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@AIRBUSA380
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 ofthe 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 Services31707 Blagnac Cedex
FRANCE
Issue: Nov 01/08 Rev: Oct 01/09
@A380AIRPLANE CHARACTERISTICS
HIGHLIGHTS
Revision No. 8 - Oct 01/09
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 2
Section 2-1
Subject 2-1-1
General Airplane Characteristics Data R ADDED WEIGHT VARIANT WV000 TOWV003DESCRIPTION TITLE UPDATED
CHAPTER 5
Section 5-4
Subject 5-4-9
Engine Oil Servicing R
FIGURE Ground Service Connections -Engine Oil Servicing - GP 7200 Engines
R
VFG Oil Servicing R
FIGURE Ground Service Connections -VFG Oil Servicing - TRENT 900 Engines
R
FIGURE Ground Service Connections -VFG Oil Servicing - GP 7200 Engines
R
Starter Oil Servicing R
FIGURE Ground Service Connections -Starter Oil Servicing - GP 7200 Engines
R
Section 5-8
Subject 5-8-0
Ground Towing Requirements R PART EFFECTIVITYADDED/REVISED/DELETEDNOTE AMENDED
FIGURE Ground Towing Requirements -Ground Towing Requirements A380-800Models
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Towing Requirements -Typical Tow Bar configuration 1
N ILLUSTRATION ADDED
HIGHLIGHTSPage 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Towing Requirements -Typical Tow Bar configuration 2
N ILLUSTRATION ADDED
FIGURE Ground Towing Requirements -Nose Gear Towing Fittings
N ILLUSTRATION ADDED
FIGURE Ground Towing Requirements -Maximum Extension of the NLG ShockAbsorber
N ILLUSTRATION ADDED
CHAPTER 6
Section 6-3
Subject 6-3-0
Danger Areas of the Engines R
CHAPTER 7
Section 7-1
Subject 7-1-0
General Information R
Section 7-4
Subject 7-4-0
Landing Gear Loading on Pavement R
Subject 7-4-2
Wing Gear and Body Gear Loading onPavement
R
Section 7-5
Subject 7-5-0
Flexible Pavement Requirements - USArmy Corps of Engineers Design Method
R
Section 7-6
Subject 7-6-0
General R
Section 7-7
Subject 7-7-0
Rigid Pavement Requirements - PortlandCement Association Design Method
R
Section 7-8
HIGHLIGHTSPage 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
Subject 7-8-0
Rigid Pavement Requirements - LCNConversion
R
Subject 7-8-3
Radius of Relative Stiffness (Other valuesof E and µ)
R
Section 7-9
Subject 7-9-0
ACN/PCN Reporting System R
CHAPTER 8
Section 8-1
Subject 8-1-0
Possible Future Derivative Airplanes R
CHAPTER 9
Section 9-1
Subject 9-1-0
FIGURE Scaled Drawing -- 1 cm. = 500cm. - A380-800 Models
R ILLUSTRATION REVISED
FIGURE Scaled Drawing -- 1 cm. = 500cm. - A380-800F Models
R ILLUSTRATION REVISED
FIGURE Scaled Drawing -- 1 cm. = 500cm. - A380-800 Models
R ILLUSTRATION REVISED
FIGURE Scaled Drawing -- 1 cm. = 500cm. - A380-800F Models
R ILLUSTRATION REVISED
Section 9-2
Subject 9-2-0
Scaled Drawing - 1 in. = 50 ft. R
FIGURE Scaled Drawing -- 1 in. = 50 ft. -A380-800 Models
R ILLUSTRATION REVISED
FIGURE Scaled Drawing -- 1 in. = 50 ft. -A380-800F Models
R ILLUSTRATION REVISED
FIGURE Scaled Drawing -- 1 in. = 50 ft. -A380-800 Models
R ILLUSTRATION REVISED
HIGHLIGHTSPage 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Scaled Drawing -- 1 in. = 50 ft. -A380-800F Models
R ILLUSTRATION REVISED
HIGHLIGHTSPage 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
LIST OF EFFECTIVE CONTENT
Revision No. 8 - Oct 01/09
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 1
Subject 1-1-0
Purpose Jun 01/07
Subject 1-2-0
Introduction Nov 01/08
Subject 1-2-1
Glossary Nov 01/08
CHAPTER 2
Subject 2-1-0
General Airplane Characteristics Jun 01/07
Subject 2-1-1
General Airplane Characteristics Data R Oct 01/09
Subject 2-2-0
General Airplane Dimensions Data Jun 01/07
FIGURE General Airplane Dimensions - General Airplane Dimensions Nov 01/08
Subject 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
L.E.C.Page 1
Oct 01/09
@A380AIRPLANE 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
Nov 01/08
Subject 2-6-0
Cargo Compartments Jun 01/07
Subject 2-6-1
Location and Dimensions - Pax Jun 01/07
FIGURE 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 01/07
FIGURE Cargo Compartments - Loading Combinations (Sheet 1) Jun 01/07
FIGURE Cargo Compartments - Loading Combinations (Sheet 2) Jun 01/07
Subject 2-7-0
L.E.C.Page 2
Oct 01/09
@A380AIRPLANE 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
L.E.C.Page 3
Oct 01/09
@A380AIRPLANE 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 Nov 01/08
Subject 3-2-0
Payload /Range Jun 01/07
L.E.C.Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Subject 3-2-1
Payload/Range - Pax 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
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 3-3-1
Take 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 01/07
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
L.E.C.Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Subject 3-4-0
Landing Field Length Jun 01/07
Subject 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
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 01/07
Subject 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
L.E.C.Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Subject 4-5-0
Runway and Taxiway Turn Paths Jun 01/07
Subject 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
L.E.C.Page 7
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
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 5
Subject 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 31/08
FIGURE 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
L.E.C.Page 8
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
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 5-3-1
Typical 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 01/07
FIGURE Ground Service Connections - Ground Service ConnectionsLayout - A380-800F Models
Jun 01/07
Subject 5-4-2
Grounding Points 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 5-4-3
Hydraulic System Nov 01/08
FIGURE Ground Service Connections - Hydraulical Reservoir ServicingPanel
Jun 01/07
FIGURE Ground Service Connections - Hydraulic Ground Connections Jun 01/07
L.E.C.Page 9
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Subject 5-4-4
Electrical System - Pax Nov 01/08
FIGURE Ground Service Connections - Electrical Service Panel -A380-800 Models
Jun 01/07
Electrical System - Freighter Nov 01/08
FIGURE Ground Service Connections - Electrical Service Panel -A380-800F Models
Jun 01/07
Subject 5-4-5
Oxygen System Nov 01/08
FIGURE Ground Service Connections - Oxygen System Jun 01/07
Subject 5-4-6
Fuel System 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 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 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 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 Oct 01/09
L.E.C.Page 10
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Ground Service Connections - Engine Oil Servicing - TRENT900 Engines
Jun 01/07
FIGURE Ground Service Connections - Engine Oil Servicing - GP7200 Engines
R Oct 01/09
VFG Oil Servicing R Oct 01/09
FIGURE Ground Service Connections - VFG Oil Servicing - TRENT900 Engines
R Oct 01/09
FIGURE Ground Service Connections - VFG Oil Servicing - GP 7200Engines
R Oct 01/09
Starter Oil Servicing R Oct 01/09
FIGURE Ground Service Connections - Starter Oil Servicing - TRENT900 Engines
Jun 01/07
FIGURE Ground Service Connections - Starter Oil Servicing - GP7200 Engines
R Oct 01/09
APU Oil Servicing Nov 01/08
FIGURE Ground Service Connections - APU Oil Servicing Jun 01/07
Subject 5-4-10
Vacuum Toilet System - Pax Nov 01/08
FIGURE Ground Service Connections - Vacuum Toilet System -A380-800 Models
Jun 01/07
Vacuum Toilet System - Freighter 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
L.E.C.Page 11
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Starting Pneumatic Requirements (three highpressure ground carts) - Ambient Temperature -40˚C (-40˚F), SeaLevel - 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 highpressure 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
L.E.C.Page 12
Oct 01/09
@A380AIRPLANE 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
L.E.C.Page 13
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Ground Towing Requirements R Oct 01/09
FIGURE Ground Towing Requirements - Ground TowingRequirements A380-800 Models
R Oct 01/09
FIGURE Ground Towing Requirements - Typical Tow Barconfiguration 1
N Oct 01/09
FIGURE Ground Towing Requirements - Typical Tow Barconfiguration 2
N Oct 01/09
FIGURE Ground Towing Requirements - Nose Gear Towing Fittings N Oct 01/09
FIGURE Ground Towing Requirements - Maximum Extension of theNLG Shock Absorber
N Oct 01/09
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
L.E.C.Page 14
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
Engine Exhaust Temperatures - Breakaway Power Jun 01/07
FIGURE Engine Exhaust Temperatures - Breakaway Power - TRENT900 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
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 6-2-0
Airport and Community Noise Data Jun 01/07
Subject 6-2-1
Airport and Community Noise Data Nov 01/08
FIGURE Airport and Community Noise Data - TRENT 900 Engines Nov 01/08
FIGURE Airport and Community Noise Data - GP 7200 Engines Nov 01/08
Subject 6-3-0
Danger Areas of the Engines R Oct 01/09
Subject 6-3-1
Danger 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
L.E.C.Page 15
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CONTENT CHGCODE
LAST REVISIONDATE
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
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. ECSConditions
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 Oct 01/09
Subject 7-2-0
Landing Gear Footprint - Pax Nov 01/08
FIGURE Landing Gear Footprint - MRW 512 000 kg - A380-800Models
Nov 01/08
FIGURE Landing Gear Footprint - MRW 562 000 kg - A380-800Models
Nov 01/08
FIGURE Landing Gear Footprint - MRW 571 000 kg - A380-800Models
Nov 01/08
L.E.C.Page 16
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CONTENT CHGCODE
LAST REVISIONDATE
Landing Gear Footprint - Freighter Nov 01/08
FIGURE Landing Gear Footprint - MRW 592 000 kg - A380-800FModels
Nov 01/08
FIGURE Landing Gear Footprint - MRW 602 000 kg - A380-800FModels
Nov 01/08
Subject 7-3-0
Maximum Pavement Loads - Pax Nov 01/08
FIGURE Maximum Pavement Loads - MRW 512 000 kg - A380-800Models
Nov 01/08
FIGURE Maximum Pavement Loads - MRW 562 000 kg - A380-800Models
Nov 01/08
FIGURE Maximum Pavement Loads - MRW 571 000 kg - A380-800Models
Nov 01/08
Maximum Pavement Loads - Freighter Jun 01/07
FIGURE Maximum Pavement Loads - Freighter - MRW 592 000 kg -A380-800F Models
Nov 01/08
FIGURE Maximum Pavement Loads - MRW 602 000 kg- A380-800FModels
Nov 01/08
Subject 7-4-0
Landing Gear Loading on Pavement R Oct 01/09
Subject 7-4-1
Landing Gear Loading on Pavement - Pax Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 512 000 kg -A380-800 Models
Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 562 000 kg -A380-800 Models
Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 571 000 kg -A380-800 Models
Nov 01/08
Landing Gear Loading on Pavement - Freighter Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 592 000kg -A380-800F Models
Nov 01/08
FIGURE Landing Gear Loading on Pavement - MRW 602 000kg -A380-800F Models
Nov 01/08
Subject 7-4-2
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CONTENT CHGCODE
LAST REVISIONDATE
Wing Gear and Body Gear Loading on Pavement R Oct 01/09
Subject 7-4-3
Wing Gear and Body Gear Loading on Pavement - Pax Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 512000 kg - A380-800 Models
Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 562000 kg - A380-800 Models
Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 571000 kg - A380-800 Models
Nov 01/08
Wing Gear and Body Gear Loading on Pavement - Freighter Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 592000 kg - A380-800F Models
Nov 01/08
FIGURE Wing Gear and Body Gear Loads on Pavement - MRW 602000 kg - A380-800F Models
Nov 01/08
Subject 7-5-0
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method
R Oct 01/09
Subject 7-5-1
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method - Pax
Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW512 000 kg - A380-800 Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW512 000 kg - A380-800 Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW562 000 kg - A380-800 Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW562 000 kg - A380-800 Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW571 000 kg - A380-800 Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW571 000 kg - A380-800 Models
Nov 01/08
L.E.C.Page 18
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CONTENT CHGCODE
LAST REVISIONDATE
Flexible Pavement Requirements - US Army Corps of EngineersDesign Method - Freighter
Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW592 000 kg - A380-800F Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW592 000 kg - A380-800F Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 4 Wheel Bogie - MRW602 000 kg - A380-800F Models
Nov 01/08
FIGURE Flexible Pavement Requirements -- 6 Wheel Bogie - MRW602 000 kg - A380-800F Models
Nov 01/08
Subject 7-6-0
General R Oct 01/09
Subject 7-6-1
Flexible Pavement Requirements - LCN Conversion - Pax Nov 01/08
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW512 000 kg - A380-800 Models
Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW512 000 kg - A380-800 Models
Nov 01/08
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW562 000 kg - A380-800 Models
Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW562 000 kg - A380-800 Models
Nov 01/08
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW571 000 kg - A380-800 Models
Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW571 000 kg - A380-800 Models
Nov 01/08
For A380-800F ModelsFlexible Pavement Requirements - LCNConversion - Freighter
Jun 01/07
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW592 000 kg - A380-800F Models
Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW592 000 kg - A380-800F Models
Nov 01/08
L.E.C.Page 19
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@A380AIRPLANE CHARACTERISTICS
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Flex Pavement Requirements LCN - 4 Wheel Bogie - MRW602 000 kg - A380-800F Models
Nov 01/08
FIGURE Flex Pavement Requirements LCN - 6 Wheel Bogie - MRW602 000 kg - A380-800F Models
Nov 01/08
Subject 7-7-0
Rigid Pavement Requirements - Portland Cement Association DesignMethod
R Oct 01/09
Subject 7-7-1
Rigid Pavement Requirements - Portland Cement Association DesignMethod - Pax
Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 512000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 512000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 562000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 562000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 571000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 571000 kg - A380-800 Models
Nov 01/08
Rigid Pavement Requirements - Portland Cement Association DesignMethod - Freighter
Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 592000 kg - A380-800F Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 592000 kg - A380-800F Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 4 Wheel Bogie - MRW 602000 kg - A380-800F Models
Nov 01/08
FIGURE Rigid Pavement Requirements - 6 Wheel Bogie - MRW 602000 kg - A380-800F Models
Nov 01/08
Subject 7-8-0
Rigid Pavement Requirements - LCN Conversion R Oct 01/09
L.E.C.Page 20
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CONTENT CHGCODE
LAST REVISIONDATE
Subject 7-8-1
Radius of Relative Stiffness Jun 01/07
FIGURE Radius of Relative Stiffness - Radius of Relative Stiffness Jun 01/07
Subject 7-8-2
Rigid Pavement Requirements - LCN Conversion - Pax Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW512 000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW512 000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW562 000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW562 000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW571 000 kg - A380-800 Models
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW571 000 kg - A380-800 Models
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
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW592 000 kg - A380-800F Models
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 4 Wheel Bogie - MRW602 000 kg - A380-800F Models
Nov 01/08
FIGURE Rigid Pavement Requirements LCN - 6 Wheel Bogie - MRW602 000 kg - A380-800F Models
Nov 01/08
Subject 7-8-3
Radius of Relative Stiffness (Other values of E and µ) R Oct 01/09
Subject 7-8-4
Radius of Relative Stiffness (Other values of E and µ) Nov 01/08
FIGURE Radius of Relative Stiffness - Radius of Relative Stiffness Jun 01/07
Subject 7-9-0
L.E.C.Page 21
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CONTENT CHGCODE
LAST REVISIONDATE
ACN/PCN Reporting System R Oct 01/09
Subject 7-9-1
Aircraft Classification Number - Flexible Pavement - Pax Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW512 000 kg - A380-800 Models
Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW562 000 kg - A380-800 Models
Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW571 000 kg - A380-800 Models
Nov 01/08
Aircraft Classification Number - Flexible Pavement - Freighter Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW592 000 kg - A380-800F Models
Nov 01/08
FIGURE Aircraft Classification Number - Flexible Pavement - MRW602 000 kg - A380-800F Models
Nov 01/08
Subject 7-9-2
Aircraft Classification Number - Rigid Pavement - Pax Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 512000 kg - A380-800 Models
Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 562000 kg - A380-800 Models
Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 571000 kg - A380-800 Models
Nov 01/08
Aircraft Classification Number - Rigid Pavement - Freighter Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 592000 kg - A380-800F Models
Nov 01/08
FIGURE Aircraft Classification Number - Rigid Pavement - MRW 602000 kg - A380-800F Models
Nov 01/08
CHAPTER 8
Subject 8-1-0
Possible Future Derivative Airplanes R Oct 01/09
CHAPTER 9
L.E.C.Page 22
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CONTENT CHGCODE
LAST REVISIONDATE
Subject 9-1-0
Scaled Drawing - 1 cm. = 500 cm. Jun 01/07
FIGURE Scaled Drawing -- 1 cm. = 500 cm. - A380-800 Models R Oct 01/09
FIGURE Scaled Drawing -- 1 cm. = 500 cm. - A380-800F Models R Oct 01/09
FIGURE Scaled Drawing -- 1 cm. = 500 cm. - A380-800 Models R Oct 01/09
FIGURE Scaled Drawing -- 1 cm. = 500 cm. - A380-800F Models R Oct 01/09
Subject 9-2-0
Scaled Drawing - 1 in. = 50 ft. R Oct 01/09
FIGURE Scaled Drawing -- 1 in. = 50 ft. - A380-800 Models R Oct 01/09
FIGURE Scaled Drawing -- 1 in. = 50 ft. - A380-800F Models R Oct 01/09
FIGURE Scaled Drawing -- 1 in. = 50 ft. - A380-800 Models R Oct 01/09
FIGURE Scaled Drawing -- 1 in. = 50 ft. - A380-800F Models R Oct 01/09
L.E.C.Page 23
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@A380AIRPLANE 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 View
2-4-1 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 Doors
2-7-3 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 Information
3-2-0 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)
T.O.C.Page 1
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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 Runway
4-5-4 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 Connections
5-4-1 Ground Service Connections Layout
5-4-2 Grounding Points
5-4-3 Hydraulic System
5-4-4 Electrical System
5-4-5 Oxygen System
T.O.C.Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
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
T.O.C.Page 3
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@A380AIRPLANE CHARACTERISTICS
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.
