400
MAXIMUM PASSENGER PAYLOAD
MAXIMUM STRUCTURAL PAYLOAD
RANGE (km)
P A Y L O A D ( t )
RANGE (nm)
ISA / NO WIND
TYPICAL INTERNATIONAL FLIGHT PROFILE
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.
THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
P A Y L O A D ( x 1 0 0 0 l b )
200 nm DIVERSION5% TRIP FUEL ALLOWANCE, 30 min HOLDING
L_AC_030201_1_0080101_01_00
Payload/RangeISA Conditions - GP 7200 Engines
3-2-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Payload/Range - Freighter
1. This section gives the payload/range at ISA conditions.
3-2-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
0
20
40
60
80
100
120
140
160
4000 4500 5000 5500 6000 6500 7000 7500 8000 8500 9000 9500 100000
50
100
150
200
250
300
3507400 8400 9400 10400 11400 12400 13400 14400 15400 16400 17400 18400
MAXIMUM STRUCTURAL PAYLOAD
RANGE (km)
P A Y L O A D ( t )
RANGE (nm)
ISA / NO WINDTYPICAL INTERNATIONAL FLIGHT PROFILE
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
P A Y L O A D ( x 1 0 0 0 l b )
200 nm DIVERSION5% TRIP FUEL ALLOWANCE, 30 min HOLDING
L_AC_030201_1_0060101_01_00
Payload/RangeISA Conditions - TRENT 900 Engines
3-2-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
RANGE (km)
P A Y L O A D ( t )
RANGE (nm)
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
0
20
40
60
80
100
120
140
160
4000 4500 5000 5500 6000 6500 7000 7500 8000 8500 9000 9500 10000 105000
50
100
150
200
250
300
350
7400 8400 9400 10400 11400 12400 13400 14400 15400 16400 17400 18400 19400
MAXIMUM STRUCTURAL PAYLOAD
TYPICAL INTERNATIONAL FLIGHT PROFILE
P A Y L O A D ( x 1 0 0 0 l b )
ISA / NO WIND
200 nm DIVERSION5% TRIP FUEL ALLOWANCE, 30 min HOLDING
L_AC_030201_1_0090101_01_00
Payload/RangeISA Conditions - GP 7200 Engines
3-2-1
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@A380 AIRPLANE CHARACTERISTICS
3-3-0 Take Off Weight Limitation
**ON A/C A380-800 Models A380-800F Models
Take Off Weight Limitation
1. Take Off Weight Limitation
3-3-0
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@A380 AIRPLANE CHARACTERISTICS
3-3-1 ISA Conditions
**ON A/C A380-800 Models
Take Off Weight Limitation - Pax
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
RUNWAY LENGTH (ft)
RUNWAY LENGTH (m)
T A K E − O F F W E I G H T ( t )
300
350
400
450
500
550
600
650
1500 2000 2500 3000 3500 4000 4500 5000 5500660
760
860
960
1060
1160
1260
1360
5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 16000 17000 18000
0
2000
6000
4000
8000
T A K E − O F F W E I G H T ( x 1 0 0 0 l b )
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0010101_01_00
Take-Off Weight LimitationISA Conditions - TRENT 900 Engines
3-3-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
RUNWAY LENGTH (ft)
RUNWAY LENGTH (m)
T A K E − O F F W E I G H T ( t )
300
350
400
450
500
550
600
650
1500 2000 2500 3000 3500 4000 4500 5000 5500660
760
860
960
1060
1160
1260
1360
5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 16000 17000 18000
0
2000
6000
4000
8000
T A K E − O F F W E I G H T ( x 1 0 0 0 l b )AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0080101_01_00
Take-Off Weight LimitationISA Conditions - GP 7200 Engines
3-3-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Take-Off Weight Limitation - Freighter
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
300
350
400
450
500
550
600
650
700
1500 2000 2500 3000 3500 4000 4500 5000 5500660
760
860
960
1060
1160
1260
1360
1460
5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 16000 17000 18000
RUNWAY LENGTH (ft)
RUNWAY LENGTH (m)
T A K E − O F F W E I G H T ( t )
02000
6000
4000
8000
T A K E − O F F W E I G H T ( x 1 0 0 0 l b )
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0060101_01_00
Take-Off Weight LimitationISA Conditions - TRENT 900 Engines
3-3-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
300
350
400
450
500
550
600
650
700
1500 2000 2500 3000 3500 4000 4500 5000 5500660
760
860
960
1060
1160
1260
1360
1460
5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 16000 17000 18000
RUNWAY LENGTH (ft)
RUNWAY LENGTH (m)
T A K E − O F F W E I G H T ( t )
0 2000
6000
4000
8000
T A K E − O F F W E I G H T ( x 1 0 0 0 l b )
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0090101_01_00
Take-Off Weight LimitationISA Conditions - GP 7200 Engines
3-3-1
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@A380 AIRPLANE CHARACTERISTICS
3-3-2 ISA + 15 ˚C (59 ˚F)
**ON A/C A380-800 Models
ISA + 15 ˚C (59 ˚F) - Pax
1. This section gives the take-off weight limitation at ISA +15˚C (59˚F) conditions.
3-3-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
RUNWAY LENGTH (ft)
RUNWAY LENGTH (m)
T A K E − O F F W E I G H T ( t )
300
350
400
450
500
550
600
650
1500 2000 2500 3000 3500 4000 4500 5000 5500660
760
860
960
1060
1160
1260
1360
5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 16000 17000 18000
0
2000
6000
4000
8000
T A
K E − O F F W E I G H T ( x 1 0 0 0 l b )AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030302_1_0010101_01_00
Take-Off Weight LimitationISA + 15 ˚C (59 ˚F) - TRENT 900 Engines
3-3-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
ISA + 15 ˚C (59 ˚F) - Freighter
1. This section gives the take-off weight limitation at ISA +15˚C (59˚F) conditions.
3-3-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
300
350
400
450
500
550
600
650
700
1500 2000 2500 3000 3500 4000 4500 5000 5500660
760
860
960
1060
1160
1260
1360
1460
5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 16000 17000 18000
RUNWAY LENGTH (ft)
RUNWAY LENGTH (m)
T A K E − O F F W E I G H T ( t )
02000
6000
4000
8000
AIRFIELD PRESSURE ALTITUDE (ft)
T A K E − O F F W E I G H T ( x 1 0 0 0 l b )
L_AC_030302_1_0060101_01_00
Take-Off Weight LimitationISA + 15 ˚C (59 ˚F) - TRENT 900 Engines
3-3-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
300
350
400
450
500
550
600
650
700
1500 2000 2500 3000 3500 4000 4500 5000 5500660
760
860
960
1060
1160
1260
1360
1460
5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 16000 17000 18000
RUNWAY LENGTH (ft)
RUNWAY LENGTH (m)
T A K E − O F F W E I G H T ( t )
02000
6000
4000
8000
T A K E − O F F W E I G H T ( x 1 0 0 0 l b )
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030302_1_0090101_01_00
Take-Off Weight LimitationISA + 15 ˚C (59 ˚F) - GP 7200 Engines
3-3-2
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@A380 AIRPLANE CHARACTERISTICS
3-4-0 Landing Field Length
**ON A/C A380-800 Models A380-800F Models
Landing Field Length
1. Landing Field Length
3-4-0
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@A380 AIRPLANE CHARACTERISTICS
3-4-1 Landing Field Length
**ON A/C A380-800 Models
Landing Field Length - Pax
1. This section gives the landing field length.
3-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1400
1500
1600
1700
1800
1900
2000
2100
2200
2300
2400
2500
2600
2700
2800
280 300 320 340 360 380 400 420 440 4604600
5000
5400
5800
6200
6600
7000
7400
7800
8200
8600
9000
620 670 720 770 820 870 920 970
GROSS WEIGHT (t)
VALID FOR ALL TEMPERATURES
AIRFIELD ELEVATION (ft)
0
2000
6000
4000
8000
L A N D
I N G F I E L D L E N G T H ( f t )
L A N D
I N G F I E L D L E N G T H ( m )
GROSS WEIGHT (x 1000 lb)
L_AC_030401_1_0010101_01_01
Landing Field LengthLanding Field Length - A380-800 Models
3-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Landing Field Length - Freighter
1. This section gives the landing field length.
3-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
1400
1500
1600
1700
1800
1900
2000
2100
2200
2300
2400
2500
2600
2700
2800
280 300 320 340 360 380 400 420 440 4604600
5000
5400
5800
6200
6600
7000
7400
7800
8200
8600
9000
620 670 720 770 820 870 920 970
GROSS WEIGHT (t)
VALID FOR ALL TEMPERATURES
0
2000
6000
4000
8000
L A N D
I N G F I E L D L E N G T H ( m )
L A N D
I N G F I E L D L E N G T H ( f t )
GROSS WEIGHT (x 1000 lb)
AIRFIELD ELEVATION (ft)
L_AC_030401_1_0030101_01_00
Landing Field LengthLanding Field Length - A380-800F Models
3-4-1
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@A380 AIRPLANE CHARACTERISTICS
3-5-0 Final Approach Speed
**ON A/C A380-800 Models A380-800F Models
Final Approach Speed
1. Final Approach Speed
3-5-0
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@A380 AIRPLANE CHARACTERISTICS
3-5-1 Final Approach Speed
**ON A/C A380-800 Models
Final Approach Speed - Pax
1. This section gives the final approach speed.
3-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
120
125
130
135
140
145
150
155
250 270 290 310 330 350 370 390 410 430 450 470
550 600 650 700 750 800 850 900 950 1000
GROSS WEIGHT (t)
GROSS WEIGHT (x 1000 lb)
F I N A L A P P R O A C H S P E E D ( V r e f k t C A S )
160
VALID FOR ALL TEMPERATURES
L_AC_030501_1_0010101_01_00
Final Approach Speed (CG=29%)A380-800 Models
3-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Final Approach Speed - Freighter
1. This section gives the final approach speed.
3-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
NOTE: THESE CURVES ARE GIVEN FOR INFORMATION ONLY.THE APPROVED VALUES ARE STATED IN THE "OPERATING MANUALS"SPECIFIC TO THE AIRLINE OPERATING THE AIRCRAFT.
120
125
130
135
140
145
150
155
250 270 290 310 330 350 370 390 410 430 450 470
550 600 650 700 750 800 850 900 950 1000
GROSS WEIGHT (t)
GROSS WEIGHT (x 1000 lb)
F I N A L A P P R O
A C H S P E E D ( V r e f k t C A S )
160
VALID FOR ALL TEMPERATURES
L_AC_030501_1_0030101_01_00
Final Approach Speed (CG=29%)A380-800F Models
3-5-1
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@A380 AIRPLANE CHARACTERISTICS
4-2-0 Turning Radii
**ON A/C A380-800 Models A380-800F Models
Turning Radii
1. This section gives the turning radii.
4-2-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
R4
R3
R5
R6
SEE PAGE 2 FOR DIMENSIONS
55°
60°
65°
29.83 m ( 97.9 ft )
70°
L_AC_040200_1_0010101_01_00
Turning RadiiTurning Radii (Sheet 1)
4-2-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
2100.16328.6
TYPEOF
TURN
20
STEERINGANGLE
17.9
EFFECTIVESTEERING
ANGLE
mft
135.45444.4
101.01331.4
115.87380.1
278.86258.7
25 22.7mft
113.14371.2
80.12262.9
94.90311.4
265.69215.5
30 27.5mft
98.90324.5
67.33220.9
81.91268.7
256.84186.535 32.1
mft
88.97291.9
58.83193.0
73.13239.9
250.59166.0
40 36.6mft
81.61267.8
52.89173.5
66.84219.3
246.02151.0
45 41.0mft
75.94249.1
48.61159.5
62.16203.9
242.61139.8
50 45.1mft
71.43234.4
45.45149.1
58.57192.2
140.13131.6
55 51.2mft
67.02219.9
43.22141.8
55.43181.9
137.64123.5
60 57.3mft
62.60205.4
40.98134.5
52.29171.5
135.15115.3
65 63.4mft
58.18190.9
38.75127.1
49.15161.2
132.66
107.2
70 69.5m
ft
53.76
176.4
36.52
119.8
46.01
150.9
R3 R4 R5 R6
A380−800/800F TURNING RADII
NOTE:
TYPE 1 TURNS USE :ASYMMETRIC THRUST − BOTH ENGINES ON THE INSIDE OF THE TURN TO BE AT IDLE THRUSTDIFFERENTIAL BRAKING − BRAKING APPLIED TO THE WING GEAR WHEELS ON THE INSIDE OF
TYPE 2 TURNS USE :SYMMETRIC THRUST AND NO BRAKING.
THE TURN.
L_AC_040200_1_0020101_01_00
Turning RadiiTurning Radii (Sheet 2)
4-2-0
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@A380 AIRPLANE CHARACTERISTICS
4-3-0 Minimum Turning Radii
**ON A/C A380-800 Models A380-800F Models
Minimum Turning Radii
1. This section gives the minimum turning radii.
4-3-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
R4
R3
R5 Y
R6
( T U R N I N G
W I D T H )
55 °
60 °
65 °
29.83 m ( 97.9 ft )
70 °
TURN PERFORMED WITH ASYMMETRIC THRUST AND DIFFERENTIAL BRAKINGNOTE:
EffectiveSteering
AngleY
m
ft70° 69.5°
A380−800/800F Minimum Turning Radius
SteeringAngle
Typeof
Turn
11.08
36.3
A
50.91
167.0
R3
32.66
107.2
R4
53.76
176.4
R5
36.52
119.8
R6
46.01
150.91
L_AC_040300_1_0010101_01_00
Minimum Turning Radii
4-3-0
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@A380 AIRPLANE CHARACTERISTICS
4-4-0 Visibility from Cockpit in Static Position
**ON A/C A380-800 Models A380-800F Models
Visibility from Cockpit in Static Position
1. This section gives the visibility from cockpit in static position.
4-4-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
7.17 m(23.52 ft)
4.97 m
(16.3 ft)
20.28 m
(66.53 ft)
CAPTAIN AND F/O EYE’S POSITION
107°
121°
107°
121°
26.9°
19.5°
2.05 m
(6.72 ft)
27°
24°
27°
24°
L_AC_040400_1_0010101_01_00
Visibility from Cockpit in Static Position
4-4-0
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@A380 AIRPLANE CHARACTERISTICS
4-5-0 Runway and Taxiway Turn Paths
**ON A/C A380-800 Models A380-800F Models
Runway and Taxiway Turn Paths
1. Runway and Taxiway Turn Paths
4-5-0
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@A380 AIRPLANE CHARACTERISTICS
4-5-1 135˚ Turn - Runway to Taxiway
**ON A/C A380-800 Models A380-800F Models
135˚ Turn - Runway to Taxiway
1. This section gives the 135˚ turn -- runway to taxiway.
4-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
NLG PATH
COCKPIT TRACKPARALLEL TOGUIDE LINE
NOMINAL OFFSET
TAXIWAY GUIDELINE
WLG PATH
FAA GROUP V JUDGEMENTAL OVERSTEER METHOD
45.7 m(150 ft)
R 45.7 m (150 ft)
R 25.9 m (85 ft)
6.62 m (21.7 ft)
22.9 m (75 ft)
4.99 m (16.4 ft)
7 m (23 ft)
L_AC_040501_1_0010101_01_00
135˚ Turn -- Runway to Taxiway135˚ Turn -- Runway to Taxiway (Sheet 1)
4-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
TAXIWAY GUIDELINE
WLG PATH
60 m
(196.9 ft) R 25.5 m (83.7 ft)5.81 m
(19.1 ft)
(98.4 ft)
FAA GROUP VI COCKPIT TRACKS CENTRELINE METHOD
30 m
R 51 m (167.3 ft)
L_AC_040501_1_0020101_01_00
135˚ Turn -- Runway to Taxiway135˚ Turn -- Runway to Taxiway (Sheet 2)
4-5-1
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@A380 AIRPLANE CHARACTERISTICS
4-5-2 90˚ Turn - Runway to Taxiway
**ON A/C A380-800 Models A380-800F Models
90˚ Turn - Runway to Taxiway
1. This section gives the 90˚ turn -- runway to taxiway.
4-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
NLG PATH
COCKPIT TRACKPARALLEL TOGUIDELINE
TAXIWAYGUIDELINE
WLG PATH
9.21 m 4.94 m (16.2 ft)
45.7 m(150 ft)
R 45.7 m (150 ft)
R 25.9 m (85 ft)
(30.2 ft)
7 m (23 ft)
22.9 m (75 ft)
FAA GROUP V JUDGEMENTAL OVERSTEER METHOD
L_AC_040502_1_0010101_01_00
90˚ Turn -- Runway to Taxiway90˚ Turn -- Runway to Taxiway (Sheet 1)
4-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
TAXIWAYGUIDELINE
WLG PATH
FAA GROUP VI COCKPIT TRACKS CENTRELINE METHOD
60 m(196.9 ft)
R 25.5 m (83.7 ft)
R 51 m (167.3 ft)
10.24 m
(33.6 ft)
30 m
(98.4 ft)
L_AC_040502_1_0020101_01_00
90˚ Turn -- Runway to Taxiway90˚ Turn -- Runway to Taxiway (Sheet 2)
4-5-2
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@A380 AIRPLANE CHARACTERISTICS
4-5-3 180˚ Turn on a Runway
**ON A/C A380-800 Models A380-800F Models
180˚ Turn on a Runway
1. This section gives the 180˚ turn on a runway.
4-5-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
4.5 m
(14.8 ft)
4.5 m
(14.8 ft)
60.0 m (196.9 ft)
51.0 m (167.3 ft)
R36.6 m (119.9 ft)
0.7 m(2.2 ft)
16.8 m
(55.0 ft)31.2 m
(102.4 ft)
23.2 m
(76.2 ft)
R46.0 m
(150.9 ft)
R54.0 m (177.1 ft)
70° NOSE GEAR STEERING ASYMMETRIC THRUST AND BRAKING
ON A 60.0 m (196.9 ft) WIDE RUNWAY.
L_AC_040503_1_0010101_01_00
180˚ Turn on a Runway
4-5-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
COCKPIT TRACKPARALLEL TOGUIDELINE
NLG PATH
TAXIWAYGUIDELINE
WLG PATH
FAA GROUP V JUDGEMENTAL OVERSTEER METHOD
22.9 m
(75 ft)
(29 ft)
8.85 m 4.94 m
(16.2 ft)
22.9 m
(75.0 ft)
R 25.9 m (85 ft)
R 45.7 m (150 ft)
NOMINAL OFFSET
7 m (23 ft)
L_AC_040504_1_0010101_01_00
90˚ Turn -- Taxiway to Taxiway90˚ Turn -- Taxiway to Taxiway (Sheet 1)
4-5-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
TAXIWAYGUIDELINE
WLG PATH
FAA GROUP VI COCKPIT TRACKS CENTRELINE METHOD
30 m
(98.4 ft)
R 25.5 m (83.7 ft)
30 m
(98.4 ft)
R 51 m (167.3 ft)
8.67 m
(28.5 ft)
75 m (246.1 ft)
L_AC_040504_1_0020101_01_00
90˚ Turn -- Taxiway to Taxiway90˚ Turn -- Taxiway to Taxiway (Sheet 2)
4-5-4
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@A380 AIRPLANE CHARACTERISTICS
4-5-5 135˚ Turn - Taxiway to Taxiway
**ON A/C A380-800 Models A380-800F Models
135˚ Turn - Taxiway to Taxiway
1. This section gives the 135˚ turn - taxiway to taxiway.
4-5-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
NLG PATH
COCKPIT TRACKPARALLEL TO
GUIDELINE
TAXIWAYGUIDELINE
WLG PATH
FAA GROUP V JUDGEMENTAL OVERSTEER METHOD
22.9 m
(75 ft)
(23 ft)
4.99 m (16.4 ft)
8.47 m
(27.8 ft)
22.9 m(75 ft)
R 25.9 m (85 ft)
R 45.7 m (150 ft)
7 m
L_AC_040505_1_0010101_01_00
135˚ Turn -- Taxiway to Taxiway135˚ Turn -- Taxiway to Taxiway (Sheet 1)
4-5-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
TAXIWAY GUIDELINE
WLG PATH
FAA GROUP VI COCKPIT TRACKS CENTRELINE METHOD
R 25.5 m (83.7 ft)7.37 m
(24.2 ft)
(98.4 ft)
30 m
(98.4 ft)
R 51 m (167.3 ft)
30 m
L_AC_040505_1_0020101_01_00
135˚ Turn -- Taxiway to Taxiway135˚ Turn -- Taxiway to Taxiway (Sheet 2)
4-5-5
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@A380 AIRPLANE CHARACTERISTICS
4-6-0 Runway Holding Bay (Apron)
**ON A/C A380-800 Models A380-800F Models
Runway Holding Bay (Apron)
1. This section gives the runway holding bay (Apron).
4-6-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
6.1 m
(20 ft)
109.7 m
(360 ft)
6.1 m
(20 ft)
COORDINATE WITH USING AIRLINE FOR SPECIFIC PLANNED OPERATING PROCEDURE
12.2 m
(40 ft)
L_AC_040600_1_0010101_01_00
Runway Holding Bay (Apron)
4-6-0
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@A380 AIRPLANE CHARACTERISTICS
4-7-0 Airplane Parking
**ON A/C A380-800 Models A380-800F Models
Airplane Parking
1. The following figures and charts show the rectangular space required for parking against the terminalbuilding :
A. Steering Geometry
B. Minimum Parking Space Requirements
4-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
PARKING45° ENTRY PUSH OUT
7 0 . 3 1 m ( 2 3 0 . 7 f t )
7 7 . 0 7 m ( 2 5 2 . 9
f t )
80.81 m (265.1 ft)
PARKING
STRAIGHT ENTRY PUSH BACK
94.64 m (310.5 ft)
L_AC_040700_1_0010101_01_00
Airplane ParkingSteering Geometry
4-7-0
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@A380 AIRPLANE CHARACTERISTICS
4-8-0 Airplane Mooring
**ON A/C A380-800 Models A380-800F Models
General
1. This section provides information on airplane mooring.
4-8-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
FWD
SLING
TOWING FITTING
MOVABLE PIN
LOCKING SCREW
HOOK
HOOK PIN
MOORING POINT
A
L_AC_040800_1_0010101_01_00
Airplane Mooring
4-8-0
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@A380 AIRPLANE CHARACTERISTICS
TERMINAL SERVICING
5-1-0 Airplane Servicing Arrangements
**ON A/C A380-800 Models A380-800F ModelsAirplane Servicing Arrangements
1. This section provides typical ramp layouts, showing the various GSE items in position during typicalturn--round scenarios.
These ramp layouts show typical arrangements only. Each operator will have its own specificrequirements/regulations for the positioning and operation on the ramp.
For each ramp layout, the associated typical turn-round time is given in a Chart in the section 5-2 forpassenger aircraft and section 5-3 for cargo aircraft.
