maintenance facility planning
TRANSCRIPT
@AIRBUSA380
MAINTENANCE FACILITY PLANNING
MFP
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© AIRBUS S.A.S. 2005. All rights reserved.
AIRBUS S.A.S.Customer Services
Technical Data Support and Services31707 Blagnac Cedex
FRANCE
Issue: Nov 01/08 Rev: Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
HIGHLIGHTS
Revision No. 8 - Oct 01/09
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
CHAPTER 1
Section 1-3
General Airplane Characteristics Data R ADDED WEIGHT VARIANT WV000 TOWV003DESCRIPTION TITLE UPDATED
Section 1-10
FIGURE Door Clearances - Aft CargoCompartment Doors - A380-800 Models
R
FIGURE Door Clearances - Lower DeckAft Cargo Doors - A380-800F Models
R
FIGURE Door Clearances - Upper DeckCargo Door - A380-800F Models
R
FIGURE Door Clearances - Lower DeckForward Cargo Door - A380-800F Models
R
CHAPTER 2
Section 2-3
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 2-8
Towing R NOTE AMENDED
HIGHLIGHTSPage 1
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@A380MAINTENANCE FACILITY PLANNING
LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE Ground Towing Requirements -Ground Towing Requirements A380-800Models
R ILLUSTRATION REVISED
FIGURE Ground Towing Requirements -Typical Tow Bar configuration 1
R ILLUSTRATION REVISED
FIGURE Ground Towing Requirements -Typical Tow Bar configuration 2
R ILLUSTRATION REVISED
FIGURE Ground Towing Requirements -Nose Gear Towing Fittings
R ILLUSTRATION REVISEDPART EFFECTIVITYADDED/REVISED/DELETED
FIGURE Ground Towing Requirements -Maximum Extension of the NLG ShockAbsorber
N ILLUSTRATION ADDED
Section 2-9
Ground Maneuvering R
FIGURE Turning Radii - Turning Radii(Sheet 1)
R
FIGURE Turning Radii - Turning Radii(Sheet 2)
R
FIGURE 135˚ Turn - Runway to Taxiway- 135˚ Turn - Runway to Taxiway (Sheet1)
R ILLUSTRATION REVISED
FIGURE 135˚ Turn - Runway to Taxiway- 135˚ Turn - Runway to Taxiway (Sheet2)
R ILLUSTRATION REVISED
FIGURE 90˚ Turn - Runway to Taxiway -90˚ Turn - Runway to Taxiway (Sheet 1)
R ILLUSTRATION REVISED
FIGURE 90˚ Turn - Runway to Taxiway -90˚ Turn - Runway to Taxiway (Sheet 2)
R ILLUSTRATION REVISED
FIGURE 180˚ Turn on a Runway - 180˚Turn on a Runway
R ILLUSTRATION REVISED
FIGURE 90˚ Turn - Taxiway to Taxiway- 90˚ Turn - Taxiway to Taxiway (Sheet1)
R ILLUSTRATION REVISED
HIGHLIGHTSPage 2
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LOCATIONS CHGCODE
DESCRIPTIONS OF CHANGE
FIGURE 90˚ Turn - Taxiway to Taxiway- 90˚ Turn - Taxiway to Taxiway (Sheet2)
R ILLUSTRATION REVISED
FIGURE 135˚ Turn - Taxiway to Taxiway- 135˚ Turn - Taxiway to Taxiway (Sheet1)
R ILLUSTRATION REVISED
FIGURE 135˚ Turn - Taxiway to Taxiway- 135˚ Turn - Taxiway to Taxiway (Sheet2)
R ILLUSTRATION REVISED
Section 2-11
Operating Conditions R
CHAPTER 3
Section 3-1
Airplane Maintenance Jacking R
FIGURE Jacking Points Location -Jacking Points Location
R ILLUSTRATION REVISED
Section 3-14
Power Plant R
FIGURE Fan Cowls - TRENT 900 Engines R
FIGURE Fan Cowls - Engine 1-2-3-4 - GP7200 Engines
N ILLUSTRATION ADDED
FIGURE Fan Exhaust Cowls - Engine 1-4- GP 7200 Engines
N ILLUSTRATION ADDED
FIGURE Thrust Reverser - Engine 2-3 -GP 7200 Engines
N ILLUSTRATION ADDED
HIGHLIGHTSPage 3
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@A380MAINTENANCE FACILITY PLANNING
LIST OF EFFECTIVE CONTENT
Revision No. 8 - Oct 01/09
CONTENT CHGCODE
LAST REVISIONDATE
CHAPTER 0
Section 0-1
Introduction Jun 01/07
Section 0-2
Alphabetical Index Nov 01/08
Section 0-3
Section Index Nov 01/08
Section 0-4
Glossary Nov 01/08
CHAPTER 1
Section 1-1
Airplane Overall Dimensions and Outline Basic Reference Drawing Jun 01/07
FIGURE Airplane Overall Dimensions and Outline Basic ReferenceDrawing - A380-800 Models
Jun 01/07
FIGURE Airplane Overall Dimensions and Outline Basic ReferenceDrawing - A380-800F Models
Jun 01/07
Section 1-2
Airplane Dimensions Jun 01/07
FIGURE Airplane Dimensions - Airplane Dimensions (Sheet 1) Nov 01/08
FIGURE Airplane Dimensions - Airplane Dimensions (Sheet 2) Jun 01/07
Section 1-3
General Airplane Characteristics Data R Oct 01/09
Section 1-4
Zoning and Access Jun 01/07
FIGURE Aircraft Zoning - Major Zones Jun 01/07
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 100 (Sheet 1) Jun 01/07
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 100 (Sheet 2) Jun 01/07
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 200 Jun 01/07
L.E.C.Page 1
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LAST REVISIONDATE
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 300 Jun 01/07
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 400 - TRENT 900Engines
Jan 31/08
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 400 -- GP 7200Engines
Jan 31/08
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 500/600 Jun 01/07
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 700 Jun 01/07
FIGURE Aircraft Zoning - Major Sub-Zones - Zone 800 Jun 01/07
Section 1-5
Fuselage Frames / Stations Jun 01/07
FIGURE Fuselage Frames/Stations - Sections Identification -A380-800 Models
Jun 01/07
FIGURE Fuselage Frames/Stations - Sections Identification -A380-800F Models
Jun 01/07
FIGURE Fuselage Frames/Stations - Section 11/12 - A380-800Models
Jun 01/07
FIGURE Fuselage Frames/Stations - Section 11/12 - A380-800FModels
Jun 01/07
FIGURE Fuselage Frames/Stations - Section 13 - A380-800 Models Jun 01/07
FIGURE Fuselage Frames/Stations - Section 13 - A380-800F Models Jun 01/07
FIGURE Fuselage Frames/Stations - Section 15/21 - A380-800Models
Jun 01/07
FIGURE Fuselage Frames/Stations - Section 15/21 - A380-800FModels
Jun 01/07
FIGURE Fuselage Frames/Stations - Section 18 - A380-800 Models Jun 01/07
FIGURE Fuselage Frames/Stations - Section 18 - A380-800F Models Jun 01/07
FIGURE Fuselage Frames/Stations - Section 19 Jun 01/07
Section 1-6
Wing Ribs / Stations Jun 01/07
FIGURE Wing Ribs/Stations - Wing Ribs/Stations (Sheet 1) Jun 01/07
FIGURE Wing Ribs/Stations - Wing Ribs/Stations (Sheet 2) Jun 01/07
FIGURE Wing Ribs/Stations - Wing Ribs/Stations (Sheet 3) Jun 01/07
L.E.C.Page 2
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Wing Ribs/Stations - Flap Track Positions Jan 31/08
Section 1-7
Center of Gravity Limits Nov 01/08
FIGURE Center of Gravity Limits - MTOW 510000 kg- A380-800Models
Nov 01/08
FIGURE Center of Gravity Limits - MTOW 560000 kg - A380-800Models
Nov 01/08
FIGURE Center of Gravity Limits - MTOW 569000 kg - A380-800Models
Nov 01/08
FIGURE Center of Gravity Limits - MTOW 590000 kg - A380-800FModels
Nov 01/08
FIGURE Center of Gravity Limits - MTOW 600000 kg - A380-800FModels
Nov 01/08
Section 1-8
Airplane Attitude Nov 01/08
FIGURE NLG Shock-Absorber Deflection - NLG Shock-AbsorberDeflection - A380-800 Models
Nov 01/08
FIGURE NLG Shock-Absorber Deflection - NLG Shock-AbsorberDeflection - A380-800F Models
Nov 01/08
FIGURE NLG Tire Deflection 50 % Load - NLG Tire Deflection 50 %Load - A380-800 Models
Nov 01/08
FIGURE NLG Tire Deflection 100 % Load - NLG Tire Deflection 100% Load - A380-800 Models
Nov 01/08
FIGURE NLG Tire Deflection 50 % Load - NLG Tire Deflection 50 %Load - A380-800F Models
Nov 01/08
FIGURE NLG Tire Deflection 100 % Load - NLG Tire Deflection 100% Load - A380-800F Models
Nov 01/08
FIGURE WLG Shock-Absorber Deflection - WLG Shock-AbsorberDeflection - A380-800 Models
Nov 01/08
FIGURE WLG Shock-Absorber Deflection - WLG Shock-AbsorberDeflection - A380-800F Models
Nov 01/08
FIGURE WLG Tire Deflection 25 % Load - WLG Tire Deflection 25% Load - A380-800 Models
Nov 01/08
FIGURE WLG Tire Deflection 50 % Load - WLG Tire Deflection 50% Load - A380-800 Models
Nov 01/08
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE WLG Tire Deflection 25 % Load - WLG Tire Deflection 25% Load - A380-800F Models
Nov 01/08
FIGURE WLG Tire Deflection 50 % Load - WLG Tire Deflection 50% Load - A380-800F Models
Nov 01/08
FIGURE BLG Shock-Absorber Deflection - BLG Shock-AbsorberDeflection - A380-800 Models
Nov 01/08
FIGURE BLG Shock-Absorber Deflection - BLG Shock-AbsorberDeflection - A380-800F Models