T.O.C.Page 4
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@A380AIRPLANE CHARACTERISTICS
SCOPE
1-1-0 Purpose
**ON A/C A380-800 Models A380-800F Models
Purpose
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.
1-1-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
CORRESPONDENCECorrespondence concerning this publication should be directed to :
AIRBUS S.A.S.Technical Data Support and Services1 Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
1-1-0Page 2
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@A380AIRPLANE CHARACTERISTICS
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.
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@A380AIRPLANE CHARACTERISTICS
CHAPTER 6 : OPERATING CONDITIONS
This chapter contains data and safety/environmental precautions related to engine and APUoperation 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.
1-2-0Page 2
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@A380AIRPLANE CHARACTERISTICS
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 Modulus
FAA 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 Weight
MTW 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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@A380AIRPLANE CHARACTERISTICS
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 footft/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 meterm/s meter per second
m2 square meter
m3 cubic meter
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@A380AIRPLANE CHARACTERISTICS
min minutemm millimeterMN/m3 MegaNewton per cubic meter
MPa MegaPascalnm 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 itemsare 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.
1-2-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
AIRPLANE DESCRIPTION
2-1-0 General Airplane Characteristics
**ON A/C A380-800 Models A380-800F Models
General Airplane Characteristics
1. General Airplane Characteristics
2-1-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
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 CharacteristicsWV000 WV001 WV002 WV003
Kilograms 562 000 512 000 571 000 571 000Maximum RampWeight (MRW) Pounds 1 238 998 1 128 766 1 258 839 1 258 839
Kilograms 560 000 510 000 569 000 510 000Maximum TakeoffWeight (MTOW) Pounds 1 234 588 1 124 357 1 254 430 1 124 357
Kilograms 386 000 394 000 391 000 395 000Maximum LandingWeight (MLW) Pounds 850 984 868 621 862 007 870 826
Kilograms 361 000 372 000 366 000 373 000Maximum Zero FuelWeight (MZFW) Pounds 795 869 820 119 806 892 822 324
Trent 970Engines
270 364 kg (596 050 lb)EstimatedOperating EmptyWeight (OEW) GP 7270
Engines270 630 kg (596 637 lb)
Kilograms 90 636 101 636 95 636 102 636EstimatedMaximum PayloadTrent 970 Pounds 199 818 224 069 210 841 226 274
Kilograms 90 370 101 370 95 370 102 370EstimatedMaximum PayloadGP 7270 Pounds 199 232 223 483 210 255 225 687
Standard SeatingCapacity <1> Three-Class 555
Liters 323 546US gallons 85 472
Kilograms(density =0.785 kg/l)
253 983
Usable FuelCapacity
Pounds 559 937Cubic meters 2100Pressurized Fuselage
Volume (A/C nonequipped, main andupper deck)
Cubic feet 74 161
Cubic meters 775PassengerCompartmentVolume (main deck) Cubic feet 27 369
2-1-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
Aircraft CharacteristicsCubic meters 530Passenger
CompartmentVolume (upperdeck)
Cubic feet 18 717
Cubic meters 12Cockpit Volume
Cubic feet 424Cubic meters 256Usable Cargo
CompartmentVolume <2>
Cubic feet 9040
<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 (Water volume) : 131 m3 (4626 ft3)- Lower deck aft cargo compartment (Water volume) : 107.8 m3 (3807 ft3)- Lower bulk cargo compartment (Water volume) : 17.2 m3 (607 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 OffWeight (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 FuelWeight (MZFW) pounds 886 258 886 258
kilograms 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 536 494 536 494
2-1-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
Aircraft Characteristicscubic 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 containerized volume) : 90 m3 (3 157 ft3)- lower deck aft cargo compartment (usable containerized 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)<2> Usable fuel capacity with center tank : 355 850 l (94 005 US gal)
2-1-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
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.
2-2-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
DB1A
0 4 8 12 16METERS
0 10 20 30 40 50FEET
NOTE: FOR DOORDIMENSIONS AND LOCATION,SEE CHAPTER 2−7.
68.854 m (225.90 ft)
29.598 m (97.11 ft)
7.142 m(23.43 ft)
30.372 m (99.65 ft)
79.750 m (261.65 ft)
12.456 m(40.87 ft)
33.578 m (110.16 ft) − WLG
36.854 m (120.91 ft) − BLG
5.264 m(17.27 ft)
51.400 m (168.64 ft)
4.972 m (16.31 ft)
29.943 m (98.23 ft)
22.228 m (72.92 ft)
72.727 m (238.61 ft)
70.400 m (230.97 ft)
8.410 m (27.60 ft)8.557 m (28.07 ft)
46.972 m (154.11 ft)
72.571 m (238.09 ft)
3.983 m(13.07 ft)
L_AC_020200_1_0010101_01_01
52.065 m (170.82 ft)
General Airplane Dimensions
2-2-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-3-0 Ground Clearances
**ON A/C A380-800 Models
Ground Clearances - Pax
1. This section gives ground clearances of A380-800 Models.
2-3-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**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
30.279.324.817.33.56.210.113.4
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
29.979.024.617.13.56.210.113.4
3.303.23
7.42
2.592.381.829.2024.178.225.941.302.273.264.31
4.2
10.810.6
24.336.135.98.57.86.0
30.279.3
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
30.980.127.319.8
7.510.714.2
5.125.12
9.2212.8212.824.414.273.6811.1426.1110.12
3.147.84
4.135.126.18
16.816.8
30.242.142.114.514.012.136.685.733.225.710.313.516.820.3
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
16.716.816.917.025.825.926.0
5.145.135.135.127.897.887.88
5.145.135.135.127.897.887.88
16.916.816.816.825.925.925.8
5.325.295.265.258.068.038.01
17.517.317.317.226.526.326.3
5.235.295.345.378.008.078.11
17.217.417.517.626.326.526.6
7.157.157.15
9.909.909.90
23.523.523.523.532.532.532.5
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
DE1E2F1F2F3GHJ1J2K1K2L2L3
1.05
3.053.14
7.1310.7610.842.352.271.669.21
24.187.555.27
1.903.084.10
C3 3.27
M2M3M4M5U1U2U3
5.095.135.165.187.857.907.92
L4L5L6M1
4.675.015.215.07
Ground ClearancesA380-800 Models
2-3-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Ground Clearances - Freighter
1. This section gives ground clearances of A380-800F models.
2-3-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
K2 K1
L2L3 L4 L5 L6 J2 J1
F3
D A1 C3
C1F1
E1 E2
G H
F2C2
C4
A5A6
A/CCONFIGURATION
MRWFWD CG
MRWAFT CG
OWEMID CG
m ft m ft m ft m ftA1
C1C2C3C4DE1E2F1F2F3GHJ1J2K1K2L2L3L4L5L6
m ft
10.2
5.4 5.4
A5A6
300tAFT CG
A/C JACKEDFDL = 7.3 m
(24.0 ft)
5.035.167.803.023.127.935.157.0910.7310.832.322.261.639.21
24.187.545.261.031.883.054.084.654.995.19
16.516.925.69.9
26.016.923.335.235.57.67.4
30.279.324.7
3.46.210.013.415.316.417.0
5.125.107.873.093.077.995.107.19
10.7910.782.382.221.649.08
24.057.485.201.051.883.054.064.634.965.16
16.816.725.810.110.126.216.723.635.435.47.87.3
29.878.924.517.13.56.210.013.315.216.316.9
5.345.248.083.303.228.195.257.4111.0010.922.592.371.819.19
24.168.215.931.292.263.254.304.935.335.60
17.517.226.510.810.626.917.224.336.135.88.57.85.930.179.326.919.44.27.410.714.116.217.518.4
5.215.417.993.213.368.125.387.2710.9211.072.512.491.859.48
24.458.376.081.282.303.304.375.025.435.71
17.117.726.210.511.026.617.723.835.836.38.28.26.131.180.227.520.04.27.510.814.316.517.818.7
7.257.2510.005.225.2210.127.259.3212.9212.924.514.373.7811.2426.2110.227.94
4.235.226.286.917.327.60
23.823.832.817.117.133.223.830.642.442.414.814.312.436.986.033.526.010.613.917.120.622.724.024.9
17.23.24
L_AC_020300_1_0030101_01_00
Ground clearancesA380-800F Models
2-3-0Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
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
2-4-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
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
2-4-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**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
2-4-1Page 2
Oct 01/09
@A380AIRPLANE 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
2-4-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Standard Configuration - Freighter
1. This section gives the standard configuration of A380-800F models.
2-4-1Page 4
Oct 01/09
@A380AIRPLANE 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
2-4-1Page 5
Oct 01/09
@A380AIRPLANE 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
2-5-0Page 1
Oct 01/09
@A380AIRPLANE 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.
2-5-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
UPPER DECKBUSINESS CLASS 6 ABREAST
UPPER DECKTOURIST 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
2-5-1Page 2
Oct 01/09
@A380AIRPLANE 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
2-5-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Typical Configuration - Freighter
1. This section gives the typical configuration of A380-800F models.
2-5-1Page 4
Oct 01/09
@A380AIRPLANE 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
2-5-1Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-6-0 Cargo Compartments
**ON A/C A380-800 Models A380-800F Models
Cargo Compartments
1. Cargo Compartments
2-6-0Page 1
Oct 01/09
@A380AIRPLANE 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.
2-6-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
FO
RW
AR
D A
FT
CA
RG
O
CO
MP
AR
TM
EN
T)
LOW
ER
DE
CK
FO
RW
AR
D C
AR
GO
CO
MP
AR
TM
EN
T
LOW
ER
DE
CK
FO
RW
AR
D A
FT
CA
RG
OC
OM
PA
RT
ME
NT
(T−
SH
AP
ED
LOW
ER
DE
CK
RE
AR
AF
T C
AR
GO
CO
MP
AR
TM
EN
T
LOW
ER
DE
CK
BU
LK C
AR
GO
CO
MP
AR
TM
EN
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)
FR
17F
R44
FR
57F
R90
FR
86F
R17
FR
44F
R57
FR
90F
R86
2.8 m
17.4 m(685.04 in)
L_AC_020601_1_0010101_01_00
Cargo CompartmentsLocation and Dimensions
2-6-1Page 2
Oct 01/09
@A380AIRPLANE 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.
2-6-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
LOW
ER
DE
CK
FO
RW
AR
D C
AR
GO
CO
MP
AR
TM
EN
T
LOW
ER
DE
CK
FO
RW
AR
D A
FT
CA
RG
OC
OM
PA
RT
ME
NT
(T−
SH
AP
ED
CO
MP
AR
TM
EN
T)
RE
AR
AF
T C
AR
GO
CO
MP
AR
TM
EN
T
LOW
ER
DE
CK
BU
LK C
AR
GO
CO
MP
AR
TM
EN
T
UP
PE
R D
EC
KC
AR
GO
CO
MP
AR
TM
EN
TM
AIN
DE
CK
CA
RG
O C
OM
PA
RT
ME
NT LO
WE
R D
EC
KA
FT
CA
RG
OC
OM
PA
RT
ME
NT
LOW
ER
DE
CK
FO
RW
AR
D C
AR
GO
CO
MP
AR
TM
EN
T
LOW
ER
DE
CK
FO
RW
AR
D A
FT
CA
RG
OC
OM
PA
RT
ME
NT
(T−
SH
AP
ED
CO
MP
AR
TM
EN
T)
LOW
ER
DE
CK
RE
AR
AF
T C
AR
GO
CO
MP
AR
TM
EN
T
LOW
ER
DE
CK
BU
LK C
AR
GO
CO
MP
AR
TM
EN
T
UP
PE
R D
EC
KC
AR
GO
CO
MP
AR
TM
EN
TM
AIN
DE
CK
CA
RG
O C
OM
PA
RT
ME
NT LO
WE
R D
EC
KA
FT
CA
RG
OC
OM
PA
RT
ME
NT
FR
95
FR
27F
R21
FR
17
FR
90
L_AC_020601_1_0020101_01_00
Cargo CompartmentsLocation and Dimensions (Sheet 1)
2-6-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
FR
17F
R44
/45
FR
72
UP
PE
R D
EC
K
LOW
ER
DE
CK
MA
IN D
EC
K
FR
95
FR
90F
R86
FR
27F
R95
FR
57
UP
PE
R D
EC
K
LOW
ER
DE
CK
FR
21F
R95
FR
94
3.7 m(145.7 in)
43.2 m(1700.79 in)
4.3 m(170 in)
47.2 m(1858.27 in)
3.1 m(122.8 in) 17.4 m
(685.04 in)
2.8 m(110.2 in)
8.2 m(322.8 in)
9.7 m(381.9 in)
1.1 m(43.3 in)
2.8 m(110.2 in)
L_AC_020601_1_0030101_01_00
Cargo CompartmentsLocation and Dimensions (Sheet 2)
2-6-1Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-6-2 Loading Combinations
**ON A/C A380-800 Models
Loading Combinations - Pax
1. This section gives cargo compartments loading combinations.
2-6-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
ST
AN
DA
RD
: 20
LD−
3 O
R 7
PA
LLE
TS
88
in /
96 in
X 1
25 in
OP
TIO
N: 2
2 LD
−3
OR
7 P
ALL
ET
S 8
8 in
/ 96
in X
125
inS
TA
ND
AR
D: 1
6 LD
−3
OR
6 L
D−
3 3
PA
LLE
TS
88
in /
96 in
X 1
25 in
OP
TIO
N: 6
PA
LLE
TS
88
in /
96 in
X 1
25 in
L_AC_020602_1_0010101_01_00
Cargo CompartmentsLoading Combinations
2-6-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Loading Combinations - Freighter
1. This section gives cargo compartments loading combinations.
2-6-2Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
MA
IN D
EC
K L
OA
DIN
G 2
9 U
LD’S
LOW
ER
DE
CK
LO
AD
ING
36
LD−
3 O
R 6
LD
−3
+ 1
0 P
ALL
ET
S 8
8 in
OR
96
in X
125
in
UP
PE
R D
EC
K L
OA
DIN
G 2
5 U
DL’
S (
CO
NT
OU
RE
D P
ALL
ET
S)
L_AC_020602_1_0020101_01_00
Cargo CompartmentsLoading Combinations (Sheet 1)
2-6-2Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
UP
PE
R D
EC
K L
OA
DIN
G 5
3 A
YY
MA
IN D
EC
K L
OA
DIN
G 3
3 A
MJ
UP
PE
R D
EC
K L
OA
DIN
G 5
3 A
YY
MA
IN D
EC
K L
OA
DIN
G 3
3 A
MJ
L_AC_020602_1_0030101_01_00
Cargo CompartmentsLoading Combinations (Sheet 2)
2-6-2Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-7-0 Door Clearances
**ON A/C A380-800 Models
Door Clearances - Pax
1. This section gives Door Clearances.
2-7-0Page 1
Oct 01/09
@A380AIRPLANE 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
2-7-0Page 2
Oct 01/09
@A380AIRPLANE 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
2-7-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Door Clearances - Freighter
1. This section gives door clearances.
2-7-0Page 4
Oct 01/09
@A380AIRPLANE 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
2-7-0Page 5
Oct 01/09
@A380AIRPLANE 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
2-7-0Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-7-1 Forward Doors
**ON A/C A380-800 Models A380-800F Models
Forward Doors
1. This section gives forward doors clearances.
2-7-1Page 1
Oct 01/09
@A380AIRPLANE 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)
01NOTE:
FREE AISLE
01
01
L_AC_020701_1_0010101_01_00
Door ClearancesForward Doors
2-7-1Page 2
Oct 01/09
@A380AIRPLANE 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.
2-7-2Page 1
Oct 01/09
@A380AIRPLANE 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
01NOTE:
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
2-7-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Upper Deck Door - Freighter
1. This section gives upper deck door clearances.
2-7-2Page 3
Oct 01/09
@A380AIRPLANE 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
2-7-2Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-7-3 Aft Doors
**ON A/C A380-800 Models
Aft Doors - Pax
1. This section gives aft doors clearances.
2-7-3Page 1
Oct 01/09
@A380AIRPLANE 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 OFTHE SCUFF PLATE AND THE MOSTEXTERNAL POINT OF THE DOOR SKIN
01NOTE:
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
2-7-3Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aft Doors - Freighter
1. This section gives aft doors clearances.
2-7-3Page 3
Oct 01/09
@A380AIRPLANE 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 OFTHE SCUFF PLATE AND THE MOSTEXTERNAL POINT OF THE DOOR SKIN
01NOTE:
MAIN DECK DOORM5L
FREE AISLE 01
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
2-7-3Page 4
Oct 01/09
@A380AIRPLANE 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.
2-7-4Page 1
Oct 01/09
@A380AIRPLANE 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 FR81A2945 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
2-7-4Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aft Cargo Compartment Doors - Freighter
1. This section gives aft cargo compartment doors clearances.
2-7-4Page 3
Oct 01/09
@A380AIRPLANE 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
2-7-4Page 4
Oct 01/09
@A380AIRPLANE 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 FR81A2945 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
2-7-4Page 5
Oct 01/09
@A380AIRPLANE 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.