5-1-0
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@A380 AIRPLANE CHARACTERISTICS
5-1-1 Typical Ramp Layout - Two Bridges - Standard Servicing Via Main Deck and Upper Deck
**ON A/C A380-800 Models
Typical Ramp Layout - Two Bridges - Standard Servicing
1. This section gives the typical ramp layout - two bridges - servicing via main deck and upper deck.
5-1-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
0 5 10METERS
0 16 32
FEET
2 2
RL28/B1A/800/STD
GATE DIMENSIONS (A380 + 7.50 m (24.60 ft)):
− STORAGE AREA: 2 x 931 m (2 x 10021 ft )
AC: AIR COND UNIT GPU: GROUND POWER UNIT
AIR: AIR START UNIT LV: LAVATORY VEHICLE
CAT: CATERING VEHICLE
CLEAN: CLEANING VEHICLE TOW: TOWING TRACTOR
WV: POTABLE WATER VEHICLE
CONVEYOR: CONVEYOR BELT
FUEL: FUEL HYDRANT DISPENSER
PL: PALLET/CONTAINER LOADER
− WIDTH: 87.50 m (287 ft)
− LENGTH: 80.20 m (263 ft)
F U E L
F U E L
G . P . U
G . P . U
TOW
C L E A N
C A T
P L
P L
C ON V E Y OR
WV
C L E A N
C A T
A I R
A C
L V
C A T
U D C A T
UDCAT: UPPER DECK CATERING VEHICLE
L_AC_050101_1_0010101_01_00
Baseline Ramp Layout -- Two BridgesServicing Via Main and Upper Decks
5-1-1
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@A380 AIRPLANE CHARACTERISTICS
5-1-2 Typical Ramp Layout - Two Bridges - Servicing Via Main Deck
**ON A/C A380-800 Models
Typical Ramp Layout - Two Bridges - Servicing Via Main Deck
1. This section gives the typical ramp layout - two bridges - servicing via main deck.
5-1-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
RL01/B1A/800/STD
F U E L
F U E L
G . P . U
G . P . U
TOW
C L E A N
C A T
P L
P L
C ON V E Y OR
WV
C L E A N
C A T
A I R
A C
0 5 10METERS
0 16 32
FEET
C A T
L V
2 2
GATE DIMENSIONS (A380 + 7.50 m (24.60 ft)):
− STORAGE AREA: 2 x 931 m (2 x 10021 ft )
AC: AIR COND UNIT GPU: GROUND POWER UNIT
AIR: AIR START UNIT LV: LAVATORY VEHICLE
CAT: CATERING VEHICLE
CLEAN: CLEANING VEHICLE TOW: TOWING TRACTORWV: POTABLE WATER VEHICLECONVEYOR: CONVEYOR BELT
FUEL: FUEL HYDRANT DISPENSER
PL: PALLET/CONTAINER LOADER
− WIDTH: 87.50 m (287 ft)
− LENGTH: 80.20 m (263 ft)
C A T
L_AC_050102_1_0010101_01_00
Typical Ramp Layout -- Two BridgesServicing Via Main Deck
5-1-2
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@A380 AIRPLANE CHARACTERISTICS
5-1-3 Opportunities of Direct Upper Deck Access for Airport and Airlines
**ON A/C A380-800 Models
Opportunities of Direct Upper Deck Access for Airport and Airlines
1. This section gives the opportunities of direct upper deck access for airport and airlines.
5-1-3
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@A380 AIRPLANE CHARACTERISTICS
5-1-4 Baseline Ramp Layout
**ON A/C A380-800F Models
Baseline Ramp Layout
1. This section gives the typical ramp layout - cargo aircraft servicing.
5-1-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
F U E L
F U E L
G . P . U
G . P . U
TOW
P L
P L
C O N V E Y O R
0 5 10METERS
0 16 32FEET
L V
RL04/B1/800F/STD
P L P
L
2 2
GATE DIMENSIONS (A380 + 7.50 m (24.60 ft)):
− STORAGE AREA: 2 x 931 m (2 x 10021 ft )
AC: AIR COND UNIT
GPU: GROUND POWER UNIT
AIR: AIR START UNIT
LV: LAVATORY VEHICLE
TOW: TOWING TRACTORWV: POTABLE WATER VEHICLE
CONVEYOR: CONVEYOR BELT
FUEL: FUEL HYDRANT DISPENSER
PS: PASSENGER STAIRS
A I R
PL: PALLET/CONTAINER LOADER
− WIDTH: 87.50 m (287 ft)
− LENGTH: 80.20 m (263 ft)
P S P
S
WV
L_AC_050104_1_0010101_01_00
Baseline Ramp Layout
5-1-4
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@A380 AIRPLANE CHARACTERISTICS
5-2-0 Terminal Operation - Passenger Aircraft
**ON A/C A380-800 Models
Terminal Operation - Passenger Aircraft
1. This section provides typical turn-round time charts showing the typical times for ramp activitiesduring aircraft turn--round.
Actual times may vary due to each operator’s specific practice and operating conditions.
For each turn--round time chart, the associated typical ramp layout is given in section 5-1.
2. ASSUMED TURN-ROUND TIME PARAMETERS
A. PASSENGER BOARDING/DEBOARDING (PB/D) → 100% (555 pax) passenger exchange :
- Doors (type A - 42″ wide) used : M1L and M2L (main deck) and U1R (upper deck).- PB/D rate : boarding = 15 pax/min / deboarding = 25 pax/min- Last Pax Seating Allowance (LPS) = + 4 min- 60″ stair flow rate : up-flow = 14 pax/min / down-flow = 18 pax/min
B. CARGO → Full LD-3 exchange (22 + 16) LD-3 and bulk exchange of 2 000 kg (4 409 lb) :
- LD-3 off-loading/loading times : off-loading = 1.4 min/LD-3 / loading = 1.7 min/LD-3- Pallet loading times : off-loading = 2.5 min/pallet / loading = 2.9 min/pallet- bulk off-loading/loading times : off-loading = 9.2 min/t / loading = 10.5 min/t
C. REFUELLING→ Block fuel for Nominal Range through 4 nozzles :
- 261 200 liters (67 364 US gallons) at 40 psi (48 min)- dispenser positioning or removal = 3 min (fuel truck change) / if any = 5 min
D. CLEANING→ Full cleaning :
- Crew adapted to match catering time
E. CATERING → Full catering :
- average truck capacity = 30 Full Size Trolley Equivalent (FSTE)- simultaneous catering and PB/D = not represented- inbound/outbound FSTE = mixed in the same truck- FSTE exchange time :
5-2-0
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@A380 AIRPLANE CHARACTERISTICS
5-2-2 Typical Turn-Round Time - Two Bridges - Servicing Via Main Deck
**ON A/C A380-800 Models
Typical Turn-Round Time - Two Bridges - Servicing Via Main Deck
1. Typical Turn-Round Time - Two Bridges - Servicing via Main Deck
5-2-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
BRIDGES
TURNAROUND TIME IN MINUTES
LD−3 CARGO FWD
LD−3 CARGO AFT
FREIGHT
BULK
CLEANING
POTABLE WATER
WASTE WATER
REFUELLING
126’
CATERING @M2R
CATERING @M4R
CATERING @M5L
CATERING @U1R
CATERING @U3R
0 10 20 30 40 50 60 70 80 90 100 120110
DEPLANING/
0 10 20 30 40 50 60 70 80 90 100 120110
CABIN
STANDARD 555 PAX PAX 555 TWO BRIDGES(M1,M2) MD CATERING
BOARDING&LPS
2 2
37
0
13
17 20
22 4
21
84
36
20
0
0
0
48
28
20
30
31
18
EQUIPMENTPOSITIONING / REMOVAL
L_AC_050202_1_0010101_01_00
Typical Turn-Round Time -- Two BridgesServicing Via Main Deck
5-2-2
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@A380 AIRPLANE CHARACTERISTICS
5-3-0 Terminal Operation - Cargo Aircraft
**ON A/C A380-800F Models
Terminal Operation - Cargo Aircraft
1. Terminal Operation - Cargo Aircraft
5-3-0
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@A380 AIRPLANE CHARACTERISTICS
5-3-1 Typical Turn-Round Time
**ON A/C A380-800F Models
Typical Turn-Round Time
1. The A380-800F can achieve turn-round times of 120 ± 20 minutes depending on ULD layouts on thethree decks.
NOTE : These values are similar to other wide-body freighter aircraft in similar operating conditions
5-3-1
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@A380 AIRPLANE CHARACTERISTICS
5-4-0 Ground Service Connections
**ON A/C A380-800 Models A380-800F Models
Ground Service Connections
1. Ground Service Connections
5-4-0
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@A380 AIRPLANE CHARACTERISTICS
5-4-1 Ground Service Connections Layout
**ON A/C A380-800 Models
Ground Service Connections Layout - Pax
1. This section gives the ground service connections layout.
5-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1 − PRESSURE REFUEL CONNECTORS2 − HYDRAULIC RESERVOIR SERVICING PANEL
(RESERVOIR FILLING AND RESERVOIR PRESSURISATION)3 − ENGINE OIL FILLING4 − VF GENERATOR OIL FILLING5 − TOILET AND WASTE SERVICE PANEL
6 − GROUND ELECTRICAL POWER7 − LOW PRESSURE PRECONDITIONED AIR
DB1A
8 − YELLOW HYDRAULIC GROUND CONNECTOR9 − GREEN HYDRAULIC GROUND CONNECTOR10 − POTABLE WATER SERVICE PANEL11 − APU OIL FILLING12 − HIGH PRESSURE AIR ENGINE START13 − REFUEL/DEFUEL CONTROL PANEL14 − OXYGEN SYSTEM
4 3 4 3 11
7 11
5
3
4
8
3
4
6
14
12 10
13
2
94
3
4
3
1
5
1
L_AC_050401_1_0010101_01_00
15
15
15 − POTABLE WATER DRAIN PANEL
Ground Service ConnectionsGround Service Connections Layout - A380-800 Models
5-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Ground Service Connections Layout - Freighter
1. This section gives the ground service connections layout.
5-4-1
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@A380 AIRPLANE CHARACTERISTICS
5-4-2 Grounding Points
**ON A/C A380-800 Models A380-800F Models
Grounding Points
1. Grounding Points
DISTANCE: Meters (ft)
AFT OF NOSEFROM AIRPLANECENTERLINE
MEAN HEIGHTFROM GROUND
On Nose Landing Gear 5.713 (18.7) 0.182 (0.6) On the RHside
1.385 (4.5)
On left Wing Gear leg 34.207 (112.2) 5.949 (19.5) 1.237 (4.0)
On right Wing Gear leg 34.207 (112.2) 5.949 (19.5) 1.237 (4.0)
On left Body Gear leg
(Outboard)37.158 (121.9) 2.852 (9.4) 1.379 (4.5)
On left Body Gear leg(Inboard)
37.158 (121.9) 2.412 (7.9) 1.379 (4.5)
On right Body Gear leg(Outboard)
37.158 (121.9) 2.852 (9.4) 1.379 (4.5)
On right Body Gear leg(Inboard)
37.158 (121.9) 2.412 (7.9) 1.379 (4.5)
A. The grounding stud on each landing gear is designed for use with a clip-on connector, such asan Appleton TGR.
B. The grounding studs are used to connect the airplane to approved ground connection on theramp or in the hangar for:
(1) refuel/defuel operations
(2) maintenance operations
(3) bad weather conditions.
5-4-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
A
GROUNDPOINT
L_AC_050402_1_0010101_01_00
Ground Points NLG
5-4-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND POINTA
A
L_AC_050402_1_0020101_01_00
Ground Point WLG
5-4-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUNDPOINTS
(RIGHT ONE SHOWN LEFT ONE SIMILAR)
A
A
L_AC_050402_1_0030101_01_00
Ground Points BLG
5-4-2
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@A380 AIRPLANE CHARACTERISTICS
5-4-3 Hydraulic System
**ON A/C A380-800 Models A380-800F Models
Hydraulic System
1. Door Location
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF
NOSE R SIDE L SIDE
MEANHEIGHT
FROMGROUND
-- Green hydraulic groundconnectors : (Access door 469FL)
34.67 (113.7) 14.90 (48.88) 5.08 (16.66)
-- Yellow hydraulic groundconnector : (Access door 479FL)
34.67 (113.7) 14.90 (48.88) 5.08 (16.66)
-- Hydraulic Reservoir ServicingPanel : (Access door 197CB)
31.89 (104.63) 2.34 (7.67) 1.71 (5.61)
A. Reservoir Pressurization
(1) One connector ETRTO V0.09.6, 1/4 in.
B. ReservoirFilling
(1) One connector AE96993E, 1/4 in.
5-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
B
RESERVOIRPRESSURIZATION
CONNECTOR
RESERVOIR FILLINGCONNECTOR
Z190
A
B
L_AC_050403_1_0010101_01_00
Ground Service ConnectionsHydraulical Reservoir Servicing Panel
5-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
Z460
Z470 B C
A
SELF SEALINGGND CONNECTOR
GREEN HP
SELF SEALINGGND CONNECTOR
GREEN SUCTION
SELF SEALINGGND CONNECTOR
YELLOW HP
SELF SEALINGGND CONNECTOR
YELLOW SUCTION
B C
A
FOR LH PYLON FOR RH PYLON
A
L_AC_050403_1_0020101_01_00
Ground Service ConnectionsHydraulic Ground Connections
5-4-3
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@A380 AIRPLANE CHARACTERISTICS
5-4-4 Electrical System
**ON A/C A380-800 Models
Electrical System - Pax
1. Electrical System
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF
NOSE R SIDE L SIDE
MEANHEIGHT
FROMGROUND
-- Right side access door : 134AR 5.99 (19.65) 0.45 (1.47) 2.59 (8.49)
-- Left side access door : 133AL 5.99 (19.65) 0.45 (1.47) 2.59 (8.49)
A. External Power Receptacles :(1) four standard ISO R461 receptacles - 90 KVA each.
B. Power supply :
(1) three phase, 115V, 400 Hz.
C. Electrical connectors for servicing :
(1) AC outlets : HUBBEL 5258
(2) DC outlets : HUBBEL 7472
(3) Vacuum cleaner outlets : HUBBEL 5258
5-4-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
A
B
A
B
EXTERNAL POWER RECEPTABLES
EXTERNAL POWER RECEPTABLES
L_AC_050404_1_0010101_01_00
Ground Service ConnectionsElectrical Service Panel - A380-800 Models
5-4-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
A
EXTERNAL POWER RECEPTABLES
A
L_AC_050404_1_0030101_01_00
Ground Service ConnectionsElectrical Service Panel - A380-800F Models
5-4-4
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@A380 AIRPLANE CHARACTERISTICS
5-4-5 Oxygen System
**ON A/C A380-800 Models A380-800F Models
Oxygen System
1. Door Location
NOTE : INTERNAL CHARGING CONNECTION PROVIDED
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND-- Access door : 272AFZ 7.45 (24.44) 2.23 (7.32) 3.25 (10.66)
Zero, one or two service connections (external charging in the avionics compartment) MS22066 Std
5-4-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
AL_AC_050405_1_0010101_01_00
Ground Service ConnectionsOxygen System
5-4-5
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@A380 AIRPLANE CHARACTERISTICS
5-4-6 Fuel System
**ON A/C A380-800 Models A380-800F Models
Fuel System
1. Refuel/Defuel Control Panel
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF
NOSE R SIDE L SIDE
MEANHEIGHT
FROMGROUND
-- Refuel/Defuel control panel : (Accessdoor 199KB)
48 (159.48) 0.68 (2.23) 1.98 (6.50)
2. Refuel/Defuel ConnectorsDISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHT
FROMGROUND
-- refuel/defuel coupling, left: (Accessdoor 522GB)
31.89 (104.62)17.97
(58.95)5.94
(19.49)
-- refuel/defuel coupling, right: (Accessdoor 622GB)
31.89 (104.62)17.97
(58.95)5.94
(19.49)
A. Refuel/Defuel couplings :
(1) Standard ISO R45, 2.5 in., two per wing
B. Refuel pressure :
(1) Max. pressure : 3.45 bar (50 psi)
5-4-6
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
Z190
HI LVL
HI LVL
APU EMERGENCY
INCREASE
DECREASE
PRESELECT
PRESELECT (PFQ)
OVERFLOWFAULT
SHUTOFFTEST
NORMAL
BATTERY
POWER SUPPLY
ACTUAL (FOB)
STATUS
MANREFUEL
XFR
DEFUEL
AUTO
REFUELOFF
MODE SELECT
FEED 1
FEED 1
L OUTR
L OUTR
R MID
OPEN
SHUT
R MID
R INR
R INR
TRIM
TRIM
L INR
L INR
L MID
L MID
R OUTROPEN
SHUT
R OUTR
FEED 4
FEED 4
FEED 3
FEED 3
FEED 2
FEED 2
SHUTDOWN
REFUEL/DEFUEL VALVES
kg
B
42QU
BA
A
L_AC_050406_1_0010101_01_00
Ground Service ConnectionsRefuel/Defuel Control Panel
5-4-6
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
REFUEL PRESSURE
REFUEL / DEFUEL COUPLINGS
Z500
Z600 A
LH SIDE SHOWN
RH SIDE SYMETRICAL
B
B
A
A
L_AC_050406_1_0020101_01_00
Ground Service ConnectionsPressure Refuel Connections
5-4-6
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@A380 AIRPLANE CHARACTERISTICS
5-4-7 Pneumatic System
**ON A/C A380-800 Models A380-800F Models
Pneumatic System
1. Low Pressure Connectors
DISTANCE : Meters (ft)
FROM AIRPLANE CERNTERLINEAFT OF NOSE R SIDE L SIDE MEAN HEIGHT
FROM GROUNDaccess doors191GB
21.85 (71.69) 1.24 (4.07) 2.08 (6.82)
access doors191JB
22.36 (73.36) 1.76 (5.77) 2.08 (6.82)
access doors
191HB
21.85 (71.69) 1.24 (4.07) 2.08 (6.82))
access doors191KB
22.36 (73.36) 1.76 (5.77) 2.08 (6.82)
A. Connectors :
(1) Four standard MS33562 (ISO1034), 8 in.
2. High Pressure Connectors
DISTANCE : Meters (ft)
FROM AIRPLANE CERNTERLINE
AFT OF NOSE R SIDE L SIDE MEAN HEIGHTFROM GROUND
-- access doors193BB
25.37 (83.23) 0.2 (0.66) 1.78 (5.84)
A. Connectors :
(1) Three standard MS33740 (ISO2026), 3 in.
5-4-7
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
LOW PRESSURE AIR CONNECTOR
Z190
B
B
B
B
A
A
B
L_AC_050407_1_0010101_01_00
Ground Service ConnectionsLow Pressure Preconditioned Air
5-4-7
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
HIGH PRESSURE AIR CONNECTORS
Z190
BA
A
B
L_AC_050407_1_0020101_01_00
Ground Service ConnectionsHigh Pressure Preconditioned Air
5-4-7
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@A380 AIRPLANE CHARACTERISTICS
5-4-8 Potable Water System
**ON A/C A380-800 Models
Potable Water System - Pax
1. Potable Water System
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND- Potable water ground service panel:access door 199NB
43.67 (143.27) 0.37 (1.21) 2.18 (7.15)
- Potable water drain panel:access door 133BL
9.83 (32.25) 0.3 (0.98) 2.74 (8.99)
A. Connectors :
(1) Fill/Drain Nipple, 3/4 in.
B. Capacity :
(1) Standard configuration - six tanks : 1700 l (449 USgal)
(2) Optional : 2266 l (598 USgal)
C. Filling pressure :
(1) Max Filling Pressure: 8.6 bar (125 psi)
5-4-8
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
80LWL PRE
1000
0 /
PRESS UP OR DOWN TO PRESET
0
50
DOWN PRESET WATER UP
MENUSELECT
DRAIN FILL
NORMAL
FILL/DRAIN NIPPLE
Z190
BA
A
BL_AC_050408_1_0010101_01_00
Ground Service ConnectionsPotable Water Ground Service Panel - A380-800 Models
5-4-8
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
ACCESS DOOR
DRAIN NIPPLE
FWD CARGOFWD CARGOCOMPARTMENTDOOR
DRAIN VALVECONTROL HANDLE
Z130A
B
B
A
L_AC_050408_1_0040101_01_00
Ground Service ConnectionsPotable Water Drain Panel - A380-800 Models
5-4-8
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Potable Water System - Freighter
1. Potable Water System
DISTANCE : Meters (ft)FROM AIRPLANE
CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEANHEIGHTFROM
GROUND
-- access door TBD 5.99 (19.65) 0.45 (1.48) 2.59 (8.50)
A. Connectors :
(1) Fill/Drain Nipple, 3/4 in.
B. Capacity :(1) Standard configuration - one tank : 80 l (21 USgal)
(2) Option available for reservoir of 160 l (42 USgal)
C. Filling pressure :
(1) Max Filling Pressure: 8.6 bar (125 psi)
5-4-8
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
SWITCH FOR PANEL CLOSING FILL/DRAIN NIPPLE TANK FULL INDICATOR
OVERFLOW NIPPLEHANDLE
L_AC_050408_1_0030101_01_00
C
O
A
A
Ground Service ConnectionsPotable Water Ground Service Panel - A380-800F Models
5-4-8
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@A380 AIRPLANE CHARACTERISTICS
5-4-9 Oil System
**ON A/C A380-800 Models A380-800F Models
Engine Oil Servicing
1. Engine Oil Servicing (TRENT900 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
-- Engine 1 (access door 416BR) 32.65 (107.12)23.58
(77.36)4.24 (13.91)
-- Engine 2 (access door 426BR) 24.98 (81.96)12.74
(41.79)3.08 (10.10)
-- Engine 3 (access door 436BR) 32.65 (107.12)16.61
(54.49)3.08 (10.10)
-- Engine 4 (access door 446BR) 24.98 (81.96)27.45
(90.05)4.24 (13.91)
2. Engine Oil Servicing (GP7200 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSE R SIDE L SIDE
MEANHEIGHT
FROMGROUND
-- Engine 1 (access door TBD) 33.03 (108.37) 27.42 (89.96) 4.4 (14.44)
-- Engine 2 (access door TBD) 25.35 (83.17) 16.62 (54.53) 3.13 (10.27)
-- Engine 3 (access door TBD) 25.35 (83.17) 12.78 (41.93) 3.13 (10.27)
-- Engine 4 (access door TBD) 33.03 (108.37) 23.62 (77.49) 4.4 (14.44)
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
A
L_AC_050409_1_0090101_01_00
Ground Service ConnectionsEngine Oil Servicing - TRENT 900 Engines
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
VFG Oil Servicing
1. VFG oil servicing (TRENT900 Engines)
DISTANCE : Meters (ft)FROM AIRPLANE
CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEANHEIGHTFROM
GROUND
-- Engine 1 (access door 415CL) 33.17 (108.83)26.14
(85.76)2.56 (8.39)
-- Engine 2 (access door 425CL) 25.57 (83.89)15.31
(50.22)1.33 (4.36)
-- Engine 3 (access door 435CL) 25.57 (83.89)13.93
(45.70)1.33 (4.36)
-- Engine 4 (access door 445CL) 33.17 (108.83)24.90
(81.69)2.56 (8.39)
2. VFG oil servicing (GP7200 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHT
FROM
GROUND-- Engine 1 (access door TBD) 34.49 (113.16) 25.43 (83.43) 2.63 (8.63)
-- Engine 2 (access door TBD) 26.81 (87.96) 14.63 (48.00) 1.36 (4.46)
-- Engine 3 (access door TBD) 26.81 (87.96) 14.63 (48.00) 1.36 (4.46)
-- Engine 4 (access door TBD) 34.49 (113.16) 25.43 (83.43) 2.63 (8.63)
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
SIGHT GLASSOIL LEVEL
A
A
OIL FILLER PLUG
L_AC_050409_1_0110101_01_00
Ground Service ConnectionsVFG Oil Servicing - TRENT 900 Engines
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
P W V
E − 0 1 4 1 6 ( 0 8 0 5 )
VFG
PRESSURE
FILL VALVE
OVERFLOW
DRAIN VALVE
DUST
CAP
DUST
CAP
A
B
A
B
L_AC_050409_1_0120101_01_00
Ground Service ConnectionsVFG Oil Servicing - GP 7200 Engines
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
OIL FILL PLUG
OILSIGHTGLASS
A
L_AC_050409_1_0130101_01_00
Ground Service ConnectionsStarter Oil Servicing - TRENT 900 Engines
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
OIL FILLER CAP
OIL TANK
SIGHTGLASS
A
A
L_AC_050409_1_0140101_01_00
Ground Service ConnectionsStarter Oil Servicing - GP 7200 Engines
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
APU Oil Servicing
1. APU Oil
DISTANCE : Meters (ft)FROM AIRPLANE
CENTERLINEAFT OF NOSE
R SIDE L SIDE
MEANHEIGHT
FROMGROUND
-- access doors : 315AL, 315AR 67.55 (221.62) 0.44 (1.44) 6.83 (22.40)
A. Capacity :
(1) 18.13L (4.35 USgal)
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
Z310
FULL MARK
VISUAL SIGHT−GLASS
FILL CAP
B
A
FWD
FR117
FR112C
B
A
C
L_AC_050409_1_0150101_01_00
Ground Service ConnectionsAPU Oil Servicing
5-4-9
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@A380 AIRPLANE CHARACTERISTICS
5-4-10 Vacuum Toilet System
**ON A/C A380-800 Models
Vacuum Toilet System - Pax
1. Waste Water System
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHT
FROMGROUND
-- access door 171AL 53.31 (174.90) 0.26 (0.85) 3.40 (11.15)
A. Connectors :
(1) flushing and filling : 1 in.