Nov 01/08
FIGURE BLG Tire Deflection 16.7 % Load - BLG Tire Deflection 16.7% Load - A380-800 Models
Nov 01/08
FIGURE BLG Tire Deflection 25 % Load - BLG Tire Deflection 25 %Load - A380-800 Models
Nov 01/08
FIGURE BLG Tire Deflection 33.3 % Load - BLG Tire Deflection 33.3% Load - A380-800 Models
Nov 01/08
FIGURE BLG Tire Deflection 50 % Load - BLG Tire Deflection 50 %Load - A380-800 Models
Nov 01/08
FIGURE BLG Tire Deflection 16.7 % Load - BLG Tire Deflection 16.7% Load - A380-800F Models
Nov 01/08
FIGURE BLG Tire Deflection 25 % Load - BLG Tire Deflection 25 %Load - A380-800F Models
Nov 01/08
FIGURE BLG Tire Deflection 33.3 % Load - BLG Tire Deflection 33.3% Load - A380-800F Models
Nov 01/08
FIGURE BLG Tire Deflection 50 % Load - BLG Tire Deflection 50 %Load - A380-800F Models
Nov 01/08
FIGURE WLG Tire Deflection Notes - WLG Tire Deflection Jun 01/07
FIGURE BLG Tire Deflection Notes - BLG Tire Deflection Jun 01/07
FIGURE BLG Tire Deflection Notes - BLG Tire Deflection Notes Jun 01/07
Section 1-9
Ground Clearances Jun 01/07
FIGURE Ground Clearances - A380-800 Models Jun 01/07
FIGURE Ground Clearances - A380-800F Models Jun 01/07
FIGURE Ground Clearances - Leading Edge Slats - Extended -A380-800 Models
Jun 01/07
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Ground Clearances - Leading Edge Slats - Extended -A380-800F Models
Jun 01/07
FIGURE Ground Clearances - Trailing Edge Flaps - Extended Jun 01/07
FIGURE Ground Clearances - Spoilers - Extended - A380-800 Models Jun 01/07
FIGURE Ground Clearances - Spoilers - Extended - A380-800F Models Jun 01/07
FIGURE Ground Clearances - Ailerons - Down Jun 01/07
FIGURE Ground Clearances - Ailerons - Up Jun 01/07
FIGURE Ground Clearances - Flap Tracks - Extended Jun 01/07
FIGURE Ground Clearances - Forward Nose Landing Gear Doors Jun 01/07
FIGURE Ground Clearances - Aft Nose Landing Gear Doors Jun 01/07
FIGURE Ground Clearances - Wing Landing Gear Doors Jun 01/07
FIGURE Ground Clearances - Body Landing Gear Doors - Sheet 1/2 Jun 01/07
FIGURE Ground Clearances - Body Landing Gear Doors - Sheet 2/2 Jun 01/07
FIGURE Ground Clearances - APU Doors Jun 01/07
Section 1-10
Door Clearances 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
FIGURE Door Clearances - Door Location (Sheet 1) - A380-800FModels
Jun 01/07
FIGURE Door Clearances - Door Location (Sheet 2) - A380-800FModels
Jun 01/07
FIGURE Door Clearances - Forward Doors Jun 01/07
FIGURE Door Clearances - Main and Upper Deck Doors - A380-800Models
Jun 01/07
FIGURE Door Clearances - Upper Deck Doors - A380-800F Models Jun 01/07
FIGURE Door Clearances - Aft Doors - A380-800 Models Jun 01/07
FIGURE Door Clearances - Aft Doors - A380-800F Models Jun 01/07
FIGURE Door Clearances - Aft Cargo Compartment Doors -A380-800 Models
R Oct 01/09
L.E.C.Page 5
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Door Clearances - Main Deck Cargo Door - A380-800FModels
Jun 01/07
FIGURE Door Clearances - Lower Deck Aft Cargo Doors - A380-800FModels
R Oct 01/09
FIGURE Door Clearances - Forward Cargo Compartment Doors -A380-800 Models
Jun 01/07
FIGURE Door Clearances - Upper Deck Cargo Door - A380-800FModels
R Oct 01/09
FIGURE Door Clearances - Lower Deck Forward Cargo Door -A380-800F Models
R Oct 01/09
Section 1-11
Fuselage Cross-sections Jun 01/07
FIGURE Fuselage Cross-Section - Section 11/12 - FR0 to FR7 Jun 01/07
FIGURE Fuselage Cross-Section - Section 11/12 - FR8 to FR11 Jun 01/07
FIGURE Fuselage Cross-Section - Section 11/12 - FR12 to FR15 Jun 01/07
FIGURE Fuselage Cross-Section - Section 11/12 - FR15A to FR17C Jun 01/07
FIGURE Fuselage Cross-Section - Section 11/12 - FR18A to FR19B Jun 01/07
FIGURE Fuselage Cross-Section - Section 11/12 - FR20 to FR22 Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR23 to FR26 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR23 to FR26 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR27 to FR28 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR27 to FR28 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR29 to FR30 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR29 to FR30 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR31 to FR32 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR31 to FR32 -A380-800F Models
Jun 01/07
L.E.C.Page 6
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Fuselage Cross-Section - Section 13 - FR33 to FR34 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR33 to FR34 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR35 to FR36 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR35 to FR36 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR37 to FR38 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 13 - FR37 to FR38 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR39 to FR40 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR39 to FR40 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR41 to FR42 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR41 to FR42 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR43 to FR44 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR43 to FR44 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR45 to FR48 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR45 to FR48 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR49 to FR50 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR49 to FR50 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR51 to FR54 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR51 to FR54 -A380-800F Models
Jun 01/07
L.E.C.Page 7
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Fuselage Cross-Section - Section 15/21 - FR55 to FR58 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR55 to FR58 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR59 to FR60 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR59 to FR60 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR61 to FR64 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR61 to FR64 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR65 to FR68 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR65 to FR68 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR69 to FR70 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR65 to FR68 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR71 to FR72 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR71 to FR72 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR73 to FR74 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 15/21 - FR73 to FR74 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR75 to FR78 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR75 to FR78 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR79 to FR81 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR82 to FR83 -A380-800 Models
Jun 01/07
L.E.C.Page 8
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LAST REVISIONDATE
FIGURE Fuselage Cross-Section - Section 18 - FR82 to FR83 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR84 to FR85 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR84 to FR85 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR86 to FR89 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR86 to FR89 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR90 to FR92 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR90 to FR92 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR93 to FR95 -A380-800 Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 18 - FR93 to FR95 -A380-800F Models
Jun 01/07
FIGURE Fuselage Cross-Section - Section 19 - FR96 to FR98 Jun 01/07
FIGURE Fuselage Cross-Section - Section 19 - FR99 to FR102 Jun 01/07
FIGURE Fuselage Cross-Section - Section 19 - FR103 to FR106 Jun 01/07
FIGURE Fuselage Cross-Section - Section 19 - FR107 to FR110 Jun 01/07
FIGURE Fuselage Cross-Section - Section 19 - FR111 to FR114 Jun 01/07
FIGURE Fuselage Cross-Section - Section 19.1 - FR115 to FR119 Jun 01/07
Section 1-12
Nose Contours Jun 01/07