2-7-5Page 1
Oct 01/09
@A380AIRPLANE 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
2-7-5Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Forward Cargo Compartment Doors - Freighter
1. This section gives forward cargo compartment doors clearances.
2-7-5Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
A−A
SEECHAPTER
2−3
3237 mm(127 in)
2478 mm(97.6 in)
2184 mm(85.98 in)
4748 mm(186.93 in)
3796 mm(149 in)
FWDA
A
L_AC_020705_1_0020101_01_01
Door ClearancesUpper Deck Cargo Door - A380-800F Models
2-7-5Page 4
Oct 01/09
@A380AIRPLANE 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
2-7-5Page 5
Oct 01/09
@A380AIRPLANE 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.
2-7-6Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
AIR
CR
AF
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
2-7-6Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
0.75 m (2.46 ft)
A
A
AIR
CR
AF
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
2-7-6Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-7-7 Wing Landing Gear Doors
**ON A/C A380-800 Models A380-800F Models
Wing Landing Gear Doors
1. This section gives wing landing gear doors clearances.
2-7-7Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND LINE
AIR
CR
AF
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
2-7-7Page 2
Oct 01/09
@A380AIRPLANE 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.
2-7-8Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND LINE
AIR
CR
AF
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)
2-7-8Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND LINE
AIR
CR
AF
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)
2-7-8Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
2-7-9 APU Doors
**ON A/C A380-800 Models A380-800F Models
APU Doors
1. This section gives APU doors clearances.
2-7-9Page 1
Oct 01/09
@A380AIRPLANE 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
2-7-9Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
AIRPLANE PERFORMANCE
3-1-0 General Information
**ON A/C A380-800 Models A380-800F Models
General 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
3-1-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
3-2-0 Payload / Range
**ON A/C A380-800 Models A380-800F Models
Payload /Range
1. Payload / Range
3-2-0Page 1
Oct 01/09
@A380AIRPLANE 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.
3-2-1Page 1
Oct 01/09
@A380AIRPLANE 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)
PA
YLO
AD
(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.
100
120
PA
YLO
AD
(x
1000
lb)
200 nm DIVERSION5% TRIP FUEL ALLOWANCE, 30 min HOLDING
L_AC_030201_1_0010101_01_00
Payload/RangeISA Conditions - TRENT 900 Engines
3-2-1Page 2
Oct 01/09
@A380AIRPLANE 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)
PA
YLO
AD
(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.
PA
YLO
AD
(x
1000
lb)
200 nm DIVERSION5% TRIP FUEL ALLOWANCE, 30 min HOLDING
L_AC_030201_1_0080101_01_00
Payload/RangeISA Conditions - GP 7200 Engines
3-2-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Payload/Range - Freighter
1. This section gives the payload/range at ISA conditions.
3-2-1Page 4
Oct 01/09
@A380AIRPLANE 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)
PA
YLO
AD
(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.
PA
YLO
AD
(x
1000
lb)
200 nm DIVERSION5% TRIP FUEL ALLOWANCE, 30 min HOLDING
L_AC_030201_1_0060101_01_00
Payload/RangeISA Conditions - TRENT 900 Engines
3-2-1Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
RANGE (km)
PA
YLO
AD
(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
3507400 8400 9400 10400 11400 12400 13400 14400 15400 16400 17400 18400 19400
MAXIMUM STRUCTURAL PAYLOAD
TYPICAL INTERNATIONAL FLIGHT PROFILE
PA
YLO
AD
(x
1000
lb)
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
3-2-1Page 6
Oct 01/09
@A380AIRPLANE 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
3-3-0Page 1
Oct 01/09
@A380AIRPLANE 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.
3-3-1Page 1
Oct 01/09
@A380AIRPLANE 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)
TA
KE
−O
FF
WE
IGH
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
TA
KE
−O
FF
WE
IGH
T (
x 10
00 lb
)
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0010101_01_00
Take-Off Weight LimitationISA Conditions - TRENT 900 Engines
3-3-1Page 2
Oct 01/09
@A380AIRPLANE 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)
TAK
E−O
FF W
EIG
HT
(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
TA
KE
−OF
F W
EIG
HT
(x
1000
lb)AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0080101_01_00
Take-Off Weight LimitationISA Conditions - GP 7200 Engines
3-3-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Take-Off Weight Limitation - Freighter
1. This section gives the take-off weight limitation at ISA conditions.
3-3-1Page 4
Oct 01/09
@A380AIRPLANE 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)
TA
KE
−O
FF
WE
IGH
T (
t)
02000
6000
4000
8000
TA
KE
−O
FF
WE
IGH
T (
x 10
00 lb
)
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0060101_01_00
Take-Off Weight LimitationISA Conditions - TRENT 900 Engines
3-3-1Page 5
Oct 01/09
@A380AIRPLANE 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)
TA
KE
−O
FF
WE
IGH
T (
t)
0 2000
6000
4000
8000
TA
KE
−O
FF
WE
IGH
T (
x 10
00 lb
)
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030301_1_0090101_01_00
Take-Off Weight LimitationISA Conditions - GP 7200 Engines
3-3-1Page 6
Oct 01/09
@A380AIRPLANE 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.
3-3-2Page 1
Oct 01/09
@A380AIRPLANE 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)
TA
KE
−O
FF
WE
IGH
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
TA
KE
−O
FF
WE
IGH
T (
x 10
00 lb
)AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030302_1_0010101_01_00
Take-Off Weight LimitationISA + 15 ˚C (59 ˚F) - TRENT 900 Engines
3-3-2Page 2
Oct 01/09
@A380AIRPLANE 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)
TA
KE
−O
FF
WE
IGH
T (
t)
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
TA
KE
−O
FF
WE
IGH
T (
x 10
00 lb
)300
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030302_1_0080101_01_00
Take-Off Weight LimitationISA + 15 ˚C (59 ˚F) - GP 7200 Engines
3-3-2Page 3
Oct 01/09
@A380AIRPLANE 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.
3-3-2Page 4
Oct 01/09
@A380AIRPLANE 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)
TA
KE
−O
FF
WE
IGH
T (
t)
02000
6000
4000
8000
AIRFIELD PRESSURE ALTITUDE (ft)
TA
KE
−O
FF
WE
IGH
T (
x 10
00 lb
)
L_AC_030302_1_0060101_01_00
Take-Off Weight LimitationISA + 15 ˚C (59 ˚F) - TRENT 900 Engines
3-3-2Page 5
Oct 01/09
@A380AIRPLANE 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)
TA
KE
−O
FF
WE
IGH
T (
t)
02000
6000
4000
8000
TA
KE
−O
FF
WE
IGH
T (
x 10
00 lb
)
AIRFIELD PRESSURE ALTITUDE (ft)
L_AC_030302_1_0090101_01_00
Take-Off Weight LimitationISA + 15 ˚C (59 ˚F) - GP 7200 Engines
3-3-2Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
3-4-0 Landing Field Length
**ON A/C A380-800 Models A380-800F Models
Landing Field Length
1. Landing Field Length
3-4-0Page 1
Oct 01/09
@A380AIRPLANE 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.
3-4-1Page 1
Oct 01/09
@A380AIRPLANE 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
LAN
DIN
G F
IELD
LE
NG
TH
(ft)
LAN
DIN
G F
IELD
LE
NG
TH
(m
)
GROSS WEIGHT (x 1000 lb)
L_AC_030401_1_0010101_01_01
Landing Field LengthLanding Field Length - A380-800 Models
3-4-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Landing Field Length - Freighter
1. This section gives the landing field length.
3-4-1Page 3
Oct 01/09
@A380AIRPLANE 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
LAN
DIN
G F
IELD
LE
NG
TH
(m
)
LAN
DIN
G F
IELD
LE
NG
TH
(ft)
GROSS WEIGHT (x 1000 lb)
AIRFIELD ELEVATION (ft)
L_AC_030401_1_0030101_01_00
Landing Field LengthLanding Field Length - A380-800F Models
3-4-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
3-5-0 Final Approach Speed
**ON A/C A380-800 Models A380-800F Models
Final Approach Speed
1. Final Approach Speed
3-5-0Page 1
Oct 01/09
@A380AIRPLANE 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.
3-5-1Page 1
Oct 01/09
@A380AIRPLANE 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)
FIN
AL
AP
PR
OA
CH
SP
EE
D (
Vre
f kt C
AS
)
160
VALID FOR ALL TEMPERATURES
L_AC_030501_1_0010101_01_00
Final Approach Speed (CG=29%)A380-800 Models
3-5-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Final Approach Speed - Freighter
1. This section gives the final approach speed.
3-5-1Page 3
Oct 01/09
@A380AIRPLANE 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)
FIN
AL
AP
PR
OA
CH
SP
EE
D (
Vre
f kt C
AS
)
160
VALID FOR ALL TEMPERATURES
L_AC_030501_1_0030101_01_00
Final Approach Speed (CG=29%)A380-800F Models
3-5-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
GROUND MANEUVERING
4-1-0 General Information
**ON A/C A380-800 Models A380-800F Models
General
1. This section provides airplane turning capability and maneuvering characteristics.
For ease of presentation, this data has been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provides for a normal allowance for tire slippage. As such,it reflects the turning capability of the aircraft in favorable operating circumstances. This data shouldonly be used as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft type.
In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems. Airlineoperating techniques will vary in the level of performance, over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea or high risk of jet blast damage. For these reasons, ground maneuvering requirements should becoordinated with the using airlines prior to layout planning.
4-1-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
4-2-0 Turning Radii
**ON A/C A380-800 Models A380-800F Models
Turning Radii
1. This section gives the turning radii.
4-2-0Page 1
Oct 01/09
@A380AIRPLANE 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)
4-2-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
2 100.16328.6
TYPEOF
TURN
20
STEERINGANGLE
17.9
EFFECTIVESTEERING
ANGLE
mft
135.45444.4
101.01331.4
115.87380.1
2 78.86258.7
25 22.7 mft
113.14371.2
80.12262.9
94.90311.4
2 65.69215.5
30 27.5 mft
98.90324.5
67.33220.9
81.91268.7
2 56.84186.5
35 32.1 mft
88.97291.9
58.83193.0
73.13239.9
2 50.59166.0
40 36.6 mft
81.61267.8
52.89173.5
66.84219.3
2 46.02151.0
45 41.0 mft
75.94249.1
48.61159.5
62.16203.9
2 42.61139.8
50 45.1 mft
71.43234.4
45.45149.1
58.57192.2
1 40.13131.6
55 51.2 mft
67.02219.9
43.22141.8
55.43181.9
1 37.64123.5
60 57.3 mft
62.60205.4
40.98134.5
52.29171.5
1 35.15115.3
65 63.4 mft
58.18190.9
38.75127.1
49.15161.2
1 32.66107.2
70 69.5 mft
53.76176.4
36.52119.8
46.01150.9
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)
4-2-0Page 3
Oct 01/09
@A380AIRPLANE 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.
4-3-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
R4
R3
R5
Y
R6
(TU
RN
ING
WID
TH
)
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
4-3-0Page 2
Oct 01/09
@A380AIRPLANE 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.
4-4-0Page 1
Oct 01/09
@A380AIRPLANE 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
4-4-0Page 2
Oct 01/09
@A380AIRPLANE 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
4-5-0Page 1
Oct 01/09
@A380AIRPLANE 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.
4-5-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
NLG PATH
COCKPIT TRACKPARALLEL TOGUIDE LINE
NOMINAL OFFSET
TAXIWAY GUIDELINEWLG 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)
4-5-1Page 2
Oct 01/09
@A380AIRPLANE 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)
4-5-1Page 3
Oct 01/09
@A380AIRPLANE 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.
4-5-2Page 1
Oct 01/09
@A380AIRPLANE 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)
4-5-2Page 2
Oct 01/09
@A380AIRPLANE 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)
4-5-2Page 3
Oct 01/09
@A380AIRPLANE 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.
4-5-3Page 1
Oct 01/09
@A380AIRPLANE 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 BRAKINGON A 60.0 m (196.9 ft) WIDE RUNWAY.
L_AC_040503_1_0010101_01_00
180˚ Turn on a Runway
4-5-3Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
4-5-4 90˚ Turn - Taxiway to Taxiway
**ON A/C A380-800 Models A380-800F Models
90˚ Turn - Taxiway to Taxiway
1. This section gives the 90˚ turn - taxiway to taxiway.
4-5-4Page 1
Oct 01/09
@A380AIRPLANE 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)
4-5-4Page 2
Oct 01/09
@A380AIRPLANE 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)
4-5-4Page 3
Oct 01/09
@A380AIRPLANE 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.
4-5-5Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
NOTE:
NLG PATH
COCKPIT TRACKPARALLEL TOGUIDELINE
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)
4-5-5Page 2
Oct 01/09
@A380AIRPLANE 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)
4-5-5Page 3
Oct 01/09
@A380AIRPLANE 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).
4-6-0Page 1
Oct 01/09
@A380AIRPLANE 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)
4-6-0Page 2
Oct 01/09
@A380AIRPLANE 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
4-7-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
PARKING45° ENTRY PUSH OUT
70.3
1 m
(23
0.7
ft)77
.07
m (
252.
9 ft)
80.81 m (265.1 ft)
PARKINGSTRAIGHT ENTRY PUSH BACK
94.64 m (310.5 ft)
L_AC_040700_1_0010101_01_00
Airplane ParkingSteering Geometry
4-7-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
0 10 20 30 40 50 60 70 80 90 100 110 120
10
20
30
40
50
60
70
80
90
100
0
20
40
60
80
100
120
140
160
180
200
220
240
260
280
300
0 20 40 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340 360
45° ENTRY PUSH OUT
DISTANCEOUT
FROM TERMINAL
DISTANCE ALONG TERMINAL (m)
DISTANCE ALONG TERMINAL (ft)
(m)(ft)
STRAIGHT ENTRY PUSH BACK
L_AC_040700_1_0020101_01_00
Airplane ParkingMinimum Parking Space Requirements
4-7-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
4-8-0 Airplane Mooring
**ON A/C A380-800 Models A380-800F Models
General
1. This section provides information on airplane mooring.
4-8-0Page 1
Oct 01/09
@A380AIRPLANE 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
4-8-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
TERMINAL SERVICING
5-1-0 Airplane Servicing Arrangements
**ON A/C A380-800 Models A380-800F Models
Airplane 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.
5-1-0Page 1
Oct 01/09
@A380AIRPLANE 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.
5-1-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
0 5 10METERS
0 16 32FEET
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 UNITAIR: AIR START UNIT LV: LAVATORY VEHICLECAT: CATERING VEHICLECLEAN: CLEANING VEHICLE TOW: TOWING TRACTOR
WV: POTABLE WATER VEHICLECONVEYOR: CONVEYOR BELTFUEL: FUEL HYDRANT DISPENSER
PL: PALLET/CONTAINER LOADER
− WIDTH: 87.50 m (287 ft)− LENGTH: 80.20 m (263 ft)
FUEL
FUEL
G.P
.U
G.P
.U
TOW
CLE
AN
CA
T
PL
PL
CO
NV
EY
OR
WV
CLE
AN
CA
T
AIR
AC
LV
CA
T
UD
CA
T
UDCAT: UPPER DECK CATERING VEHICLE
L_AC_050101_1_0010101_01_00
Baseline Ramp Layout -- Two BridgesServicing Via Main and Upper Decks
5-1-1Page 2
Oct 01/09
@A380AIRPLANE 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.
5-1-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
RL01/B1A/800/STD
FUEL
FUEL
G.P
.U
G.P
.U
TOW
CLE
AN
CA
T
PL
PL
CO
NV
EY
OR
WV
CLE
AN
CA
T
AIR
AC
0 5 10METERS
0 16 32FEET
CA
T
LV
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 UNITAIR: AIR START UNIT LV: LAVATORY VEHICLECAT: CATERING VEHICLECLEAN: CLEANING VEHICLE TOW: TOWING TRACTOR
WV: POTABLE WATER VEHICLECONVEYOR: CONVEYOR BELTFUEL: FUEL HYDRANT DISPENSER
PL: PALLET/CONTAINER LOADER
− WIDTH: 87.50 m (287 ft)− LENGTH: 80.20 m (263 ft)
CA
T
L_AC_050102_1_0010101_01_00
Typical Ramp Layout -- Two BridgesServicing Via Main Deck
5-1-2Page 2
Oct 01/09
@A380AIRPLANE 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.
5-1-3Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_050103_0_AAM0_01_04
BA
SE
LIN
E
HIG
H
VE
RY
HIG
H
BA
SE
LIN
E
SC
EN
AR
IOS
PR
OD
UC
T &
SE
RV
ICE
DIF
FE
RE
NT
IAT
ION
TU
RN
−R
OU
ND
TIM
E(T
RT
)
OP
PO
RT
UN
ITIE
S O
F D
IRE
CT
UP
PE
R D
EC
K (
UD
) A
CC
ES
SF
OR
AIR
PO
RT
S &
AIR
LIN
ES
M2
U1
U1
M1
M2
BE
NE
FIT
S R
EA
LIS
ED
DE
PE
ND
LA
RG
ELY
ON
CA
BIN
LA
YO
UT
& B
OA
RD
ING
PR
OC
ED
UR
ES
SIM
ILA
R T
O B
AS
ELI
NE
MD
AC
CE
SS
M1
M2
SIM
ILA
R T
O B
AS
ELI
NE
MD
AC
CE
SS
L_AC_050103_1_0010101_01_00
Opportunities of Direct Upper Deck Accessfor Airport and Airlines
5-1-3Page 2
Oct 01/09
@A380AIRPLANE 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.