(2) draining : 4 in.
B. Capacity : 2100 l
C. Operating pressure for the waste tank rinsing process: 50 psi (max 125 psi)
D. Flow rate : 40 l/min
5-4-10
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
WASTETANKDRAIN VALVEOPEN
UPPERDECK
MAINDECK
RH LH RH LH
CLOSE
CONTROLLEVER
CONNECTIONWASTE DRAIN
FILL AND RINSE
CONNECTION
FWDB
Z160
FR86FR91A
A
B
L_AC_050410_1_0010101_01_00
Ground Service ConnectionsVacuum Toilet System - A380-800 Models
5-4-10
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Z130A
FR22
FR38
CONTROL LEVERWASTE DRAIN
FILL AND RINSE
CONNECTION
CONNECTION
B
FWD
A
BL_AC_050410_1_0020101_01_00
Ground Service ConnectionsVacuum Toilet System - A380-800F Models
5-4-10
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@A380 AIRPLANE CHARACTERISTICS
5-5-0 Engine Starting Pneumatic Requirements
**ON A/C A380-800 Models A380-800F Models
Engine Starting Pneumatic Requirements
1. Engine Starting Pneumatic Requirements
5-5-0
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@A380 AIRPLANE CHARACTERISTICS
5-5-1 Outside Air Temperature = -40 ˚C (-40 ˚F)
**ON A/C A380-800 Models A380-800F Models
Outside Air Temperature = -40 ˚C (-40 ˚F)
1. This section provides the engine starting pneumatic requirements for an ambient temperature of -40˚C (-40˚F).
5-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E
S S U R E ( b a r s )
T = 60°C
RR −40° 2 CONNECTIONS SEA LEVEL
T = 85°C
T = 135°C
T = 235°C
T = 260°C
T = 260°C
T = 85°C
T = 185°C
T = 60°CT = 135°C
T = 235°C
T = 185°C
1.00
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
90s
SEA LEVEL
120s
L_AC_050501_1_0010101_01_00
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature -40 ˚C (-40 ˚F), sea level - TRENT 900 Engines
5-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
110s
T = 270°C
70s
T = 245°C
T = 195°C
T = 140°C
T = 90°C
T = 65°C
T = 90°C
T = 140°C
T = 270°C
T = 245°C
T = 195°C
T = 65°C
T = 90°C
T = 65°C
T = 140°C
T = 195°C
T = 245°C
T = 90°C
T = 140°C
T = 195°C
T = 245°C
T = 270°C
EA −40° 2 CONNECTIONS
T = 270°C
L_AC_050501_1_0020101_01_00
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature -40˚C (-40˚F), sea level - GP 7200 Engines
5-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
RR −40° 3 CONNECTIONS SEA LEVEL
T = 85°C
T = 255°CT = 235°C
T = 135°C
T = 185°C
T = 60°C
T = 235°C
T = 255°C T = 185°C
T = 55°C
T = 130°C
T = 80°C
1.00
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
90s
SEA LEVEL
120s
L_AC_050501_1_0030101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature -40˚C (-40˚F), Sea Level - TRENT 900 Engines
5-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
110s
70s
T = 65°C
T = 65°C
T = 90°C
EA −40° 3 CONNECTIONS
T = 65°C
T = 90°C
T = 90°C
T = 270°C
T = 270°C
T = 270°C
T = 270°C
T = 140°C
T = 140°C
T = 140°C
T = 140°C
T = 195°C
T = 245°C
T = 195°C
T = 245°C
T = 245°C
T = 195°C
T = 195°C
T = 245°C
T = 90°C
L_AC_050501_1_0040101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature -40˚C (-40˚F), Sea Level - GP 7200 Engines
5-5-1
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@A380 AIRPLANE CHARACTERISTICS
5-5-2 Outside Air Temperature = 15 ˚C (59 ˚F)
**ON A/C A380-800 Models A380-800F Models
Outside Air Temperature = 15 ˚C (59 ˚F)
1. This section provides the engine starting pneumatic requirements for an ambient temperature of +15˚C (+59.0 ˚F)
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E
S S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
RR 15° 2 CONNECTIONS SEA LEVEL
T = 130°C
T = 180°C
T = 230°C
T = 255°C T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°CT = 260°C
T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°C
T = 260°C
T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°C
T = 260°C
60s
SEA LEVEL
90s
110s
70s
L_AC_050502_1_0010101_01_00
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature +15˚C (+59˚F), Sea Level - TRENT 900 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
L_AC_050502_1_0020101_01_00
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E
S S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
110s
70s
T = 60°C
EA 15° 2 CONNECTIONS
T = 85°C
T = 135°C
T = 190°C
T = 240°C
T = 265°C
T = 60°C
T = 85°C
T = 135°C
T = 265°C
T = 265°C
T = 240°C
T = 190°C
T = 240°C
T = 85°C
T = 60°C
T = 85°C
T = 135°C
T = 135°C
T = 190°C
T = 190°C
T = 240°C
T = 265°C
T = 60°C
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature +15˚C (+59˚F), Sea Level - GP 7200 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
RR 15° 2 CONNECTIONS 5000 FT
T = 55°C
T = 80°C
T = 230°C
T = 230°C
T = 255°C
T = 180°C
T = 80°C
T = 55°CT = 130°C
T = 255°C
T = 180°C
T = 130°C
1.00
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
90s
5000 FT
110s
L_AC_050502_1_0030101_01_00
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature +15˚C (+59˚F), 5000FT Level - TRENT 900 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
90s
110s
70s
EA 15° 3 CONNECTIONS 5000 FT
T = 60°C
T = 60°C
T = 85°C
T = 135°C
T = 60°C
T = 85C
T = 60°C
T = 85°CT = 135°C
T = 265°C
T = 240°C
T = 85°C
T = 135°C
T = 265°C
T = 190°C
T =190°C T = 135°C
T = 265°C
T = 190°C
T = 240°C
T = 240°C
T = 240°C
T = 265°C
T = 190°C
5000 FT
L_AC_050502_1_0040101_01_00
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature +15˚C (+59˚F), 5000FT Level - GP 7200 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
RR 15° 3 CONNECTIONS SEA LEVEL
T = 130°C
T = 180°C
T = 230°C
T = 255°CT = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°CT = 255°C
T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°C
T = 255°C
T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°C
T = 255°C
1.00
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
110s
70s
L_AC_050502_1_0050101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature +15˚C (+59˚F), Sea Level - TRENT 900 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E
S S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
110s
70s
T = 60°C
EA 15° 3 CONNECTIONS
T = 85°C
T = 85°C
T = 60°C
T = 135°C
T = 60°C
T =240°C
T = 265°C
T = 265°C
T = 240°C
T =190°CT =190°C
T =190°C
T =135°C
T =135°C
T = 85°C
T =190°C
T = 265°C
T = 240°C
T = 265°C
T = 240°C
T = 85°C
T = 60°C
T =135°C
L_AC_050502_1_0060101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature +15˚C (+59˚F), Sea Level - GP 7200 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S
S U R E ( b a r s )
RR 15° 3 CONNECTIONS 5000 FT
T = 255°C T = 230°C
T = 80°C
T = 55°C
T = 130°C
T = 180°C
T = 255°C
T = 230°CT = 130°C
T = 55°C
T = 80°C
T = 180°C
1.00
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
90s
5000 FT
110°C
L_AC_050502_1_0070101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature +15˚C (+59˚F), 5000FT Level - TRENT 900 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S
S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
5000 FT
90s
110s
70s
T = 60°C
EA 15° 2 CONNECTIONS 5000 FT
T = 85°C
T = 60°C
T = 85°C
T = 135°C
T = 60°C
T = 85°C
T = 60°C
T = 85°C
T = 135°C
T = 190°C
T = 240°C
T = 135°C
T = 190°C
T = 240°C
T = 265°C
T = 265°C
T = 240°C
T = 190°C
T = 265°C
T = 240°CT = 190°C
T = 135°C
T = 265°C
L_AC_050502_1_0080101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature +15˚C (+59˚F), 5000FT Level - GP 7200 Engines
5-5-2
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@A380 AIRPLANE CHARACTERISTICS
5-5-3 Outside Air Temperature = 50˚C (122 ˚F)
**ON A/C A380-800 Models A380-800F Models
Outside Air Temperature = 50˚C (122 ˚F)
1. This section provides the engine starting pneumatic requirements for an ambient temperature of +55˚C (+131.0 ˚F).
5-5-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E
S S U R E ( b a r s )
RR 55° 2 CONNECTIONS SEA LEVEL
T = 180°C
T = 230°CT = 255°C
T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°CT = 255°C
T = 55°C
T = 80°CT = 230°C
T = 130°C
T = 180°CT = 255°C
T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°C
T = 255°C
1.00
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
120°C
70s
L_AC_050503_1_0010101_01_00
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature +55˚C (+131˚F), Sea Level - TRENT 900 Engines
5-5-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
110s
70s
T = 60°C
T = 85°C
T = 190°C
T = 135°C
T = 85°C
T = 60°C
T = 85°C
T = 135°C
T = 60°C
T = 265°C
T = 60°C
T = 85°C
T = 135°C
T = 190°C
T = 240°C
T = 265°C
T = 190°C
T = 265°C
T = 240°C
T = 190°C
T = 240°C
T = 240°C
T = 265°C
T = 135°C
GROUND CART MASS FLOW (kg/s)
EA 55° 2 CONNECTIONS
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
L_AC_050503_1_0020101_01_00
Engine Starting Pneumatic Requirements (two high pressure ground carts)Ambient Temperature +55˚C (+131˚F), Sea Level - GP 7200 Engines
5-5-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S
S U R E ( b a r s )
RR 55° 3 CONNECTIONS SEA LEVEL
T = 180°CT = 230°C
T = 255°C
T = 55°C
T = 80°C
T = 130°C
T = 180°C
T = 230°CT = 255°C
T = 55°CT = 130°C
T = 80°C
T = 180°C
T = 230°CT = 255°C
T = 255°C
1.00
4.50
4.00
3.50
2.50
1.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
120°C
70s
T = 130°C T = 55°C
T = 80°C
T = 180°C
T = 230°C
L_AC_050503_1_0030101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature +55˚C (+131˚F), Sea Level - TRENT 900 Engines
5-5-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
G R O U N D C A R T O U T P U T A B S P R E S S U R E ( b a r s )
4.50
4.00
3.50
3.00
2.50
2.001.20 1.40 1.60 1.80 2.00 2.20 2.40 2.60 2.80 3.00
60s
SEA LEVEL
90s
110s
70s
EA 55° 3 CONNECTIONS
T = 60°C
T = 85°C
T = 60°C
T = 85°C
T = 135°C
T = 60°C
T = 85°C
T = 60°C
T = 85°C
T = 135°C
T = 190°C
T = 240°C
T = 265°C
T = 135°C
T = 190°C
T = 265°C
T = 190°C
T = 135°C
T = 240°C
T = 265°C
T = 190°C
T = 265°C
T = 240°C
T = 240°C
L_AC_050503_1_0040101_01_00
Engine Starting Pneumatic Requirements (three high pressure ground carts)Ambient Temperature +55˚C (+131˚F), Sea Level - GP 7200 Engines
5-5-3
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@A380 AIRPLANE CHARACTERISTICS
5-6-0 Ground Pneumatic Power Requirements
**ON A/C A380-800 Models A380-800F Models
Ground Pneumatic Power Requirements
1. Ground Pneumatic Power Requirements
5-6-0
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@A380 AIRPLANE CHARACTERISTICS
5-6-1 Heating
**ON A/C A380-800 Models A380-800F Models
Heating
1. This section provides the ground pneumatic power requirements heating.
5-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
20
7.0
6.5
6.0
5.5
5.0
4.5
4.0
3.5
3.0
2.5
2.0
PULL UP
30 40 50 60 70 80 90
LPGC PERFORMANCE − CABIN PULL UP
TIME TO HEAT CABINTO 21 °C (69.8 °C)
ON GROUNDPULL UP
kg/sec min
3.03.54.04.55.05.56.06.5
8065554842.5383531.6
T O T A L M
A S S F L O W
P E R A I R C R A F T ( k g / s e c )
TIME TO HEAT CABIN TO 21 °C (MINUTES)
PULL UP: INITIAL CABIN TEMPERATURE AT −23 °C, HEAT UP TO 21 °C ON GROUND,
TEMPERATURE AT THE GROUND CONNECTION: 70 °C
TOTAL LPGCAIR FLOW
L_AC_050601_1_0010101_01_00
Ground Pneumatic Power Requirements HeatingGround Pneumatic Power Requirements Heating - A380-800 Models
5-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
20
7.0
6.5
6.0
5.5
5.0
4.5
4.0
3.5
3.0
2.5
2.0
CARGO PULL UP
30 40 50 60 70 80
LPGC PERFORMANCE − CARGO/COURIER PULL UP
PULL UP TIME
[kg/sec][min]
3.03.54.05.05.56.5
776150363124
T O T A L
M A S S F L O W
P E R A I R C R A F T ( k g / s e c )
TIME TO HEAT COMPARTMENT TO 21 °C (MINUTES)
INITIAL TEMPERATURE AT −23°C OAT, COURIER AND CARGO COMPARTMENT HEATING TO 21°C,ASSUMED LPGC INLET TEMPERATURE 70°C.
TOTAL LPGCAIR FLOW
504135272520
CARGO COURIER
COURIER PULL UP
10
L_AC_050601_1_0020101_01_00
Ground Pneumatic Power Requirements HeatingGround Pneumatic Power Requirements Heating - A380-800F Models
5-6-1
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@A380 AIRPLANE CHARACTERISTICS
5-6-2 Cooling
**ON A/C A380-800 Models A380-800F Models
Cooling
1. This section provides the ground pneumatic power requirements cooling.
5-6-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
20
7.0
6.5
6.0
5.5
5.0
4.5
4.0
3.5
3.0
2.5
2.0
30 40 50 60 70 80 90
kg/sec min
TOTAL LPGCAIR FLOW
TIME TO COOL CABINTO 27 °C (80.6 °C)
ON GROUNDPULL DOWN
−−−−875838
30
3.03.54.04.55.05.56.0
6.5
PULL DOWN
LPGC PERFORMANCE − CABIN PULL DOWN
TIME TO COOL CABIN TO 27 °C (MINUTES)
SAME BOUNDARY CONDITIONS AS BEFORE
T O T A L
M A S S F L O W
P E R A I R C R A F T ( k g / s e c )
(IN ADDITION BLENDS DOWN FOR THE PULL DOWN CASE), HP AND LP FANS ON
PULL DOWN:INITIAL CABIN TEMPERATURE AT 38 °C, COOL DOWN TO 27 °C ON GROUNDTEMPERATURE AT THE GROUND CONNECTION: 1.5 °C
L_AC_050602_1_0010101_01_00
Ground Pneumatic Power Requirements CoolingGround Pneumatic Power Requirements Cooling - A380-800 Models
5-6-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
20
7.0
6.5
6.0
5.5
5.0
4.5
4.0
3.5
3.0
2.5
2.0
CARGO PULL DOWN
30 40 50 60 70 80
LPGC PERFORMANCE − CARGO/COURIER PULL DOWN
PULL DOWN TIME
[kg/sec][min]
3.03.54.05.05.5
6.5
6247372521
15
T O T A L
M A S S F L O W
P E R A I R C R A F T ( k g / s e c )
TIME TO COOL COURIER COMPARTMENT TO 27°C AND
INITIAL TEMPERATURE AT 38°C OAT, COURIER COMPARTMENT COOL DOWN TO 27°C AND CARGO
COMPARTMENT COOL DOWN TO 24°C, ASSUMED LPGC INLET TEMPERATURE 1.5°C
TOTAL LPGCAIR FLOW
4031251715
12
CARGO COURIER
COURIER PULL DOWN
10
CARGO COMPARTMENT TO 24°C (MINUTES)
L_AC_050602_1_0020101_01_00
Ground Pneumatic Power Requirements CoolingGround Pneumatic Power Requirements Cooling - A380-800F Models
5-6-2
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@A380 AIRPLANE CHARACTERISTICS
5-7-0 Preconditioned Airflow Requirements
**ON A/C A380-800 Models A380-800F Models
Preconditioned Airflow Requirements
1. This section provides the preconditioned airflow requirements.
5-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
NOTE:
INLET TEMPERATURE (C°)
−40 −20 0 20 40 60 80 100 120 140
INLET TEMPERATURE (F°)
C3 CURVE ASSUMES:
IFE = IN−FLIGHT ENTERTAINMENT SYSTEM.OAT = OUTSIDE AIR TEMPERATURE.
3
4
5
6
7
− SAME CONDITIONS AS C1 BUT WITHOUT PASSENGERS
AT CONNECTION
T O T A L F R E S H
A I R F L O W ( k g / s )
C1 CURVE ASSUMES:
COOLING CASES ARE C1, C2 AND C3.
HEATING CASES ARE C4, C5 AND C6.
− SAME CONDITIONS AS C1 BUT WITH IFE OFF VIDEO OPERATION 0% PC OPERATION 0%
− LPGC AIR AT 45% RH− AIRCRAFT CONFIGURED IN STANDARD ZONES− CABIN TEMPERATURE: 27°C (80.6°F)− MAX. PASSENGER LOAD, 19 ATTENDANTS, 5 CREW MEMBERS− HP RECIRCULATION: ON ( HP FILTER CONDITION: NEW CARTRIDGE )− SOLAR RADIATION IS INCLUDED IN CALCULATIONS− IFE: ON− VIDEO OPERATION 75%, PC OPERATION 13%− BOTH AVIONIC VALVES OFF− CARGO VALVES ON ( CARGO FLOW SETTING NORMAL )
C4, C5 AND C6 CURVES ASSUME:− LPGC AIR AT 45% RH− AIRCRAFT CONFIGURED IN STANDARD ZONES− CABIN TEMPERATURE: 21°C (69.8°F)− NO PASSENGER, 0 ATTENDANT, 0 CREW MEMBER− HP RECIRCULATION: ON ( HP FILTER CONDITION: NEW CARTRIDGE )− SOLAR RADIATION IS NOT INCLUDED− IFE: OFF− VIDEO OPERATION 0%, PC OPERATION 0%− CABIN LIGHTING OFF, GALLEY POWER OFF− BOTH AVIONIC VALVES OFF− CARGO VALVES OFF ( CARGO FLOW SETTING NORMAL )
C2 CURVE ASSUMES:
6.5 O A T
: − 3 0
° C
( − 2 2 ° F )
( − 9
. 4 ° F )
O A T
: − 2
3 ° C
O A T
: −
4 0
° C
( − 4 0 ° F )
O A T : 3 8 ° C
( 1 0 0
. 4 ° F )
40 mbar
50 mbar
60 mbar
70 mbar
80 mbar
90 mbar
C1 C2
C6
O A T
: 3 8 °
C ( 1 0 0 . 4 ° F )
O A T
: 3 8 °
C ( 1 0 0
. 4 ° F )
Maximum allowed mass flow
C5
−40 −30 −20 −10 0 10 20 30 40 50 60
C4
C3
L_AC_050700_1_0010101_01_00
Preconditioned Airflow RequirementsPreconditioned Airflow Requirements - A380-800 Models
5-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
LPGC INLET TEMPERATURE (C°)
−40 −20 0 20 40 60 80 100 120 140
LPGC INLET TEMPERATURE (F°)
TOTAL FLOW LIMIT AT 6,5 KG/S DUE TO CPCS (CABIN PRESSURE CONTROL SYSTEM), MAX RESIDUALPRESSURE 2MBAR WITH CLOSED DOORS
3
4
5
6
7
COMPARTMENT
T O T A L F L O W
( k g / s )
COOLING CASES [1] ASSUMES:
− SAME AS COOLING [1], BUT MAX COURIER LOAD AND 3kW TRANSPORT LOAD PER CARGO
− HOT DAY (ISA +23°)− STANDARD AIRFLOW DISTRIBUTION− STABILIZED CARGO COMPARTMENT TEMPERATURE 24°C, COURIER COMPARTMENT 27°C− NO OCCUPANT LOAD, EMPTY CARGO COMPARTMENT− NO HIGH PRESSURE RECIRCULATION, LOW PRESSURE RECIRC ON− LOWER DECK CARGO: VENTILATION ONLY
HEATING CASE ASSUMES:− COLD DAY (ISA −38°C)− STANDARD AIRFLOW DISTRIBUTION− STABILIZED CARGO AND COURIER COMPARTMENT TEMPERATURE 21°C− NO OCCUPANT LOAD, EMPTY CARGO COMPARTMENT− NO HIGH PRESSURE RECIRCULATION, LOW PRESSURE RECIRC ON− LOWER DECK CARGO: VENTILATION ONLY
COOLING CASE [2] WITH COMPARTMENT LOADS:
6.5
Maximum allowed mass flow
5 15 25 35 45
2
55
160 180
65
courier comp hot day [1]cargo comp hot day [1]courier hot day w load [2]cargo hot day w load [2]cargo comp cold daycourier comp cold day
200 220
daycold
−5
hotday
L_AC_050700_1_0020101_01_00
Preconditioned Airflow RequirementsPreconditioned Airflow Requirements - A380-800F Models
5-7-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
0
4
8
1 2 1 6
2 4 2 8 3 2 3 6 4 0 4 4 4 8 5 2 5 6 6 0 6 4 6 8 7 2
0
1
2
3
4
0
0 . 5
1
1 . 5
2
2 0
0 4 8 1 2
1 6
2 0
2 4
2 8
3 2
3 6
4 0
4 4
4 8
5 2
5 6
6 0
0 4 8 1 2
1 6
2 0
2 4
3 2
3 6
4 0
4 4
4 8
5 2
5 6
6 0
3 0
0
3 5
0
4 0
0
4 5
0 4 8 0
5 0
0
5 5
0
6 0
0
D R A W B A R P U L L ( t )
A I R C R A F T W E I G H T ( t )
T O T A L T R A C T I O N W
H E E L L O A D ( t )
N O O F E N G I N E S
A T I D L E
S L O P E ( % )
D R Y C
O N C
R E T E
= 0 . 8
2 8
W E T C
O N C
R E T E
= 0 .
5 7
H A R D S N O W
= 0 . 2
N O T E : − U N U S U A L B R E A K A W A Y C
O N D I T I O N S N O T S H O W N
− S T R A I G H T − L I N E T O W
I C E
=
0 . 0
5
E X A M P L E
L_AC_050800_1_0010101_01_01
Ground Towing RequirementsA380-800 Models
5-8-0
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@A380 AIRPLANE CHARACTERISTICS
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A380-800 Models A380-800F ModelsEngine Exhaust Velocities and Temperatures
1. GeneralThis section shows the estimated engine exhaust efflux velocity and temperature contours forMaximum Take-off, Breakaway and Idle conditions for the A380 engine models.