FIGURE Nose Contours - Level Positions - A380-800 Models Jun 01/07
FIGURE Nose Contours - Level Positions - A380-800F Models Jan 31/08
FIGURE Nose Contours - Contour Points at Frame Positions -A380-800 Models
Nov 01/08
FIGURE Nose Contours - Contour Points at Frame Positions -A380-800F Models
Nov 01/08
FIGURE Nose Contours - Upper and Lower Contours - A380-800Models
Jun 01/07
L.E.C.Page 9
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Nose Contours - Upper and Lower Contours - A380-800FModels
Jun 01/07
Section 1-13
Vertical Stabilizer Contours Jun 01/07
FIGURE Vertical Stabilizer Contours - Level Positions Jun 01/07
FIGURE Vertical Stabilizer Contours - Vertical Stabilizer Contours Jun 01/07
Section 1-14
Horizontal Stabilizer Contours Jun 01/07
FIGURE Horizontal Stabilizer Contours - Horizontal StabilizerContours (Sheet 1)
Jun 01/07
FIGURE Horizontal Stabilizer Contours - Horizontal StabilizerContours (Sheet 2)
Jun 01/07
FIGURE Horizontal Stabilizer Contours - Level Positions Jun 01/07
Section 1-15
Tail Contours Jun 01/07
FIGURE Tail Contours - Tail Contours Jun 01/07
FIGURE Tail Contours - Level Positions Jan 31/08
Section 1-16
General Nov 01/08
FIGURE Wing Profile - Rib Locations Jun 01/07
FIGURE Wing Profile - Rib Positions Jun 01/07
FIGURE Wing Profile - Wing Profile Jun 01/07
Section 1-17
Nacelle Contours Nov 01/08
FIGURE Nacelle Contours - Nacelle Contours - TRENT 900 Engines Jan 31/08
FIGURE Nacelle Contours - Nacelle Contours - GP 7200 Engines Jan 31/08
CHAPTER 2
Section 2-1
Airplane Servicing Arrangement Jun 01/07
FIGURE Typical Ramp Layout -- Two Bridges - Servicing Via Mainand Upper Decks
Jun 01/07
L.E.C.Page 10
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Typical Ramp Layout -- Two Bridges - Servicing Via MainDeck
Jun 01/07
FIGURE Opportunities of Direct Upper Deck Access - for Airport andAirlines
Jun 01/07
FIGURE Typical Ramp Layout - Typical Ramp Layout Jun 01/07
Section 2-2
Turnaround Stations Jun 01/07
FIGURE Baseline Turn-Round Time -- Two Bridges - Servicing ViaMain and Upper Decks
Jun 01/07
FIGURE Typical Turn-Round Time -- Two Bridges - Servicing ViaMain Deck
Jun 01/07
Section 2-3
Ground Service Connections and Locations Jun 01/07
FIGURE Ground Service Connections Layout - A380-800 Models Jun 01/07
FIGURE Ground Service Connections Layout - A380-800F Models Jun 01/07
Hydraulic System Nov 01/08
FIGURE Ground Service Connections - Hydraulic Reservoir ServicingPanel
Jun 01/07
FIGURE Ground Service Connections - Hydraulic Ground Connections Jun 01/07
Electrical System Nov 01/08
FIGURE Ground Service Connections - Electrical Service Panel -A380-800 Models
Jun 01/07
FIGURE Ground Service Connections - Electrical Service Panel -A380-800F Models
Jun 01/07
Fuel System Nov 01/08
FIGURE Ground Service Connections - Refuel/Defuel Control Panel Jun 01/07
FIGURE Ground Service Connections - Pressure Refuel Connectors Jun 01/07
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
Potable Water System Nov 01/08
L.E.C.Page 11
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Ground Service Connections - Potable Water Ground ServicePanel - A380-800 Models
Jun 01/07
FIGURE Ground Service Connections - Potable Water Ground ServicePanel - A380-800F Models
Jun 01/07
FIGURE Ground Service Connections - Potable Water Drain Panel Jun 01/07
Engine Oil Servicing R Oct 01/09
FIGURE Ground Service Connections - Engine Oil Servicing - TRENT900 Engines
Jan 31/08
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
Jan 31/08
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
Vacuum Toilet System Nov 01/08
FIGURE Ground Service Connections - Vacuum Toilet System -A380-800 Models
Jun 01/07
FIGURE Ground Service Connections - Vacuum Toilet System -A380-800F Models
Jun 01/07
Oxygen System Nov 01/08
FIGURE Ground Service Connections - Oxygen System Jun 01/07
Section 2-4
Interior Arrangements Jun 01/07
FIGURE Interior Arrangements - Plan View - Standard Configuration- Upper Deck
Jun 01/07
L.E.C.Page 12
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Interior Arrangements - Plan View - Standard Configuration- Main Deck
Jun 01/07
FIGURE Interior Arrangements - Plan View - Standard Configuration- Cargo Compartments
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
FIGURE Interior Arrangements - Cross-section - Typical Configuration Jun 01/07
Section 2-5
Escape Slides Nov 01/08
FIGURE Escape Slides/Rafts - Location Jan 31/08
FIGURE Escape Slides/Rafts - Dimensions Jun 01/07
Section 2-6
Galley Jun 01/07
FIGURE General Location of Transversal Galleys - General Location ofTransversal Galleys
Jun 01/07
FIGURE General Layout - Transversal Galley (Sheet 1) Jun 01/07
FIGURE General Layout - Transversal Galley (Sheet 2) Jun 01/07
FIGURE General Location - Longitudinal Galleys Jun 01/07
FIGURE General Layout - Longitudinal Galleys (Sheet 1) Jun 01/07
FIGURE General Layout - Longitudinal Galleys (Sheet 2) Jun 01/07
Section 2-7
Cargo Jun 01/07
FIGURE Cargo Compartments - Location and Dimensions - A380-800Models
Jun 01/07
FIGURE Cargo Compartments - Location and Dimensions -A380-800F Models (Sheet 1)
Jun 01/07
FIGURE Cargo Compartments - Location and Dimensions -A380-800F Models (Sheet 2)
Jun 01/07
FIGURE Cargo Compartments - Loading Combinations - A380-800Models
Jun 01/07
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Cargo Compartments - Loading Combinations - A380-800FModels (Sheet 1)
Jun 01/07
FIGURE Cargo Compartments - Loading Combinations - A380-800FModels (Sheet 2)
Jun 01/07
Section 2-8
Towing 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
R Oct 01/09
FIGURE Ground Towing Requirements - Typical Tow Barconfiguration 2
R Oct 01/09
FIGURE Ground Towing Requirements - Nose Gear Towing Fittings R Oct 01/09
FIGURE Ground Towing Requirements - Maximum Extension of theNLG Shock Absorber
N Oct 01/09
Section 2-9
Ground Maneuvering R Oct 01/09
FIGURE Turning Radii - Turning Radii (Sheet 1) R Oct 01/09
FIGURE Turning Radii - Turning Radii (Sheet 2) R Oct 01/09
FIGURE Minimum Turning Radii - (Sheet 1) Nov 01/08
FIGURE Minimum Turning Radii - (Sheet 2) Jun 01/07
FIGURE 135˚ Turn - Runway to Taxiway - 135˚ Turn - Runway toTaxiway (Sheet 1)
R Oct 01/09
FIGURE 135˚ Turn - Runway to Taxiway - 135˚ Turn - Runway toTaxiway (Sheet 2)
R Oct 01/09
FIGURE 90˚ Turn - Runway to Taxiway - 90˚ Turn - Runway toTaxiway (Sheet 1)
R Oct 01/09
FIGURE 90˚ Turn - Runway to Taxiway - 90˚ Turn - Runway toTaxiway (Sheet 2)
R Oct 01/09
FIGURE 180˚ Turn on a Runway - 180˚ Turn on a Runway R Oct 01/09
FIGURE 90˚ Turn - Taxiway to Taxiway - 90˚ Turn - Taxiway toTaxiway (Sheet 1)
R Oct 01/09
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE 90˚ Turn - Taxiway to Taxiway - 90˚ Turn - Taxiway toTaxiway (Sheet 2)
R Oct 01/09
FIGURE 135˚ Turn - Taxiway to Taxiway - 135˚ Turn - Taxiway toTaxiway (Sheet 1)
R Oct 01/09
FIGURE 135˚ Turn - Taxiway to Taxiway - 135˚ Turn - Taxiway toTaxiway (Sheet 2)
R Oct 01/09
FIGURE Runway Holding Bay (Apron) - Runway Holding Bay(Apron)
Jun 01/07
Section 2-10
Airplane Parking Jun 01/07
FIGURE Airplane Parking - Steering Geometry Jun 01/07
FIGURE Airplane Parking - Steering Geometry - Minimum ParkingSpace Requirements
Jun 01/07
Section 2-11
Operating Conditions R Oct 01/09
FIGURE Engine Exhaust Velocities - Ground Idle Power - TRENT 900Engines
Jan 31/08
FIGURE Engine Exhaust Velocities - Ground Idle Power - GP 7200Engines
Jan 31/08
FIGURE Engine Exhaust Temperatures - Ground Idle Power --TRENT 900 Engines
Jan 31/08
FIGURE Engine Exhaust Temperatures - Ground Idle Power -- GP7200 Engines
Jan 31/08
FIGURE Engine Exhaust Velocities - Breakaway Power -- TRENT 900Engines
Jan 31/08
FIGURE Engine Exhaust Velocities - Breakaway Power -- GP 7200Engines
Jan 31/08
FIGURE Engine Exhaust Temperatures - Breakaway Power -- TRENT900 Engines
Jan 31/08
FIGURE Engine Exhaust Temperature - Breakaway Power -- GP 7200Engines
Jan 31/08
FIGURE Engine Exhaust Velocities - Max. Take-Off Power -- TRENT900 Engines
Jan 31/08
L.E.C.Page 15