5-1-4Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
FUEL
FUEL
G.P
.UG
.P.U
TOW
PL
PL
CO
NV
EY
OR
0 5 10METERS
0 16 32FEET
LV
RL04/B1/800F/STD
PL PL
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 UNITLV: LAVATORY VEHICLE
TOW: TOWING TRACTORWV: POTABLE WATER VEHICLE
CONVEYOR: CONVEYOR BELTFUEL: FUEL HYDRANT DISPENSER
PS: PASSENGER STAIRS
AIR
PL: PALLET/CONTAINER LOADER
− WIDTH: 87.50 m (287 ft)− LENGTH: 80.20 m (263 ft)
PS P
S
WV
L_AC_050104_1_0010101_01_00
Baseline Ramp Layout
5-1-4Page 2
Oct 01/09
@A380AIRPLANE 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 :
5-2-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
(1) dedicated door-galley = 1.5 min/FSTE
(2) cart circulation (1 seat zone) = + 0.5 min/FSTE
(3) cart circulation (> 1 seat zone) = + 1.0 min/FSTE
(4) via lift :- dedicated door to single lift = 2.0 min/FSTE
F. GROUND HANDLING/SERVICING
- start of operations :
(1) bridges = t0 = 0
(2) others = t0 + 1 min- vehicle positioning/removal = 2 min (fuel truck excluded)- upper deck vehicle positioning/removal = 3 min- clearance between GSE = 0.5 m (20 in)- Ground Power Unit (GPU) = up to 4 × 90 kVA- air conditioning = two carts- potable water (standard/option) = 1 700/2 500 liters (495/660 US gal) at 60 l/min
(23 US gal/min).- waste water = discharge and rinsing- dollies per tractor = 4 to 6
5-2-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
5-2-1 Typical Turn-Round Time - Two Bridges - Standard Servicing Via Main Deck and Upper Deck
**ON A/C A380-800 Models
Typical Turn-Round Time - Two Bridges - Standard Servicing Via Main Deck and Upper Decks
1. Typical Turn-Round Time - Two Bridges - Servicing via Main Deck and Upper Decks
5-2-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
BRIDGES
DEBOARDING/BOARDING&LPS
LD−3 CARGO FWD
LD−3 CARGO AFT
FREIGHT
BULK
CLEANING
POTABLE WATER
WASTE WATER
REFUELLING
DB1A
CATERING AT M2R
CATERING AT M4R
CATERING AT M1R
CATERING AT M5R
CATERING AT U1R
CATERING AT U3L
0 10 20 30 40 50 60 70 80 90
TURN−ROUND TIME IN MINUTES
2
14 422
3731
22
0 0
18 21
30
21
20
48
CRITICAL PATH
90’
2
27
36
EQUIPMENTPOSITIONING / REMOVAL
0 10 20 30 40 50 60 70 80 90
32
36
20
L_AC_050201_1_0020101_01_00
Typical Turn-Round Time -- Two BridgesServicing Via Main and Upper Decks
5-2-1Page 2
Oct 01/09
@A380AIRPLANE 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
5-2-2Page 1
Oct 01/09
@A380AIRPLANE 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
5-2-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
5-3-0 Terminal Operation - Cargo Aircraft
**ON A/C A380-800F Models
Terminal Operation - Cargo Aircraft
1. Terminal Operation - Cargo Aircraft
5-3-0Page 1
Oct 01/09
@A380AIRPLANE 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.
5-3-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
5-4-0 Ground Service Connections
**ON A/C A380-800 Models A380-800F Models
Ground Service Connections
1. Ground Service Connections
5-4-0Page 1
Oct 01/09
@A380AIRPLANE 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.
5-4-1Page 1
Oct 01/09
@A380AIRPLANE 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 PANEL6 − 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
7 115
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
5-4-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Ground Service Connections Layout - Freighter
1. This section gives the ground service connections layout.
5-4-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F 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 PANEL6 − GROUND ELECTRICAL POWER7 − LOW PRESSURE PRECONDITIONED AIR
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
DB1A
5 4 3 4 3 11
7 11
8
6
12
13
2
94
3
4
3
1
14
10
13
4
3
4
L_AC_050401_1_0030101_01_00
Ground Service ConnectionsGround Service Connections Layout - A380-800F Models
5-4-1Page 4
Oct 01/09
@A380AIRPLANE 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.
5-4-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
A
GROUNDPOINT
L_AC_050402_1_0010101_01_00
Ground Points NLG
5-4-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND POINT A
A
L_AC_050402_1_0020101_01_00
Ground Point WLG
5-4-2Page 3
Oct 01/09
@A380AIRPLANE 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
5-4-2Page 4
Oct 01/09
@A380AIRPLANE 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
MEANHEIGHTFROM
GROUND-- 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.
5-4-3Page 1
Oct 01/09
@A380AIRPLANE 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
5-4-3Page 2
Oct 01/09
@A380AIRPLANE 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
5-4-3Page 3
Oct 01/09
@A380AIRPLANE 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
MEANHEIGHTFROM
GROUND-- 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
5-4-4Page 1
Oct 01/09
@A380AIRPLANE 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
5-4-4Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Electrical System - Freighter
1. Electrical System
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF
NOSE R SIDE L SIDE
MEANHEIGHTFROM
GROUND-- access door : TBD 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
5-4-4Page 3
Oct 01/09
@A380AIRPLANE 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
5-4-4Page 4
Oct 01/09
@A380AIRPLANE 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
5-4-5Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
AL_AC_050405_1_0010101_01_00
Ground Service ConnectionsOxygen System
5-4-5Page 2
Oct 01/09
@A380AIRPLANE 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
MEANHEIGHTFROM
GROUND
-- Refuel/Defuel control panel : (Accessdoor 199KB)
48 (159.48) 0.68 (2.23) 1.98 (6.50)
2. Refuel/Defuel Connectors
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
-- 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)
5-4-6Page 1
Oct 01/09
@A380AIRPLANE 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
AUTOREFUEL
OFF
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
5-4-6Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
REFUEL PRESSURE
REFUEL / DEFUEL COUPLINGS
Z500
Z600 ALH SIDE SHOWN
RH SIDE SYMETRICAL
B
B
A
A
L_AC_050406_1_0020101_01_00
Ground Service ConnectionsPressure Refuel Connections
5-4-6Page 3
Oct 01/09
@A380AIRPLANE 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 doors191HB
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 CERNTERLINEAFT OF NOSE R SIDE L SIDE MEAN HEIGHT
FROM GROUND-- access doors193BB
25.37 (83.23) 0.2 (0.66) 1.78 (5.84)
A. Connectors :
(1) Three standard MS33740 (ISO2026), 3 in.
5-4-7Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
LOW PRESSURE AIR CONNECTOR
Z190
BB
B
BA
A
B
L_AC_050407_1_0010101_01_00
Ground Service ConnectionsLow Pressure Preconditioned Air
5-4-7Page 2
Oct 01/09
@A380AIRPLANE 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
5-4-7Page 3
Oct 01/09
@A380AIRPLANE 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)
5-4-8Page 1
Oct 01/09
@A380AIRPLANE 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
5-4-8Page 2
Oct 01/09
@A380AIRPLANE 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
5-4-8Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Potable Water System - Freighter
1. Potable Water System
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER 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)
5-4-8Page 4
Oct 01/09
@A380AIRPLANE 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
5-4-8Page 5
Oct 01/09
@A380AIRPLANE 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) 24.98 (81.96)16.61
(54.49)3.08 (10.10)
-- Engine 4 (access door 446BR) 32.65 (107.12)27.45
(90.05)4.24 (13.91)
2. Engine Oil Servicing (GP7200 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
-- Engine 1 (access door 415CL) 33.03 (108.37) 27.42 (89.96) 4.4 (14.44)
-- Engine 2 (access door 425CL) 25.35 (83.17) 16.62 (54.53) 3.13 (10.27)
-- Engine 3 (access door 435CL) 25.35 (83.17) 12.78 (41.93) 3.13 (10.27)
-- Engine 4 (access door 445CL) 33.03 (108.37) 23.62 (77.49) 4.4 (14.44)
5-4-9Page 1
Oct 01/09
@A380AIRPLANE 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
5-4-9Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
PW
VE
−002
36 (1
007)
"T" HANDLE
OIL TANKFILLER CAP
OIL TANKSIGHT GAGE
PINENGAGEMENT
A
B
BFWD
A
L_AC_050409_1_0100101_01_01
Ground Service ConnectionsEngine Oil Servicing - GP 7200 Engines
5-4-9Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
VFG Oil Servicing
1. VFG oil servicing (TRENT900 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER 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
MEANHEIGHTFROM
GROUND-- Engine 1 34.49 (113.16) 25.43 (83.43) 2.63 (8.63)
-- Engine 2 26.81 (87.96) 14.63 (48.00) 1.36 (4.46)
-- Engine 3 26.81 (87.96) 14.63 (48.00) 1.36 (4.46)
-- Engine 4 34.49 (113.16) 25.43 (83.43) 2.63 (8.63)
For VFG (GP7200 Engines), open:- Fan Exhaust Cowl (engine 1 - 4)- Thrust Reverser Cowl (engine 2 -3)
5-4-9Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
1
B
8
7
DISCONNECT WHEN ONLY DROPS 4
2
65
3
COME OUT SLOWLY
OIL LEVEL
A
B
L_AC_050409_1_0110101_01_01
Ground Service ConnectionsVFG Oil Servicing - TRENT 900 Engines
5-4-9Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
OIL LEVEL
DISCONNECT WHEN ONLY DROPSCOME OUT SLOWLY
2
3
4
7
8
6
C
1
C
CASE DRAINPLUG
A
5
B
B
L_AC_050409_1_0120101_01_01
Ground Service ConnectionsVFG Oil Servicing - GP 7200 Engines
5-4-9Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
Starter Oil Servicing
1. Starter Oil Servicing (TRENT900 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
-- Engine 1 39.78 (130.51)25.78
(84.57)2.59 (8.49)
-- Engine 2 32.15 (105.49)14.94
(49.01)1.39 (4.56)
-- Engine 3 32.15 (105.49)14.42
(47.30)1.39 (4.56)
-- Engine 4 39.78 (130.51)25.25
(82.84)2.59 (8.49)
2. Starter Oil Servicing (GP7200 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND-- Engine 1 40.42 (132.61) 27.34 (89.70) 3.35 (10.99)
-- Engine 2 32.74 (107.41) 16.55 (54.30) 2.47 (8.10)
-- Engine 3 32.74 (107.41) 12.71 (41.70) 2.47 (8.10)
-- Engine 4 40.42 (132.61) 23.53 (77.20) 3.35 (10.99)
For access to Starter Oil Servicing, open Fan Cowl
5-4-9Page 7
Oct 01/09
@A380AIRPLANE 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
5-4-9Page 8
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
PW
VE
−005
49 (
0308
)
PNEUMATIC STARTER
MAGNETICCHIP
DETECTOR
STARTER CONTROL VALVE
V−BANDCLAMP
AND QADADAPTER
FILLPORT
5000ES 4005KS
A
A
L_AC_050409_1_0140101_01_01
Ground Service ConnectionsStarter Oil Servicing - GP 7200 Engines
5-4-9Page 9
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
APU Oil Servicing
1. APU Oil
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND-- access doors : 315AL, 315AR 67.55 (221.62) 0.44 (1.44) 6.83 (22.40)
A. Capacity :
(1) 18.13L (4.35 USgal)
5-4-9Page 10
Oct 01/09
@A380AIRPLANE 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
5-4-9Page 11
Oct 01/09
@A380AIRPLANE 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
MEANHEIGHTFROM
GROUND-- 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
5-4-10Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
WASTE TANK DRAIN VALVEOPEN
UPPERDECK
MAINDECK
RH LH RH LH
CLOSE
CONTROLLEVER
CONNECTIONWASTE DRAIN
FILL AND RINSECONNECTION
FWDB
Z160
FR86FR91A
A
B
L_AC_050410_1_0010101_01_00
Ground Service ConnectionsVacuum Toilet System - A380-800 Models
5-4-10Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Vacuum Toilet System - Freighter
1. Waste Water System
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM GROUND
-- access door TBD 11.11 (36.45) 2.48 (8.14 ft) 3.51 (11.52)
A. Connectors :
(1) flushing and filling : 1 in.
(2) draining : 4 in.
B. Capacity : 80 l
C. Operating pressure for the waste tank rinsing process: 50 psi (max 125 psi)
D. Flow rate : 40 l/min
5-4-10Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Z130 A
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
5-4-10Page 4
Oct 01/09
@A380AIRPLANE 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
5-5-0Page 1
Oct 01/09
@A380AIRPLANE 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).
5-5-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
RR −40° 3 CONNECTIONS SEA LEVEL
T = 85°C
T = 255°C T = 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
5-5-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-1Page 5
Oct 01/09
@A380AIRPLANE 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)
5-5-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-2Page 2
Oct 01/09
@A380AIRPLANE 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)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-2Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-2Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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°CT = 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
5-5-2Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-2Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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°CT = 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
5-5-2Page 7
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-2Page 8
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-2Page 9
Oct 01/09
@A380AIRPLANE 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).
5-5-3Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-3Page 2
Oct 01/09
@A380AIRPLANE 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
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
5-5-3Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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
70sT = 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
5-5-3Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
1.00
GROUND CART MASS FLOW (kg/s)
GR
OU
ND
CA
RT
OU
TP
UT
AB
S P
RE
SS
UR
E (
ba
rs)
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°CT = 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
5-5-3Page 5
Oct 01/09
@A380AIRPLANE 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
5-6-0Page 1
Oct 01/09
@A380AIRPLANE 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.
5-6-1Page 1
Oct 01/09
@A380AIRPLANE 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
TO
TA
L M
AS
S F
LOW
PE
R A
IRC
RA
FT
(kg
/sec
)
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
5-6-1Page 2
Oct 01/09
@A380AIRPLANE 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
TO
TA
L M
AS
S F
LOW
PE
R A
IRC
RA
FT
(kg
/sec
)
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
5-6-1Page 3
Oct 01/09
@A380AIRPLANE 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.
5-6-2Page 1
Oct 01/09
@A380AIRPLANE 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
2.030 40 50 60 70 80 90
kg/sec min
TOTAL LPGCAIR FLOW
TIME TO COOL CABINTO 27 °C (80.6 °C)
ON GROUNDPULL DOWN
−−−−87583830
3.03.54.04.55.05.56.06.5
PULL DOWN
LPGC PERFORMANCE − CABIN PULL DOWN
TIME TO COOL CABIN TO 27 °C (MINUTES)
SAME BOUNDARY CONDITIONS AS BEFORE
TO
TA
L M
AS
S F
LOW
PE
R A
IRC
RA
FT
(kg
/sec
)
(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
5-6-2Page 2
Oct 01/09
@A380AIRPLANE 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]
3.03.54.05.05.56.5
624737252115
TO
TA
L M
AS
S F
LOW
PE
R A
IRC
RA
FT
(kg
/sec
)
TIME TO COOL COURIER COMPARTMENT TO 27°C AND
INITIAL TEMPERATURE AT 38°C OAT, COURIER COMPARTMENT COOL DOWN TO 27°C AND CARGOCOMPARTMENT COOL DOWN TO 24°C, ASSUMED LPGC INLET TEMPERATURE 1.5°C
TOTAL LPGCAIR FLOW
403125171512
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
5-6-2Page 3
Oct 01/09
@A380AIRPLANE 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.
5-7-0Page 1
Oct 01/09
@A380AIRPLANE 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
TO
TA
L F
RE
SH
AIR
FLO
W (
kg/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
OA
T: −
30°
C (
−22°
F)
(−9.
4°F
)O
AT
: −23
°C
OA
T: −
40°
C (
−40
°F
)
OA
T: 3
8°C
(100
.4°F
)
40 mbar
50 mbar
60 mbar
70 mbar
80 mbar
90 mbar
C1 C2C6
OAT
: 38°
C (100
.4°F
)
OAT:
38°
C (100
.4°F
)
Maximum allowed mass flow
C5
−40 −30 −20 −10 0 10 20 30 40 50 60
C4C3
L_AC_050700_1_0010101_01_00
Preconditioned Airflow RequirementsPreconditioned Airflow Requirements - A380-800 Models
5-7-0Page 2
Oct 01/09
@A380AIRPLANE 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
TO
TA
L F
LOW
(kg
/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:
6.5Maximum allowed mass flow
5 15 25 35 452
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
5-7-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
5-8-0 Ground Towing Requirements
**ON A/C A380-800 Models A380-800F Models
Ground Towing Requirements
1. This section provides information on aircraft Towing.
The A380-800/800F is designed with means for conventional towing or towbarless towing.Information on towbarless towing can be found in SIL 09-002 and chapter 9 of the AircraftMaintenance Manual.It is possible to tow or push the aircraft, at maximum ramp weight with engines at zero or up to idlethrust, using a towbar attached to the nose gear leg. The towbar fitting is installed at the front ofthe leg (optional towing fitting for towing from the rear of the NLG available).The body gears have attachment points for towing or debogging (for details refer to chapter 7 of theAircraft Recovery Manual).
NOTE : Information on aircraft towing procedures and corresponding aircraft limitations are given inchapter 9 of the Aircraft Maintenance Manual.
A. Figure 1: Ground Towing Requirements A380-800 Models shows the chart to determine thetowbar pull and tow tractor mass requirements as function of the following physicalcharacteristics:- Aircraft weight,- Slope,- Number of engines at idle.The chart is based on the A380-800 engine type with the biggest idle thrust. The chart istherefore valid for all A380-800 models.
B. Figure : Typical Tow Bar configuration 1 and Figure : Typical Tow Bar configuration 2 givesguidelines for the towbar.
2. Towbar design guidelines
The aircraft towbar shall respect the following norms:- SAE AS 1614, ”Main Line Aircraft TowBar Attach Fitting Interface”,- SAE ARP1915 Revision C, ”Aircraft TowBar”,- ISO 8267-1, ”Aircraft - Towbar attachment fitting - Interface requirements - Part 1: Main line
aircraft”,- ISO 9667, ”Aircraft ground support equipment - Towbars”,- IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Towbar”.
A standard type towbar should be equipped with a damping system to protect the nose gear againstjerks and with towing shear pins:- A traction shear pin calibrated at 62000 daN (139381.53 lbf),- A torsion pin calibrated at 4800 m.daN (424778.76 lbf.in).
5-8-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
The towing head is designed according to SAE/AS 1614 (issue C) cat. V.