Contours are available for both Rolls-Royce’s Trent 900 engine and the Engine Alliance’s GP7200engine.
The Maximum Take-off data are presented at the maximum thrust rating for all the A380 engine
models, including the A380-800F Freighter version. Therefore, contours hereafter include contours of the A380-800 Passenger version.
The Breakaway data are presented at a rating corresponding to the minimum thrust level required toinitiate movement of an A380-800F model at its maximum ramp weight from static position and onuphill ground.
The Idle data are directly provided by the engine manufacturers.
In the charts, longitudinal distances are measured from the inboard engine core nozzle exit station,while lateral distances are measured from the aircraft fuselage centreline.
A. Data from Rolls-Royce’s Trent 900:
The estimated efflux data are presented at ISA+15˚C (30˚C), Sea Level Static and negligiblewind conditions.The analysis assumes that the core and bypass streams are fully mixed and calculates the jetbehaviour in free, still air and therefore does not take into account effects such as on-winginstallation, ground entrainment and ambient wind conditions.Velocity contours are presented at 50 ft/s (15 m/s), 100 ft/s (30 m/s) and 150 ft/s (46 m/s),while temperature contours are presented at 104 ˚F (40˚C), 122˚F (50˚C) and 172˚F
(60˚C).
B. Data from Engine Alliance’s GP7200:
6-1-0
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@A380 AIRPLANE CHARACTERISTICS
The estimated efflux data are presented at ISA+15˚C (30˚C), Sea Level Static with 20 ktheadwind. It also assumed ground plane and proximity effects. Velocity contours are presentedat 35 MPH (15 m/s), 65 MPH (30 m/s) and 105 MPH (46 m/s), while temperature contoursare presented at 122˚F (50˚C), 212˚F (100˚C) and 392˚F (200˚C). Engine Alliance strongly
recommends that jet blast studies using their contours include the effect of a 20-knot headwind.
6-1-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
d e h 0 0 0
2 3 1 7
10
20
0
0 40 60
20
80
30
100 120
40 50
140 160
60
180 200
METERS
FEET
ELEVATION
PLAN
0
5
10
15
20
40
60
m ft
50 ft/sec(15 m/sec)
100 ft/sec(30 m/sec)
150 ft/sec(46 m/sec)
100 ft/sec(30 m/sec)
150 ft/sec(46 m/sec)
50 ft/sec(15 m/sec)
0
5
10
15
20
40
60
m ft
60
60
60
15
15
15
15
220
L_AC_060101_1_0010101_01_00
Engine Exhaust VelocitiesGround Idle Power - TRENT 900 Engines
6-1-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
ALL VELOCITY VALUES ARE IN STATUE MILES PER HOUR.
FEET
(METERS)
GROUND PLANE
CONVERSION FACTOR
1 MPH = 1.6 km/h
300
(91)
140
(43)
ELEVATION
FEET
(METERS)
0
0
PLAN
150
(46)
0
70
(21)
P W V
E − 0 0 2
2 4 ( 0 2 0 7 )
AIRPLANECL
105 MPH
65 MPH
35 MPH
DANGER (KEEP OUT) ZONES 35 MPH
(169 km/h)
(105 km/h)
(56 km/h)
105 MPH65 MPH
35 MPH
(169 km/h)(105 km/h)
(56 km/h)
FEET
(METERS)
140
0
70
(21)
L_AC_060101_1_0020101_01_01
NOTE:
Engine Exhaust VelocitiesGround Idle Power - GP 7200 Engines
6-1-1
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@A380 AIRPLANE CHARACTERISTICS
6-1-2 Engine Exhaust Temperatures - Ground Idle Power
**ON A/C A380-800 Models A380-800F Models
Engine Exhaust Temperatures - Ground Idle Power
1. This section gives engine exhaust temperatures at ground idle power.
6-1-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
10
20 40 60
20 30
80 100 120
40
140 160
500
0
METERS
FEET
20
40
60
15
0
10
5
m ft
ELEVATION
PLAN
d e h 0 0 0 2 3 1 6
20
40
60
15
0
10
5
m ft
140°F(60°C)122°F(50°C) 104°F(40°C)
140°F(60°C)
122°F(50°C)
104°F(40°C)
80
100
120
20
25
30
35
L_AC_060102_1_0010101_01_01
GROUND IDLE POWER
Engine Exhaust TemperaturesGround Idle Power - TRENT 900 Engines
6-1-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
FEET
(METERS)
GROUND PLANEELEVATION FEET
(METERS)
0
0
PLAN AIRPLANECL
0
70
(21)
0
70
(21)
105
(32)
ALL TEMPERATURES ARE IN FAHRENHEIT (CELSIUS).
392°F (200°C)
212°F (100°C)
122°F (50°C)
150
(46)
75
(23)
225
(69)
105
(32)
35
(11)
35
(11)
P W V
E − 0 0 2
2 6 ( 0 2 0 7 )
392°F (200°C)
122°F (50°C)
212°F (100°C)
NOTE:
L_AC_060102_1_0020101_01_01
Engine Exhaust TemperaturesGround Idle Power - GP 7200 Engines
6-1-2
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@A380 AIRPLANE CHARACTERISTICS
6-1-3 Engine Exhaust Velocities - Breakaway Power
**ON A/C A380-800 Models A380-800F Models
Engine Exhaust Velocities - Breakaway Power
1. This section gives engine exhaust velocities at breakaway power.
6-1-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
d e h 0 0 0
2 3 1 9
100METERS 00FEET 40 80
20 40 60 80
120 160 200 240 280 320 360
5
10
15
40
60
ftm
20
50 ft/sec(15 m/sec)
100 ft/sec(30 m/sec)
150 ft/sec(46 m/sec)
ELEVATION
PLAN
50 ft/sec(15 m/sec)
100 ft/sec(30 m/sec)
150 ft/sec(46 m/sec)
5
10
15
40
0
60
ftm
20
0
80
100
120
20
25
30
35
L_AC_060103_1_0010101_01_00
Engine Exhaust VelocitiesBreakaway Power - TRENT 900 Engines
6-1-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
ALL VELOCITY VALUES ARE IN STATUE MILES PER HOUR.
CONVERSION FACTOR
1 MPH = 1.6 km/h
P W V
E − 0 2 2
0 0 ( 0 2 0 7 )
DANGER (KEEP OUT) ZONES 35 MPH
NOTE:
L_AC_060103_1_0020101_01_01
FEET
(METERS)
GROUND PLANE
140
(43)
ELEVATION
0
70
(21)
PLAN AIRPLANECL
FEET
(METERS)
0
0
150
(46)
300
(91)
450
(137)
105 MPH65 MPH
35 MPH(169 km/h)(105 km/h)
(56 km/h)
105 MPH
(169 km/h) 65 MPH
(105 km/h) 35 MPH
(56 km/h)
FEET
140
(43)
0
70
(21)
Engine Exhaust VelocitiesBreakaway Power - GP 7200 Engines
6-1-3
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@A380 AIRPLANE CHARACTERISTICS
6-1-4 Engine Exhaust Temperatures - Breakaway Power
**ON A/C A380-800 Models A380-800F Models
Engine Exhaust Temperatures - Breakaway Power
1. This section gives engine exhaust temperatures at breakaway power.
6-1-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
ELEVATION
20 40 60 80 100 120 140 160
40302010METERS 0
0FEET
520
10
40
60
15
m ft
0
d e h 0 0 0 2 3 1 8
520
10
40
60
15
m ft
PLAN
140°F(60°C)
122°F(50°C)
104°F(40°C)
140°F(60°C)
122°F(50°C)
104°F(40°C)
0
80
100
120
20
25
30
35
180
50
L_AC_060104_1_0010101_01_01
BREAKAWAY POWER(11% MAX TAKE−OFF THRUST)
Engine Exhaust TemperaturesBreakaway Power - TRENT 900 Engines
6-1-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
AIRPLANECL
NOTE : ALL TEMPERATURES ARE IN FAHRENHEIT (CELSIUS).
392°F (200°C)
212°F (100°C)
122°F (50°C)
392°F (200°C)
212°F (100°C)
122°F (50°C)
FEET
(METERS)
GROUND PLANEELEVATION
FEET
(METERS)
0
0
PLAN
0
70
(21)
0
70
(21)
105
(32)
150
(46)
75
(23)
225
(69)
105
(32)
35
(11)
35
(11)
PW VE−02201 (0805)
L_AC_060104_1_0020101_01_00
Engine Exhaust TemperaturesBreakaway Power - GP 7200 Engines
6-1-4
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@A380 AIRPLANE CHARACTERISTICS
6-1-5 Engine Exhaust Velocities - Max Take-off Power
**ON A/C A380-800 Models A380-800F Models
Engine Exhaust Velocities - Max Take-off Power
1. This section gives engine exhaust velocities at max take-off power.
6-1-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
d e h 0 0 0
2 3 1 5
20
100 200 300 400 500 600 700 800
40 60 80 100 120 140 160 180 200 220 240METERS 0
FEET
0
20
10 40
80m ft
TO1800 ft(540 m)
TO1800 ft(540 m)
PLAN
ELEVATION
50 ft/sec(15 m/sec)
100 ft/sec(30 m/sec)
150 ft/sec(46 m/sec)
0
20
10 40
80
m ft
120
160
30
40
60
50 ft/sec(15 m/sec)
100 ft/sec(30 m/sec)
150 ft/sec(46 m/sec)
L_AC_060105_1_0010101_01_00
Engine Exhaust VelocitiesMax. Take-Off Power - TRENT 900 Engines
6-1-5
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
L_AC_060105_1_0020101_01_01
ALL VELOCITY VALUES ARE IN STATUE MILES PER HOUR.
CONVERSION FACTOR
1 MPH = 1.6 km/h
P W V
E − 0 0 2
2 5 ( 0 2 0 7 )
DANGER (KEEP OUT) ZONES 35 MPH
NOTE:
FEET
(METERS)
GROUND PLANE
300 450 600
140
(43)
ELEVATION
FEET
0 150
0
70
(21)
(91) (137) (183)0 (46)
(METERS)
PLAN AIRPLANECL
65 MPH
OUT TO
1090 ft
(332 m)
105 MPH
OUT TO
724 ft
(221 m)
35 MPH
OUT TO
1553 ft
(473 m)
FEET
(METERS)
140
(43)
0
70
(21)
65 MPH
OUT TO
1090 ft
(332 m)
105 MPH
OUT TO
724 ft
(221 m)
35 MPH
OUT TO
1553 ft
(473 m)
Engine Exhaust VelocitiesMax. Take-Off Power - GP 7200 Engines
6-1-5
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@A380 AIRPLANE CHARACTERISTICS
6-1-6 Engine Exhaust Temperatures - Max Take-off Power
**ON A/C A380-800 Models A380-800F Models
Engine Exhaust Temperatures - Max Take-off Power
1. This section gives engine exhaust temperatures at max take-off power.
6-1-6
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
d e h 0 0
0 2 3 1 4
20METERS 0
FEET 0 40 80 120
40 60
160
80
200 240 280 320
100
360
120
400
20
40
60
10
5
15
0
ftm
ELEVATION
PLAN
20
40
60
10
5
15
0
ftm
80
100
120
15
20
25
30
35
140°F(60 C)
122°F(50 C)
104°F(40 C)
TO540 ft
(162 m)
140°F(60 C)
122°F(50 C)
104°F(40 C)
TO540 ft
(162 m)
L_AC_060106_1_0010101_01_01
MAX TAKE−OFF POWER
Engine Exhaust TemperaturesMax Take-Off Power - TRENT 900 Engines
6-1-6
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
70(21)
35(11)
105(32)
E−00227 (0704)PW V
FEET(METERS)
0ELEVATION
0 PLAN
0
0
FEET
(METERS)
75
(23)
150
(46)
225
(69)
AIRPLANE
GROUND PLANE
392°F (200°C)
212°F (100°C)
122°F (50°C)
392°F (200°C)212°F (100°C)
122°F (50°C)
NOTE : ALL TEMPERATURES ARE IN FAHRENHEIT (CELSIUS).
CL
70(21)
35(11)
105(32)
L_AC_060106_1_0020101_01_00
Engine Exhaust TemperaturesMax Take-Off Power - GP 7200 Engines
6-1-6
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@A380 AIRPLANE CHARACTERISTICS
6-2-1 Airport and Community Noise Data
**ON A/C A380-800 Models A380-800F Models
Airport and Community Noise Data
1. RR TRENT 900 Engines
A. Description of Test ConditionsThe arc of circle (radius = 60m), with microphones 1.2 m high, is centered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Meteorological DataThe meteorological parameters measured 1.6 m from the ground on the day of test were asfollows:- Temperature: 32˚C- Relative humidity: 31%- Atmospheric pressure: 996 hPa- Wind speed: Negligible- No rain
2. EA GP7200 Engines
A. Description of Test ConditionsThe arc of circle (radius = 60m), with microphones 1.2 m high, is centered on the position of the noise reference point.A.P.U. : off ; E.C.S. : Packs off.
B. Meteorological Data
The meteorological parameters measured 1.6 m from the ground on the day of test were asfollows:- Temperature: 12˚C- Relative humidity: 90%- Atmospheric pressure: 1015 hPa- Wind speed: Negligible- No rain
6-2-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
0°10°20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°160°
170° 180° 190°200°
210°
220°
230°
240°
250°
260°
270°
280°
290°
300°
310°
320°
330°340°
350°
DB (A)
75
80
85
90
95
100
105
110
MAX THRUST POSSIBLEON BRAKES
4 ENGINES RUNNING
GROUND IDLE4 ENGINES RUNNING
L_AC_060201_1_0030101_01_01
Airport and Community Noise DataTRENT 900 Engines
6-2-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
0°10°20°
30°
40°
50°
60°
70°
80°
90°
100°
110°
120°
130°
140°
150°160°
170° 180° 190°200°
210°
220°
230°
240°
250°
260°
270°
280°
290°
300°
310°
320°
330°340°
350°
DB (A)
75
80
85
90
95
100
105
110
MAX THRUST POSSIBLEON BRAKES
4 ENGINES RUNNING
GROUND IDLE4 ENGINES RUNNING
L_AC_060201_1_0010101_01_01
Airport and Community Noise DataGP 7200 Engines
6-2-1
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@A380 AIRPLANE CHARACTERISTICS
6-3-0 Danger Areas of the Engines
**ON A/C A380-800 Models A380-800F Models
Danger Areas of the Engines
1. Danger Areas of the Engines
6-3-0
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@A380 AIRPLANE CHARACTERISTICS
6-3-1 Danger Areas of the Engines - Ground Idle Power
**ON A/C A380-800 Models A380-800F Models
Danger Areas of the Engines - Ground Idle Power
1. This section gives danger areas of the engines at ground idle power conditions.
6-3-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
B
15 ft(4.6 m)
5 ft(1.5 m)
A
A
A
B
AREA A − INTAKE SUCTION DANGER AREA
AREA B − ENTRY CORRIDOR
AREA C − EXHAUST DANGER AREA (AFT OF EXHAUST NOZZLE)
277 ft (84 m) − GROUND IDLE (20 kt HEADWIND)
33°
P W V
E − 0 2 1 9 7 ( 0 2 0 7 )
C
C C
C
L_AC_060301_1_0020101_01_01
Danger Areas of the EnginesGround Idle Power - GP 7200 Engines
6-3-1
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@A380 AIRPLANE CHARACTERISTICS
6-3-2 Danger Areas of the Engines - Max. Take-Off Power
**ON A/C A380-800 Models A380-800F Models
Danger Areas of the Engines - Max. Take-Off Power
1. This section gives danger areas of the engines at max take-off power conditions.
6-3-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
d e h 0 0 0
1 5 1 5
INTAKE SUCTION DANGER AREA MAX TAKE−OFF POWER
EXHAUST DANGER AREA
8.9 m(29 ft)
30TO 548.6 m (1800 ft) AFT OF EXHAUST NOZZLES
L_AC_060302_1_0010101_01_00
Danger Areas of the EnginesMax Take-Off Power - TRENT 900 Engines
6-3-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
AREA B − ENTRY CORRIDOR
AREA C − EXHAUST DANGER AREA (AFT OF EXHAUST NOZZLE)
1553 ft (473 m) − MAXIMUM TAKEOFF (20 kt HEADWIND)
B
AREA A − INTAKE SUCTION DANGER AREA
A
C
A
B
C
41°
32 ft(9.8 m)
11 ft(3.4 m)
E − 0 2 1 9 9 ( 0 2 0 7 )
P W V
L_AC_060302_1_0020101_01_01
Danger Areas of the EnginesMax Take-Off Power - GP 7200 Engines
6-3-2
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@A380 AIRPLANE CHARACTERISTICS
6-3-3 Danger Areas of the Engines - Breakaway Power
**ON A/C A380-800 Models A380-800F Models
Danger Areas of the Engines - Breakaway Power
1. This section gives danger areas of the engines at breakaway power.
6-3-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
d e h 0 0 0
1 5 1 4
INTAKE SUCTION DANGER AREA BREAKAWAY POWER
EXHAUST DANGER AREA
6.0 m(20 ft)
4 ENGINE BREAKAWAY
30TO 123.4 m (405 ft) AFT OF EXHAUST NOZZLES
L_AC_060303_1_0010101_01_00
Danger Areas of the EnginesBreakaway Power - TRENT 900 Engines
6-3-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
B
C
AREA A − INTAKE SUCTION DANGER AREA
AREA B − ENTRY CORRIDOR
AREA C − EXHAUST DANGER AREA (AFT OF EXHAUST NOZZLE)
415 ft (126 m) − BREAKAWAY (20 kt HEADWIND)
B
A A
A
C
38°
P W V
E − 0 2 1
9 8 ( 0 2 0 7 )
20 ft(6.10 m)
6.5 ft(1.98 m)
L_AC_060303_1_0020101_01_01
Danger Areas of the EnginesBreakaway Power - GP 7200 Engines
6-3-3
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@A380 AIRPLANE CHARACTERISTICS
6-4-0 APU Exhaust Velocities and Temperatures
**ON A/C A380-800 Models A380-800F Models
APU Exhaust Velocities and Temperatures
1. APU Exhaust Velocities and Temperatures
6-4-0
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@A380 AIRPLANE CHARACTERISTICS
6-4-1 APU Exhaust Velocities and Temperatures
**ON A/C A380-800 Models A380-800F Models
APU Exhaust Velocities and Temperatures
1. This section gives APU exhaust velocities and temperatures in max. ECS conditions.
6-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
D
I S T A N C E F R O M A I R C R A F T C E N T E R L I N E
0 10 20 30 40 50 60 70 80 90 100
30
6
10
20
0
−10
−20
FEET
D I S T A N C E F R O M A I R C R A F T C E N T E R L I N E
DISTANCE DOWNSTREAM FROM NOZZLEMETERS
10
20
0
−10
−20
FEET
NOTE: THE DATA GIVEN IS BASED ON THE FOLLOWING ASSUMPTIONS:
−SEA LEVEL STATIC CONDITIONS−ISA + 23 °C (73 °F)−NO WIND
100
30
DISTANCE DOWNSTREAM FROM NOZZLEMETERS
0 3 6 9 12 15 18 21 24 27
3
0
−3
−6
0 80 90
0 3 6 9 12 15 18 21 24 27
3
6
0
−3
−6
574 °C (1065 °F)
260 °C (500 °F)
149 °C (300 °F)
316 °C (600 °F)
204 °C (400 °F)93 °C (200 °F)
10 20 30 40 50 60 70
46 m/s (150 ft/s)
27 m/s (90 ft/s)
68 m/s (223 ft/s)
37 m/s (120 ft/s)
18 m/s (60 ft/s)
9 m/s (30 ft/s)
L_AC_060401_1_0010101_01_00
APU Exhaust Velocities and TemperaturesMax. ECS Conditions
6-4-1
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@A380 AIRPLANE CHARACTERISTICS
6-4-2 APU Exhaust Velocities and Temperatures - MES Conditions
**ON A/C A380-800 Models A380-800F Models
APU Exhaust Velocities and Temperatures - MES Conditions
1. This section gives the APU exhaust velocities and temperatures in MES conditions.
6-4-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
L_AC_060402_0_AAM0_01_00
NOTE: THE DATA GIVEN IS BASED ON THE FOLLOWING ASSUMPTIONS:
−SEA LEVEL STATIC CONDITIONS−ISA + 23 °C (73 °F)−NO WIND
0 10 20 30 40 50 60 70 80 90 100
30
10
20
0
−10
−20
FEET
DISTANCE DOWNSTREAM FROM NOZZLEMETERS
10
20
0
−10
−20
FEET100
0 3 6 9 12 15 18 21 24 27 30
−6
D
I S T A N C E F R O M A I R C R A F T C E N T E R L I N E
DISTANCE DOWNSTREAM FROM NOZZLEMETERS
0 3 6 9 12 15 18 21 24 27
3
6
0
−3
−6
D I S T A N C E F R O M A I R C R
A F T C E N T E R L I N E
0 10 20 30 40 50 60 70 80 90
3
6
0
−3
458 °C (857 °F)
260 °C (500 °F)
149 °C (300 °F)
316 °C (600 °F)
204 °C (400 °F)
46 m/s (150 ft/s)
27 m/s (90 ft/s)
80 m/s (263 ft/s)
37 m/s (120 ft/s)
18 m/s (60 ft/s)
9 m/s (30 ft/s)
93 °C (200 °F)
L_AC_060402_1_0010101_01_00
APU Exhaust Velocities and TemperaturesMES Conditions
6-4-2
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@A380 AIRPLANE CHARACTERISTICS
PAVEMENT DATA
7-1-0 General Information
**ON A/C A380-800 Models A380-800F ModelsGeneral Information
1. A brief description of the pavement charts that follow will help in airport planning.
To help 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 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.
Section 7-2-0, gives basic data on the landing gear footprint configuration, maximum ramp weightsand tire sizes and pressures configuration.
Section 7-3-0, shows maximum vertical and horizontal pavement loads for certain critical conditionsat the tire-ground interfaces.
Section 7-4-0 contains charts to find these loads throughout the stability limit of the airplane at rest
on the pavement.
Section 7-4-2 gives examples of the distribution of the main landing load to the wing and bodylanding gears.
Section 7-4-3 shows the distribution of the main landing gear load to the wing and body gears.
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 to show flexible pavement design curves.The report was prepared by the U.S. Army Corps Engineer Waterways Experiment Station, Soil andPavement Laboratory, Vicksburg, Mississippi.
The line showing 10 000 coverages is used to calculate the Aircraft Classification Number (ACN).
7-1-0
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@A380 AIRPLANE CHARACTERISTICS
The procedure that follows is used to develop flexible pavement design curves such as those shown inSection 7-5-1.
A. With the scale for pavement thickness at the bottom and the scale for CBR at the top, an
arbitrary load line is drawn representing 10 000 coverages.
B. Incremental values of the weight on the main landing gear are then plotted.
C. Annual departure lines are drawn based on the load lines of the weight on the main landing gearthat is shown on the graph.
Section 7-7-1 gives the rigid pavement design curves that have been prepared with the use of the Westergaard Equation. This is in general accordance with the procedures outlined in thePortland Cement Association publications, ″ Design of Concrete Airport Pavement″ , 1973 and″ Computer Program for Airport Pavement Design″ , (Program PDILB), 1967 both by Robert G.Packard.
2. The procedure that follows is used to develop rigid pavement design curves such as those shown inSection 7-7-1
A. With the scale for pavement thickness on the left and the scale for allowable working stress onthe right, an arbitrary line load line is drawn. This represents the main landing gear maximumweight to be shown.