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Engine Exhaust Velocities - Max. Take-Off Power -- GP 7200Engines
Jan 31/08
FIGURE Engine Exhaust Temperatures - Max. Take-Off Power --TRENT 900 Engines
Jan 31/08
FIGURE Engine Exhaust Temperatures - Max. Take-Off Power -- GP7200 Engines
Jan 31/08
FIGURE APU Exhaust Velocities and Temperatures - Max. ECSConditions
Jun 01/07
FIGURE APU Exhaust Velocities and Temperatures - MES Conditions Jun 01/07
FIGURE Airport and Community Noise Data - TRENT 900 Engines Nov 01/08
FIGURE Airport and Community Noise Data - GP 7200 Engines Nov 01/08
FIGURE Danger Areas of the Engines - Ground Idle Power - TRENT900 Engines
Jan 31/08
FIGURE Danger Areas of the Engines - Ground Idle Power - GP7200Engines
Jan 31/08
FIGURE Danger Areas of the Engines - Max Take-Off Power -TRENT 900 Engines
Jan 31/08
FIGURE Danger Areas of the Engines - Max. Take-Off Power - GP7200 Engines
Jan 31/08
FIGURE Danger Areas of the Engines - Breakaway Power - TRENT900 Engines
Jan 31/08
FIGURE Danger Areas of the Engines - Breakaway Power - GP 7200Engines
Jan 31/08
Section 2-12
Airplane Mooring Jun 01/07
FIGURE Airplane Mooring - Airplane Mooring Jun 01/07
CHAPTER 3
Section 3-1
Airplane Maintenance Jacking R Oct 01/09
FIGURE Jacking Points Location - Jacking Points Location R Oct 01/09
FIGURE Jacking Dimensions - Jacking Dimensions Jun 01/07
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Jacks and Safety Stay Adapter - Jacks and Safety StayAdapter
Jun 01/07
Section 3-2
Landing Gear Jacking for Wheel Change Jun 01/07
FIGURE Nose Landing Gear Jacking Point Heights - A380-800Models
Jan 31/08
FIGURE Wing Landing Gear Jacking Point Heights - A380-800Models
Jan 31/08
FIGURE Body Landing Gear Jacking Point Heights - A380-800Models
Jan 31/08
FIGURE Nose Landing Gear Jacking Point Loads - A380-800 Models Nov 01/08
FIGURE Nose Landing Gear Jacking Point Loads - A380-800F Models Nov 01/08
FIGURE Wing Landing Gear Jacking Point Loads - A380-800 Models Nov 01/08
FIGURE Wing Landing Gear Jacking Point Loads - A380-800FModels
Nov 01/08
FIGURE Body Landing Gear Jacking Point Loads - A380-800 Models Nov 01/08
FIGURE Body Landing Gear Jacking Point Loads - A380-800F Models Nov 01/08
Section 3-3
Leveling, Symmetry and Alignment Jun 01/07
FIGURE Location of Leveling Points - Location of Leveling Points Jun 01/07
Section 3-4
De-icing and Washing Nov 01/08
Section 3-5
Air Conditioning Nov 01/08
FIGURE Air Conditioning - General Layout Jun 01/07
FIGURE Air Conditioning - Air Generation Unit (AGU) Jun 01/07
Section 3-6
Communications Jun 01/07
FIGURE Communications - Location of Antennas Jan 31/08
Section 3-7
Electrical Power Nov 01/08
FIGURE Electrical Power - General Schematic Jun 01/07
L.E.C.Page 17
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Electrical Power - AC and DC Distribution Jun 01/07
FIGURE Electrical Power - Component Location Jun 01/07
Section 3-8
Flight Controls Nov 01/08
FIGURE Control Surface Travel - Rudder (Sheet 1) Jun 01/07
FIGURE Control Surface Travel - Rudder (Sheet 2) Jun 01/07
FIGURE Control Surface Travel - Trimmable Horizontal Stabilizer andElevator (Sheet 1)
Jun 01/07
FIGURE Control Surface Travel - Trimmable Horizontal Stabilizer andElevator (Sheet 2)
Jun 01/07
Section 3-9
Hydraulic Power Jun 01/07
FIGURE Hydraulic Power System - Symbols Jun 01/07
FIGURE Main Hydraulic Power System - Architecture Jun 01/07
FIGURE Green Hydraulic System - General Jun 01/07
FIGURE Yellow Hydraulic System - General Jun 01/07
FIGURE Hydraulic Power - Distribution Jun 01/07
Section 3-10
Landing Gear Jun 01/07
FIGURE Landing Gear - Nose Gear and Doors Jun 01/07
FIGURE Landing Gear - Nose Gear Servicing Points Jun 01/07
FIGURE Landing Gear - Wing Gear and Doors Jun 01/07
FIGURE Landing Gear - Wing Gear Servicing Points Jun 01/07
FIGURE Landing Gear - Body Gear and Doors Jun 01/07
FIGURE Landing Gear - Body Gear Servicing Points Jun 01/07
FIGURE Landing Gear - Landing Gear Footprint - A380-800 Models Jun 01/07
FIGURE Landing Gear - Landing Gear Footprint - A380-800F Models Jun 01/07
Section 3-11
Exterior Lighting Jun 01/07
L.E.C.Page 18
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Exterior Lighting - Exterior Lighting Available in Flight(Sheet 1)
Jun 01/07
FIGURE Exterior Lighting - Exterior Lighting Available in Flight(Sheet 2)
Jun 01/07
FIGURE Exterior Lighting - Exterior Lighting for Ground Use -A380-800 Models
Jun 01/07
FIGURE Exterior Lighting - Exterior Lighting for Ground Use -A380-800F Models
Jun 01/07
Section 3-12
Navigation Jun 01/07
FIGURE Navigation - Location of Antennas Jun 01/07
Section 3-13
Auxiliary Power Unit Jun 01/07
FIGURE Auxiliary Power Unit - APU Access Doors Jun 01/07
FIGURE Auxiliary Power Unit - General Layout Jun 01/07
Section 3-14
Power Plant R Oct 01/09
FIGURE Engine Dimensions - GP 7200 Engines Jan 31/08
FIGURE Engine Dimensions - TRENT 900 Engines Jan 31/08
FIGURE Fan Cowls - TRENT 900 Engines R Oct 01/09
FIGURE Fan Cowls - Engine 1-2-3-4 - GP 7200 Engines N Oct 01/09
FIGURE Fan Exhaust Cowls - Engine 1-4 - GP 7200 Engines N Oct 01/09
FIGURE Thrust Reverser - Engine 2-3 - GP 7200 Engines N Oct 01/09
Section 3-15
Component Sizes and Weights Nov 01/08
Section 3-16
Component Handling Nov 01/08
FIGURE Droop Nose 1 - CG Location Jun 01/07
FIGURE Droop Nose 2 - CG Location Jun 01/07
FIGURE Slat 2 - CG Location Jun 01/07
FIGURE Slat 3 - CG Location Jun 01/07
L.E.C.Page 19
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CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Slat 4 - CG Location Jun 01/07
FIGURE Slat 5 - CG Location Jun 01/07
FIGURE Slat 6 - CG Location Jun 01/07
FIGURE Slat 7 - CG Location Jun 01/07
FIGURE Inboard Aileron - CG Location Nov 01/08
FIGURE Mid Aileron - CG Location Nov 01/08
FIGURE Outboard Aileron - CG Location Nov 01/08
FIGURE Spoiler 1 - CG Location Nov 01/08
FIGURE Spoiler 2 - CG Location Nov 01/08
FIGURE Spoiler 3 - CG Location Nov 01/08
FIGURE Spoiler 4 - CG Location Nov 01/08
FIGURE Spoiler 5 - CG Location Nov 01/08
FIGURE Spoiler 6 - CG Location Nov 01/08
FIGURE Spoiler 7 - CG Location Nov 01/08
FIGURE Spoiler 8 - CG Location Nov 01/08
FIGURE Horizontal Stabilizer - CG Location Jun 01/07
FIGURE Vertical Stabilizer and Rudder - CG Location (Sheet 1) Jun 01/07
FIGURE Vertical Stabilizer and Rudder - CG Location (Sheet 2) Jun 01/07
FIGURE Tail cone - CG Location Jun 01/07
Section 3-17
Suggested Hangar Arrangement Jun 01/07
FIGURE Suggested Hangar Arrangement - Nose--in Position (Sheet 1) Jun 01/07
FIGURE Suggested Hangar Arrangement - Nose--in Position (Sheet 2) Jun 01/07
FIGURE Suggested Hangar Arrangement - Tail--in Position (Sheet 1) Jun 01/07
FIGURE Suggested Hangar Arrangement - Tail--in Position (Sheet 2) Jun 01/07
Section 3-18
Landing Gear Maintenance Pits Jun 01/07
FIGURE Maintenance Pits - Maintenance Pit Envelopes Jun 01/07
FIGURE Maintenance Pits - Necessary Depths Jun 01/07
L.E.C.Page 20
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@A380MAINTENANCE FACILITY PLANNING
CONTENT CHGCODE
LAST REVISIONDATE
FIGURE Maintenance Pits - Maintenance Pit Envelopes - WLG PitDimensions
Jun 01/07
FIGURE Maintenance Pits - Maintenance Pit Envelopes - BLG PitDimensions
Jun 01/07
Section 3-19
Suggested Workstands Nov 01/08
FIGURE General Arrangement - (Sheet 1) Jun 01/07
FIGURE General Arrangement - (Sheet 2) Jun 01/07
FIGURE Cargo Compartment Platform - (Sheet 1) Jun 01/07
FIGURE Cargo Compartment Platform - (Sheet 2) Jun 01/07
FIGURE Engine Platform - Engine Platform Jun 01/07
FIGURE WLG/BLG Compartment Platform - WLG/BLGCompartment Platform
Jun 01/07
FIGURE Rear Fuselage Platform - Rear Fuselage Platform Jun 01/07
FIGURE Hydraulic Platform -- Giraffe - Hydraulic Platform -- Giraffe Jun 01/07
FIGURE Pax Door Platform -- Main and Upper Decks - Pax DoorPlatform -- Main and Upper Decks
Jun 01/07
FIGURE Fuselage Platform - Fuselage Platform Jun 01/07
FIGURE Inner Wing Platform - Inner Wing Platform Jun 01/07
FIGURE Outer Wing Platform - Outer Wing Platform Jun 01/07