3. Maximum Extension of the NLG Shock Absorber.
- Measure the dimension H between the two red marks on the left side of the NLG.- Make sure that the dimension H of the NLG is never more than 295 mm (11.6 in.) when you tow
the aircraft (the compression of the shock absorber is 340 mm (13.4 in.)).
5-8-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
L_AC_050800_1_0010101_01_02
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A380 AT 560 t, AT 1.5% SLOPE,2 ENGINES AT IDLE AND FOR WET TARMAC CONDITIONS:
−ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (560 t),−FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),−FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 4,−FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED NUMBER OF ENGINES (2),−FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,−THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (34.4 t),−SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE.
THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (60.4 t).
00
5
10
15
20
25
30
35
40
45
50
10 20 30 40 50 60 70 80 0 1 2 3 4 0 0.5 1.0 1.5 2.0
BREAKAWAY RESISTANCE 4%# OF ENGINES ON FOR PB:2ENGINE THRUST 1779.3 daN 600
550500
450
400
350
300
TRACTOR WEIGHT [ t ] NO OF ENGINES AT IDLE SLOPE [ % ]
2 ENGINES ON1.5% SLOPE
A/C WEIGHT [ t ]DRAWBAR PULL [ t ]
WET C
ONCRETE =
0.5
7
HARD SNOW = 0.2
ICE = 0.05
DR
Y C
ON
CR
ETE
=
0.8
34.4
60.4
560
Ground Towing RequirementsGround Towing Requirements A380-800 Models
5-8-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
D1
MF
M
LONGHOLE BLOCKINGLATERAL MOVEMENTS
HOLES FOR SPARE SHEAR PINS
MF
LOCKING/UNLOCKING HANDLE
SHEAR PIND1
L
F F
Fshear
F
Mshear
Fshear
Lshear
M = Fshear
x L
Mshear
= Fshear
x Lshear
Mshear
= F x D1 (Mshear
< M)
D1 = (M/L) x Lshear
/ F
Fshear
= M / L
Mshear
= (M/L) x Lshear
D1 = (M x Lshear
/ (F x L)
A
AL_AC_050800_1_0020101_01_00
Ground Towing RequirementsTypical Tow Bar configuration 1
5-8-0Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
MF
D2
OVERSIZED HOLEWRT RETENTION BOLT
M
L
F
F/2
F/2
D2
D2 = (2 x Mshear
) / F D2 = (2 x M x Lshear
) / (F x L)
F M D1 D2
62000 4800 69.7 148.6
[daN] [m.daN] [mm] [mm]
RESULTS FOR A TOWBAR LENGTH OF Lshear
/L = 0.90
Fshear
Fshear
Lshear
Mshear
M = Fshear
x L
Mshear
= Fshear
x Lshear
Mshear
= F/2 x D2 (Mshear
< M)
Fshear
= M / L
Mshear
= (M / L) x Lshear
L_AC_050800_1_0030101_01_00
Ground Towing RequirementsTypical Tow Bar configuration 2
5-8-0Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
A
0.200 m(7.9 in)
A
0.555 m(21.85 in)
L_AC_050800_1_0040101_01_00
Ground Towing RequirementsNose Gear Towing Fittings
5-8-0Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
TOP OF TORQUELINK STOP
SHOULDER OF MAINFITTING LOWERBEARING
DETAIL A
DETAIL B
A
H
A
B
A
L_AC_050800_1_0050101_01_00
Ground Towing RequirementsMaximum Extension of the NLG Shock Absorber
5-8-0Page 7
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
OPERATING CONDITIONS
6-1-0 Engine Exhaust Velocities and Temperatures
**ON A/C A380-800 Models A380-800F Models
Engine 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 enginemodels, including the A380-800F Freighter version. Therefore, contours hereafter include contours ofthe 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:
6-1-0Page 1
Oct 01/09
@A380AIRPLANE 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 stronglyrecommends that jet blast studies using their contours include the effect of a 20-knot headwind.
6-1-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
6-1-1 Engine Exhaust Velocities - Ground Idle Power
**ON A/C A380-800 Models A380-800F Models
Engine Exhaust Velocities - Ground Idle Power
1. This section gives engine exhaust velocities at ground idle power.
6-1-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
deh0
0023
17
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
60m 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
6-1-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
ALL VELOCITY VALUES ARE IN STATUE MILES PER HOUR.
FEET(METERS)
GROUND PLANE
CONVERSION FACTOR1 MPH = 1.6 km/h
300
(91)
140(43)
ELEVATION
FEET
(METERS)
0
0
PLAN
150
(46)
0
70(21)
PW
VE
−00
224
(020
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
6-1-1Page 3
Oct 01/09
@A380AIRPLANE 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.
6-1-2Page 1
Oct 01/09
@A380AIRPLANE 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
deh0
0023
16
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
6-1-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
FEET(METERS)
GROUND PLANEELEVATIONFEET
(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)
PW
VE
−00
226
(020
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
6-1-2Page 3
Oct 01/09
@A380AIRPLANE 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.
6-1-3Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
deh0
0023
19
100METERS 0
0FEET 40 80
20 40 60 80
120 160 200 240 280 320 360
5
10
1540
60ftm
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
1540
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
6-1-3Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
ALL VELOCITY VALUES ARE IN STATUE MILES PER HOUR.
CONVERSION FACTOR1 MPH = 1.6 km/h
PW
VE
−02
200
(020
7)
DANGER (KEEP OUT) ZONES 35 MPH
NOTE:
L_AC_060103_1_0020101_01_01
FEET(METERS)
GROUND PLANE
140(43)
ELEVATION0
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
6-1-3Page 3
Oct 01/09
@A380AIRPLANE 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.
6-1-4Page 1
Oct 01/09
@A380AIRPLANE 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
deh0
0023
18
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
6-1-4Page 2
Oct 01/09
@A380AIRPLANE 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 PLANEELEVATIONFEET
(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
6-1-4Page 3
Oct 01/09
@A380AIRPLANE 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.
6-1-5Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
deh0
0023
15
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
6-1-5Page 2
Oct 01/09
@A380AIRPLANE 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 FACTOR1 MPH = 1.6 km/h
PW
VE
−00
225
(020
7)
DANGER (KEEP OUT) ZONES 35 MPH
NOTE:
FEET(METERS)
GROUND PLANE
300 450 600
140(43)
ELEVATIONFEET
0 150
0
70(21)
(91) (137) (183)0 (46)
(METERS)
PLAN AIRPLANECL
65 MPHOUT TO1090 ft(332 m)
105 MPHOUT TO724 ft(221 m)
35 MPHOUT TO1553 ft(473 m)
FEET(METERS)
140(43)
0
70(21)
65 MPHOUT TO1090 ft(332 m)
105 MPHOUT TO724 ft(221 m)
35 MPHOUT TO1553 ft(473 m)
Engine Exhaust VelocitiesMax. Take-Off Power - GP 7200 Engines
6-1-5Page 3
Oct 01/09
@A380AIRPLANE 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.
6-1-6Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
deh0
0023
14
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) TO
540 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
6-1-6Page 2
Oct 01/09
@A380AIRPLANE 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
6-1-6Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
6-2-0 Airport and Community Noise Data
**ON A/C A380-800 Models A380-800F Models
Airport and Community Noise Data
1. Airport and Community Noise Data
6-2-0Page 1
Oct 01/09
@A380AIRPLANE 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 ofthe 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 ofthe 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: 12˚C- Relative humidity: 90%- Atmospheric pressure: 1015 hPa- Wind speed: Negligible- No rain
6-2-1Page 1
Oct 01/09
@A380AIRPLANE 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
6-2-1Page 2
Oct 01/09
@A380AIRPLANE 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
6-2-1Page 3
Oct 01/09
@A380AIRPLANE 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
The intake suction danger areas, which are plotted in this chapter, correspond to very low suctionvelocities in order to prevent very low density objects (hat, handkerchief) from ingestion by engines.The primary aim of those danger areas is to protect the people working around the engines.
Regarding the risk of ingesting typical loose objects, which can be found on ground at the edge ofrunways/taxiways paved areas (loose gravels for example), it was demonstrated that the A380 outerengines are high enough above ground so that the risk og ingestion is remote in the followingconditions:- at usual taxiway thrust (i.e. up to the breakaway power setting), even if the loose objects are
below the A380 outer engines.- at usual take-off thrust (i.e. up to the maximum take-off power setting), if the loose objects are
beyond 3 meters from the A380 outer engines centreline.
6-3-0Page 1
Oct 01/09
@A380AIRPLANE 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.
6-3-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
deh0
0015
13
INTAKE SUCTION DANGER AREA MINIMUM IDLE POWER
EXHAUST DANGER AREA
ENTRY CORRIDOR
4.5 m(15 ft)
1.3 m(4 ft 3 in)
30TO 70 m (230 ft) AFT OF EXHAUST NOZZLES
L_AC_060301_1_0010101_01_00
Danger Areas of the EnginesGround Idle Power - TRENT 900 Engines
6-3-1Page 2
Oct 01/09
@A380AIRPLANE 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°
PW
VE
−021
97 (0
207)
C
C C
C
L_AC_060301_1_0020101_01_01
Danger Areas of the EnginesGround Idle Power - GP 7200 Engines
6-3-1Page 3
Oct 01/09
@A380AIRPLANE 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.
6-3-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
deh0
0015
15
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
6-3-2Page 2
Oct 01/09
@A380AIRPLANE 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−
0219
9 (0
207)
PW
V
L_AC_060302_1_0020101_01_01
Danger Areas of the EnginesMax Take-Off Power - GP 7200 Engines
6-3-2Page 3
Oct 01/09
@A380AIRPLANE 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.
6-3-3Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
deh0
0015
14
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
6-3-3Page 2
Oct 01/09
@A380AIRPLANE 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°
PW
VE
−02
198
(020
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
6-3-3Page 3
Oct 01/09
@A380AIRPLANE 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
6-4-0Page 1
Oct 01/09
@A380AIRPLANE 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.
6-4-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
DIS
TA
NC
E F
RO
M A
IRC
RA
FT
CE
NT
ER
LIN
E
0 10 20 30 40 50 60 70 80 90 100
30
6
10
20
0
−10
−20
FEET
DIS
TA
NC
E F
RO
M A
IRC
RA
FT
CE
NT
ER
LIN
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
6-4-1Page 2
Oct 01/09
@A380AIRPLANE 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.
6-4-2Page 1
Oct 01/09
@A380AIRPLANE 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
DIS
TA
NC
E F
RO
M A
IRC
RA
FT
CE
NT
ER
LIN
E
DISTANCE DOWNSTREAM FROM NOZZLEMETERS
0 3 6 9 12 15 18 21 24 27
3
6
0
−3
−6
DIS
TA
NC
E F
RO
M A
IRC
RA
FT
CE
NT
ER
LIN
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
6-4-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
PAVEMENT DATA
7-1-0 General Information
**ON A/C A380-800 Models A380-800F Models
General 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.
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 reston 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).
7-1-0Page 1
Oct 01/09
@A380AIRPLANE 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, anarbitrary 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 ofthe 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.
7-1-0Page 2
Oct 01/09
@A380AIRPLANE 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 onthe pavement.Numerically the ACN is two times the derived single wheel load (expressed in thousands ofkilograms).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:
PCNPAVEMENT TYPE SUBGRADE
CATEGORYTIRE-PRESSURE
CATEGORYEVALUATION
METHODR - 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)
7-1-0Page 3
Oct 01/09
@A380AIRPLANE 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.
7-2-0Page 1
Oct 01/09
@A380AIRPLANE 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 Loading on 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
7-2-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070200_1_0040101_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
562 000 kg (1 239 000 lb)
See Section 7−4−1 Figure: Landing Gear Loadingon Pavement − MRW 562 000 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)
Landing Gear FootprintMRW 562 000 kg - A380-800 Models
7-2-0Page 3
Oct 01/09
@A380AIRPLANE 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
7-2-0Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Landing Gear Footprint - Freighter
1. This section gives the Landing Gear Footprint.
7-2-0Page 5
Oct 01/09
@A380AIRPLANE 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 Loadingon 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
7-2-0Page 6
Oct 01/09
@A380AIRPLANE 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
7-2-0Page 7
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
7-3-0 Maximum Pavement Loads
**ON A/C A380-800 Models
Maximum Pavement Loads - Pax
1. This section gives Maximum Pavement Loads.
7-3-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070300_1_0050101_01_00
H
VV
V(N
G)
(WG
)(B
G)
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
V(W
G)
MA
XIM
UM
VE
RT
ICA
L W
ING
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
V(B
G)
MA
XIM
UM
VE
RT
ICA
L B
OD
Y G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T A
FT
CG
HM
AX
IMU
M H
OR
IZO
NT
AL
GR
OU
ND
LO
AD
FR
OM
BR
AK
ING
(1)
FW
D C
G =
35.
81 %
MA
C(2
)A
FT
CG
= 4
3 %
MA
C(3
)B
RA
KE
D W
ING
GE
AR
(4)
BR
AK
ED
BO
DY
GE
AR
NO
TE
:A
LL L
OA
DS
CA
LCU
LAT
ED
US
ING
AIR
PLA
NE
MA
XIM
UM
RA
MP
WE
IGH
T
12
34
56
7
MO
DE
L
lbkg
lbkg
VN
G
kglb
lbkg
lbkg
lbkg
lbkg
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
VW
G(P
ER
ST
RU
T)
VB
G(P
ER
ST
UT
)H
(PE
R S
TR
UT
)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
MA
XIM
UM
RA
MP
WE
IGH
T
−80
0
ST
AT
IC L
OA
DA
T M
OS
T F
WD
CG
(1)
1 12
8 77
551
2 00
087
700
39 7
7014
7 42
566
880
214
750
97 4
1032
2 12
514
6 11
0
70 1
75(3
)
105
250(
4)
31 8
30(3
)
47 7
40(4
)
171
800(
3)
257
700(
4)
77 9
30(3
)
116
890(
4)
2S
TA
TIC
BR
AK
ING
DE
CE
LER
AT
ION
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
@
10 ft
/s²
Maximum Pavement LoadsMRW 512 000 kg - A380-800 Models
7-3-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
H
VV
V(N
G)
(WG
)(B
G)
(1)
(2)
(3)
(4)
BR
AK
ED
BO
DY
GE
AR
NO
TE
:
FW
D C
G =
37.
5 %
MA
C
AF
T C
G =
43.
0 %
MA
C
BR
AK
ED
WIN
G G
EA
R
ALL
LO
AD
S C
ALC
ULA
TE
D U
SIN
G A
IRP
LAN
E M
AX
IMU
M R
AM
P W
EIG
HT
L_AC_070300_0_AAM0_01_02
V V(W
G)
V(B
G)
H
MA
XIM
UM
VE
RT
ICA
L W
ING
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
12
34
56
7
MO
DE
L
lbkg
−80
0
lbkg
VN
G
kglb
lbkg
lb
2
kglb
kglb
kg
2A
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
VW
G(P
ER
ST
RU
T)
VB
G(P
ER
ST
UT
)H
(PE
R S
TR
UT
)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
MA
XIM
UM
RA
MP
WE
IGH
T
ST
AT
IC L
OA
DA
T M
OS
T F
WD
CG
(1)
(NG
)M
AX
IMU
M V
ER
TIC
AL
NO
SE
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
FO
RW
AR
D C
G
MA
XIM
UM
VE
RT
ICA
L B
OD
Y G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T A
FT
CG
1 23
9 00
056
2 00
087
825
39 8
4015
3 40
069
590
235
725
106
920
353
575
160
380
77 0
25(3
)
115
525(
4)
34 9
40(3
)
52 4
00(4
)
188
575(
3)
282
850(
4)
85 5
40(3
)
128
300(
4)
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
L_AC_070300_1_0010101_01_01
Maximum Pavement LoadsMRW 562 000 kg - A380-800 Models
7-3-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
H
VV
V(N
G)
(WG
)(B
G)
(1)
(2)
(3)
(4)
BR
AK
ED
BO
DY
GE
AR
NO
TE
:
FW
D C
G =
37.
8 %
MA
C
AF
T C
G =
41.
0 %
MA
C
BR
AK
ED
WIN
G G
EA
R
ALL
LO
AD
S C
ALC
ULA
TE
D U
SIN
G A
IRP
LAN
E M
AX
IMU
M R
AM
P W
EIG
HT
L_AC_070300_0_AAM0_01_02
V V(W
G)
V(B
G)
H
MA
XIM
UM
VE
RT
ICA
L W
ING
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
12
34
56
7
MO
DE
L
lbkg
−80
0
lbkg
VN
G
kglb
lbkg
lb
2
kglb
kglb
kg
2A
T IN
ST
AN
TA
NE
OU
SB
RA
KIN
GC
OE
FF
ICIE
NT
= 0
.8
VW
G(P
ER
ST
RU
T)
VB
G(P
ER
ST
UT
)H
(PE
R S
TR
UT
)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
MA
XIM
UM
RA
MP
WE
IGH
T
ST
AT
IC L
OA
DA
T M
OS
T F
WD
CG
(1)
(NG
)M
AX
IMU
M V
ER
TIC
AL
NO
SE
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
FO
RW
AR
D C
G
MA
XIM
UM
VE
RT
ICA
L B
OD
Y G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T A
FT
CG
1 25
8 85
057
1 00
087
725
39 7
9015
4 35
070
010
237
475
107
710
356
200
161
570
78 2
50(3
)
117
375(
4)
35 4
90(3
)
53 2
40(4
)
189
975(
3)
284
950(
4)
86 1
70(3
)
129
260(
4)
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
L_AC_070300_1_0030101_01_00
Maximum Pavement LoadsMRW 571 000 kg - A380-800 Models
7-3-0Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Maximum Pavement Loads - Freighter
1. This section gives Maximum Pavement Loads.
7-3-0Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
H
V(W
G)
V(B
G)
H
MA
XIM
UM
VE
RT
ICA
L W
ING
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
(1)
(2)
(3)
(4)
BR
AK
ED
WIN
G G
EA
R
BR
AK
ED
BO
DY
GE
AR
MA
XIM
UM
VE
RT
ICA
L B
OD
Y G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T A
FT
CG
NO
TE
:
AF
T C
G =
42.