B. All values of the subgrade modulus (k values) are then plotted.
C. Additional load lines for the incremental values of weight on the main landing gear are drawn onthe basis of the curve for k = 80 MN/m3 already shown on the graph.
All Load Classification Number (LCN) curves shown in Section 7-6-1 and Section 7-8-2 havebeen developed from a computer program based on data provided in the International CivilAviation Organisation (ICAO) document 7920-AN/865/2, Aerodrome Manual, Part 2,″ Aerodrome Physical Characteristics″ , Second Edition, 1965.
The flexible pavement charts in Section 7-6-1 show LCN against equivalent single wheel load,and equivalent single wheel load against pavement thickness.
The rigid pavement charts in Section 7-8-2 show LCN against equivalent single wheel loadagainst radius of relative stiffness.
Section 7-9-0 provides ACN data prepared according to the ACN/PCN system as referenced inICAO Annex 14, ″ Aerodromes″ , Volume 1 ”Aerodrome Design and Operations” Fourth EditionJuly 2004, incorporating Amendments 1 to 6.
The ACN/PCN system provides a standardized international airplane/pavement rating systemreplacing the various S, T, TT, LCN, AUW, ISWL, etc., rating systems used throughout theworld.
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@A380 AIRPLANE CHARACTERISTICS
ACN is the Aircraft Classification Number and PCN is the corresponding PavementClassification Number.An aircraft having an ACN equal to or less than the PCN can operate without restriction on
the pavement.
Numerically the ACN is two times the derived single wheel load (expressed in thousands of kilograms).The derived single wheel load is defined as the load on a single tire inflated to 1.25 MPa (181psi) that would have the same pavement requirements as the aircraft.Computationally, the ACN/PCN system uses PCA program PDILB for rigid pavement andS-77-1 for 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:
PCN
PAVEMENT TYPE SUBGRADECATEGORY TIRE-PRESSURECATEGORY EVALUATIONMETHODR - Rigid A - HighLow W - No Limit T - Technical
F - Flexible B - Medium X - To 1.5 MPa(217 psi)
U - Using aircraft
C - Low Y - To 1 MPa(145 psi)
D - Ultra Low Z - To 0.5 MPa(73 psi)
Section 7-9-1 show the aircraft ACN values for flexible pavements. The four subgrade categoriesare :- 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 show the aircraft ACN for rigid pavements.
The four subgrade categories are :- A High Strength Subgrade k = 150 MN/m3 (550 pci)
- B Medium Strength Subgrade k = 80 MN/m3 (300 pci)- C Low Strength Subgrade k = 40 MN/m3 (150 pci)- D Ultra Low Strength Subgrade k = 20 MN/m3 ( 75 pci)
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@A380 AIRPLANE CHARACTERISTICS
7-2-0 Landing Gear Footprint
**ON A/C A380-800 Models
Landing Gear Footprint - Pax
1. This section gives the Landing Gear Footprint.
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070200_1_0030101_01_00
1 050 mm(41.3 in)
1 550 mm(61.0 in)
1 530 mm(60.2 in)
NOSE LANDINGGEAR
BODY LANDINGGEAR
1 350 mm
(53.1 in)
1 700 mm
(66.9 in)
(60.2 in)
1 530 mm
12 456 mm(40.87 ft)
28 606 mm (93.85 ft)
31 882 mm (104.6 ft)
5 264 mm(17.27 ft)
WING LANDINGGEAR
1 700 mm(66.9 in)
1 700 mm(66.9 in)
14 336 mm(47.03 ft)
7 344 mm(24.1 ft)
MAXIMUM RAMP WEIGHT
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
BODY GEAR TIRE SIZE
BODY GEAR TIRE PRESSURE
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE
512 000 kg (1 128 775 lb)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MRW 512 000 kg − A380−800 Models
1270 x 455R22 32PR or 50 x 20R22 34PR
14.1 bar (205 psi)
1400 x 530R23 40PR
14 bar (203 psi)
1400 x 530R23 40PR
14 bar (203 psi)
Landing Gear FootprintMRW 512 000 kg - A380-800 Models
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1 050 mm(41.3 in)
1 550 mm(61.0 in)
1 530 mm(60.2 in)
NOSE LANDINGGEAR
BODY LANDINGGEAR
1 350 mm(53.1 in)
1 700 mm
(66.9 in)
(60.2 in)
1 530 mm
12 456 mm(40.87 ft)
28 606 mm (93.85 ft)
31 882 mm (104.6 ft)
5 264 mm(17.27 ft)
WING LANDINGGEAR
1 700 mm(66.9 in)
1 700 mm(66.9 in)
14 336 mm(47.03 ft)
7 344 mm(24.1 ft)
MAXIMUM RAMP WEIGHT
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
BODY GEAR TIRE SIZE
BODY GEAR TIRE PRESSURE
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE
571 000 kg (1 258 850 lb)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MRW 571 000 kg − A380−800 Models
1270 x 455R22 32PR or 50 x 20R22 34PR
14.1 bar (205 psi)
1400 x 530R23 40PR
15 bar (218 psi)
1400 x 530R23 40PR
15 bar (218 psi)
L_AC_070200_1_0050101_01_00
Landing Gear FootprintMRW 571 000 kg - A380-800 Models
7-2-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Landing Gear Footprint - Freighter
1. This section gives the Landing Gear Footprint.
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
1 050 mm(41.3 in)
1 550 mm(61.0 in)
1 530 mm(60.2 in)
NOSE LANDINGGEAR
BODY LANDINGGEAR
1 350 mm(53.1 in)
1 800 mm
(70.9 in)
(60.2 in)
1 530 mm
12 456 mm(40.87 ft)
28 606 mm (93.85 ft)
31 882 mm (104.6 ft)
5 264 mm(17.27 ft)
WING LANDINGGEAR
1 700 mm(66.9 in)
1 700 mm(66.9 in)
14 336 mm(47.03 ft)
7 344 mm(24.1 ft)
MAXIMUM RAMP WEIGHT
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
BODY GEAR TIRE SIZE
BODY GEAR TIRE PRESSURE
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE
592 000 kg (1 305 125 lb)
See Section 7−4−1 Figure: Landing Gear Loading
on Pavement − MRW 592 000 kg − A380−800F Models
14.9 bar (216 psi)
1400 x 530R23 42PR
16.1 bar (234 psi)
1400 x 530R23 42PR
16.1 bar (234 psi)
50 x 20R22 34PR
L_AC_070200_1_0060101_01_00
Landing Gear FootprintMRW 592 000 kg - A380-800F Models
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
1 050 mm(41.3 in)
1 550 mm(61.0 in)
1 530 mm(60.2 in)
NOSE LANDINGGEAR
BODY LANDINGGEAR
1 350 mm(53.1 in)
1 800 mm
(70.9 in)
(60.2 in)
1 530 mm
12 456 mm(40.87 ft)
28 606 mm (93.85 ft)
31 882 mm (104.6 ft)
5 264 mm(17.27 ft)
WING LANDINGGEAR
1 700 mm(66.9 in)
1 700 mm(66.9 in)
14 336 mm(47.03 ft)
7 344 mm(24.1 ft)
MAXIMUM RAMP WEIGHT
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
BODY GEAR TIRE SIZE
BODY GEAR TIRE PRESSURE
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE
602 000 kg (1 327 175 lb)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MRW 602 000 kg − A380−800F Models
50 x 20R22 34PR
14.9 bar (216 psi)
1400 x 530R23 42PR
16.1 bar (234 psi)
1400 x 530R23 42PR
16.1 bar (234 psi)
L_AC_070200_1_0070101_01_00
Landing Gear FootprintMRW 602 000 kg - A380-800F Models
7-2-0
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@A380 AIRPLANE CHARACTERISTICS
7-3-0 Maximum Pavement Loads
**ON A/C A380-800 Models
Maximum Pavement Loads - Pax
1. This section gives Maximum Pavement Loads.
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070300_1_0050101_01_00
H
V
V
V
( N G )
( W G )
( B G )
V ( N G )
M A X I M
U M V E R T I C A L N O S E G E A R G R O U N D L O A D A T M O S T F O R W A R D C G
V ( W G )
M A X I M
U M V E R T I C A L W I N G G E A R G R O U N D L O
A D A T M O S T A F T C G
V ( B G )
M A X I M
U M V E R T I C A L B O D Y G E A R G R O U N D L O A D A T M O S T A F T C G
H
M A X I M
U M H O R I Z O N T A L G R O U N D L O A D F R O M
B R A K I N G
( 1 )
F W D C
G = 3 5 . 8 1 % M A C
( 2 )
A F T C G
= 4 3 % M A C
( 3 )
B R A K E
D W I N G G E A R
( 4 )
B R A K E
D B O D Y G E A R
N O T E : A L L L O
A D S C A L C U L A T E D U S I N G A I R P L A N E M A X I M U M R A M P W E I G H T
1
2
3
4
5
6
7
M O D E L
l b
k g
l b
k g
V N G
k g
l b
l b
k g
l b
k g
l b
k g
l b
k g
A T I N S T A N
T A N E O U S
B R A
K I N G
C O E F F I C I E N T = 0 . 8
V W G
( P E R S T R U T )
V B G
( P E R S
T U T )
H
( P E R S T R U T )
S T A T I C L O A D
A T M A X A F T
C G ( 2 )
S T A T I C
L O A D
A T M A X A F T
C G ( 2 )
M A X I M U M
R A M P
W E I G H T
− 8 0 0
S T A T I C L O A D
A T M O S T F W D
C G ( 1 )
1 1 2 8 7 7 5 5 1 2 0 0 0 8 7 7 0 0
3 9 7 7 0 1 4 7 4 2 5
6 6 8 8 0
2 1 4 7 5 0 9 7 4 1 0 3 2 2 1 2 5 1 4 6 1 1 0
7 0 1 7 5 ( 3 )
1 0 5 2 5 0 ( 4 )
3 1 8 3 0 ( 3 )
4 7 7 4 0 ( 4 )
1 7 1 8 0 0 ( 3 )
2 5 7 7 0 0 ( 4 )
7 7 9 3 0 ( 3 )
1 1 6 8 9 0 ( 4 )
2
S T A T I C B R A K I N G
D E
C E L E R A T I O N
S T A T I C B R A K I N G
@ 1
0 f t / s
D E C E L E R A T I O N
@
1 0 f t / s ²
Maximum Pavement LoadsMRW 512 000 kg - A380-800 Models
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
H
V
V
V
( N G )
( W G )
( B G )
( 1 )
( 2 )
( 3 )
( 4 )
B R A K E D
B O D Y G E A R
N O T E :
F W D C G
= 3 7 . 5 % M A C
A F T C G =
4 3 . 0 % M A C
B R A K E D
W I N G G E A R
A L L L O A D S C A L C U L A T E D U S I N G A I R P L A N E M A X
I M U M R A M P W E I G H T
L_AC_070300_0_AAM0_01_02
V V ( W G )
V ( B G )
H
M A X I M U M V E R T I C A L W I N G G E A R G R O U N D L O A D A T M O S T A F T C G
M A X I M U M H O R I Z O N T A L G R O U N D L O A D F R O M B
R A K I N G
1
2
3
4
5
6
7
M O D E L
l b
k g
− 8 0 0
l b
k g
V N G
k g
l b
l b
k g
l b
2
k g
l b
k g
l b
k g
2
A T I N S T A N
T A N E O U S
B R A K I N G
C O E F F I C I E N T = 0 . 8
V W G
( P E R S T R U T )
V B G
( P E R S
T U T )
H
( P E R S T R U T )
S T A T I C L O A D
A T M A X A F T
C G ( 2 )
S T A T I C
L O A D
A T M A X A F T
C G ( 2 )
M A X I M U M
R A M P
W E I G H T
S T A T I C L O A D
A T M O S T F W D
C G ( 1 )
( N G ) M A X I M U M V E R T I C A L N O S E G E A R G R O U N D L O A
D A T M O S T F O R W A R D C G
M A X I M U M V E R T I C A L B O D Y G E A R G R O U N D L O A
D A T M O S T A F T C G
1 2 3 9 0 0 0 5 6 2 0 0 0 8 7 8 2 5 3 9 8 4 0
1 5 3 4 0 0
6 9 5 9 0
2 3 5 7 2 5 1 0 6 9 2 0 3 5 3 5 7 5 1 6 0 3 8 0
7 7 0 2 5 ( 3 )
1 1 5 5 2 5 ( 4 )
3 4 9 4 0 ( 3 )
5 2 4 0 0 ( 4 )
1 8 8 5 7 5 ( 3 )
2 8 2 8 5 0 ( 4 )
8 5 5 4 0 ( 3 )
1 2 8 3 0 0 ( 4 )
S T A T I C B R A K I N G
@ 1
0 f t / s
D E
C E L E R A T I O N
S T A T I C B R A K I N G
@ 1
0 f t / s
D E C E L E R A T I O N
L_AC_070300_1_0010101_01_01
Maximum Pavement LoadsMRW 562 000 kg - A380-800 Models
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
H
V
V
V
( N G )
( W G )
( B G )
( 1 )
( 2 )
( 3 )
( 4 )
B R A K E D
B O D Y G E A R
N O T E :
F W D C G
= 3 7 . 8 % M A C
A F T C G =
4 1 . 0 % M A C
B R A K E D
W I N G G E A R
A L L L O A D S C A L C U L A T E D U S I N G A I R P L A N E M A X
I M U M R A M P W E I G H T
L_AC_070300_0_AAM0_01_02
V V ( W G )
V ( B G )
H
M A X I M U M V E R T I C A L W I N G G E A R G R O U N D L O A D A T M O S T A F T C G
M A X I M U M H O R I Z O N T A L G R O U N D L O A D F R O M B
R A K I N G
1
2
3
4
5
6
7
M O D E L
l b
k g
− 8 0 0
l b
k g
V N G
k g
l b
l b
k g
l b
2
k g
l b
k g
l b
k g
2
A T I N S T A N
T A N E O U S
B R A K I N G
C O E F F I C I E N T = 0 . 8
V W G
( P E R S T R U T )
V B G
( P E R S
T U T )
H
( P E R S T R U T )
S T A T I C L O A D
A T M A X A F T
C G ( 2 )
S T A T I C
L O A D
A T M A X A F T
C G ( 2 )
M A X I M U M
R A M P
W E I G H T
S T A T I C L O A D
A T M O S T F W D
C G ( 1 )
( N G ) M A X I M U M V E R T I C A L N O S E G E A R G R O U N D L O A
D A T M O S T F O R W A R D C G
M A X I M U M V E R T I C A L B O D Y G E A R G R O U N D L O A
D A T M O S T A F T C G
1 2 5 8 8 5 0 5 7 1 0 0 0 8 7 7 2 5 3 9 7 9 0
1 5 4 3 5 0
7 0 0 1 0
2 3 7 4 7 5 1 0 7 7 1 0 3 5 6 2 0 0 1 6 1 5 7 0
7 8 2 5 0 ( 3 )
1 1 7 3 7 5 ( 4 )
3 5 4 9 0 ( 3 )
5 3 2 4 0 ( 4 )
1 8 9 9 7 5 ( 3 )
2 8 4 9 5 0 ( 4 )
8 6 1 7 0 ( 3 )
1 2 9 2 6 0 ( 4 )
S T A T I C B R A K I N G
@ 1
0 f t / s
D E
C E L E R A T I O N
S T A T I C B R A K I N G
@ 1
0 f t / s
D E C E L E R A T I O N
L_AC_070300_1_0030101_01_00
Maximum Pavement LoadsMRW 571 000 kg - A380-800 Models
7-3-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Maximum Pavement Loads - Freighter
1. This section gives Maximum Pavement Loads.
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
H
V ( W G )
V ( B G )
H
M A X I M U M V E R T I C A L W I N G G E A R G R O U N D L O A D A T M O S T A F T C G
M A X I M U M H O R I Z O N T A L G R O U N D L O A D F R O M B
R A K I N G
( 1 )
( 2 )
( 3 )
( 4 )
B R A K E D
W I N G G E A R
B R A K E D
B O D Y G E A R
M A X I M U M V E R T I C A L B O D Y G E A R G R O U N D L O A
D A T M O S T A F T C G
N O T E :
A F T C G =
4 2 . 8 % M A C
F W D C G
= 3 6 . 0 % M A C
A L L L O A D S C A L C U L A T E D U S I N G A I R P L A N E M A X
I M U M R A M P W E I G H T
V
V
V
( N G )
( W G )
( B G )
V ( N G ) M A X I M U M V E R T I C A L N O S E G E A R G R O U N D L O A
D A T M O S T F O R W A R D C G
1
2
3
4
5
6
7
M O D E L
l b
k g
l b
k g
V N G
k g
l b
l b
k g
l b
2
k g
l b
k g
l b
k g
A T I N S T A N
T A N E O U S
B R A K I N G
C O E F F I C I E N T = 0 . 8
V W G
( P E R S T R U T )
V B G
( P E R S
T U T )
H
( P E R S T R U T )
S T A T I C L O A D
A T M A X A F T
C G ( 2 )
S T A T I C
L O A D
A T M A X A F T
C G ( 2 )
M A X I M U M
R A M P
W E I G H T
− 8 0 0
F
S T A T I C L O A D
A T M O S T F W D
C G ( 1 )
1 3 0 5 1 2 5 5 9 2 0 0 0 1 0 0 4 0 0 4 5 5 4 0
1 6 9 4 7 5
7 6 8 7 0
2 4 8 1 0 0 1 1 2 5 3 0 3 7 2 1 2 5 1 6 8 8 0 0
8 1 1 2 5 ( 3 )
1 2 1 7 0 0 ( 4 )
3 6 8 0 0 ( 3 )
5 5 2 0 0 ( 4 )
1 9 8 4 7 5 ( 3 )
2 9 7 7 0 0 ( 4 )
9 0 0 3 0 ( 3 )
1 3 5 0 4 0 ( 4 )
2
S T A T I C B R A K I N G
@ 1
0 f t / s
D E
C E L E R A T I O N
S T A T I C B R A K I N G
@ 1
0 f t / s
D E C E L E R A T I O N
L_AC_070300_1_0020101_01_01
Maximum Pavement Loads - FreighterMRW 592 000 kg - A380-800F Models
7-3-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
H
V ( W G )
V ( B G )
H
M A X I M U M V E R T I C A L W I N G G E A R G R O U N D L O A D A T M O S T A F T C G
M A X I M U M H O R I Z O N T A L G R O U N D L O A D F R O M B
R A K I N G
( 1 )
( 2 )
( 3 )
( 4 )
B R A K E D
W I N G G E A R
B R A K E D
B O D Y G E A R
M A X I M U M V E R T I C A L B O D Y G E A R G R O U N D L O A
D A T M O S T A F T C G
N O T E :
A F T C G =
4 2 . 7 % M A C
F W D C G
= 3 6 . 3 % M A C
A L L L O A D S C A L C U L A T E D U S I N G A I R P L A N E M A X
I M U M R A M P W E I G H T
V
V
V
( N G )
( W G )
( B G )
V ( N G ) M A X I M U M V E R T I C A L N O S E G E A R G R O U N D L O A
D A T M O S T F O R W A R D C G
1
2
3
4
5
6
7
M O D E L
l b
k g
l b
k g
V N G
k g
l b
l b
k g
l b
2
k g
l b
k g
l b
k g
A T I N S T A N
T A N E O U S
B R A K I N G
C O E F F I C I E N T = 0 . 8
V W G
( P E R S T R U T )
V B G
( P E R S
T U T )
H
( P E R S T R U T )
S T A T I C L O A D
A T M A X A F T
C G ( 2 )
S T A T I C
L O A D
A T M A X A F T
C G ( 2 )
M A X I M U M
R A M P
W E I G H T
− 8 0 0
F
S T A T I C L O A D
A T M O S T F W D
C G ( 1 )
1 3 2 7 1 7 5 6 0 2 0 0 0 1 0 0 4 7 5 4 5 5 8 0
1 7 0 7 2 5
7 7 4 4 0
2 5 2 1 7 5 1 1 4 3 8 0 3 7 8 2 5 0 1 7 1 5 8 0
8 2 5 0 0 ( 3 )
1 2 3 7 5 0 ( 4 )
3 7 4 2 0 ( 3 )
5 6 1 3 0 ( 4 )
2 0 1 7 5 0 ( 3 )
3 0 2 6 0 0 ( 4 )
9 1 5 1 0 ( 3 )
1 3 7 2 6 0 ( 4 )
2
S T A T I C B R A K I N G
@ 1
0 f t / s
D E
C E L E R A T I O N
S T A T I C B R A K I N G
@ 1
0 f t / s
D E C E L E R A T I O N
L_AC_070300_1_0040101_01_00
Maximum Pavement LoadsMRW 602 000 kg- A380-800F Models
7-3-0
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@A380 AIRPLANE CHARACTERISTICS
7-4-0 Landing Gear Loading on Pavement
**ON A/C A380-800 Models A380-800F Models
Landing Gear Loading on Pavement
1. GeneralThe Main Landing Gear Group consists of two Wing Gears (4 Wheel Bogies) plus two Body Gears (6Wheel Bogies).
- A380-800 models :
In the example shown in Section 7-4-1 with MRW 512000 kg, the Gross Aircraft Weight is450000 kg (992080 lb) and the percentage of weight on the Main Landing gear is 95.1 %.For these conditions the total weight on the Main Landing Gear Group is 428000 kg (943580 lb).
In the example shown in Section 7-4-1 with MRW 562000 kg, the Gross Aircraft Weight is450000 kg (992080 lb) and the percentage of weight on the Main Landing gear is 95.1 %.For these conditions the total weight on the Main Landing Gear Group is 428000 kg (943580 lb).
In the example shown in Section 7-4-1 with MRW 571000 kg, the Gross Aircraft Weight is450000 kg (992080 lb) and the percentage of weight on the Main Landing gear is 94.3 %.For these conditions the total weight on the Main Landing Gear Group is 424400 kg (935040 lb).
- A380-800F models :
In the example shown in Section 7-4-1 with MRW 592000 kg, the Gross Aircraft Weight is
450000 kg (992080 lb) and the percentage of weight on the Main Landing gear is 95.04 %.For these conditions the total weight on the MLG Group is 427700 (942920 lb).
In the example shown in Section 7-4-1 with MRW 602000 kg, the Gross Aircraft Weight is450000 kg (992080 lb) and the percentage of weight on the Main Landing gear is 95 %.For these conditions the total weight on the MLG Group is 427500 (942475 lb).