CHAPTER 4
Section 4-1
Batteries Shop Jun 01/07
Section 4-2
VFG Generator Shop Jun 01/07
Section 4-3
Composite Repair Shop Jun 01/07
Section 4-4
Electrical Accessories Shop Jun 01/07
Section 4-5
Electrical Wire Marking Shop Jun 01/07
L.E.C.Page 21
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CONTENT CHGCODE
LAST REVISIONDATE
Section 4-6
Engine and APU Shop Jun 01/07
Section 4-7
Fuel Component Shop Jun 01/07
Section 4-8
Hydraulic Component Shop Jun 01/07
Section 4-9
I.E.R.A. Shop Jun 01/07
Section 4-10
Interior Equipment Shop Jun 01/07
Section 4-11
Laboratory Test of Fluids Jun 01/07
Section 4-12
Metal Shop Jun 01/07
Section 4-13
Painting Shop Jun 01/07
Section 4-14
Pneumatic Component Shop Jun 01/07
Section 4-15
Life Jacket, Escape Slide / Raft Shop Jun 01/07
Section 4-16
Surface Heat Treatment Shop Jun 01/07
Section 4-17
Tube Repair Shop Jun 01/07
Section 4-18
Tire/Wheel and Brake Shop Jun 01/07
CHAPTER 5
Section 5-1
General Jun 01/07
L.E.C.Page 22
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@A380MAINTENANCE FACILITY PLANNING
TABLE OF CONTENTS
0 INTRODUCTION
0-1 Introduction
0-2 Alphabetical Index
0-3 Section Index
0-4 Glossary
1 GENERAL INFORMATION
1-1 Airplane Overall Dimensions and Outline Basic Reference
1-2 Airplane Dimensions
1-3 General Airplane Characteristics
1-4 Zoning and Access
1-5 Fuselage Frames / Stations
1-6 Wing Ribs / Stations
1-7 Center of Gravity Limits
1-8 Airplane Attitude
1-9 Ground Clearances
1-10 Door Clearances
1-11 Fuselage Cross-sections
1-12 Nose Contours
1-13 Vertical Stabilizer Contours
1-14 Horizontal Stabilizer Contours
1-15 Tail Contours
1-16 Wing Profile
1-17 Nacelle Contours
2 TERMINAL AND RAMP
2-1 Airplane Servicing Arrangement
2-2 Turnaround Stations
2-3 Ground Service Connections and Locations
2-4 Interior Arrangements
2-5 Escape Slides
2-6 Galley
2-7 Cargo
2-8 Towing
2-9 Ground Maneuvering
T.O.C.Page 1
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2-10 Airplane Parking
2-11 Operating Conditions
2-12 Airplane Mooring
3 LINE MAINTENANCE AND HANGAR
3-1 Airplane Maintenance Jacking
3-2 Landing Gear Jacking for Wheel Change
3-3 Leveling, Symmetry and Alignment
3-4 De-icing and Washing
3-5 Air Conditioning
3-6 Communications
3-7 Electrical Power
3-8 Flight Controls
3-9 Hydraulic Power
3-10 Landing Gear
3-11 Exterior Lighting
3-12 Navigation
3-13 Auxiliary Power Unit
3-14 Power Plant
3-15 Component Sizes and Weights
3-16 Component Handling
3-17 Suggested Hangar Arrangement
3-18 Landing Gear Maintenance Pits
3-19 Suggested Workstands
4 COMPONENT REPAIR/OVERHAUL AND FUNCTIONAL TEST
4-1 Batteries Shop
4-2 VFG Generator Shop
4-3 Composite Repair Shop
4-4 Electrical Accessories Shop
4-5 Electrical Wire Marking Shop
4-6 Engine and APU Shop
4-7 Fuel Component Shop
4-8 Hydraulic Component Shop
4-9 I.E.R.A. Shop
4-10 Interior Equipment Shop
4-11 Laboratory Test of Fluids
4-12 Metal Shop
T.O.C.Page 2
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4-13 Painting Shop
4-14 Pneumatic Component Shop
4-15 Life Jacket, Escape Slide / Raft Shop
4-16 Surface Heat Treatment Shop
4-17 Tube Repair Shop
4-18 Tire/Wheel and Brake Shop
5 VENDORS LIST
5-1 Vendors Information
T.O.C.Page 3
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@A380MAINTENANCE FACILITY PLANNING
INTRODUCTION
0-1 Introduction
**ON A/C A380-800 Models A380-800F Models
Introduction
1. PURPOSE
This A380 MAINTENANCE FACILITY PLANNING (MFP) manual is issued for the A380-800 andA380-800F series aircraft to provide necessary data to airlines for maintenance 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.
2. CORRESPONDENCE
Correspondence concerning this publication should be directed to :AIRBUS S.A.S.Technical Data Support and Services1 Rond Point Maurice BELLONTE31707 BLAGNAC CEDEXFRANCE
3. CONTENTS
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This manual comprises 5 sections :
Section 0 : INTRODUCTION
Section 1 : GENERAL INFORMATION
This section contains general dimensional and other basic data.It covers :- aircraft dimensions,- zoning, fuselage frame and wing stations,- cross-sections and profile for fuselage, wings and tail,- ground clearances and travel limits of movable parts,- aircraft center of gravity limits and aircraft attitude.
Section 2 : TERMINAL AND RAMP
This section contains the ground equipment required for the aircraft servicing at turn-round stations.It covers :- suggested servicing arrangement around the aircraft,- estimated servicing times for turn-round,- ground service connections and locations with their characteristics,- cargo compartment loading and unloading,- ground maneuvering capabilities and characteristics.
Section 3 : LINE MAINTENANCE AND HANGAR
This section outlines the technical data and requirements related to maintenance functions, regardlessof whether these would be performed inside or outside the hangar or on the ramp.It includes :- description of the main aircraft systems,- the aircraft jacking, leveling and the landing gear lifting,- the main removable components weight and handling,- the suggested hangar arrangement with the corresponding workstands.
Section 4 : COMPONENT REPAIR/OVERHAUL AND FUNCTIONAL TEST
This section contains the data and requirements relative to aircraft components repair/overhaul andfunctional testing.
Section 5 : VENDORS LIST
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0-2 Alphabetical Index
**ON A/C A380-800 Models A380-800F Models
Alphabetical Index
1. Alphabetical index
Subject Section
Air Conditioning 3-5
Airplane Attitude 1-8
Airplane Dimensions 1-2
Airplane Maintenance Jacking 3-1
Airplane Overall Dimensions and Outline BasicReference Drawing
1-1
Airplane Parking 2-10
Airplane Servicing Arrangement 2-1
Auxiliary Power Unit 3-13
Batteries Shop 4-1
Cargo Compartments - Loading and Unloading 2-7
Center of Gravity Limits 1-7
Communications 3-6Component Handling 3-16
Component Sizes and Weights 3-15
Composite Repair Shop 4-3
De-icing and Washing 3-4
Door Clearances 1-10Electrical Accessories Shop 4-4
Electrical Power 3-7Electrical Wire Marking Shop 4-5
Engine and APU Shop 4-6
Escape Slides/Rafts 2-5
Exterior Lighting 3-11
Flight Controls 3-8
Fuel Component Shop 4-7
Fuselage Cross-sections 1-11
Fuselage Frames/Stations 1-5
Galleys 2-6
General Airplane Characteristics 1-3
Generator Shop 4-2
0-2Page 1
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Ground Clearances 1-9Ground Maneuvering 2-9
Ground Service Connections and Locations 2-3Horizontal Stabilizer Contours 1-14Hydraulic Component Shop 4-8
Hydraulic Power 3-9
I E R A Shop 4-9
Interior Arrangements 2-4
Interior Equipment Shop 4-10
Laboratory Test of Fluids 4-11
Landing Gear 3-10
Landing Gear Jacking for Wheel Change 3-2
Landing Gear Maintenance Pits 3-18
Leveling, Symmetry and Alignment 3-3
Life Jacket, Escape Slide/raft Shop 4-15
Machine Shop 4-12
Nacelle Contours 1-17Navigation 3-12
Nose Contours 1-12Operating Conditions 2-11
Painting Shop 4-13
Pneumatic Component Shop 4-14
Power Plant 3-14Suggested Hangar Arrangement 3-17
Suggested Workstands 3-19
Surface Heat Treatment Shop 4-16
Tail Contours 1-15Terminal Operation 2-2
Tire/Wheel and Brake Shop 4-18
Towing 2-8
Tube Repair Shop 4-17
Vendors Information 5-1Vertical Stabilizer Contours 1-13Wing Profile 1-16
Wing Ribs/Stations 1-6
Zoning 1-4
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0-3 Section Index
**ON A/C A380-800 Models A380-800F Models
Section Index
1. Section index
SECTION 0: INTRODUCTION0-0 Table Of Contents0-1 Introduction0-2 Alphabetical Index
0-3 Section Index0-4 Glossary
SECTION 1: LINE MAINTENANCE AND HANGAR1-0 Table Of Contents1-1 Airplane Overall Dimensions and Outline Basic Reference drawing
1-2 Airplane Dimensions
1-3 General Airplane Characteristics
1-4 Zoning
1-5 Fuselage Frames/Stations
1-6 Wing Ribs/Stations
1-7 Center of Gravity Limits
1-8 Airplane Attitude
1-9 Ground Clearances1-10 Door Clearances1-11 Fuselage Cross-sections