8 %
MA
C
FW
D C
G =
36.
0 %
MA
C
ALL
LO
AD
S C
ALC
ULA
TE
D U
SIN
G A
IRP
LAN
E M
AX
IMU
M R
AM
P W
EIG
HT
VV
V(N
G)
(WG
)(B
G)
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
12
34
56
7
MO
DE
L
lbkg
lbkg
VN
G
kglb
lbkg
lb
2
kglb
kglb
kg
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
VW
G(P
ER
ST
RU
T)
VB
G(P
ER
ST
UT
)H
(PE
R S
TR
UT
)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
MA
XIM
UM
RA
MP
WE
IGH
T
−80
0F
ST
AT
IC L
OA
DA
T M
OS
T F
WD
CG
(1)
1 30
5 12
559
2 00
010
0 40
045
540
169
475
76 8
7024
8 10
011
2 53
037
2 12
516
8 80
0
81 1
25(3
)
121
700(
4)
36 8
00(3
)
55 2
00(4
)
198
475(
3)
297
700(
4)
90 0
30(3
)
135
040(
4)
2S
TA
TIC
BR
AK
ING
@ 1
0 ft/
sD
EC
ELE
RA
TIO
N
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
L_AC_070300_1_0020101_01_01
Maximum Pavement Loads - FreighterMRW 592 000 kg - A380-800F Models
7-3-0Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
H
V(W
G)
V(B
G)
H
MA
XIM
UM
VE
RT
ICA
L W
ING
GE
AR
GR
OU
ND
LO
AD
AT
MO
ST
AF
T C
G
MA
XIM
UM
HO
RIZ
ON
TA
L G
RO
UN
D L
OA
D F
RO
M B
RA
KIN
G
(1)
(2)
(3)
(4)
BR
AK
ED
WIN
G G
EA
R
BR
AK
ED
BO
DY
GE
AR
MA
XIM
UM
VE
RT
ICA
L B
OD
Y G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T A
FT
CG
NO
TE
:
AF
T C
G =
42.
7 %
MA
C
FW
D C
G =
36.
3 %
MA
C
ALL
LO
AD
S C
ALC
ULA
TE
D U
SIN
G A
IRP
LAN
E M
AX
IMU
M R
AM
P W
EIG
HT
VV
V(N
G)
(WG
)(B
G)
V(N
G)
MA
XIM
UM
VE
RT
ICA
L N
OS
E G
EA
R G
RO
UN
D L
OA
D A
T M
OS
T F
OR
WA
RD
CG
12
34
56
7
MO
DE
L
lbkg
lbkg
VN
G
kglb
lbkg
lb
2
kglb
kglb
kg
AT
INS
TA
NT
AN
EO
US
BR
AK
ING
CO
EF
FIC
IEN
T =
0.8
VW
G(P
ER
ST
RU
T)
VB
G(P
ER
ST
UT
)H
(PE
R S
TR
UT
)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
ST
AT
IC L
OA
DA
T M
AX
AF
TC
G (
2)
MA
XIM
UM
RA
MP
WE
IGH
T
−80
0F
ST
AT
IC L
OA
DA
T M
OS
T F
WD
CG
(1)
1 32
7 17
560
2 00
010
0 47
545
580
170
725
77 4
4025
2 17
511
4 38
037
8 25
017
1 58
0
82 5
00(3
)
123
750(
4)
37 4
20(3
)
56 1
30(4
)
201
750(
3)
302
600(
4)
91 5
10(3
)
137
260(
4)
2S
TA
TIC
BR
AK
ING
@ 1
0 ft/
sD
EC
ELE
RA
TIO
N
ST
AT
IC B
RA
KIN
G@
10
ft/s
DE
CE
LER
AT
ION
L_AC_070300_1_0040101_01_00
Maximum Pavement LoadsMRW 602 000 kg- A380-800F Models
7-3-0Page 7
Oct 01/09
@A380AIRPLANE 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, Figure: Landing Gear Loading on Pavement - MRW 512000 kg - A380-800 Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) and thepercentage of weight on the Main Landing gear is 95.1 %.For these conditions the total weight on the Main Landing Gear Group is 428 000 kg (943 580lb).
In the example shown in Section 7-4-1 Figure: Landing Gear Loading on Pavement - MRW 562000 kg - A380-800 Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) and thepercentage of weight on the Main Landing gear is 95.1 %.For these conditions the total weight on the Main Landing Gear Group is 428 000 kg (943 580lb).
In the example shown in Section 7-4-1 Figure: Landing Gear Loading on Pavement - MRW 571000 kg - A380-800 Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) and thepercentage of weight on the Main Landing gear is 94.3 %.For these conditions the total weight on the Main Landing Gear Group is 424 400 kg (935 040lb).
- A380-800F Models :
In the example shown in Section 7-4-1, Figure: Landing Gear Loading on Pavement - MRW 592000 kg - A380-800F Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) and thepercentage of weight on the Main Landing gear is 95.04 %.For these conditions the total weight on the MLG Group is 427 700 (942 920 lb).
In the example shown in Section 7-4-1, Figure: Landing Gear Loading on Pavement - MRW 602000 kg - A380-800F Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) and thepercentage of weight on the Main Landing gear is 95 %.For these conditions the total weight on the MLG Group is 427 500 (942 475 lb).
7-4-0Page 1
Oct 01/09
@A380AIRPLANE 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.
7-4-1Page 1
Oct 01/09
@A380AIRPLANE 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
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
GR
OU
P −
x 1
000
kg
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
x 1
000
kg
420
CG FOR ACNCALCULATIONS
MTOW = 510 000 kg
MLW = 394 000 kg
MZFW = 372 000 kg
TAKE OFF &LANDING
TAKE OFF
LANDING
95.1 % WEIGHT ON MLG GROUP
L_AC_070401_1_0050101_01_00
Landing Gear Loading on PavementMRW 512 000 kg - A380-800 Models
7-4-1Page 2
Oct 01/09
@A380AIRPLANE 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
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
GR
OU
P −
x 1
000
kg
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
x 1
000
kg
MTOW = 560 000 kg
CG FOR ACNCALCULATIONS
MLW = 386 000 kg
LANDING
95.1 % WEIGHT ON 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
7-4-1Page 3
Oct 01/09
@A380AIRPLANE 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
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
GR
OU
P −
x 1
000
kg
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
x 1
000
kg
MLW = 391 000 kg
MZFW = 366 000 kg
MTOW = 569 000 kg
CG FOR ACNCALCULATIONS
TAKE OFF &LANDING
TAKE OFF
LANDING
94.3 % WEIGHT ON MLG GROUP
Landing Gear Loading on PavementMRW 571 000 kg - A380-800 Models
7-4-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Landing Gear Loading on Pavement - Freighter
1. This section gives Landing Gear Loading on Pavement.
7-4-1Page 5
Oct 01/09
@A380AIRPLANE 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
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
GR
OU
P −
x 1
000
kg
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
600
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
x 1
000
kg
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 % WEIGHT ON MLG GROUP
Landing Gear Loading on PavementMRW 592 000kg - A380-800F Models
7-4-1Page 6
Oct 01/09
@A380AIRPLANE 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
WE
IGH
T O
N M
AIN
LA
ND
ING
GE
AR
GR
OU
P −
x 1
000
kg
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
600
PERCENTAGE MAC
AIR
CR
AF
T G
RO
SS
WE
IGH
T −
x 1
000
kg
CG FOR ACNCALCULATIONS
MTOW = 600 000 kg
MLW = 427 000 kg
MZFW = 379 000 kg
TAKE OFF &LANDING
TAKE OFF
LANDING
95 % WEIGHT ON MLG GROUP
Landing Gear Loading on PavementMRW 602 000kg - A380-800F Models
7-4-1Page 7
Oct 01/09
@A380AIRPLANE 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, Figure: Wing Gear and Body Gear Loads on Pavement -MRW 512 000 kg - A380-800 Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) at AftCG for ACN Calculations.For these conditions the load on the two Wing Gears is 171 200 kg (377 430 lb) and the load on thetwo Body Gears is 256 800 kg (566 150 lb).The total weight on the Main Landing Gear Group is 428 000 kg (943 580 lb).
In the example shown in Section 7-4-3, Figure: Wing Gear and Body Gear Loads on Pavement -MRW 562 000 kg - A380-800 Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) at AftCG for ACN Calculations.For these conditions the load on the two Wing Gears is 171 200 kg (377 430 lb) and the load on thetwo Body Gears is 256 800 kg (566 150 lb).The total weight on the Main Landing Gear Group is 428 000 kg (943 580 lb).
In the example shown in Section 7-4-3, Figure: Wing Gear and Body Gear Loads on Pavement -MRW 571 000 kg - A380-800 Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) at AftCG for ACN Calculations.For these conditions the load on the two Wing Gears is 169 800 kg (374 345 lb) and the load on thetwo Body Gears is 254 700 kg (561 515 lb).The total weight on the Main Landing Gear Group is 424 500 kg (935 860 lb).
- A380-800F models :
In the example shown in Section 7-4-3, Figure: Wing Gear and Body Gear Loads on Pavement -MRW 592 000 kg - A380-800F Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) at AftCG for ACN Calculations.For these conditions the load on the two Wing Gears is 171 100 kg (377 210 lb) and the load on thetwo Body Gears is 256 600 kg (565 710 lb).The total weight on the Main Landing Gear Group is 427 700 kg (942 920 lb).
7-4-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
In the example shown in Section 7-4-3, Figure: Wing Gear and Body Gear Loads on Pavement -MRW 602 000 kg - A380-800F Models, the Gross Aircraft Weight is 450 000 kg (992 080 lb) at AftCG for ACN Calculations.For these conditions the load on the two Wing Gears is 171 000 kg (376 990 lb) and the load on thetwo Body Gears is 256 500 kg (565 485 lb).The total weight on the Main Landing Gear Group is 427 500 kg (942 475 lb).
7-4-2Page 2
Oct 01/09
@A380AIRPLANE 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.
7-4-3Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070403_1_0050101_01_00
100
120
140
160
180
200
220
240
260
280
300
320
340 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
LOAD ON BODY GEARS OR LOAD ON WING GEARS
CG
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
See
Sec
tion
7−4−
1 F
igur
e: L
andi
ng G
ear
Load
ing
on P
avem
ent −
MR
W 5
12 0
00 k
g −
A38
0−80
0 M
odel
s
[x 1
000
kg]
[x 1000 kg]70
0
600
500
400
300
[x 1000 lb]
WIN
G G
EA
RS
BO
DY
GE
AR
S
AIR
CR
AF
T G
RO
SS
WE
IGH
T
600
700
800
900
1000
1100
1200
1300
[x 1
000
lb]
Wing Gear and Body Gear Loads on PavementMRW 512 000 kg - A380-800 Models
7-4-3Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070403_1_0060101_01_00
100
120
140
160
180
200
220
240
260
280
300
320
340 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
LOAD ON BODY GEARS OR LOAD ON WING GEARS
CG
FO
R A
CN
CA
LCU
LAT
ION
S: 4
3 %
MA
C.
See
Sec
tion
7−4−
1 F
igur
e: L
andi
ng G
ear
Load
ing
on P
avem
ent −
MR
W 5
62 0
00 k
g −
A38
0−80
0 M
odel
s
600
700
800
900
1000
1100
1200
1300
[x 1
000
kg]
[x 1
000
lb]
[x 1000 kg]70
0
600
500
400
300
[x 1000 lb]
WIN
G G
EA
RS
BO
DY
GE
AR
S
Wing Gear and Body Gear Loads on PavementMRW 562 000 kg - A380-800 Models
7-4-3Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070403_1_0070101_01_00
100
120
140
160
180
200
220
240
260
280
300
320
340 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
LOAD ON BODY GEARS OR LOAD ON WING GEARS
CG
FO
R A
CN
CA
LCU
LAT
ION
S: 4
1 %
MA
C.
See
Sec
tion
7−4−
1 F
igur
e: L
andi
ng G
ear
Load
ing
on P
avem
ent −
MR
W 5
71 0
00 k
g −
A38
0−80
0 M
odel
s
600
700
800
900
1000
1100
1200
1300
[x 1
000
kg]
[x 1
000
lb]
[x 1000 kg]70
0
600
500
400
300
[x 1000 lb]
BO
DY
GE
AR
S
WIN
G G
EA
RS
Wing Gear and Body Gear Loads on PavementMRW 571 000 kg - A380-800 Models
7-4-3Page 4
Oct 01/09
@A380AIRPLANE 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.
7-4-3Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070403_1_0080101_01_00
100
120
140
160
180
200
220
240
260
280
300
320
340 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
LOAD ON BODY GEARS OR LOAD ON WING GEARS
CG
FO
R A
CN
CA
LCU
LAT
ION
S: 4
2.8
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
gon
Pav
emen
t − M
RW
592
000
kg
− A
380−
800F
Mod
els
600
700
800
900
1000
1100
1200
1300
[x 1
000
kg]
[x 1
000
lb]
[x 1000 kg]
700
600
500
400
300
[x 1000 lb]
WIN
G G
EA
RS
BO
DY
GE
AR
S
Wing Gear and Body Gear Loads on PavementMRW 592 000 kg - A380-800F Models
7-4-3Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070403_1_0090101_01_00
100
120
140
160
180
200
220
240
260
280
300
320
340 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
LOAD ON BODY GEARS OR LOAD ON WING GEARS
CG
FO
R A
CN
CA
LCU
LAT
ION
S: 4
2.7
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
gon
Pav
emen
t − M
RW
602
000
kg
− A
380−
800F
Mod
els
600
700
800
900
1000
1100
1200
1300
[x 1
000
kg]
[x 1
000
lb]
[x 1000 kg]70
0
600
500
400
300
[x 1000 lb]
BO
DY
GE
AR
S
WIN
G G
EA
RS
Wing Gear and Body Gear Loads on PavementMRW 602 000 kg - A380-800F Models
7-4-3Page 7
Oct 01/09
@A380AIRPLANE 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 typical example shown in Section 7-5-1, Figure: Flexible Pavement Requirements - 4 WheelBogie - MRW 512 000 kg - A380-800 Models.- a CBR value of 10- an Annual Departure level of 3 000- and the load on one Wing Landing Gear of 90 000 kg (198 420 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).
7-5-0Page 1
Oct 01/09
@A380AIRPLANE 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.
7-5-1Page 1
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE 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 GEAR 97 410 kg (214 750 lb)
10 000 COVERAGES USED FOR ACN CALCULATIONS
MAXIMUM POSSIBLE WING GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000*20 YEAR PAVEMENT LIFE
ALPHA FACTOR = 0.8
Flexible Pavement Requirements -- 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-5-1Page 2
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 14 BAR (203 PSI)
8050
MAXIMUM POSSIBLE WING GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
10 000 COVERAGES USED FOR ACN CALCULATIONS
ANNUAL DEPARTURES* 1 200 3 000 6 000 25 000*20 YEAR PAVEMENT 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
7-5-1Page 3
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
8050
MAXIMUM POSSIBLE WING GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ALPHA FACTOR = 0.8
10 000 COVERAGES USED FOR ACN CALCULATIONS
ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000*20 YEAR PAVEMENT 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
7-5-1Page 4
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
80
60 8040 50
50
10 000 COVERAGES USED FOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR 160 380 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 BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES* 1 200 3 000 6 000 25 000*20 YEAR PAVEMENT LIFE
L_AC_070501_1_0020101_01_01
Flexible Pavement Requirements -- 6 Wheel BogieMRW 562 000 kg - A380-800 Models
7-5-1Page 5
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 16.1 BAR (234 PSI)
60 80
60 8040 50
50
10 000 COVERAGES USED FOR 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 WING GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000*20 YEAR PAVEMENT LIFE
L_AC_070501_1_0120101_01_00
Flexible Pavement Requirements -- 4 Wheel BogieMRW 571 000 kg - A380-800 Models
7-5-1Page 6
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
60 80
60 8050
50
10 000 COVERAGES USED FOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR 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)
MAXIMUM POSSIBLE BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES* 1 200 3 000 6 000 25 000*20 YEAR PAVEMENT LIFE
L_AC_070501_1_0060101_01_00
Flexible Pavement Requirements -- 6 Wheel BogieMRW 571 000 kg - A380-800 Models
7-5-1Page 7
Oct 01/09
@A380AIRPLANE 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.
7-5-1Page 8
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE 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 WING GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES* 1 200 3 000 6 000 15 000 25 000*20 YEAR PAVEMENT LIFE
L_AC_070501_1_0130101_01_00
Flexible Pavement Requirements -- 4 Wheel BogieMRW 592 000 kg - A380-800F Models
7-5-1Page 9
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 16.1 BAR (234 PSI)
60 80
8050
50
10 000 COVERAGES USED FOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR 168 800 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 BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES* 1 200 3 000 6 000 25 000*20 YEAR PAVEMENT LIFE
L_AC_070501_1_0040101_01_01
Flexible Pavement Requirements -- 6 Wheel BogieMRW 592 000 kg - A380-800F Models
7-5-1Page 10
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 15 BAR (218 PSI)
80
60 8040 50
50
10 000 COVERAGES USED FOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR 160 380 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 BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
ANNUAL DEPARTURES* 1 200 3 000 6 000 25 000*20 YEAR PAVEMENT LIFE
L_AC_070501_1_0140101_01_00
Flexible Pavement Requirements -- 4 Wheel BogieMRW 602 000 kg - A380-800F Models
7-5-1Page 11
Oct 01/09
@A380AIRPLANE 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 TIRESTIRE PRESSURE CONSTANT AT 16.1 BAR (234 PSI)
60 80
80
40
50
50
10 000 COVERAGES USED FOR ACN CALCULATIONS
WEIGHT ON ONE BODY LANDING GEAR 171 580 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 BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
PAVEMENT LIFE
ANNUAL DEPARTURES* 1 200 3 000 6 000 25 000*20 YEAR
L_AC_070501_1_0080101_01_00
Flexible Pavement Requirements -- 6 Wheel BogieMRW 602 000 kg - A380-800F Models
7-5-1Page 12
Oct 01/09
@A380AIRPLANE 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, Figure: Flex Pavement Requirements LCN - 4 WheelBogie - MRW 512 000 kg - A380-800 Models, the thickness (h) is shown at 508 mm (20 in.) with anLCN of 82. For these conditions the weight on one Wing Landing Gear is 90 000 kg (198 420 lb).