7-4-0
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@A380 AIRPLANE CHARACTERISTICS
7-4-1 Landing Gear Loading on Pavement
**ON A/C A380-800 Models
Landing Gear Loading on Pavement - Pax
1. This section gives Landing Gear Loading on Pavement.
7-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
5450464238343026
260
280
300
320
340
360
380
400
440
460
480
500
520
540
88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
W E I G H T O N M A I N L A N D I N G G E A R G R O U P −
x 1 0 0 0 k g
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
PERCENTAGE MAC
A I R C R A F T G R O S S W E I G H T − x 1 0 0 0 k g
420
CG FOR ACNCALCULATIONS
MTOW = 510 000 kg
MLW = 394 000 kg
MZFW = 372 000 kg
TAKE OFF &LANDING
TAKE OFF
LANDING
95.1 % WEIGHTON MLG GROUP
L_AC_070401_1_0050101_01_00
Landing Gear Loading on PavementMRW 512 000 kg - A380-800 Models
7-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
5450464238343026
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
W E I G H T O N M A I N L A N D I N G G E A R G R O U P − x 1 0 0 0 k g
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
PERCENTAGE MAC
A I R C R A F T G R O S S W E I G H T − x 1 0 0
0 k g
MTOW = 560 000 kg
CG FOR ACNCALCULATIONS
MLW = 386 000 kg
LANDING
95.1 % WEIGHTON MLG GROUP
TAKE OFF
TAKE OFF &LANDING
MZFW = 361 000 kg
L_AC_070401_1_0060101_01_00
Landing Gear Loading on PavementMRW 562 000 kg - A380-800 Models
7-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070401_1_0070101_01_00
5450464238343026
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
W E I G H T O N M A I N L A N D I N G G E A R G R O U P
− x 1 0 0 0 k g
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
PERCENTAGE MAC
A I R C R A F T G R O S S W E I G H T − x 1 0 0 0 k g
MLW = 391 000 kg
MZFW = 366 000 kg
MTOW = 569 000 kg
CG FOR ACNCALCULATIONS
TAKE OFF &LANDING
TAKE OFF
LANDING
94.3 % WEIGHTON MLG GROUP
Landing Gear Loading on PavementMRW 571 000 kg - A380-800 Models
7-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Landing Gear Loading on Pavement - Freighter
1. This section gives Landing Gear Loading on Pavement.
7-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070401_1_0080101_01_00
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
600
88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
W
E I G H T O N M A I N L A N D I N G G E A R G R O U
P − x 1 0 0 0 k g
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
600
A I R C R A F T G R O S S W E I G H T − x 1 0 0 0 k g
5450464238343026
PERCENTAGE MAC
CG FOR ACNCALCULATIONS
MTOW = 590 000 kg
MLW = 427 000 kg
MZFW = 402 000 kg
TAKE OFF &LANDING
TAKE OFF
LANDING
95.04 % WEIGHTON MLG GROUP
Landing Gear Loading on PavementMRW 592 000kg - A380-800F Models
7-4-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070401_1_0090101_01_00
5450464238343026
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
600
88 90 92 94 96 98 100
PERCENTAGE OF WEIGHT ON MAIN GEAR GROUP
W
E I G H T O N M A I N L A N D I N G G E A R G R O U
P − x 1 0 0 0 k g
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
600
PERCENTAGE MAC
A I R C R A F T G R O S S W E I G H T − x 1 0 0 0 k g
CG FOR ACNCALCULATIONS
MTOW = 600 000 kg
MLW = 427 000 kg
MZFW = 379 000 kg
TAKE OFF &LANDING
TAKE OFF
LANDING
95 % WEIGHTON MLG GROUP
Landing Gear Loading on PavementMRW 602 000kg - A380-800F Models
7-4-1
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@A380 AIRPLANE CHARACTERISTICS
7-4-2 Wing Gear and Body Gear Loading on Pavement
**ON A/C A380-800 Models A380-800F Models
Wing Gear and Body Gear Loading on Pavement
1. General
The Main Landing Gear Group consists of two Wing Gears (4 Wheel Bogies) and two Body Gears (6Wheel Bogies).
- A380-800 models :
In the example shown in Section 7-4-3 with MRW 512000 kg, the Gross Aircraft Weight is 450000 kg(992080 lb) at Aft CG for ACN Calculations (see Section 7-4-1, Page 1)For these conditions the load on the two Wing Gears is 171200 kg (377430 lb) and the load on the
two Body Gears is 256800 kg (566150 lb).The total weight on the Main Landing Gear Group is 428000 kg (943580 lb).
In the example shown in Section 7-4-3 with MRW 562000 kg, the Gross Aircraft Weight is 450000 kg(992080 lb) at Aft CG for ACN Calculations (see Section 7-4-1, Page 1)For these conditions the load on the two Wing Gears is 171200 kg (377430 lb) and the load on thetwo Body Gears is 256800 kg (566150 lb).The total weight on the Main Landing Gear Group is 428000 kg (943580 lb).
In the example shown in Section 7-4-3 with MRW 571000 kg, the Gross Aircraft Weight is 450000 kg(992080 lb) at Aft CG for ACN Calculations (see Section 7-4-1, Page 2)
For these conditions the load on the two Wing Gears is 169800 kg (374345 lb) and the load on thetwo Body Gears is 254700 kg (561515 lb).The total weight on the Main Landing Gear Group is 424500 kg (935860 lb).
- A380-800F models :
In the example shown in Section 7-4-3 with MRW 592000 kg, the Gross Aircraft Weight is 450000 kg(992080 lb) at Aft CG for ACN Calculations (see Section 7-4-1, Page 3)For these conditions the load on the two Wing Gears is 171100 kg (377210 lb) and the load on thetwo Body Gears is 256600 kg (565710 lb).The total weight on the Main Landing Gear Group is 427700 kg (942920 lb).
In the example shown in Section 7-4-3 with MRW 602000 kg, the Gross Aircraft Weight is 450000 kg(992080 lb) at Aft CG for ACN Calculations (see Section 7-4-1, Page 4)For these conditions the load on the two Wing Gears is 171000 kg (376990 lb) and the load on thetwo Body Gears is 256500 kg (565485 lb).The total weight on the Main Landing Gear Group is 427500 kg (942475 lb).
7-4-2
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@A380 AIRPLANE CHARACTERISTICS
7-4-3 Wing Gear and Body Gear Loading on Pavement
**ON A/C A380-800 Models
Wing Gear and Body Gear Loading on Pavement - Pax
1. This section gives the Wing Gear and Body Gear Loading on Pavement.
7-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070403_1_0050101_01_00
1 0 0
1 2 0
1 4 0
1 6 0
1 8 0
2 0 0
2 2 0
2 4 0
2 6 0
2 8 0
3 0 0
3 2 0
3 4 0 2
6 0
2 8 0
3 0 0 3
2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8
0
6 0 0
L O A D O N B O D Y G E A R S O R L O A D O N W I N G G E A R S
C G F O R
A C N C A L C U L A T I O N S : 4 3 % M A C .
S e e S e c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m
e n t − M R W 5 1 2 0 0 0 k g − A 3 8 0 − 8 0 0 M o d e l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 k g ]
7 0 0
6 0 0
5 0 0
4 0 0
3 0 0
[ x 1 0 0 0 l b ]
W I N G G E A R S
B
O D Y
G E A R S
A I R C R A F T G R O S S W E I G H T
6 0 0
7 0 0
8 0 0
9 0 0
1 0 0 0
1 1 0 0
1 2 0 0
1 3 0 0
[ x 1 0 0 0 l b ]
Wing Gear and Body Gear Loads on PavementMRW 512 000 kg - A380-800 Models
7-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070403_1_0060101_01_00
1 0 0
1 2 0
1 4 0
1 6 0
1 8 0
2 0 0
2 2 0
2 4 0
2 6 0
2 8 0
3 0 0
3 2 0
3 4 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0 5 8 0
6 0 0
A I R C R A F T G R O S S W E I G H T
L O A D O N B O D Y G E A R S O R L O A D O N W I N G G E A R S
C G F O R
A C N C A L C U L A T I O N S : 4 3 % M A C .
S e e S e c
t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e n t − M R W 5 6 2 0 0 0 k g − A 3 8 0 − 8 0 0 M o d
e l s
6 0 0
7
0 0
8 0 0
9 0 0
1
0 0 0
1 1 0 0
1 2 0 0
1 3 0 0
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
[ x 1 0 0 0 k g ]
7 0 0
6 0 0
5 0 0
4 0 0
3 0 0
[ x 1 0 0 0 l b ]
W I N G G E A R S
B O D Y G E A R S
Wing Gear and Body Gear Loads on PavementMRW 562 000 kg - A380-800 Models
7-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070403_1_0070101_01_00
1 0 0
1 2 0
1 4 0
1 6 0
1 8 0
2 0 0
2 2 0
2 4 0
2 6 0
2 8 0
3 0 0
3 2 0
3 4 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E I G
H T
L O A D O N B O D Y G E A R S O R L O A D O N W I N G G E A R S
C G F O R A C N C A L C U L A T I O N S : 4 1 % M A C .
S e e S
e c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n
g
o n P a
v e m e n t − M R W
5 7 1 0 0 0 k g − A 3 8 0 − 8 0 0 M
o d e l s
6 0 0
7 0 0
8 0 0
9 0 0
1 0
0 0
1 1 0 0
1 2 0 0
1 3 0 0
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
[ x 1 0 0 0 k g ]
7 0 0
6 0 0
5 0 0
4 0 0
3 0 0
[ x 1 0 0 0 l b ]
B
O D Y
G E A R S
W I N G G E A R S
Wing Gear and Body Gear Loads on PavementMRW 571 000 kg - A380-800 Models
7-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Wing Gear and Body Gear Loading on Pavement - Freighter
1. This section gives the Wing Gear and Body Gear Loading on Pavement.
7-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070403_1_0080101_01_00
1 0 0
1 2 0
1 4 0
1 6 0
1 8 0
2 0 0
2 2 0
2 4 0
2 6 0
2 8 0
3 0 0
3 2 0
3 4 0 2
6 0
2 8 0
3 0 0 3
2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8
0
6 0 0
A I R C R A F T G R O S S W E I G H T
L O A D O N B O D Y G E A R S O R L O A D O N W I N G G E A R S
C G F O R A C N C A L C U L A T I O N S : 4 2 . 8 % M A C .
S e e S e
c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e n t − M R W
5 9 2 0 0 0 k g − A 3 8 0 − 8 0 0 F M
o d e l s
6 0 0
7 0 0
8 0 0
9 0 0
1 0 0 0
1 1 0 0
1 2 0 0
1 3 0 0
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
[ x 1 0 0 0 k g ]
7 0 0
6 0 0
5 0 0
4 0 0
3 0 0
[ x 1 0 0 0 l b ]
W I N G G E A R S
B O D Y
G E A R S
Wing Gear and Body Gear Loads on PavementMRW 592 000 kg - A380-800F Models
7-4-3
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070403_1_0090101_01_00
1 0 0
1 2 0
1 4 0
1 6 0
1 8 0
2 0 0
2 2 0
2 4 0
2 6 0
2 8 0
3 0 0
3 2 0
3 4 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E
I G H T
L O A D O N B O D Y G E A R S O R L O A D O N W I N G G E A R S
C G F O R
A C N C A L C U L A T I O N S : 4 2 . 7 % M A C .
S e e S e c
t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e n t − M R W 6 0 2 0 0 0 k g − A 3 8 0 − 8 0 0 F M o
d e l s
6 0 0
7 0 0
8 0 0
9 0 0
1 0 0 0
1 1 0 0
1 2 0 0
1 3 0 0
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
[ x 1 0 0 0 k g ]
7 0 0
6 0 0
5 0 0
4 0 0
3 0 0
[ x 1 0 0 0 l b ]
B O D Y G E A R S
W I N G G E A R S
Wing Gear and Body Gear Loads on PavementMRW 602 000 kg - A380-800F Models
7-4-3
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@A380 AIRPLANE CHARACTERISTICS
7-5-0 Flexible Pavement Requirements - US Army Corps of Engineers Design Method
**ON A/C A380-800 Models A380-800F Models
Flexible Pavement Requirements - US Army Corps of Engineers Design Method
1. General
To find a Flexible Pavement Thickness, the Subgrade Strength (CBR), the Annual Departure Leveland the weight on one Main Landing Gear must be known.
In the example shown in Section 7-5-1 with MRW 512000 kg, for:- a CBR value of 10- an Annual Departure level of 3 000- and the load on one Wing Landing Gear of 90000 kg (198420 lb) the required Flexible Pavement
Thickness is 54 cm (21 inches).
The line showing 10 000 Coverages is used to calculate Aircraft Classification Number (ACN).
7-5-0
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@A380 AIRPLANE CHARACTERISTICS
7-5-1 Flexible Pavement Requirements - US Army Corps of Engineers Design Method S-77-1
**ON A/C A380-800 Models
Flexible Pavement Requirements - US Army Corps of Engineers Design Method - Pax
1. This section gives Flexible Pavement Requirements.
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070501_1_0090101_01_00
30 40 6020151063
6
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT AT 14 BAR (203 PSI)
8050
3 10 15 20 30 40 50 60 80
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
WEIGHT ON ONE WING LANDING GEAR97 410 kg (214 750 lb)
10 000 COVERAGES USEDFOR ACN CALCULATIONS
MAXIMUM POSSIBLE WINGGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ANNUALDEPARTURES*1 2003 0006 00015 00025 000
*20 YEARPAVEMENT LIFE
ALPHA FACTOR = 0.8
Flexible Pavement Requirements -- 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070501_1_0100101_01_00
6
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 50 60 80
30 40 6020151063
[INCHES]
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT AT 14 BAR (203 PSI)
8050
MAXIMUM POSSIBLE WINGGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
10 000 COVERAGES USEDFOR ACN CALCULATIONS
ANNUALDEPARTURES*1 2003 0006 00025 000*20 YEARPAVEMENT LIFE
146 110 kg (322 125 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)120 000 kg (264 550 lb)
WEIGHT ON ONE BODY LANDING GEAR
Flexible Pavement Requirements -- 6 Wheel BogieMRW 512 000 kg - A380-800 Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
6
SUBGRADE STRENGTH − CBR
3 10 15 20 30 40 50 60 80
30 40 6020151063
[INCHES]
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
8050
MAXIMUM POSSIBLE WINGGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ALPHA FACTOR = 0.8
10 000 COVERAGES USEDFOR ACN CALCULATIONS
ANNUALDEPARTURES*1 2003 0006 000
15 00025 000*20 YEARPAVEMENT LIFE
WEIGHT ON ONE WING LANDING GEAR
100 000 kg (220 460 lb)90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
106 920 kg (235 725 lb)
L_AC_070501_1_0110101_01_00
Flexible Pavement Requirements -- 4 Wheel BogieMRW 562 000 kg - A380-800 Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
30 40 6020151063
3 106 15 20 30
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
80
60 8040 50
50
10 000 COVERAGES USEDFOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR160 380 kg (353 575 lb)150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)120 000 kg (264 550 lb)
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ANNUALDEPARTURES*1 2003 0006 00025 000
*20 YEARPAVEMENT LIFE
L_AC_070501_1_0020101_01_01
Flexible Pavement Requirements -- 6 Wheel BogieMRW 562 000 kg - A380-800 Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
30 4020151063
3 106 15 20 30
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.1 BAR (234 PSI)
60 80
60 8040 50
50
10 000 COVERAGES USEDFOR ACN CALCULATIONS
WEIGHT ON ONE WING LANDING GEAR112 530 kg (248 100 lb)100 000 kg (220 460 lb)
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
MAXIMUM POSSIBLE WINGGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ANNUALDEPARTURES*1 2003 0006 00015 00025 000
*20 YEARPAVEMENT LIFE
L_AC_070501_1_0120101_01_00
Flexible Pavement Requirements -- 4 Wheel BogieMRW 571 000 kg - A380-800 Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
30 4020151063
3 106 15 20 30 40
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
60 80
60 8050
50
10 000 COVERAGES USEDFOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR161 570 kg (356 200 lb)150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)120 000 kg (264 550 lb)
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ANNUALDEPARTURES*1 2003 0006 00025 000
*20 YEARPAVEMENT LIFE
L_AC_070501_1_0060101_01_00
Flexible Pavement Requirements -- 6 Wheel BogieMRW 571 000 kg - A380-800 Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Flexible Pavement Requirements - US Army Corps of Engineers Design Method - Freighter
1. This section gives Flexible Pavement Requirements.
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
30 40 6020151063
3 106 15 20 30 40 60
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.1 BAR (234 PSI)
80
8050
50
10 000 COVERAGES USEDFOR ACN CALCULATIONS
WEIGHT ON ONE WING LANDING GEAR114 380 kg (252 175 lb)100 000 kg (220 460 lb)
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
MAXIMUM POSSIBLE WINGGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ANNUALDEPARTURES*1 2003 0006 00015 000
25 000*20 YEARPAVEMENT LIFE
L_AC_070501_1_0130101_01_00
Flexible Pavement Requirements -- 4 Wheel BogieMRW 592 000 kg - A380-800F Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
3 6 10 15 20 4030
60403020156 103
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.1 BAR (234 PSI)
60 80
8050
50
10 000 COVERAGES USEDFOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR168 800 kg (372 125 lb)150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)120 000 kg (264 550 lb)
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ANNUALDEPARTURES*1 2003 0006 00025 000*20 YEAR
PAVEMENT LIFE
L_AC_070501_1_0040101_01_01
Flexible Pavement Requirements -- 6 Wheel BogieMRW 592 000 kg - A380-800F Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
30 40 6020151063
3 106 15 20 30
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
80
60 8040 50
50
10 000 COVERAGES USEDFOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR160 380 kg (353 575 lb)150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)120 000 kg (264 550 lb)
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
ANNUALDEPARTURES*1 2003 0006 00025 000
*20 YEARPAVEMENT LIFE
L_AC_070501_1_0140101_01_00
Flexible Pavement Requirements -- 4 Wheel BogieMRW 602 000 kg - A380-800F Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
3020151063
3 106 15 20 30 40 60
[INCHES]
SUBGRADE STRENGTH − CBR
10 15 20 30 40 60 80 100 120 150 180
[CENTIMETERS]
FLEXIBLE PAVEMENT THICKNESS
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT AT 16.1 BAR (234 PSI)
60 80
80
40
50
50
10 000 COVERAGES USEDFOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR171 580 kg (378 250 lb)150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)120 000 kg (264 550 lb)
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
PAVEMENT LIFE
ANNUALDEPARTURES*1 2003 0006 00025 000*20 YEAR
L_AC_070501_1_0080101_01_00
Flexible Pavement Requirements -- 6 Wheel BogieMRW 602 000 kg - A380-800F Models
7-5-1
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@A380 AIRPLANE CHARACTERISTICS
7-6-0 Flexible Pavement Requirements - LCN Conversion
**ON A/C A380-800 Models A380-800F Models
General
1. To find the airplane weight that a Flexible Pavement can support, the LCN of the pavement and thethickness (h) must be known.
In the typical example shown in Section 7-6-1 with MRW 512000 kg, the thickness (h) is shown at508 mm (20 in.) with an LCN of 82. For these conditions the weight on one Wing Landing Gear is90000 kg (198420 lb).
7-6-0
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@A380 AIRPLANE CHARACTERISTICS
7-6-1 Flexible Pavement Requirements - LCN Conversion
**ON A/C A380-800 Models
Flexible Pavement Requirements - LCN Conversion - Pax
1. This section gives Flexible Pavement Requirements - LCN Conversion.
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070601_1_0090101_01_00
F L E X I B L E P A V E M E N T T H I C
K N E S S ( I N C H E S )
1 8 0
1 2 0
1 5 0
6 0
7
0
8 0
9 0
1 0 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5
2 0
2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A
L E N T S I N G L E W H E E L L O A D S A R E D E R
I V E D B Y M E T H O D S S H O W N I N
I C A O
A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1
. 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P
R E S S U R E C O N S T A N T A T 1 4 b a r ( 2 0 3 p s
i )
F L E X I B L E P A V E M E N T T H I C K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
1 0
2 0
3 0
8 0
7 0
6 0
5 0
4 0
1 0
2 0
3 0
4 0
5 0
6 0 7
0 8 0
9 0
1 0 0
1 1 0
1 2 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
W E I G H T O N O N E W I N G
L A N
D I N G G E A R
9 7
4 1 0 k g
( 2 1 4 7 5 0 l b )
9 0
0 0 0 k g
( 1 9 8 4 2 0 l b )
8 0
0 0 0 k g
( 1 7 6 3 7 0 l b )
7 0
0 0 0 k g
( 1 5 4 3 2 5 l b )
6 0
0 0 0 k g
( 1 3 2 2 7 5 l b )
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070601_1_0100101_01_00
1 0
2 0
3 0
4 0
5 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K
N E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
5 1 0
1 5
2 0
2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T
S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M E T H O D S S H O W N I N
I C A O A E R O
D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3 S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R
E S S U R E C O N S T A N T A T 1 4 . 0 b a r ( 2 0 3 p s i )
F L E X I B L E P A V E M E N T T H I C K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
1 8 0
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
W E I G
H T O N O N E B O D Y
L A N D
I N G G E A R
1 4 6
1 1 0 k g
( 3 2 2 1 2 5 l b )
1 4 0
0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0
0 0 0 k g
( 2 8 6 6 0 0 l b )
1 2 0
0 0 0 k g
( 2 6 4 5 5 0 l b )
1 1 0
0 0 0 k g
( 2 4 2 5 0 0 l b )
M A X I M U M P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 512 000 kg - A380-800 Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1 0
2 0
3 0
4 0
5 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N E S S ( I N C H E S )
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 8 0
1 4 0
1 2 0 1 3 0
1 5 0
1 1 0
6 0
7 0
8 0
9 0
1 0 0
L O
A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y
M E T H O D S S H O W N I N
I C A O A E
R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P
R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
F L E X I B L E P A V E M E N T T H I C
K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
W E I G H T O N O N E W I N G
L
A N D I N G G E A R
1 0 6 9 2 0 k g
( 2 3 5 7 2 0 l b )
1 0 0 0 0 0 k g
( 2 2 0 4 6 0 l b )
9 0 0 0 0 k g
( 1 9 8 4 2 0 l b )
8 0 0 0 0 k g
( 1 7 6 3 7 0 l b )
7 0 0 0 0 k g
( 1 5 4 3 2 5 l b )
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
L_AC_070601_1_0010101_01_01
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 562 000 kg - A380-800 Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1 0
2 0
3 0
4 0
5 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 8
0
1 4 0
1 2 0 1 3 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5
2 0
2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B
Y M E T H O D S S H O W N I N
I C A O
A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 5 . 0 b a r ( 2 1 8 p s i )
F L E X I B L E P A V E M E N T T H I C
K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
W E
I G H T O N O N E B O D Y
L A N D I N G G E A R
1 6 0 3 8 0 k g
( 3 5 3 5 7 5 l b )
1 5 0 0 0 0 k g
( 3 3 0 7 0 0 l b )
1 4 0 0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0 0 0 0 k g
( 2 8 6 6 0 0 l b )
1 2 0 0 0 0 k g
( 2 6 4 5 5 0 l b )
M A X I M U M P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
L_AC_070601_1_0020101_01_01
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 562 000 kg - A380-800 Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1 0
2 0
3 0
4 0
5 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 8 0
1 4 0
1 2 0 1 3 0
1 5 0
1 1 0
6 0
7 0
8 0
9 0
1 0 0
L
O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5
2 0
2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M E T H O D S S H O W N I N
I C A O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c
o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
F L E X I B L E P A V E M E N T T H
I C K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3
W E
I G H T O N O N E W I N G
L A N D I N G G E A R
1 0 7 7
1 0 k g
( 2 3 7 4 7 5 l b )
1 0 0 0
0 0 k g
( 2 2 0 4 6 0 l b )
9 0 0
0 0 k g
( 1 9 8 4 2 0 l b )
8 0 0
0 0 k g
( 1 7 6 3 7 0 l b )
7 0 0
0 0 k g
( 1 5 4 3 2 5 l b )
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
L_AC_070601_1_0050101_01_00
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 571 000 kg - A380-800 Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1 0
2 0
3 0
4 0
5 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N E
S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 8 0
1 4 0
1 2 0 1 3 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M
E T H O D S S H O W N I N
I C A O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P
R E S S U R E C O N S T A N T A T 1 5 . 0 b a r ( 2 1 8 p s i )
F L E X I B L E P A V E M E N T T H I C
K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
W E I G
H T O N O N E B O D Y
L A
N D I N G G E A R
1 6 1 5 7 0
k g
( 3 5 6 2 0 0 l b )
1 5 0 0 0 0 k g
( 3 3 0 7 0 0 l b )
1 4 0 0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0 0 0 0 k g
( 2 8 6 6 0 0 l b )
1 2 0 0 0 0 k g
( 2 6 4 5 5 0 l b )
M A X I M U M P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
L_AC_070601_1_0060101_01_00
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 571 000 kg - A380-800 Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