1-12 Nose Contours1-13 Vertical Stabilizer Contours1-14 Horizontal Stabilizer Contours1-15 Tail Contours1-16 Wing Profile
1-17 Nacelle Contours
SECTION 2: TERMINAL AND RAMP2-0 Table Of Contents2-1 Airplane Servicing Arrangement
2-2 Terminal Operation
2-3 Ground Service Connections and Locations2-4 Interior Arrangements
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2-5 Escape Slides/Rafts
2-6 Galleys
2-7 Cargo Compartments - Loading and Unloading
2-8 Towing
2-9 Ground Maneuvering
2-10 Airplane Parking
2-11 Operating Conditions
SECTION 3: LINE MAINTENANCE AND HANGAR3-0 Table Of Contents3-1 Airplane Maintenance Jacking
3-2 Landing Gear Jacking for Wheel Change
3-3 Leveling, Symmetry and Alignment
3-4 De-icing and Washing
3-5 Air Conditioning
3-6 Communications3-7 Electrical Power3-8 Flight Controls
3-9 Hydraulic Power
3-10 Landing Gear
3-11 Exterior Lighting
3-12 Navigation
3-13 Auxiliary Power Unit
3-14 Power Plant3-15 Component Sizes and Weights
3-16 Component Handling
3-17 Suggested Hangar Arrangement
3-18 Landing Gear Maintenance Pits
3-19 Suggested Workstands
SECTION 4: COMPONENT REPAIR/OVERHAUL AND FUNCTIONAL TEST
4-0 Table Of Contents4-1 Batteries Shop
4-2 Generator Shop
4-3 Composite Repair Shop
4-4 Electrical Accessories Shop
4-5 Electrical Wire Marking Shop
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4-6 Engine and APU Shop
4-7 Fuel Component Shop
4-8 Hydraulic Component Shop
4-9 I E R A Shop
4-10 Interior Equipment Shop
4-11 Laboratory Test of Fluids
4-12 Machine Shop
4-13 Painting Shop
4-14 Pneumatic Component Shop
0-3Page 3
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@A380MAINTENANCE FACILITY PLANNING
0-4 Glossary
**ON A/C A380-800 Models A380-800F Models
Glossary
1. List of Abbreviations
A/C Aircraft
ADIRS Air Data Inertial Reference System
AGU Air Generation UnitAPU Auxiliary Power Unit
ATA Air Transport Association of America
BLG Body Landing Gear
CAS Calibrated Air Speed
CG Center of Gravity
C/L Center Line
FAA Federal Aviation AdministrationFDL Fuselage Datum Line
FR FrameFSTE Full Size Trolley Equivalent
FWD ForwardGPU Ground Power UnitGSE Ground Support Equipment
IERA Instrument, Electric, Radio and navigation, Avionic
ILS Instrument Landing System
ISA International Standard Atmosphere
L LeftLPS 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
NDT Non-Destructive TestNLG Nose Landing Gear
OAT Outside Air Temperature
OWE Operating Weight Empty
0-4Page 1
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@A380MAINTENANCE FACILITY PLANNING
PAX Passenger
PB/D Passenger Boarding/Deboarding
R Right
RC Reference ChordSLS Sea Level Static conditionSTA StationTBD To Be DeterminedTBIL To Be Issued LaterULD Unit Load Device US United StatesVF Variable Frequency
VFG Variable Frequency Generator
VHF Very High Frequency
VOR VHF Omnidirectional Range
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 literl/m2 liter per square meter
lb/in2 pound per square inch
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lb pound
lm/m2 lumen per square meterm meterm/s meter per second
m2 square meter
m3 cubic meter
m3/h cubic meter per hour
min minutemm millimeternm nautical milepsi pound-force per square incht tonneUS gal United States gallon
3. Design Weight TerminologyMaximum 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 take-off as limited by aircraft strength and airworthiness requirements. (This isthe maximum weight at start of the take-off run).Maximum Design Zero Fuel Weight (MZFW) :Maximum permissible weight of the aircraft less usable fuel.Operational Empty Weight (OEW) :Weight of structure, powerplant, furnishings, systems, and other items of equipment that are anintegral part of a particular aircraft configuration plus the operator’s items.The operator’s items are the flight and cabin crew and their baggage, unusable fuel, engine oil,emergency equipment, toilet chemical and fluids, galley structure, catering equipment, seats,documents, etc.Maximum Payload :Maximum Design Zero Fuel Weight (MZFW) minus Operating Weight Empty (OWE).Maximum Seating Capacity :Maximum number of passengers specifically certified or anticipated for certification.Maximum Cargo Volume :Maximum usable volume available for cargo.
Usable Fuel :
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Fuel available for aircraft propulsion.
0-4Page 4
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GENERAL INFORMATION
1-1 Airplane Overall Dimensions and Outline Basic Reference
**ON A/C A380-800 Models A380-800F Models
Airplane Overall Dimensions and Outline Basic Reference Drawing
1. This section gives the airplane overall dimensions and outline basic reference drawing.
1-1Page 1
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
DB1A
0 4 8 12 16METERS
0 10 20 30 40 50FEET
L_MF_010100_1_0050101_01_00
Airplane Overall Dimensions and Outline Basic Reference DrawingA380-800 Models
1-1Page 2
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
DB1A
0 4 8 12 16METERS
0 10 20 30 40 50FEET
L_MF_010100_1_0060101_01_00
Airplane Overall Dimensions and Outline Basic Reference DrawingA380-800F Models
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1-2 Airplane Dimensions
**ON A/C A380-800 Models A380-800F Models
Airplane Dimensions
1. This section gives airplane dimensions.
1-2Page 1
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
11.568 m(37.95 ft)
3.717 m(12.19 ft)
17.668 m (57.96 ft)
72.571 m (238.09 ft)
68.854 m (225.90 ft)
46.972 m (154.11 ft) 3.983 m (13.07 ft)
FOR DOOR DIMENSIONS ANDLOCATION, SEE SECTION 1−10.
NOTE:
29.943 m (98.23 ft)
22.228 m (72.92 ft)
L_MF_010200_1_0040101_01_01
52.065 m (170.82 ft)
Airplane DimensionsAirplane Dimensions (Sheet 1)
1-2Page 2
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
72.727 m (238.61 ft)
70.400 m (230.97 ft)
53.943 m (176.98 ft) 4.700 m(15.41 ft)
12.056 m(33.55 ft)
14.5
92 m
(47
.87
ft)12.456 m(40.87 ft)
5.264 m(17.27 ft)
79.750 m (261.65 ft)
7.142 m(23.43 ft)
30.372 m (99.65 ft)
14.336 m (47.03 ft)
29.598 m (97.11 ft)
51.400 m (168.64 ft)
8.410 m (27.60 ft)
8.557 m (28.07 ft)
14.084 m(46.20 ft)
33.578 m (110.16 ft) − WLG
36.854 m (120.91 ft) − BLG
4.972 m (16.31 ft)
L_MF_010200_1_0030101_01_00
Airplane DimensionsAirplane Dimensions (Sheet 2)
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1-3 General Airplane Characteristics
**ON A/C A380-800 Models A380-800F Models
General Airplane Characteristics Data
1. This part gives general airplane characteristics data for A380-800 models.
Airplane Characteristics
WV000 WV001 WV002 WV003Kilograms 562 000 512 000 571 000 571 000Maximum Ramp
Weight (MRW) Pounds 1 238 998 1 128 766 1 258 839 1 258 839Kilograms 560 000 510 000 569 000 510 000Maximum Takeoff
Weight (MTOW) Pounds 1 234 588 1 124 357 1 254 430 1 124 357Kilograms 386 000 394 000 391 000 395 000Maximum Landing
Weight (MLW) Pounds 850 984 868 621 862 007 870 826Kilograms 361 000 372 000 366 000 373 000Maximum Zero Fuel
Weight (MZFW) Pounds 795 869 820 119 806 892 822 324Trent 970Engines
270 364 kg (596 050 lb)Estimated OperatingEmpty Weight (OEW) GP 7270
Engines270 630 kg (596 637 lb)
Kilograms 90 636 101 636 95 636 102 636Estimated MaximumPayload Trent 970 Pounds 199 818 224 069 210 841 226 274
Kilograms 90 370 101 370 95 370 102 370Estimated MaximumPayload GP 7270 Pounds 199 232 223 483 210 255 225 687Standard SeatingCapacity <1>
Three-Class 555
Liters 323 546US gallons 85 472
Kilograms(density =0.785 kg/l)
253 983Usable Fuel Capacity
Pounds 559 937Cubic meters 2100Pressurized Fuselage
Volume (A/C nonequipped, main andupper deck)
Cubic feet 74 161
Cubic meters 775PassengerCompartment Volume(main deck) Cubic feet 27 369
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Airplane Characteristics
Cubic meters 530PassengerCompartment Volume(upper deck) Cubic feet 18 717
Cubic meters 12Cockpit Volume
Cubic feet 424Cubic meters 256Usable Cargo
Compartment Volume<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. This part gives the general airplane characteristics data for A380-800F models.