7-6-0Page 1
Oct 01/09
@A380AIRPLANE 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.
7-6-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070601_1_0090101_01_00
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
INC
HE
S)
180
120
150
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4 ba
r (2
03 p
si)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
254
508
762
1016
1524
2032
1020
3080
7060
5040
102030405060708090100
110
120
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R 9
7 41
0 kg
(
214
750
lb)
90
000
kg
(19
8 42
0 lb
) 8
0 00
0 kg
(
176
370
lb)
70
000
kg
(15
4 32
5 lb
) 6
0 00
0 kg
(
132
275
lb)
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-6-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070601_1_0100101_01_00
1020
3040
5080
7060
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4.0
bar
(203
psi
)F
LEX
IBLE
PA
VE
ME
NT
TH
ICK
NE
SS
(m
m)
254
508
762
1016
1524
2032
180
120
150
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
146
110
kg
(32
2 12
5 lb
)14
0 00
0 kg
(
308
650
lb)
130
000
kg
(28
6 60
0 lb
)12
0 00
0 kg
(
264
550
lb)
110
000
kg
(24
2 50
0 lb
)
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 512 000 kg - A380-800 Models
7-6-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1020
3040
5080
7060
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
INC
HE
S)
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
180
140
120
130
150
110
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
254
508
762
1016
1524
2032
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R10
6 92
0 kg
(
235
720
lb)
100
000
kg
(22
0 46
0 lb
)
90
00
0 k
g
(1
98
42
0 lb
)
80
00
0 k
g
(1
76
37
0 lb
)
70
00
0 k
g
(1
54
32
5 lb
)
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
L_AC_070601_1_0010101_01_01
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 562 000 kg - A380-800 Models
7-6-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1020
3040
5080
7060
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
180
140
120
130
150
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5.0
bar
(218
psi
)F
LEX
IBLE
PA
VE
ME
NT
TH
ICK
NE
SS
(m
m)
254
508
762
1016
1524
2032
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
160
380
kg
(35
3 57
5 lb
)15
0 00
0 kg
(
330
700
lb)
140
000
kg
(30
8 65
0 lb
)13
0 00
0 kg
(
286
600
lb)
120
000
kg
(26
4 55
0 lb
)
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
L_AC_070601_1_0020101_01_01
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 562 000 kg - A380-800 Models
7-6-1Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1020
3040
5080
7060
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
180
140
120
130
150
110
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
254
508
762
1016
1524
203
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R10
7 71
0 kg
(
237
475
lb)
100
000
kg
(22
0 46
0 lb
)
90
00
0 k
g
(1
98
42
0 lb
)
80
00
0 k
g
(1
76
37
0 lb
)
70
00
0 k
g
(1
54
32
5 lb
)
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
L_AC_070601_1_0050101_01_00
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 571 000 kg - A380-800 Models
7-6-1Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
1020
3040
5080
7060
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
180
140
120
130
150
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5.0
bar
(218
psi
)F
LEX
IBLE
PA
VE
ME
NT
TH
ICK
NE
SS
(m
m)
254
508
762
1016
1524
2032
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
161
570
kg
(35
6 20
0 lb
)15
0 00
0 kg
(
330
700
lb)
140
000
kg
(30
8 65
0 lb
)13
0 00
0 kg
(
286
600
lb)
120
000
kg
(26
4 55
0 lb
)
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
L_AC_070601_1_0060101_01_00
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 571 000 kg - A380-800 Models
7-6-1Page 7
Oct 01/09
@A380AIRPLANE 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.
7-6-1Page 8
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
180
140
120
130
150
110
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)F
LEX
IBLE
PA
VE
ME
NT
TH
ICK
NE
SS
(m
m)
254
508
762
1016
1524
2032
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R11
2 53
0 kg
(
248
100
lb)
100
000
kg
(22
0 46
0 lb
)
90
00
0 k
g
(1
98
42
0 lb
)
80
00
0 k
g
(1
76
37
0 lb
)
70
00
0 k
g
(1
54
32
5 lb
)
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
L_AC_070601_1_0030101_01_01
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 592 000 kg - A380-800F Models
7-6-1Page 9
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
180
140
120
130
150
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)F
LEX
IBIL
E P
AV
EM
EN
T T
HIC
KN
ES
S (
mm
)
254
508
762
1016
1524
2032
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
168
800
kg
(37
2 12
5 lb
)16
0 00
0 kg
(
352
750
lb)
150
000
kg
(33
0 70
0 lb
)14
0 00
0 kg
(
308
650
lb)
130
000
kg
(28
6 60
0 lb
)
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
L_AC_070601_1_0040101_01_01
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 592 000 kg - A380-800F Models
7-6-1Page 10
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
180
140
120
130
150
110
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)F
LEX
IBLE
PA
VE
ME
NT
TH
ICK
NE
SS
(m
m)
254
508
762
1016
1524
2032
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R11
4 38
0 kg
(
252
175
lb)
100
000
kg
(22
0 46
0 lb
)
90
00
0 k
g
(1
98
42
0 lb
)
80
00
0 k
g
(1
76
37
0 lb
)
70
00
0 k
g
(1
54
32
5 lb
)
L_AC_070601_1_0070101_01_00
Flex Pavement Requirements LCN - 4 Wheel BogieMRW 602 000 kg - A380-800F Models
7-6-1Page 11
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
6070
8050
4030
2010
102030405060708090100
110
120
FLE
XIB
LE P
AV
EM
EN
T T
HIC
KN
ES
S [I
NC
HE
S]
180
120
150
6070
8090
100
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)F
LEX
IBLE
PA
VE
ME
NT
TH
ICK
NE
SS
(m
m)
254
508
762
1016
1524
2032
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
171
580
kg
(37
8 25
0 lb
)16
0 00
0 kg
(
352
750
lb)
150
000
kg
(33
0 70
0 lb
)14
0 00
0 kg
(
308
650
lb)
130
000
kg
(28
6 60
0 lb
)
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
L_AC_070601_1_0080101_01_00
Flex Pavement Requirements LCN - 6 Wheel BogieMRW 602 000 kg - A380-800F Models
7-6-1Page 12
Oct 01/09
@A380AIRPLANE 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, Figure: Rigid Pavement Requirements - 4 Wheel Bogie- MRW 512 000 kg - A380-800 Models.- 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 90 000 kg (198 420 lb), the required Rigid Pavement
Thickness is 24 cm (9.5 inches).
7-7-0Page 1
Oct 01/09
@A380AIRPLANE 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.
7-7-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070701_1_0090101_01_00
8
9
10
11
12
13
14
15
16
[inch
es]
200
300
400
500
600
700
800
900
1000
[lb/in
²]
15
20
25
30
35
40
45
50
55
60
65
70
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 40PR TIRESTIRE PRESSURE CONSTANT = 14 BAR (203 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE WING GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE WING LANDING GEAR97 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/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
Rigid Pavement Requirements - 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-7-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070701_1_0100101_01_00
8
9
10
11
12
13
14
15
16
[inch
es]
200
300
400
500
600
700
800
900
1000
[lb/in
²]
15
20
25
30
35
40
45
50
55
60
65
70
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 40PR TIRESTIRE PRESSURE CONSTANT = 14 BAR (203 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE BODY LANDING GEAR146 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/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
Rigid Pavement Requirements - 6 Wheel BogieMRW 512 000 kg - A380-800 Models
7-7-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
(inch
es)
200
300
400
500
600
700
800
900
1000
(lb
/in²)
15
20
25
30
35
40
45
50
55
60
65
70
(kg
/cm
²)A
LLO
WA
BLE
WO
RK
ING
ST
RE
SS
1400 x 530R23 40PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K.
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(C
EN
TIM
ET
ER
S)
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE WING GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
WEIGHT ON ONE WINGLANDING GEAR
106 920 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
7-7-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
8
9
10
11
12
13
14
15
16
(inch
es)
200
300
400
500
600
700
800
900
1000
(lb
/in²)
15
20
25
30
35
40
45
50
55
60
65
70
(kg
/cm
²)A
LLO
WA
BLE
WO
RK
ING
ST
RE
SS
1400 x 530R23 40PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(C
EN
TIM
ET
ER
S)
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
WEIGHT ON ONE BODY
160 380 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)
LANDING GEAR
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
L_AC_070701_1_0020101_01_01
Rigid Pavement Requirements - 6 Wheel BogieMRW 562 000 kg - A380-800 Models
7-7-1Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
8
9
10
11
12
13
14
15
16
[inch
es]
200
300
400
500
600
700
800
900
1000
[lb/in
²]
15
20
25
30
35
40
45
50
55
60
65
70
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 40PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
40
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³k = 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
7-7-1Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
8
9
10
11
12
13
14
15
16
(inch
es)
200
300
400
500
600
700
800
900
1000
(lb
/in²)
15
20
25
30
35
40
45
50
55
60
65
70
(kg
/cm
²)A
LLO
WA
BLE
WO
RK
ING
ST
RE
SS
1400 x 530R23 40PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(C
EN
TIM
ET
ER
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 BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
L_AC_070701_1_0060101_01_00
Rigid Pavement Requirements - 6 Wheel BogieMRW 571 000 kg - A380-800 Models
7-7-1Page 7
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Rigid Pavement Requirements - Portland Cement Association Design Method - Freighter
1. This section gives Rigid Pavement Requirements.
7-7-1Page 8
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
[inch
es]
200
300
400
500
600
700
800
900
1000
[lb/in
²]
15
20
25
30
35
40
45
50
55
60
65
70
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 42PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
S]
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT 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/m³k = 40 MN/m³k = 80 MN/m³k = 150 MN/m³
L_AC_070701_1_0130101_01_00
Rigid Pavement Requirements - 4 Wheel BogieMRW 592 000 kg - A380-800F Models
7-7-1Page 9
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
(inch
es)
200
300
400
500
600
700
800
900
1000
(lb/in
²)
15
20
25
30
35
40
45
50
55
60
65
70
(kg
/cm
²)A
LLO
WA
BLE
WO
RK
ING
ST
RE
SS
1400 x 530R23 42PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(C
EN
TIM
ET
ER
S)
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE BODY GEAR LOAD AT MAXIMUM RAMP WEIGHT AND AFT CG
k = 20 MN/m³k = 40 MN/m³k = 80 MN/m³k = 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
7-7-1Page 10
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
[inch
es]
200
300
400
500
600
700
800
900
1000
[lb/in
²]
15
20
25
30
35
40
45
50
55
60
65
70
[kg/
cm²]
ALL
OW
AB
LE W
OR
KIN
G S
TR
ES
S
1400 x 530R23 42PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S[C
EN
TIM
ET
ER
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
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
7-7-1Page 11
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
8
9
10
11
12
13
14
15
16
(inch
es)
200
300
400
500
600
700
800
900
1000
(lb
/in²)
15
20
25
30
35
40
45
50
55
60
65
70
(kg
/cm
²)A
LLO
WA
BLE
WO
RK
ING
ST
RE
SS
1400 x 530R23 42PR TIRESTIRE 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 FORK = 80 MN/m³ BUT DEVIATE SLIGHTLY FOR ANY OTHER VALUES OF K
22
24
26
28
30
32
34
36
38
40
RIG
ID P
AV
EM
EN
T T
HIC
KN
ES
S(C
EN
TIM
ET
ER
S)
REFERENCE:"DESIGN OF CONCRETE AIRPORT PAVEMENTS" AND "COMPUTER PROGRAM FOR AIRPORT PAVEMENT DESIGN − PROGRAM PDILB" PORTLAND CEMENT ASSOCIATION
MAXIMUM POSSIBLE BODY GEAR LOAD AT MAXIMUM RAMP 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
7-7-1Page 12
Oct 01/09
@A380AIRPLANE 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, Figure: Rigid Pavement Requirements LCN - 4 WheelBogie - MRW 512 000 Kg - A380-800 Models, The Radius of Relative Stiffness is shown at 1 016mm (40 in.) with an LCN of 90. For these conditions the weight on one Wing Landing Gear is 90 000kg (198 420 lb).
7-8-0Page 1
Oct 01/09
@A380AIRPLANE 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.
7-8-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models A380-800F Models
WHERE
=
E
k
d
Ed 342
=
=
=
dk
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
14.014.515.015.5
16.016.517.017.5
55.3156.7858.2559.70
65.6967.2368.7570.26
61.1362.5663.9865.38
49.9851.3152.6353.94
46.5147.7548.9850.20
43.9845.1646.3247.47
55.2456.5357.8159.08
51.4152.6153.8054.98
48.6249.7550.8852.00
42.0243.1544.2645.36
40.4441.5142.5843.64
39.1140.1541.1942.21
36.1237.0838.0338.98
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
59.4361.0262.5964.15
42.9744.5746.1647.72
PORTLAND CEMENT ASSOCIATION
L_AC_070801_1_0010101_01_00
Radius of Relative Stiffness
7-8-1Page 2
Oct 01/09
@A380AIRPLANE 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.
7-8-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070802_1_0090101_01_00
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50LO
AD
CLA
SS
IFIC
AT
ION
NU
MB
ER
(LC
N)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4 ba
r (2
03 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R
97 4
10 k
g
(214
750
lb)
90
000
kg
(1
98 4
20 lb
)
80 0
00 k
g
(176
370
lb)
70
000
kg
(1
54 3
25 lb
)
60 0
00 k
g
(132
275
lb)
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 512 000 kg - A380-800 Models
7-8-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070802_1_0100101_01_00
2030
4050
100
9080
7060
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
150
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
INIC
AO
AE
RO
DR
OM
E M
AN
UA
L P
AR
T 2
PA
R 4
.1.3
S
econ
d E
ditio
n 19
65
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4 ba
r (2
03 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
102030405060708090100
110
120
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
110
6070
8090
100
505
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
146
110
kg
(3
22 1
25 lb
) 1
40 0
00 k
g
(308
650
lb)
130
000
kg
(2
86 6
00 lb
) 1
20 0
00 k
g
(264
550
lb)
110
000
kg
(2
42 5
00 lb
)
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 512 000 kg - A380-800 Models
7-8-2Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R 1
06 9
20 k
g (2
35 7
20 lb
) 1
00
00
0 k
g
(2
20
46
0 lb
) 9
0 0
00
kg
(1
98
42
0 lb
) 8
0 0
00
kg
(1
76
37
0 lb
) 7
0 0
00
kg
(1
54
32
5 lb
)
L_AC_070802_1_0010101_01_01
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 562 000 kg - A380-800 Models
7-8-2Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
16
0 3
80
kg
(35
3 5
75
lb)
15
0 0
00
kg
(33
0 7
00
lb)
14
0 0
00
kg
(30
8 6
50
lb)
13
0 0
00
kg
(28
6 6
00
lb)
12
0 0
00
kg
(26
4 5
50
lb)
L_AC_070802_1_0020101_01_01
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 562 000 kg - A380-800 Models
7-8-2Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R 1
07 7
10 k
g
(237
475
lb)
10
0 0
00
kg
(22
0 4
60
lb)
9
0 0
00
kg
(1
98
42
0 lb
) 8
0 0
00
kg
(1
76
37
0 lb
) 7
0 0
00
kg
(1
54
32
5 lb
)
L_AC_070802_1_0050101_01_00
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 571 000 kg - A380-800 Models
7-8-2Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
GW
EIG
HT
ON
ON
E B
OD
Y
LAN
DIN
G G
EA
R 1
61 5
70 k
g
(356
200
lb)
15
0 0
00
kg
(33
0 7
00
lb)
14
0 0
00
kg
(30
8 6
50
lb)
13
0 0
00
kg
(28
6 6
00
lb)
12
0 0
00
kg
(26
4 5
50
lb)
L_AC_070802_1_0060101_01_00
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 571 000 kg - A380-800 Models
7-8-2Page 7
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Rigid Pavement Requirements - LCN Conversion - Freighter
1. This section gives Rigid Pavement Requirements LCN.
7-8-2Page 8
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
42P
R T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
16.
1 ba
r (2
34 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R11
2 53
0 kg
(
248
100
lb)
100
000
kg
(22
0 46
0 lb
) 9
0 00
0 kg
(
198
410
lb)
8
0 0
00
kg
(17
6 0
00
lb)
7
0 0
00
kg
(15
4 3
25
lb)
L_AC_070802_1_0030101_01_01
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 592 000 kg - A380-800F Models
7-8-2Page 9
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)R
AD
IUS
OF
RE
LAT
IVE
ST
IFF
NE
SS
(m
m)
508
762
1016
152
203
2540
WE
IGH
T O
N O
NE
BO
DY
LA
ND
ING
GE
AR
168
800
kg
(372
125
lb)
160 0
00 k
g (
352 7
50 lb
)150 0
00 k
g (
330 7
00 lb
)140 0
00 k
g (
308 6
50 lb
)130 0
00 k
g (
286 6
00 lb
)
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
G
L_AC_070802_1_0040101_01_01
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 592 000 kg - A380-800F Models
7-8-2Page 10
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x530
R23
42P
R T
IRE
ST
IRE
PR
ES
SU
RE
CO
NS
TA
NT
AT
16.