For A380-800F ModelsFlexible Pavement Requirements - LCN Conversion - Freighter
1. This section gives Flexible Pavement Requirements - LCN Conversion.
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6 0
7 0
8 0
5 0
4 0
3 0
2 0
1 0
1 0 2
0 3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 8
0
1 4 0
1 2 0 1 3 0
1 5 0
1 1 0
6 0
7 0
8 0
9 0
1 0 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E
N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M
E T H O D S S H O W N I N
I C A O A E R
O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d
E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
F L E X I B L E P A V E M E N T T H I C K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
W E I
G H T O N O N E W I N G
L A N D I N G G E A R
1 1 2 5 3 0 k g
( 2 4 8 1 0 0 l b )
1 0 0 0 0 0 k g
( 2 2 0 4 6 0 l b )
9 0 0 0 0 k g
( 1 9 8 4 2 0 l b )
8 0 0 0 0 k g
( 1 7 6 3 7 0 l b )
7 0 0 0 0 k g
( 1 5 4 3 2 5 l b )
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
L_AC_070601_1_0030101_01_01
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 592 000 kg - A380-800F Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6 0
7 0
8 0
5 0
4 0
3 0
2 0
1 0
1 0 2
0 3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 8 0
1 4 0
1 2 0 1 3 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
L O A
D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M E
T H O D S S H O W N I N
I C A O A E R O
D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E
d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R
E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
F L E X I B I L E P A V E M E N T T H I C K
N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
W E I G H
T O N O N E B O D Y
L A N D I N G G E A R
1 6 8 8 0 0
k g
( 3 7 2 1 2 5 l b )
1 6 0 0 0 0
k g
( 3 5 2 7 5 0 l b )
1 5 0 0 0 0
k g
( 3 3 0 7 0 0 l b )
1 4 0 0 0 0
k g
( 3 0 8 6 5 0 l b )
1 3 0 0 0 0
k g
( 2 8 6 6 0 0 l b )
M A X I M U M P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
L_AC_070601_1_0040101_01_01
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 592 000 kg - A380-800F Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6 0
7 0
8 0
5 0
4 0
3 0
2 0
1 0
1 0 2
0 3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N E S S [ I N C H E S ]
1 8 0
1 4 0
1 2 0 1 3 0
1 5 0
1 1 0
6 0
7 0
8 0
9 0
1 0 0
L
O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5
2 0
2 5
3 0
3 5
4 0
4 5
5 0
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y
M E T H O D S S H O W N I N
I C A O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o
n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
F L E X I B L E P A V E M E N T T H I C K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G H T O N O N E W I N G
L A N D I N G G E A R
1 1 4 3 8 0 k g
( 2 5 2 1 7 5 l b )
1 0 0 0
0 0 k g
( 2 2 0 4 6 0 l b )
9 0 0
0 0 k g
( 1 9 8 4 2 0 l b )
8 0 0
0 0 k g
( 1 7 6 3 7 0 l b )
7 0 0
0 0 k g
( 1 5 4 3 2 5 l b )
L_AC_070601_1_0070101_01_00
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 602 000 kg - A380-800F Models
7-6-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6 0
7 0
8 0
5 0
4 0
3 0
2 0
1 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
F L E X I B L E P A V E M E N T T H I C K N
E S S [ I N C H E S ]
1 8
0
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
N O T E : E Q U I V A L E
N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M
E T H O D S S H O W N I N
I C A O A E
R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n
d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E
P R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
F L E X I B L E P A V E M E N T T H I C
K N E S S ( m m )
2 5 4
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
M A X I M U M P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G H T O N O N E B O D Y
L
A N D I N G G E A R
1 7 1 5 8
0 k g
( 3 7 8 2 5 0 l b )
1 6 0 0 0 0 k g
( 3 5 2 7 5 0 l b )
1 5 0 0 0 0 k g
( 3 3 0 7 0 0 l b )
1 4 0 0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0 0 0 0 k g
( 2 8 6 6 0 0 l b )
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
L_AC_070601_1_0080101_01_00
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 602 000 kg - A380-800F Models
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@A380 AIRPLANE CHARACTERISTICS
7-7-0 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A380-800 Models A380-800F Models
Rigid Pavement Requirements - Portland Cement Association Design Method
1. General
To determine a Rigid Pavement Thickness, the Subgrade Modulus (k), the allowable working stressand the weight on one Main Landing Gear must be known.
In the typical example shown in Section 7-7-1 with MRW 512000 kg, for:- a k value of 150 MN/m3 (550 lb/in3)- an allowable working stress of 36 kg/cm2 (500 lb/in2)- the load on one Wing Landing Gear of 90000 kg (198420 lb), the required Rigid Pavement
Thickness is 24 cm (9.5 inches).
7-7-0
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@A380 AIRPLANE CHARACTERISTICS
7-7-1 Rigid Pavement Requirements - Portland Cement Association Design Method
**ON A/C A380-800 Models
Rigid Pavement Requirements - Portland Cement Association Design Method - Pax
1. This section gives Rigid Pavement Requirements.
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070701_1_0090101_01_00
8
9
10
11
12
13
14
15
16
[ i n c h e s ]
200
300
400
500
600
700
800
900
1000
[ l b / i n ² ]
15
20
25
30
35
40
45
50
55
60
65
70
[ k g / c m ² ]
A L L O W A B L E W O R K I N G
S T R E S S
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT = 14 BAR (203 PSI)
NOTES:THE VALUES OBTAINED BYUSING THE MAXIMUM LOADREFERENCE LINE AND ANYVALUES FOR K ARE EXACT. FORLOADS LESS THAN MAXIMUM,THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATESLIGHTLY FOR ANY OTHERVALUES OF K
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C
K N E S S
[ C E N T I M E T E R S ]
REFERENCE:"DESIGN OF CONCRETEAIRPORT PAVEMENTS" AND"COMPUTER PROGRAM FORAIRPORT PAVEMENT DESIGN −PROGRAM PDILB" PORTLANDCEMENT ASSOCIATION
MAXIMUM POSSIBLE WING
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
WEIGHT ON ONE WING LANDING GEAR
97 410 kg (214 750 lb)
90 000 kg (198 420 lb)
80 000 kg (176 370 lb)
70 000 kg (154 325 lb)
k = 20 MN/m³
k = 40 MN/m³
k = 80 MN/m³
k = 150 MN/m³
Rigid Pavement Requirements - 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070701_1_0100101_01_00
8
9
10
11
12
13
14
15
16
[ i n c h e s ]
200
300
400
500
600
700
800
900
1000
[ l b / i n ² ]
15
20
25
30
35
40
45
50
55
60
65
70
[ k g / c m ² ]
A L L O W A B L E W O R K I N G
S T R E S S
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT = 14 BAR (203 PSI)
NOTES:THE VALUES OBTAINED BYUSING THE MAXIMUM LOADREFERENCE LINE AND ANYVALUES FOR K ARE EXACT. FORLOADS LESS THAN MAXIMUM,THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
SLIGHTLY FOR ANY OTHERVALUES OF K
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C
K N E S S
[ C E N T I M E T E R S ]
REFERENCE:"DESIGN OF CONCRETEAIRPORT PAVEMENTS" AND"COMPUTER PROGRAM FORAIRPORT PAVEMENT DESIGN −PROGRAM PDILB" PORTLANDCEMENT ASSOCIATION
MAXIMUM POSSIBLE BODY
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
WEIGHT ON ONE BODY LANDING GEAR
146 110 kg (322 125 lb)
140 000 kg (308 650 lb)
130 000 kg (286 600 lb)
120 000 kg (264 550 lb)
k = 20 MN/m³
k = 40 MN/m³
k = 80 MN/m³
k = 150 MN/m³
Rigid Pavement Requirements - 6 Wheel BogieMRW 512 000 kg - A380-800 Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
( i n c h e s )
200
300
400
500
600
700
800
900
1000
( l b / i n ² )
15
20
25
30
35
40
45
50
55
60
65
70
( k g / c m ² )
A L L O W A B L E W O R K I N G S T R E S
S
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT = 15 BAR (218 PSI)
NOTES:
THE VALUES OBTAINED BY
USING THE MAXIMUM LOAD
REFERENCE LINE AND ANY
VALUES FOR K ARE EXACT. FOR
LOADS LESS THAN MAXIMUM,
THE CURVES ARE EXACT FOR
K = 80 MN/m³ BUT DEVIATE
SLIGHTLY FOR ANY OTHER
VALUES OF K.
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C K N E S S
( C E N T I M E T E R S )
REFERENCE:
"DESIGN OF CONCRETE
AIRPORT PAVEMENTS" AND
"COMPUTER PROGRAM FOR
AIRPORT PAVEMENT DESIGN −
PROGRAM PDILB" PORTLAND
CEMENT ASSOCIATION
MAXIMUM POSSIBLE WINGGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
WEIGHT ON ONE WINGLANDING GEAR106 920 kg (235 725 lb)100 000 kg (230 460 lb)
90 000 kg (198 420 lb)80 000 kg (176 370 lb)70 000 kg (154 325 lb)
L_AC_070701_1_0110101_01_00
11
12
13
14
15
16
10
9
8
Rigid Pavement Requirements - 4 Wheel BogieMRW 562 000 kg - A380-800 Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
8
9
10
11
12
13
14
15
16
[ i n c h e s ]
200
300
400
500
600
700
800
900
1000
[ l b / i n ² ]
15
20
25
30
35
40
45
50
55
60
65
70
[ k g / c m ² ]
A L L O W A B L E W O R K I N G
S T R E S S
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT = 15 BAR (218 PSI)
NOTES:THE VALUES OBTAINED BYUSING THE MAXIMUM LOADREFERENCE LINE AND ANYVALUES FOR K ARE EXACT. FORLOADS LESS THAN MAXIMUM,THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
SLIGHTLY FOR ANY OTHERVALUES OF K
22
24
26
28
30
32
34
36
38
R I G I D P A V E M E N T T H I C
K N E S S
[ C E N T I M E T E R S ]
REFERENCE:"DESIGN OF CONCRETEAIRPORT PAVEMENTS" AND"COMPUTER PROGRAM FORAIRPORT PAVEMENT DESIGN −PROGRAM PDILB" PORTLANDCEMENT ASSOCIATION
40
k = 20 MN/m³
k = 40 MN/m³
k = 80 MN/m³
k = 150 MN/m³
MAXIMUM POSSIBLE WING
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
WEIGHT ON ONE WING LANDING GEAR
107 710 kg (237 475 lb)
100 000 kg (220 460 lb)
90 000 kg (198 420 lb)
80 000 kg (176 370 lb)
70 000 kg (154 325 lb)
L_AC_070701_1_0120101_01_00
Rigid Pavement Requirements - 4 Wheel BogieMRW 571 000 kg - A380-800 Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
8
9
10
11
12
13
14
15
16
( i n c h e s )
200
300
400
500
600
700
800
900
1000
( l b / i n ² )
15
20
25
30
35
40
45
50
55
60
65
70
( k g / c m ² )
A L L O W A B L E W O R K I N G S T R E S
S
1400 x 530R23 40PR TIRES
TIRE PRESSURE CONSTANT = 15 BAR (218 PSI)
NOTES:
THE VALUES OBTAINED BY
USING THE MAXIMUM LOAD
REFERENCE LINE AND ANY
VALUES FOR K ARE EXACT. FOR
LOADS LESS THAN MAXIMUM,
THE CURVES ARE EXACT FOR
K = 80 MN/m³ BUT DEVIATE
SLIGHTLY FOR ANY OTHER
VALUES OF K
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C K N E S S
( C E N T I M E T E R S )
REFERENCE:
"DESIGN OF CONCRETE
AIRPORT PAVEMENTS" AND
"COMPUTER PROGRAM FOR
AIRPORT PAVEMENT DESIGN −
PROGRAM PDILB" PORTLAND
CEMENT ASSOCIATION
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
161 570 kg (356 200 lb)150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)120 000 kg (264 550 lb)
WEIGHT ON ONE BODYLANDING GEAR
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
L_AC_070701_1_0060101_01_00
Rigid Pavement Requirements - 6 Wheel BogieMRW 571 000 kg - A380-800 Models
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
[ i n c h e s ]
200
300
400
500
600
700
800
900
1000
[ l b / i n ² ]
15
20
25
30
35
40
45
50
55
60
65
70
[ k g / c m ² ]
A L L O W A B L E W O R K I N G
S T R E S S
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT = 16.1 BAR (234 PSI)
NOTES:THE VALUES OBTAINED BYUSING THE MAXIMUM LOADREFERENCE LINE AND ANYVALUES FOR K ARE EXACT. FORLOADS LESS THAN MAXIMUM,THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATESLIGHTLY FOR ANY OTHERVALUES OF K
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C
K N E S S
[ C E N T I M E T E R S ]
REFERENCE:"DESIGN OF CONCRETEAIRPORT PAVEMENTS" AND"COMPUTER PROGRAM FORAIRPORT PAVEMENT DESIGN −PROGRAM PDILB" PORTLANDCEMENT ASSOCIATION
MAXIMUM POSSIBLE WING
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
WEIGHT ON ONE WING LANDING GEAR
112 530 kg (248 100 lb)
100 000 kg (220 460 lb)
90 000 kg (198 420 lb)
80 000 kg (176 370 lb)
70 000 kg (154 325 lb)
k = 20 MN/m³
k = 40 MN/m³
k = 80 MN/m³
k = 150 MN/m³
L_AC_070701_1_0130101_01_00
Rigid Pavement Requirements - 4 Wheel BogieMRW 592 000 kg - A380-800F Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
( i n c h e s )
200
300
400
500
600
700
800
900
1000
( l b / i n ² )
15
20
25
30
35
40
45
50
55
60
65
70
( k g / c m ² )
A L L O W A B L E W O R K I N G S T R E S S
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT = 16.1 BAR (234 PSI)
NOTES:
THE VALUES OBTAINED BY
USING THE MAXIMUM LOAD
REFERENCE LINE AND ANY
VALUES FOR K ARE EXACT. FOR
LOADS LESS THAN MAXIMUM,
THE CURVES ARE EXACT FOR
K = 80 MN/m³ BUT DEVIATE
SLIGHTLY FOR ANY OTHERVALUES OF K
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C K N E S S
( C E N T I M E T E R S )
REFERENCE:
"DESIGN OF CONCRETE
AIRPORT PAVEMENTS" AND
"COMPUTER PROGRAM FOR
AIRPORT PAVEMENT DESIGN −
PROGRAM PDILB" PORTLAND
CEMENT ASSOCIATION
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³
k = 150 MN/m³
168 800 kg (372 125 lb)160 000 kg (352 750 lb)
WEIGHT ON ONE BODYLANDING GEAR
150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)
WEIGHT ON ONE BODYLANDING GEAR
L_AC_070701_1_0040101_01_01
Rigid Pavement Requirements - 6 Wheel BogieMRW 592 000 kg - A380-800F Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
[ i n c h e s ]
200
300
400
500
600
700
800
900
1000
[ l b / i n ² ]
15
20
25
30
35
40
45
50
55
60
65
70
[ k g / c m ² ]
A L L O W A B L E W O R K I N G
S T R E S S
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT = 16.1 BAR (234 PSI)
NOTES:THE VALUES OBTAINED BYUSING THE MAXIMUM LOADREFERENCE LINE AND ANYVALUES FOR K ARE EXACT. FORLOADS LESS THAN MAXIMUM,THE CURVES ARE EXACT FORK = 80 MN/m³ BUT DEVIATE
SLIGHTLY FOR ANY OTHERVALUES OF K
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C
K N E S S
[ C E N T I M E T E R S ]
REFERENCE:"DESIGN OF CONCRETEAIRPORT PAVEMENTS" AND"COMPUTER PROGRAM FORAIRPORT PAVEMENT DESIGN −PROGRAM PDILB" PORTLANDCEMENT ASSOCIATION
k = 20 MN/m³
k = 40 MN/m³
k = 80 MN/m³
k = 150 MN/m³
WEIGHT ON ONE WING LANDING GEAR
114 380 kg (252 175 lb)
100 000 kg (220 460 lb)
90 000 kg (198 420 lb)
80 000 kg (176 370 lb)
70 000 kg (154 325 lb)
MAXIMUM POSSIBLE WING
GEAR LOAD AT MAXIMUM
RAMP WEIGHT AND AFT CG
L_AC_070701_1_0140101_01_00
Rigid Pavement Requirements - 4 Wheel BogieMRW 602 000 kg - A380-800F Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
( i n c h e s )
200
300
400
500
600
700
800
900
1000
( l b / i n ² )
15
20
25
30
35
40
45
50
55
60
65
70
( k g / c m ² )
A L L O W A B L E W O R K I N G S T R E S S
1400 x 530R23 42PR TIRES
TIRE PRESSURE CONSTANT = 16.1 BAR (234 PSI)
NOTES:
THE VALUES OBTAINED BY
USING THE MAXIMUM LOAD
REFERENCE LINE AND ANY
VALUES FOR K ARE EXACT. FOR
LOADS LESS THAN MAXIMUM,
THE CURVES ARE EXACT FOR
K = 80 MN/m³ BUT DEVIATE
SLIGHTLY FOR ANY OTHERVALUES OF K
22
24
26
28
30
32
34
36
38
40
R I G I D P A V E M E N T T H I C K N E S S
( C E N T I M E T E R S )
REFERENCE:
"DESIGN OF CONCRETE
AIRPORT PAVEMENTS" AND
"COMPUTER PROGRAM FOR
AIRPORT PAVEMENT DESIGN −
PROGRAM PDILB" PORTLAND
CEMENT ASSOCIATION
MAXIMUM POSSIBLE BODYGEAR LOAD AT MAXIMUMRAMP WEIGHT AND AFT CG
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
171 580 kg (378 250 lb)160 000 kg (352 750 lb)
WEIGHT ON ONE BODYLANDING GEAR
150 000 kg (330 700 lb)140 000 kg (308 650 lb)130 000 kg (286 600 lb)
WEIGHT ON ONE BODYLANDING GEAR
L_AC_070701_1_0080101_01_00
Rigid Pavement Requirements - 6 Wheel BogieMRW 602 000 kg - A380-800F Models
7-7-1
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@A380 AIRPLANE CHARACTERISTICS
7-8-0 Rigid Pavement Requirements - LCN Conversion
**ON A/C A380-800 Models A380-800F Models
Rigid Pavement Requirements - LCN Conversion
1. General
To find the airplane weight that a Rigid Pavement can support, the LCN of the pavement and theRadius of Relative Stiffness (L) must be Known.
In the typical example shown in Section 7-8-2 with MRW 512000 Kg, The Radius of RelativeStiffness is shown at 1016 mm (40 in.) with an LCN of 90. For these conditions the weight on oneWing Landing Gear is 90000 kg (198420 lb).
7-8-0
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@A380 AIRPLANE CHARACTERISTICS
7-8-1 Radius of Relative Stiffness
**ON A/C A380-800 Models A380-800F Models
Radius of Relative Stiffness
1. This section gives Radius of Relative Stiffness.
7-8-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
WHERE
=
E
k
d
Ed 34
2
=
=
=
d
k
3= 24.1652 4
6
3
Rigid Pavement Thickness, inches
12 (1 − ) k
Young’s Modulus = 4 x 10 psi
RADIUS OF RELATIVE STIFFNESS (L)VALUES IN INCHES
L
Subgrade Modulus, lbf/in
REFERENCE:
= Poisson’s Ratio = 0.15
6.06.57.07.5
31.4833.4335.3437.22
29.3031.11
32.8934.63
26.4728.1129.7231.29
24.6326.1627.6529.12
23.3024.7426.1527.54
22.2623.6424.9926.32
21.4222.7424.0425.32
20.7222.0023.2524.49
19.1320.3121.4722.61
8.08.59.09.5
39.0640.8842.6744.43
36.3538.0439.7141.35
32.8534.3735.8837.36
30.5731.9933.3934.77
28.9130.2531.5832.89
27.6228.9130.1731.42
26.5827.8129.0330.23
25.7026.9028.0829.24
23.7424.8425.9327.00
10.010.511.011.5
46.1847.9049.6051.28
38.8340.2841.7143.12
36.1437.4838.8140.13
34.1735.4536.7137.95
32.6533.8735.0736.26
31.4232.5933.7534.89
30.3931.5232.6433.74
28.0629.1130.1431.16
12.012.513.013.5
52.9454.5956.2257.83
49.2750.8052.3253.82
44.5245.9047.2748.63
41.4342.7243.9945.26
39.1840.4041.6142.80
37.4438.6039.7540.89
36.0237.1438.2539.35
34.8435.9236.9938.06
32.1733.1734.1635.14
14.0
14.515.015.5
16.016.517.017.5
55.31
56.7858.2559.70
65.6967.2368.7570.26
61.1362.5663.9865.38
49.98
51.3152.6353.94
46.51
47.7548.9850.20
43.98
45.1646.3247.47
55.2456.5357.8159.08
51.4152.6153.8054.98
48.6249.7550.8852.00
42.02
43.1544.2645.36
40.44
41.5142.5843.64
39.11
40.1541.1942.21
36.12
37.0838.0338.98
46.4547.5448.6149.68
44.7045.7446.7747.80
43.2344.2445.2446.23
39.9240.8541.7842.70
18.019.020.021.0
22.023.024.025.0
71.7674.7377.6680.55
83.4186.2489.0491.81
66.7869.5472.2774.96
77.6380.2682.8685.44
60.3462.8465.3067.74
70.1472.5274.8777.20
56.1558.4860.7763.04
65.2867.4969.6871.84
53.1155.3157.4759.62
61.7363.8365.9067.95
50.7452.8454.9156.96
58.9860.9862.9664.92
48.8250.8452.8454.81
56.7558.6860.5862.46
54.8956.7558.5960.41
47.2249.1751.1053.01
43.6145.4147.1948.95
50.6952.4154.1155.79
d k=75 k=100 k=150 k=200 k=250 k=300 k=350 k=400 k=550
59.43
61.0262.5964.15
42.9744.5746.1647.72
PORTLAND CEMENT ASSOCIATION
L_AC_070801_1_0010101_01_00
Radius of Relative Stiffness
7-8-1
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@A380 AIRPLANE CHARACTERISTICS