Airplane Characteristics
Airplane 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 OfWeight (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 ZeroFuel Weight (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)
243 350 243 350
Usable Fuel Capacity
pounds 536 494 536 494
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Airplane Characteristics
cubic meters 938.4 938.4Volume of cargo compartments<1> cubic feet 33 139 33 139
cubic meters 12.6 12.6Volume of Cockpitcubic 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 ft33)- 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)
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1-4 Zoning and Access
**ON A/C A380-800 Models A380-800F Models
Zoning and Access
1. General
This section provides the zone division/delimitation.
2. Aircraft Zoning
NOTE : If no side differentiation is needed (eg. : pylon, bilge area), the old numbering for ″centerzones″ is used.
A. Identification Method
(1) Zones identification is based on ATA 100 Specification.
(2) The aircraft is broken down into Zones identified, each, by a three-digit number where thefirst digit (hundreds) corresponds to the Major Zones, the second digit (tens) correspondsto the Major Sub-Zones and the third digit (units) corresponds to the Zones.
B. Identification of Major Zones, Major Sub-Zones and ZonesLocations and boundaries of the Major Zones and Major Sub-Zones are illustrated on thefollowing pages.
NOTE : Locations and boundaries of the zones are not given in this manual.
(1) Major Zones (hundreds)
(a) Major Zones boundaries are identified by :- Frame/Stations/Stringers for fuselage.- Ribs for wings and vertical/horizontal tail.- Stations for nacelle and pylon.
(b) The Major Zones are :- 100 Lower part of fuselage (below main deck floor lower datum), including
radome to forward face of aft pressure bulkead.- 200 Upper part of fuselage (above main deck floor lower datum) to forward face
of aft pressure bulkead.- 300 Stabilizer and fuselage rear section from rear of aft pressure bulkead
(including rudder and elevators).- 400 Powerplants, nacelles and pylons.- 500 Left wing.- 600 Right wing.- 700 Landing gear and landing gear doors.- 800 Passenger/crew doors, cargo compartment doors, emergency exits and
pressurized maintenance doors.
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(2) Major Sub-Zones (tens)
(a) These are divisions of the Major Zones, eg : 100 divided into 110, 120, 130, 140, etc.
(b) The sequence of Major Sub-Zones numbering for fuselage runs from the front to therear.
(3) Zones (units)
(a) These are divisions of Major Sub-Zones, eg : 120 divided into 121, 122, 123, etc.
(b) The sequence of Zones for fuselage runs from inboard to outboard, front to rear inthe wing, forward to aft and away from the floor line in the fuselage and from root totip in the vertical tail.
(c) Whenever feasible odd numbers are allocated to the zones left of fuselage or nacellecenterlines and even numbers to zones to the right.
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**ON A/C A380-800 Models
Z100Z800Z300 Z400Z700 Z600
Z500
Z200
L_MF_010400_1_0010102_01_00
Aircraft ZoningMajor Zones
1-4Page 3
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
Z110 Z130 Z150 Z170
Z120
FR0 FR17 FR46 FR56 FR72 FR86 FR91 FR95
COCKPIT FLOORLOWER DATUM
MAIN DECK FLOORLOWER DATUM
Z160Z140
L_MF_010400_1_0020102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 100 (Sheet 1)
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**ON A/C A380-800 Models
Z190
Z190
L_MF_010400_1_0030102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 100 (Sheet 2)
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**ON A/C A380-800 Models
Z220 Z230 Z240 Z250
FR36 FR61 FR80
FR95
Z290Z280Z270
FR73FR43FR21
Z210
FR5
Z260
FR16
FR14
COCKPIT FLOORLOWER DATUM LOWER DATUM
MAIN DECK FLOORLOWER DATUM
UPPER DECK FLOOR
L_MF_010400_1_0040102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 200
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**ON A/C A380-800 Models A380-800F Models
FR95
Z320
Z310
Z310
Z340
Z330
L_MF_010400_1_0050102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 300
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**ON A/C A380-800 Models A380-800F Models
OUTBOARD
INBOARD
Z450
Z410
Z480
Z440
LEFT WING(ENGINE 1)
RIGHT WING(ENGINE 4)
Z460
Z420
LEFT WING(ENGINE 2)
Z470
Z430
RIGHT WING(ENGINE 3)
L_MF_010400_1_0060102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 400 - TRENT 900 Engines
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**ON A/C A380-800 Models A380-800F Models
OUTBOARD
INBOARD
Z450
Z410
Z480
Z440
LEFT WING(ENGINE 1)
RIGHT WING(ENGINE 4)
Z460
Z420
LEFT WING(ENGINE 2)
Z470
Z430
RIGHT WING(ENGINE 3)
L_MF_010400_1_0070102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 400 -- GP 7200 Engines
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**ON A/C A380-800 Models A380-800F Models
Z630
Z630
Z630
Z630
Z690
Z630
Z660
Z680
Z670
Z610
Z610
Z610
Z640
Z650Z630
Z630
Z630
Z630
Z690
Z630
Z660
Z680
Z670
Z610
Z610
Z610
Z640
Z650
Z620Z620
Z510
Z510
Z510
Z540
Z550
Z520 Z560
Z530
Z530
Z530
Z530
Z530
Z580
Z590
Z570
L_MF_010400_1_0080102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 500/600
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**ON A/C A380-800 Models A380-800F Models
Z710 Z730Z750Z760
Z740
L_MF_010400_1_0090102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 700
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**ON A/C A380-800 Models
Z820Z820
Z850 Z850 Z850
Z830 Z830 Z830
Z840
Z860 Z860 Z860
Z840Z840 Z840Z840
Z830Z830
Z810
L_MF_010400_1_0100102_01_00
Aircraft ZoningMajor Sub-Zones - Zone 800
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1-5 Fuselage Frames / Stations
**ON A/C A380-800 Models A380-800F Models
Fuselage Frames / Stations
1. General
This section gives fuselage frame stations measured along X datum at 7330 mm from the nose.The stations (STA) are given in millimeters without conversion.
1-5Page 1
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
FR95FR74FR38
SECTION11/12
FR22FR5
SECTION 13 SECTION 15/21 SECTION 18 SECTION 19
L_MF_010500_1_0010102_01_00
Fuselage Frames/StationsSections Identification - A380-800 Models
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**ON A/C A380-800F Models
FR95FR74FR38
SECTION11/12
FR22FR5
SECTION 13 SECTION 15/21 SECTION 18 SECTION 19
L_MF_010500_1_0020102_01_00
Fuselage Frames/StationsSections Identification - A380-800F Models
1-5Page 3
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
3°
FR10A
X = 0
SECTION 12SECTION 11
10°
X = 7330
FR10 DATUM−STA 10406
FR9/STA10083
FR8/STA9763FR7/STA9437
FR6/STA9114FR5/STA8789
FR0/STA8170FR18A/STA13824
FR17C/STA13429
FR16/STA12657
FR14/STA11778
FR15A/STA12355
FR15/STA12053
FR13/STA11453FR12/STA11128
FR11A/STA10805
FR17B/STA13073
FR19B/STA14351
FR5 FR15 FR22
FR11/STA10767
FR10B
FR10 DATUM/STA10406
RADOME ANDNOSE LOWER UNIT
FR22/STA16205FR21/STA15570
FR20/STA14935FR19/STA14300
FR18/STA13646FR17/STA12991
L_MF_010500_1_0030102_01_00
Fuselage Frames/StationsSection 11/12 - A380-800 Models
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
3°
FR10A
X = 0
SECTION 12SECTION 11
10°
X = 7330
FR10 DATUM−STA 10406
FR9/STA10083
FR8/STA9763FR7/STA9437
FR6/STA9114FR5/STA8789
FR0/STA8170FR18A/STA13824
FR17C/STA13429
FR16/STA12657
FR14/STA11778
FR15A/STA12355
FR15/STA12053
FR13/STA11453FR12/STA11128
FR11A/STA10805
FR17B/STA13073
FR19B/STA14351
FR5 FR15 FR22
FR11/STA10767
FR10B
FR10 DATUM/STA10406
RADOME ANDNOSE LOWER UNIT