1 ba
r (2
34 p
si)
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S (
mm
)
508
762
1016
1524
2032
2540
MA
XIM
UM
PO
SS
IBLE
WIN
G
GE
AR
LO
AD
AT
MA
XIM
UM
R
AM
P W
EIG
HT
AN
D A
FT
CG
WE
IGH
T O
N O
NE
WIN
G
LAN
DIN
G G
EA
R11
4 38
0 kg
(
252
175
lb)
100
000
kg
(22
0 46
0 lb
) 9
0 00
0 kg
(
198
410
lb)
8
0 0
00
kg
(17
6 0
00
lb)
7
0 0
00
kg
(15
4 3
25
lb)
L_AC_070802_1_0070101_01_00
Rigid Pavement Requirements LCN - 4 Wheel BogieMRW 602 000 kg - A380-800F Models
7-8-2Page 11
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2030
4050
100
9080
7060
102030405060708090100
110
120
RA
DIU
S O
F R
ELA
TIV
E S
TIF
FN
ES
S [I
NC
HE
S]
EQUIVALENT SINGLE WHEEL LOAD [1000 lb]
120
150
6070
8090
100
50
LOA
D C
LAS
SIF
ICA
TIO
N N
UM
BE
R (
LCN
)
5101520253035404550
EQUIVALENT SINGLE WHEEL LOAD [1000 kg]
NO
TE
: EQ
UIV
ALE
NT
SIN
GLE
WH
EE
L LO
AD
S A
RE
DE
RIV
ED
BY
ME
TH
OD
S S
HO
WN
IN
ICA
O A
ER
OD
RO
ME
MA
NU
AL
PA
RT
2 P
AR
4.1
.3
Sec
ond
Edi
tion
1965
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)R
AD
IUS
OF
RE
LAT
IVE
ST
IFF
NE
SS
(m
m)
508
762
101
1524
2032
2540
MA
XIM
UM
PO
SS
IBLE
BO
DY
G
EA
R L
OA
D A
T M
AX
IMU
M
RA
MP
WE
IGH
T A
ND
AF
T C
GW
EIG
HT
ON
ON
E B
OD
Y
LAN
DIN
G G
EA
R17
1 58
0 kg
(3
78 2
50 lb
)160 0
00 k
g (
352 7
50 lb
)150 0
00 k
g (
330 7
00 lb
)140 0
00 k
g (
308 6
50 lb
)130 0
00 k
g (
286 6
00 lb
)
L_AC_070802_1_0080101_01_00
Rigid Pavement Requirements LCN - 6 Wheel BogieMRW 602 000 kg - A380-800F Models
7-8-2Page 12
Oct 01/09
@A380AIRPLANE 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, Figure: Radius of Relative Stiffness, presents ”L” values based onYoung’s Modulus (E) of 4 000 000 psi and Poisson’s Ratio (µ) of 0.15.
To find ”L” values based on other values of E and µ, see section 7-8-4, Figure: Radius of RelativeStiffness (other values of E and µ).
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, Figure: Radius of Relative Stiffness.
The effect of variations of µ on the ”L” value is treated in a similar manner.
7-8-3Page 1
Oct 01/09
@A380AIRPLANE 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.
7-8-4Page 1
Oct 01/09
@A380AIRPLANE 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
AC
TO
R
E, YOUNG S MODULUS (10 psi),
, POISSON’S RATIO
FA
CT
OR
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
7-8-4Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
7-9-0 ACN/PCN Reporting System
**ON A/C A380-800 Models A380-800F Models
ACN/PCN Reporting System
1. GeneralTo find the ACN of an aircraft on flexible or rigid pavement, the aircraft gross weight and thesubgrade strength must be known.
A380-800 model:
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MRW 512 000 kg - A380-800 Models, for an Aircraft Gross Weight of 440 000 kg (970 035 lb) andmedium subgrade strength (code B), the ACN for the flexible pavement is 46.
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MRW 562 000 kg - A380-800 Models, for an Aircraft Gross Weight of 510 000 kg (1 124 360 lb) andmedium subgrade strength (code B), the ACN for the flexible pavement is 56.
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MRW 571 000 kg - A380-800 Models, for an Aircraft Gross Weight of 510 000 kg (1 124 360 lb) andmedium subgrade strength (code B), the ACN for the flexible pavement is 55.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Flexible Pavement -MRW 512 000 kg - A380-800 Models, for an Aircraft Gross Weight of 440 000 kg (970 035 lb) andmedium subgrade strength (code B), the ACN for the rigid pavement is 46.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Flexible Pavement -MRW 562 000 kg - A380-800 Models, for an Aircraft Gross Weight of 510 000 kg (1 124 360 lb) andmedium subgrade strength (code B), the ACN for the rigid pavement is 58.5.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Flexible Pavement -MRW 571 000 kg - A380-800 Models, for an Aircraft Gross Weight of 510 000 kg (1 124 360 lb) andmedium subgrade strength (code B), the ACN for the flexible pavement is 58.
A380-800F model:
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MRW 592 000 kg - A380-800F Models, for an Aircraft Gross Weight of 510 000 (1 124 360 lb) andmedium subgrade strength (code B), the ACN for the flexible pavement is 55.
7-9-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
In the example shown in Section 7-9-1, Figure: Aircraft Classification Number - Flexible Pavement -MRW 602 000 Kg - A380-800F Models, for an Aircraft Gross Weight of 510 000 (1 124 360 lb) andmedium subgrade strength (code B), the ACN for the rigid pavement is 55.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Flexible Pavement -MRW 592 000 Kg - A380-800F Models, for an Aircraft Gross Weight of 510 000 (1 124 360 lb) andmedium subgrade strength (code B), the ACN for the rigid pavement is 60.
In the example shown in Section 7-9-2, Figure: Aircraft Classification Number - Flexible Pavement -MRW 602 000 Kg - A380-800F Models, for an Aircraft Gross Weight of 510 000 (1 124 360 lb) andmedium 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)
7-9-0Page 2
Oct 01/09
@A380AIRPLANE 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.
7-9-1Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2030405060708090100 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4 ba
r (2
03 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 43
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
g on
Pav
emen
t − M
RW
512
000
kg
− A
380−
800
Mod
els
[x10
00 k
g]
[x10
00 lb
]
L_AC_070901_1_0050101_01_00
ALP
HA
FA
CT
OR
= 0
.8
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
Aircraft Classification Number - Flexible PavementMRW 512 000 kg - A380-800 Models
7-9-1Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070901_1_0060101_01_00
2030405060708090100
110
120 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1300
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 43
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
gon
Pav
emen
t − M
RW
562
000
kg
− A
380−
800
Mod
els
[x10
00 k
g]
[x10
00 lb
]
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
Aircraft Classification Number - Flexible PavementMRW 562 000 kg - A380-800 Models
7-9-1Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070901_1_0070101_01_00
2030405060708090100
110
120 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1300
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 41
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
gon
Pav
emen
t − M
RW
571
000
kg
− A
380−
800
Mod
els
[x10
00 k
g]
[x10
00 lb
]
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
ALP
HA
FA
CT
OR
= 0
.8
Aircraft Classification Number - Flexible PavementMRW 571 000 kg - A380-800 Models
7-9-1Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aircraft Classification Number - Flexible Pavement - Freighter
1. This section gives the Aircraft Classification Number - Flexible Pavement.
7-9-1Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070901_1_0080101_01_00
2030405060708090100
110
120 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1300
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 42.
8 %
MA
C.
See
Sec
tion
7−4−
1 F
igur
e: L
andi
ng G
ear
Load
ing
on P
avem
ent −
MR
W 5
92 0
00 k
g −
A38
0−80
0F M
odel
s
[x10
00 k
g]
[x10
00 lb
]
ALP
HA
FA
CT
OR
= 0
.8
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
Aircraft Classification Number - Flexible PavementMRW 592 000 kg - A380-800F Models
7-9-1Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
L_AC_070901_1_0090101_01_00
2030405060708090100
110
120 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1300
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 42.
7 %
MA
C.
See
Sec
tion
7−4−
1 F
igur
e: L
andi
ng G
ear
Load
ing
on P
avem
ent −
MR
W 6
02 0
00 k
g −
A38
0−80
0F M
odel
s
[x10
00 k
g]
[x10
00 lb
]
ALP
HA
FA
CT
OR
= 0
.8
SU
BG
RA
DE
ST
RE
NG
TH
D −
CB
R 3
(U
LTR
A L
OW
)C
− C
BR
6 (
LOW
)B
− C
BR
10
(ME
DIU
M)
A −
CB
R 1
5 (H
IGH
)
Aircraft Classification Number - Flexible PavementMRW 602 000 kg - A380-800F Models
7-9-1Page 7
Oct 01/09
@A380AIRPLANE 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.
7-9-2Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
L_AC_070902_1_0050101_01_00
2030405060708090100 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
4 ba
r (2
03 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 43
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
gon
Pav
emen
t − M
RW
512
000
kg
− A
380−
800
Mod
els
[x10
00 k
g]
[x10
00 lb
]
SU
BG
RA
DE
ST
RE
NG
TH
D −
k =
20
MN
/m³
(ULT
RA
LO
W)
C −
k =
40
MN
/m³
(LO
W)
B −
k =
80
MN
/m³
(ME
DIU
M)
A −
k =
150
MN
/m³
(HIG
H)
Aircraft Classification Number - Rigid PavementMRW 512 000 kg - A380-800 Models
7-9-2Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2030405060708090100
110
120 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1300
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 43
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
gon
Pav
emen
t − M
RW
562
000
kg
− A
380−
800
Mod
els
[x10
00 k
g]
SU
BG
RA
DE
ST
RE
NG
TH
D −
k =
20
MN
/m³
(ULT
RA
LO
W)
C −
k =
40
MN
/m³
(LO
W)
B −
k =
80
MN
/m³
(ME
DIU
M)
A −
k =
150
MN
/m³
(HIG
H)
[x10
00 lb
]
L_AC_070902_1_0060101_01_00
Aircraft Classification Number - Rigid PavementMRW 562 000 kg - A380-800 Models
7-9-2Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
2030405060708090100
110
120 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1300
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
0PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
5 ba
r (2
18 p
si)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 41
% M
AC
.S
ee S
ectio
n 7−
4−1
Fig
ure:
Lan
ding
Gea
r Lo
adin
gon
Pav
emen
t − M
RW
571
000
kg
− A
380−
800
Mod
els
[x10
00 k
g]
[x10
00 lb
]
L_AC_070902_1_0070101_01_00
SU
BG
RA
DE
ST
RE
NG
TH
D −
k =
20
MN
/m³
(ULT
RA
LO
W)
C −
k =
40
MN
/m³
(LO
W)
B −
k =
80
MN
/m³
(ME
DIU
M)
A −
k =
150
MN
/m³
(HIG
H)
Aircraft Classification Number - Rigid PavementMRW 571 000 kg - A380-800 Models
7-9-2Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
Aircraft Classification Number - Rigid Pavement - Freighter
1. This section gives the Aircraft Classification Number - Rigid Pavement.
7-9-2Page 5
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
2030405060708090100
110
120 26
028
030
032
034
036
038
040
042
044
046
048
050
052
054
056
058
060
0
AIR
CR
AF
T G
RO
SS
WE
IGH
T
AIRCRAFT CLASSIFICATION NUMBER (ACN)
1300
1200
1100
1000
900
800
700
600
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 42.
8 %
MA
C.
See
Sec
tion
7−4−
1 F
igur
e: L
andi
ng G
ear
Load
ing
on P
avem
ent −
MR
W 5
92 0
00 k
g −
A38
0−80
0F M
odel
s
[x10
00 k
g]
[x10
00 lb
]
SU
BG
RA
DE
ST
RE
NG
TH
D −
k =
20
MN
/m³
(ULT
RA
LO
W)
C −
k =
40
MN
/m³
(LO
W)
B −
k =
80
MN
/m³
(ME
DIU
M)
A −
k =
150
MN
/m³
(HIG
H)
L_AC_070902_1_0080101_01_00
Aircraft Classification Number - Rigid PavementMRW 592 000 kg - A380-800F Models
7-9-2Page 6
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
600
1400
x 5
30R
23 4
2PR
TIR
ES
TIR
E P
RE
SS
UR
E C
ON
ST
AN
T A
T 1
6.1
bar
(234
psi
)
AC
N W
AS
DE
TE
RM
INE
D A
S R
EF
ER
EN
CE
D IN
IC
AO
AE
RO
DR
OM
E D
ES
IGN
MA
NU
AL
PA
RT
3C
HA
PT
ER
1 S
EC
ON
D E
DIT
ION
198
3.C
G U
SE
D F
OR
AC
N C
ALC
ULA
TIO
NS
: 42.
7 %
MA
C.
See
Sec
tion
7−4−
1 F
igur
e: L
andi
ng G
ear
Load
ing
on P
avem
ent −
MR
W 6
02 0
00 k
g −
A38
0−80
0F M
odel
s
[x10
00 k
g]
20406080100
120
AIRCRAFT CLASSIFICATION NUMBER (ACN)
AIR
CR
AF
T G
RO
SS
WE
IGH
T
1300
1200
1100
1000
900
800
700
600
[x10
00 lb
]
SU
BG
RA
DE
ST
RE
NG
TH
D −
k =
20
MN
/m³
(ULT
RA
LO
W)
C −
k =
40
MN
/m³
(LO
W)
B −
k =
80
MN
/m³
(ME
DIU
M)
A −
k =
150
MN
/m³
(HIG
H)
L_AC_070902_1_0090101_01_00
Aircraft Classification Number - Rigid PavementMRW 602 000 kg - A380-800F Models
7-9-2Page 7
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
DERIVATIVE AIRPLANES
8-1-0 Possible Future Derivative Airplanes
**ON A/C A380-800 Models A380-800F Models
Possible Future Derivative Airplanes
1. General
Other versions of the A380 airplane are being studied to satisfy customer requests.
In the future, this program could have new versions:- Additional passenger capacity,- Additional cargo modularity,- New design version,- Different range or payload.
If these new aircraft definitions are developed, the design and weight will be considered in accordancewith airport facilities.
8-1-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
SCALED DRAWINGS
9-1-0 Scaled Drawing - 1 cm. = 500 cm.
**ON A/C A380-800 Models A380-800F Models
Scaled Drawing - 1 cm. = 500 cm.
1. This section provides the Scaled Drawing - 1 cm = 500 cm.
9-1-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
AIR CONDITIONINGBULK CARGO COMPT DOORBODY LANDING GEARCARGO COMPT DOORELECTRICALFUEL
POTABLE WATERLAVATORYNOSE LANDING GEAR
PASSENGER/CREW DOOR
ABBLGCEF
LNLG
X
PNEUMATICPWING LANDING GEARWLG
DB1A L_AC_090100_1_0010101_01_02
E
A
NLG
XX
X
X
X
F
WLG
X
P
X
WLG
F
BLGBLG
X
X
X
X
L
C
B
C
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
H²0
H²0
LEGEND:
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
Scaled Drawing -- 1 cm. = 500 cm.A380-800 Models
9-1-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
DB1A
X
C
BLG BLG
C
B
WLG
F
A
C
X
NLG
XE
C
P
F
WLG
L_AC_090100_1_0020101_01_03
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
H²0
LEGEND:
AIR CONDITIONINGBULK CARGO COMPT DOORBODY LANDING GEARCARGO COMPT DOORELECTRICALFUEL
POTABLE WATERLAVATORYNOSE LANDING GEAR
PASSENGER/CREW DOOR
ABBLGCEF
LNLG
X
PNEUMATICPWING LANDING GEARWLG
H²0
Scaled Drawing -- 1 cm. = 500 cm.A380-800F Models
9-1-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
DB1A L_AC_090100_1_0030101_01_02
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
Scaled Drawing -- 1 cm. = 500 cm.A380-800 Models
9-1-0Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
DB1A L_AC_090100_1_0040101_01_02
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
Scaled Drawing -- 1 cm. = 500 cm.A380-800F Models
9-1-0Page 5
Oct 01/09
@A380AIRPLANE 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.
9-2-0Page 1
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
DB1AL_AC_090200_1_0010101_01_03
E
A
NLG
XX
X
X
X
F
WLG
X
P
X
WLG
F
BLGBLG
X
X
X
X
L
C
B
C
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
H²0
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
LEGEND:
AIR CONDITIONINGBULK CARGO COMPT DOORBODY LANDING GEARCARGO COMPT DOORELECTRICALFUEL
POTABLE WATERLAVATORYNOSE LANDING GEAR
PASSENGER/CREW DOOR
ABBLGCEF
LNLG
X
PNEUMATICPWING LANDING GEARWLG
H²0
Scaled Drawing -- 1 in. = 50 ft.A380-800 Models
9-2-0Page 2
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
DB1AL_AC_090200_1_0020101_01_04
X
C
BLG BLG
C
B
WLG
F
A
C
X
NLG
XE
C
P
F
WLG
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
H²0
LEGEND:
AIR CONDITIONINGBULK CARGO COMPT DOORBODY LANDING GEARCARGO COMPT DOORELECTRICALFUEL
POTABLE WATERLAVATORYNOSE LANDING GEAR
PASSENGER/CREW DOOR
ABBLGCEF
LNLG
X
PNEUMATICPWING LANDING GEARWLG
H²0
Scaled Drawing -- 1 in. = 50 ft.A380-800F Models
9-2-0Page 3
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800 Models
DB1AL_AC_090200_1_0030101_01_03
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
Scaled Drawing -- 1 in. = 50 ft.A380-800 Models
9-2-0Page 4
Oct 01/09
@A380AIRPLANE CHARACTERISTICS
**ON A/C A380-800F Models
DB1AL_AC_090200_1_0040101_01_03
010
2030
4050
60F
EE
T
04
812
1620
ME
TE
RS
0 10 20 30 40 50 60FEET
0 4 8 12 16 20METERS
NOTE: WHEN PRINTING THIS DRAWING, MAKE SURE TO ADJUST FOR PROPER SCALING
Scaled Drawing -- 1 in. = 50 ft.A380-800F Models
9-2-0Page 5
Oct 01/09