7-8-2 Rigid Pavement Requirements - LCN Conversion
**ON A/C A380-800 Models
Rigid Pavement Requirements - LCN Conversion - Pax
1. This section gives Rigid Pavement Requirements - LCN Conversion.
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070802_1_0090101_01_00
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O A D
C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5
2 0
2 5
3 0
3 5
4 0
4
5
5
0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T
S I N G L E W H E E L L O A D S A R E D E R I V E D B
Y M E T H O D S S H O W N I N
I C A O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o
n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E
S S U R E C O N S T A N T A T 1 4 b a r ( 2 0 3 p s i )
R A D I U S O F R E L A T I V E S T I F
F N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
W E I G
H T O N O N E W I N G
L A N D
I N G G
E A R
9 7 4 1 0 k g
( 2 1 4 7 5 0 l b )
9 0 0 0 0 k g
( 1 9 8 4 2 0 l b )
8 0 0 0 0 k g
( 1 7 6 3 7 0 l b )
7 0 0 0 0 k g
( 1 5 4 3 2 5 l b )
6 0 0 0 0 k g
( 1 3 2 2 7 5 l b )
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070802_1_0100101_01_00
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
R A D I U S O F R E L A T I V E S T I F F N E S S [ I N C H E S ]
1 5 0
L O A
D C L A S S I F I C A T I O N N U M B E R ( L C N )
1 0
1 5
2 0
2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S
I N G L E W H E E L L O A D S A R E D E R I V E D B Y M E T H O D S S H O W N I N
I C A O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c
o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 4 b a r ( 2 0 3 p s i )
R A D I U S O F R E L A T I V E S T I F
F N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 1 0
6 0
7 0
8 0
9 0
1 0 0
5 0
5
M A X I M U M P O S S I B L E B O D
Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G H T O N O N E B O D Y
L A
N D I N G G E A R
1 4
6 1 1 0 k g
( 3 2 2 1 2 5 l b )
1 4
0 0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3
0 0 0 0 k g
( 2 8 6 6 0 0 l b )
1 2
0 0 0 0 k g
( 2 6 4 5 5 0 l b )
1 1
0 0 0 0 k g
( 2 4 2 5 0 0 l b )
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 512 000 kg - A380-800 Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O
A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M E T H O D S S H O W N I N
I C A O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3 S
e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
R A D I U S O F R E L A T I V E S T I F F
N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G
H T O N O N E W I N G
L A N D
I N G G E A R
1 0 6 9 2 0 k g
( 2 3 5 7 2 0 l b )
1 0 0 0 0 0 k g
( 2 2 0 4 6 0 l b )
9 0
0 0 0 k g
( 1 9 8 4 2 0 l b )
8 0
0 0 0 k g
( 1 7 6 3 7 0 l b )
7 0
0 0 0 k g
( 1 5 4 3 2 5 l b )
L_AC_070802_1_0010101_01_01
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 562 000 kg - A380-800 Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0 2
0 3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O
A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M E T H O D S S H O W N I N
I C A
O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P
R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
R A D I U S O F R E L A T I V E S T I F F N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
M A X I M U M P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G
H T O N O N E B O D Y
L A N D
I N G G E A R
1 6 0 3 8 0 k g
( 3 5 3 5 7 5 l b )
1 5 0 0 0 0 k g
( 3 3 0 7 0 0 l b )
1 4 0 0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0 0 0 0 k g
( 2 8 6 6 0 0 l b )
1 2 0 0 0 0 k g
( 2 6 4 5 5 0 l b )
L_AC_070802_1_0020101_01_01
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 562 000 kg - A380-800 Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A
L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B
Y M E T H O D S S H O W N I N
I C A
O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3 S
e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
R A D I U S O F R E L A T I V E S T I F F N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G H T O N O N E W I N G
L A N
D I N G G E A R
1 0 7
7 1 0 k g
( 2 3 7 4 7 5 l b )
1 0 0 0 0 0 k g
( 2 2 0 4 6 0 l b )
9 0
0 0 0 k g
( 1 9 8 4 2 0 l b )
8 0
0 0 0 k g
( 1 7 6 3 7 0 l b )
7 0
0 0 0 k g
( 1 5 4 3 2 5 l b )
L_AC_070802_1_0050101_01_00
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 571 000 kg - A380-800 Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0 2
0 3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1
5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L
E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y
M E T H O D S S H O W N I N
I C A O
A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3 S e
c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R
E P R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
R A D I U S O F R E L A T I V E S T
I F F N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
M A X I M U M P O S S I B L E B O D
Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G H T O N O N E B O D Y
L A N
D I N G G E A R
1 6 1 5 7 0 k g
( 3 5 6 2 0 0 l b )
1 5 0 0 0 0 k g
( 3 3 0 7 0 0 l b )
1 4 0 0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0 0 0 0 k g
( 2 8 6 6 0 0 l b )
1 2 0 0 0 0 k g
( 2 6 4 5 5 0 l b )
L_AC_070802_1_0060101_01_00
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 571 000 kg - A380-800 Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Rigid Pavement Requirements - LCN Conversion - Freighter
1. This section gives Rigid Pavement Requirements LCN.
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O
A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L
E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y
M E T H O D S S H O W N I N
I C A O
A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e
c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
R A D I U S O F R E L A T I V E S T I F F N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G H T O N O N E W I N G
L A N
D I N G G E A R
1 1 2
5 3 0 k g
( 2 4 8 1 0 0 l b )
1 0 0
0 0 0 k g
( 2 2 0 4 6 0 l b )
9 0
0 0 0 k g
( 1 9 8 4 1 0 l b )
8 0
0 0 0 k g
( 1 7 6 0 0 0 l b )
7 0
0 0 0 k g
( 1 5 4 3 2 5 l b )
L_AC_070802_1_0030101_01_01
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 592 000 kg - A380-800F Models
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5
2 0
2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L
E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y
M E T H O D S S H O W N I N
I C A O
A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P
R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
R A D I U S O F R E L A T I V E S T I F F
N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2
2 0 3
2 5 4 0
W E I G H T O N O N E B O D Y
L A N
D I N G G E A R
1 6 8
8 0 0 k g
( 3 7 2 1 2 5 l b )
1 6 0
0 0 0 k g
( 3 5 2 7 5 0 l b )
1 5 0
0 0 0 k g
( 3 3 0 7 0 0 l b )
1 4 0
0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0
0 0 0 k g
( 2 8 6 6 0 0 l b )
M A X I M U M
P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
L_AC_070802_1_0040101_01_01
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 592 000 kg - A380-800F Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L
O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y M E T H O D S S H O W N I N
I C A
O A E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P
R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
R A D I U S O F R E L A T I V E S T I F F N E S S ( m m )
5 0 8
7 6 2
1 0 1 6
1 5 2 4
2 0 3 2
2 5 4 0
M A X I M U M P O S S I B L E W I N G
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E
I G H T O N O N E W I N G
L A N D I N G G E A R
1 1 4 3 8 0 k g
( 2 5 2 1 7 5 l b )
1 0 0 0 0 0 k g
( 2 2 0 4 6 0 l b )
9 0 0 0 0 k g
( 1 9 8 4 1 0 l b )
8 0 0 0 0 k g
( 1 7 6 0 0 0 l b )
7 0 0 0 0 k g
( 1 5 4 3 2 5 l b )
L_AC_070802_1_0070101_01_00
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 602 000 kg - A380-800F Models
7-8-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2 0
3 0
4 0
5 0
1 0 0
9 0
8 0
7 0
6 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
R A D I U S O F R E L A T I V E S T I F F N
E S S [ I N C H E S ]
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 l b ]
1 2 0
1 5 0
6 0
7 0
8 0
9 0
1 0 0
5 0
L O A D C L A S S I F I C A T I O N N U M B E R ( L C N )
5 1 0
1 5 2
0 2 5
3 0
3 5
4 0
4 5
5 0
E Q U I V A L E N T S I N G L E W H E E L L O A D [ 1 0 0 0 k g ]
N O T E : E Q U I V A L
E N T S I N G L E W H E E L L O A D S A R E D E R I V E D B Y
M E T H O D S S H O W N I N
I C A O A
E R O D R O M E M A N U A L P A R T 2 P A R 4 . 1 . 3
S e c o n d E d i t i o n 1 9 6 5
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
R A D I U S O F R E L A T I V E S T I F F N E S S ( m m )
5 0 8
7 6 2
1 0 1
1 5 2 4
2 0 3 2
2 5 4 0
M A X I M U M P O S S I B L E B O D Y
G E A R L O A D A T M A X I M U M
R A M P W E I G H T A N D A F T C G
W E I G
H T O N O N E B O D Y
L A N D
I N G G E A R
1 7 1 5
8 0 k g
( 3 7 8 2 5 0 l b )
1 6 0 0 0 0 k g
( 3 5 2 7 5 0 l b )
1 5 0 0 0 0 k g
( 3 3 0 7 0 0 l b )
1 4 0 0 0 0 k g
( 3 0 8 6 5 0 l b )
1 3 0 0 0 0 k g
( 2 8 6 6 0 0 l b )
L_AC_070802_1_0080101_01_00
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 602 000 kg - A380-800F Models
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@A380 AIRPLANE CHARACTERISTICS
7-8-3 Radius of Relative Stiffness (Other values of E and µ)
**ON A/C A380-800 Models A380-800F Models
Radius of Relative Stiffness (Other values of E and µ)
1. General
The chart of Section 7-8-1 presents ”L” values based on Young’s Modulus (E) of 4 000 000 psi andPoisson’s Ratio (µ) of 0.15.
To find ”L” values based on other values of E and µ, see curves of 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 table of Section 7-8-1.
The effect of variations of µ on the ”L” value is treated in a similar manner.
7-8-3
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@A380 AIRPLANE CHARACTERISTICS
7-8-4 Radius of Relative Stiffness (Other values of E and µ)
**ON A/C A380-800 Models A380-800F Models
Radius of Relative Stiffness (Other values of E and µ)
1. This section gives Radius of Relative Stiffness.
7-8-4
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.10
1.05
1.00
0.95
0.90
0.85
0.800 1 2 3 4 5
1.015
0.00 0.50 0.10 0.15 0.20 0.250.995
1.000
1.005
1.010
NOTE:
6
E F A C T O R
E, YOUNG S MODULUS (10 psi),
, POISSON’S RATIO
F A C T O R
EFFECT OF ON L VALUES
EFFECT OF E ON L VALUES
BOTH CURVES ON THIS PAGE ARE USED TO ADJUST THE L VALUES OF TABLE 7−8−1
L_AC_070804_1_0010101_01_00
Radius of Relative Stiffness
7-8-4
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@A380 AIRPLANE CHARACTERISTICS
In the example shown in Section 7-9-1, with MRW 602000 Kg, for an Aircraft Gross Weight of 510000 (1 124 360 lb) and medium subgrade strength (code B) the ACN for the rigid pavement is 55
In the example shown in Section 7-9-2, with MRW 592000 Kg, for an Aircraft Gross Weight of
510000 (1 124 360 lb) and medium subgrade strength (code B) the ACN for the rigid pavement is 60
In the example shown in Section 7-9-2, with MRW 602000 Kg, for an Aircraft Gross Weight of 510000 (1 124 360 lb) and medium subgrade strength (code B) the ACN for the rigid pavement is 60
NOTE : An aircraft with an ACN equal to or less than the reported PCN can operate on thatpavement, subject to a limitation on the tire pressure. (Ref: ICAO Aerodrome DesignManual Part 3 Chapter 1 Second Edition 1983)
7-9-0
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@A380 AIRPLANE CHARACTERISTICS
7-9-1 Aircraft Classification Number - Flexible Pavement
**ON A/C A380-800 Models
Aircraft Classification Number - Flexible Pavement - Pax
1. This section gives the Aircraft Classification Number - Flexible Pavement.
7-9-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
2 6 0
2 8 0
3 0 0
3 2
0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E S S U R E C O N
S T A N T A T 1 4 b a r ( 2 0 3 p s i )
A C N W A S D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A E R O D R O M E D E S I G N M A N U A L P A R T 3
C H A P T E R 1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E
D F O R A C N C A L C U L A T I O N S : 4 3 % M A C
.
S e e S e c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e
m e n t − M R W
5 1 2 0 0 0 k g − A 3 8 0 − 8 0 0 M o d e l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
L_AC_070901_1_0050101_01_00
A L P H
A F A C T O R = 0 . 8
S U B G
R A D E S T R E N G T H
D − C
B R 3 ( U L T R A L O W )
C − C
B R 6 ( L O W )
B − C B R 1 0 ( M E D I U M )
A − C
B R 1 5 ( H I G H )
Aircraft Classification Number - Flexible PavementMRW 512 000 kg - A380-800 Models
7-9-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070901_1_0060101_01_00
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4
0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0 4
8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 3 0 0
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
A C N W A S
D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A E R
O D R O M E D E S I G N M A N U A L P A R T 3
C H A P T E R
1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E D
F O R A C N C A L C U L A T I O N S : 4 3 % M A C .
S e e S e c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m
e n t − M R W
5 6 2 0 0 0 k g − A 3 8 0 − 8 0 0 M o d e
l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
S U B G R
A D E S T R E N G T H
D − C B R 3 ( U L T R A L O W )
C − C B R 6 ( L O W )
B − C B R 1 0 ( M E D I U M )
A − C B R 1 5 ( H I G H )
A L P H A
F A C T O R = 0 . 8
Aircraft Classification Number - Flexible PavementMRW 562 000 kg - A380-800 Models
7-9-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070901_1_0070101_01_00
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 3 0 0
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R E
S
T I R E P R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
A C N W A S
D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A E R O D R O M E D E S I G N M A N U A L P A R T 3
C H A P T E R
1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E D
F O R A C N C A L C U L A T I O N S : 4 1 % M A C .
S e e S e c t i o
n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e
n t − M R W
5 7 1 0 0 0 k g − A 3 8 0 − 8 0 0 M o d e l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
S U B G R A
D E S T R E N G T H
D − C B R
3 ( U L T R A L O W )
C − C B R
6 ( L O W )
B − C B R
1 0 ( M E D I U M )
A − C B R
1 5 ( H I G H )
A L P H A F
A C T O R = 0 . 8
Aircraft Classification Number - Flexible PavementMRW 571 000 kg - A380-800 Models
7-9-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aircraft Classification Number - Flexible Pavement - Freighter
1. This section gives the Aircraft Classification Number - Flexible Pavement.
7-9-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070901_1_0080101_01_00
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 3 0 0
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R E S S U R E C O N S T A
N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
A C N W A S D E
T E R M I N E D A S R E F E R E N C E D I N
I C A O A E R O D
R O M E D E S I G N M A N U A L P A R T 3
C H A P T E R 1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E D F O
R A C N C A L C U L A T I O N S : 4 2 . 8 % M A C .
S e e S e c t i o n 7
− 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e n t
− M R W
5 9 2 0 0 0 k g − A 3 8 0 − 8 0 0 F M o d e l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
A L P H A F A C T O R = 0 . 8
S U B G R A
D E S T R E N G T H
D − C B R
3 ( U L T R A L O W )
C − C B R
6 ( L O W )
B − C B R
1 0 ( M E D I U M )
A − C B R
1 5 ( H I G H )
Aircraft Classification Number - Flexible PavementMRW 592 000 kg - A380-800F Models
7-9-1
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070901_1_0090101_01_00
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 3 0 0
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R E S S U R E C O N S T A
N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
A C N W A S D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A E R O
D R O M E D E S I G N M A N U A L P A R T 3
C H A P T E R 1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E D F O R A C N C A L C U L A T I O N S : 4 2 . 7 % M A C .
S e e S e c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e
n t − M R W 6 0 2 0 0 0 k g − A 3 8 0 − 8 0 0 F M o d e l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
A L P H A F
A C T O R = 0 . 8
S U B G R A D E S T R E N G T H
D − C B R 3 ( U L T R A L O W )
C − C B R
6 ( L O W )
B − C B R 1 0 ( M E D I U M )
A − C B R
1 5 ( H I G H )
Aircraft Classification Number - Flexible PavementMRW 602 000 kg - A380-800F Models
7-9-1
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@A380 AIRPLANE CHARACTERISTICS
7-9-2 Aircraft Classification Number - Rigid Pavement
**ON A/C A380-800 Models
Aircraft Classification Number - Rigid Pavement - Pax
1. This section gives the Aircraft Classification Number - Rigid Pavement.
7-9-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070902_1_0050101_01_00
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R
E S
T I R E P R E S S U R E C O N S
T A N T A T 1 4 b a r ( 2 0 3 p s i )
A C N W A
S D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A E
R O D R O M E D E S I G N M A N U A L P A R T 3
C H A P T E
R 1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E
D F O R A C N C A L C U L A T I O N S : 4 3 % M A C .
S e e S e c
t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e n t − M R W
5 1 2 0 0 0 k g − A 3 8 0 − 8 0 0 M o d
e l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
S U B G R A D
E S T R E N G T H
D − k = 2 0 M N / m ³ ( U L T R A L O W )
C − k = 4 0 M N / m ³ ( L O W )
B − k = 8 0 M N / m ³ ( M E D I U M )
A − k = 1 5 0 M N / m ³ ( H I G H )
Aircraft Classification Number - Rigid PavementMRW 512 000 kg - A380-800 Models
7-9-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0
2 6 0
2 8 0
3 0 0
3 2 0 3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 3 0 0
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T I R
E S
T I R E P R E S S U R E C O N S T A N T A T 1 5 b a r ( 2 1 8 p s i )
A C N W A S D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A E R O D R O M E D E S I G N M A N U A L P A R T 3
C H A P T E R 1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E D F O R A C N C A L C U L A T I O N S : 4 3 % M A C .
S e e S e c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m
e n t − M R W 5 6 2 0 0 0 k g − A 3 8 0 − 8 0 0 M o d e
l s
[ x 1 0 0 0 k g ]
S U B G R A D E S T R E N G T H
D − k =
2 0 M
N / m ³ ( U L T R A L O W )
C − k =
4 0 M
N / m ³ ( L O W )
B − k =
8 0 M
N / m ³ ( M E D I U M )
A − k = 1 5 0 M
N / m ³ ( H I G H )
[ x 1 0 0 0 l b ]
L_AC_070902_1_0060101_01_00
Aircraft Classification Number - Rigid PavementMRW 562 000 kg - A380-800 Models
7-9-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
1 1 0
1 2 0 2
6 0
2 8 0
3 0 0
3 2 0
3 4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0
4 8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
A I R C R A F T G R O S S W E I G H T
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
1 3 0 0
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 0 P R T
I R E S
T I R E P R E S S U R E C O N
S T A N T A T 1 5 b a r ( 2 1 8 p s i )
A C N W
A S D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A
E R O D R O M E D E S I G N M A N U A L P A R T 3
C H A P T
E R 1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S
E D F O R A C N C A L C U L A T I O N S : 4 1 % M A C .
S e e S e
c t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e m e n t − M R W 5 7 1 0 0 0 k g − A 3 8 0 − 8 0 0 M o
d e l s
[ x 1 0 0 0 k g ]
[ x 1 0 0 0 l b ]
L_AC_070902_1_0070101_01_00
S U B G R A D
E S T R E N G T H
D − k = 2 0 M N / m ³ ( U L T R A L O W )
C − k = 4 0 M N / m ³ ( L O W )
B − k = 8 0 M N / m ³ ( M E D I U M )
A − k = 1 5 0 M N / m ³ ( H I G H )
Aircraft Classification Number - Rigid PavementMRW 571 000 kg - A380-800 Models
7-9-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aircraft Classification Number - Rigid Pavement - Freighter
1. This section gives the Aircraft Classification Number - Rigid Pavement.
7-9-2
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2 6 0
2 8 0
3 0 0
3 2 0 3
4 0
3 6 0
3 8 0
4 0 0
4 2 0
4 4 0
4 6 0 4
8 0
5 0 0
5 2 0
5 4 0
5 6 0
5 8 0
6 0 0
1 4 0 0 x 5 3 0 R 2 3 4 2 P R T I R E S
T I R E P R E S S U R E C O N S T A N T A T 1 6 . 1 b a r ( 2 3 4 p s i )
A C N W A S D E T E R M I N E D A S R E F E R E N C E D I N
I C A O A E
R O D R O M E D E S I G N M A N U A L P A R T 3
C H A P T E R 1 S E C O N D E D I T I O N 1 9 8 3 .
C G U S E
D F O R A C N C A L C U L A T I O N S : 4 2 . 7 % M A
C .
S e e S e c
t i o n 7 − 4 − 1 F i g u r e : L a n d i n g G e a r L o a d i n g
o n P a v e
m e n t − M R W
6 0 2 0 0 0 k g − A 3 8 0 − 8 0 0 F M o
d e l s
[ x 1 0 0 0 k g ]
2 0
4 0
6 0
8 0
1 0 0
1 2 0
A I R C R A F T C L A S S I F I C A T I O N N U M B E R ( A C N )
A I R C R A F T G R O S S W E I G H T
1 3 0 0
1 2 0 0
1 1 0 0
1 0 0 0
9 0 0
8 0 0
7 0 0
6 0 0
[ x 1 0 0 0 l b ]
S U B G R A D E
S T R E N G T H
D − k =
2 0
M N / m ³ ( U L T R A L O W )
C − k =
4 0
M N / m ³ ( L O W )
B − k =
8 0 M N / m ³ ( M E D I U M )
A − k = 1 5 0
M N / m ³ ( H I G H )
L_AC_070902_1_0090101_01_00
Aircraft Classification Number - Rigid PavementMRW 602 000 kg - A380-800F Models
7-9-2
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@A380 AIRPLANE CHARACTERISTICS
DERIVATIVE AIRPLANES
8-1-0 Possible Future Derivative Airplanes
**ON A/C A380-800 Models A380-800F ModelsPossible Future Derivative Airplanes
1. GeneralA380 Family could be extended with several derivatives in order to provide additional capabilities tothe operators. Those derivatives could impact payload capacity or range or both.
8-1-0
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@A380 AIRPLANE CHARACTERISTICS
SCALED DRAWINGS
9-1-0 Scaled Drawing - 1 cm. = 500 cm.
**ON A/C A380-800 Models A380-800F ModelsScaled Drawing - 1 cm. = 500 cm.
1. This section provides the Scaled Drawing - 1 cm = 500 cm.
9-1-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
AIR CONDITIONING
BULK CARGO COMPT DOOR
BODY LANDING GEAR
CARGO COMPT DOOR
ELECTRICAL
FUEL
POTABLE WATER
LAVATORY
NOSE LANDING GEAR
PASSENGER/CREW DOOR
A
B
BLG
C
E
F
L
NLG
X
PNEUMATICP
WING LANDING GEARWLG
H O
E
A
NLG
XX
X
X
X
F
WLG
X
P
X
WLG
F
BLGBLG
X
X
X
X
L
C
B
C
DB1A
H O
L_AC_090100_1_0010101_01_01
Scaled Drawing -- 1 cm = 500 cmA380-800 Models
9-1-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
AIR CONDITIONING
BULK CARGO COMPT DOOR
BODY LANDING GEAR
CARGO COMPT DOOR
FUEL
POTABLE WATER
LAVATORY
NOSE LANDING GEAR
A
B
BLG
F
L
NLG
X
PNEUMATICP
WING LANDING GEARWLG
H O
COURIER/CREW DOORDB1A
E ELECTRICAL
L_AC_090100_1_0020101_01_02
X
C
BLG BLG
C
B
WLG
F
A
C
X
H ONLG
XE
C
P
F
WLG
Scaled Drawing -- 1 cm = 500 cmA380-800F Models
9-1-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
DB1A L_AC_090100_1_0030101_01_01
Scaled Drawing -- 1 cm = 500 cmA380-800 Models
9-1-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
DB1A L_AC_090100_1_0040101_01_01
Scaled Drawing -- 1 cm = 500 cmA380-800F Models
9-1-0
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@A380 AIRPLANE CHARACTERISTICS
9-2-0 Scaled Drawing - 1 in. = 50 ft.
**ON A/C A380-800 Models A380-800F Models
Scaled Drawing - 1 in. = 50 ft.
1. This section provides the Scaled Drawing - 1 in = 50 ft.
9-2-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_090200_1_0010101_01_02
AIR CONDITIONING
BULK CARGO COMPT DOOR
BODY LANDING GEAR
CARGO COMPT DOOR
ELECTRICAL
FUEL
POTABLE WATER
LAVATORY
NOSE LANDING GEAR
PASSENGER/CREW DOOR
A
B
BLG
C
E
F
L
NLG
X
PNEUMATICP
WING LANDING GEARWLG
H O
E
A
NLG
XX
X
X
X
F
WLG
X
P
X
WLG
F
BLGBLG
X
H O
X
X
X
L
C
B
C
DB1A
Scaled Drawing -- 1 in = 50 ftA380-800 Models
9-2-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
AIR CONDITIONING
BULK CARGO COMPT DOOR
BODY LANDING GEAR
CARGO COMPT DOOR
FUEL
POTABLE WATER
LAVATORY
NOSE LANDING GEAR
A
B
BLG
F
L
NLG
X
PNEUMATICP
WING LANDING GEARWLG
H O
COURIER/CREW DOORDB1A
E ELECTRICAL
WLG
BLG
C
X
C
B
BLG
WLG
X
C
P
C
F
X
E
NLG
H O
A
F
L_AC_090200_1_0020101_01_03
Scaled Drawing -- 1 in = 50 ftA380-800F Models
9-2-0
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@A380 AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models