FR22/STA16205FR21/STA15570
FR20/STA14935FR19/STA14300
FR18/STA13646FR17/STA12991
L_MF_010500_1_0040102_01_00
Fuselage Frames/StationsSection 11/12 - A380-800F Models
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**ON A/C A380-800 Models
FR22/STA16205FR23/STA16840
FR24/STA17475FR25/STA18110
FR26/STA18745FR27/STA19380
FR28/STA20015FR29/STA20650
FR30/STA21285FR31/STA21920
FR32/STA22555FR33/STA23190
FR34/STA23825
FR36/STA25095FR37/STA25730
FR38/STA26365
FR35/STA24460
L_MF_010500_1_0050102_01_00
Fuselage Frames/StationsSection 13 - A380-800 Models
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**ON A/C A380-800F Models
FR22/STA16205FR23/STA16840
FR24/STA17475FR25/STA18110
FR26/STA18745FR27/STA19380
FR28/STA20015FR29/STA20650
FR30/STA21285FR31/STA21920
FR32/STA22555FR33/STA23190
FR34/STA23825
FR36/STA25095FR37/STA25730
FR38/STA26365
FR35/STA24460
L_MF_010500_1_0060102_01_00
Fuselage Frames/StationsSection 13 - A380-800F Models
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**ON A/C A380-800 Models
FR74/STA49530FR73/STA48895
FR72/STA48260FR71/STA47625
FR70/STA46990FR69/STA46355
FR68/STA45720FR67/STA45085
FR66/STA44450
FR61/STA41275FR60/STA40640
FR59/STA40005FR58/STA39370
FR57/STA38735FR56/STA38100
FR55/STA37439FR54/STA36779
FR53/STA36119FR52/STA35458
FR51/STA34798FR50/STA34137
FR49/STA33477FR48/STA32817
FR65/STA43815FR64/STA43180
FR63/STA42545FR62/STA41910
FR47/STA32156FR46/STA31496
FR45/STA30835FR44/STA30175
FR43/STA29540FR42/STA28905
FR41/STA28270FR40/STA27635
FR39/STA27000FR38/STA26365
L_MF_010500_1_0070102_01_00
Fuselage Frames/StationsSection 15/21 - A380-800 Models
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**ON A/C A380-800F Models
FR74/STA49530FR73/STA48895
FR72/STA48260FR71/STA47625
FR70/STA46990FR69/STA46355
FR68/STA45720FR67/STA45085
FR66/STA44450
FR61/STA41275FR60/STA40640
FR59/STA40005FR58/STA39370
FR57/STA38735FR56/STA38100
FR55/STA37439FR54/STA36779
FR53/STA36119FR52/STA35458
FR51/STA34798FR50/STA34137
FR49/STA33477FR48/STA32817
FR65/STA43815FR64/STA43180
FR63/STA42545FR62/STA41910
FR47/STA32156FR46/STA31496
FR45/STA30835FR44/STA30175
FR43/STA29540FR42/STA28905
FR41/STA28270FR40/STA27635
FR39/STA27000FR38/STA26365
L_MF_010500_1_0080102_01_00
Fuselage Frames/StationsSection 15/21 - A380-800F Models
1-5Page 9
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**ON A/C A380-800 Models
FR84/STA55880
FR74/STA49530
FR75/STA50165
FR76/STA50800
FR77/STA51435
FR78/STA52070
FR79/STA52705
FR80/STA53340
FR82/STA54610
FR83/STA55245
FR81/STA53975
FR85/STA56515
FR86/STA57150
FR87/STA57785
FR88/STA58420
FR89/STA59055
FR90/STA59690
FR91/STA60325
FR92/STA60960
FR93/STA61595
FR94/STA62230
FR95/STA62865
L_MF_010500_1_0090102_01_00
Fuselage Frames/StationsSection 18 - A380-800 Models
1-5Page 10
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**ON A/C A380-800F Models
FR84/STA55880
FR74/STA49530
FR75/STA50165
FR76/STA50800
FR77/STA51435
FR78/STA52070
FR79/STA52705
FR80/STA53340
FR82/STA54610
FR83/STA55245
FR81/STA53975
FR85/STA56515
FR86/STA57150
FR87/STA57785
FR88/STA58420
FR89/STA59055
FR90/STA59690
FR91/STA60325
FR92/STA60960
FR93/STA61595
FR94/STA62230
FR95/STA62865
L_MF_010500_1_0100102_01_00
Fuselage Frames/StationsSection 18 - A380-800F Models
1-5Page 11
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**ON A/C A380-800 Models A380-800F Models
X = 77730
FR103/STA67945
FR104/STA68580
FR105/STA69260
FR106/STA69940
FR107/STA70620
FR108/STA71300
FR109/STA71810
FR110/STA72320
FR95/STA62865
FR96/STA63500
FR97/STA64135
FR98/STA64770
FR99/STA65405
FR100/STA66040
FR101/STA66675
FR102/STA67310
FR95
SECTION 19 SECTION 19 − 1
FR110
L_MF_010500_1_0110102_01_00
Fuselage Frames/StationsSection 19
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@A380MAINTENANCE FACILITY PLANNING
1-6 Wing Ribs / Stations
**ON A/C A380-800 Models A380-800F Models
Wing Ribs / Stations
1. General
This section shows wing ribs/stations and dimensions.
1-6Page 1
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@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
STA0RIB1
RIB7
RIB10
RIB37
RIB34
RIB31
RIB28
RIB25
RIB22
RIB19
RIB16
RIB13
RIB4
RIB40
RIB43
RIB46
RIB49
A B C
LH WING SHOWNRH WING SYMMETRICAL
STA2516
STA4813
STA7066
STA9180
STA11409
STA13456
STA15654
STA17796
STA19903
STA22011
STA24038
STA26098
STA28325
STA30535
STA32712
STA34889
NOTE:
FRONT SPAR
THE STATION NUMBER IS THE DISTANCEIN MILLIMETERS BETWEEN RIB1 (STA0) ANDEACH RIB2 THRU 49. THE DISTANCE IS MEASURED (AT 90 DEGREES TO RIB1)BETWEEN RIB1 AND THE INTERSECTION OFEACH RIB DATUM WITH THE FRONT SPARDATUM
A
L_MF_010600_1_0010101_01_00
Wing Ribs/StationsWing Ribs/Stations (Sheet 1)
1-6Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
L_MF_010600_0_AAM0_02_00
RIB3
RIB6
RIB9
RIB12
RIB15
RIB18
RIB21
RIB24
RIB27
RIB30
RIB33
RIB36
RIB39
RIB42
RIB45
RIB48
LH WING SHOWNRH WING SYMMETRICAL
STA1856
STA4049
STA6349
STA8451
STA10674
STA12723
STA14921
STA17187
STA19186
STA21337
STA23366
STA25381
STA27583
STA29809
STA31986
STA34163NOTE:THE STATION NUMBER IS THE DISTANCEIN MILLIMETERS BETWEEN RIB1 (STA0) ANDEACH RIB2 THRU 49. THE DISTANCE IS MEASURED (AT 90 DEGREES TO RIB1)BETWEEN RIB1 AND THE INTERSECTION OFEACH RIB DATUM WITH THE FRONT SPARDATUM
FRONT SPAR
B
L_MF_010600_1_0020101_01_00
Wing Ribs/StationsWing Ribs/Stations (Sheet 2)
1-6Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
RIB2
RIB5
RIB47
RIB44
RIB41
RIB38
RIB35
RIB32
RIB29
RIB26
RIB23
RIB20
RIB17
RIB14
RIB11
RIB8
LH WING SHOWNRH WING SYMMETRICAL
STA1074
STA3289
STA5581
STA7785
STA9946
STA11998
STA14189
STA16390
STA18469
STA20620
STA22704
STA24709
STA26841
STA29067
STA31260
STA33437NOTE:THE STATION NUMBER IS THE DISTANCEIN MILLIMETERS BETWEEN RIB1 (STA0) ANDEACH RIB2 THRU 49. THE DISTANCE IS MEASURED (AT 90 DEGREES TO RIB1)BETWEEN RIB1 AND THE INTERSECTION OFEACH RIB DATUM WITH THE FRONT SPARDATUM
FRONT SPAR
C
L_MF_010600_1_0030101_01_00
Wing Ribs/StationsWing Ribs/Stations (Sheet 3)
1-6Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A380−700
9235.2 mm(363.59 in)
A380−800/800F
7330.2 mm(288.59 in)
A380−900
4155.2 mm(163.59 in)
AIRPLANE DATUM
4669
9 m
m (
1838
.54
in)
4809
4 m
m (
1893
.47
in)
5109
7 m
m (
2011
.69
in)
5258
8 m
m (
2070
.39
in)
5407
1 m
m (
2128
.79
in)
25973 mm (1022.56 in)
17649 mm (694.84 in)
21868 mm (860.95 in)
(368.66 in)9364 mm
(531.22 in)13493 mm
L_MF_010600_1_0040101_01_00
Wing Ribs/StationsFlap Track Positions
1-6Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-7 Center of Gravity Limits
**ON A/C A380-800 Models A380-800F Models
Center of Gravity Limits
1. General
This section gives center of gravity limits.
1-7Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010700_1_0040101_01_00
2728
2930
3132
3334
3536
3738
3940
4142
4344
4546
47
2725
2931
3335
3739
4143
4547
49%
MA
C26
0
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
Aircraft Weight (kg x 1000)
Max
. Tak
e−of
f Wei
ght =
510
000
kg
Max
. Lan
ding
Wei
ght =
394
000
kg
Max
. Zer
o F
uel W
eigh
t = 3
72 0
00 k
g
Take−off /
Landing
Take−off /Landing
Flight
Flight
Center of Gravity LimitsMTOW 510000 kg- A380-800 Models
1-7Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
3527
2829
3031
3233
3436
3738
3940
4142
4344
4546
47
3533
3129
2725
3739
4143
4547
49%
MA
C
AIRCRAFT WEIGHT (kg x 1000)
TAKE−OFF
MA
X. Z
ER
O F
UE
L W
EIG
HT
= 3
61 0
00kg
MA
X. L
AN
DIN
G W
EIG
HT
= 3
86 0
00kg LANDING
TAKE−OFF/LANDING
TAKE−OFF/LANDING
FLIGHT
MA
X. T
AK
E−
OF
F W
EIG
HT
= 5
60 0
00kg FLIGHT
L_MF_010700_1_0010101_01_00
Center of Gravity LimitsMTOW 560000 kg - A380-800 Models
1-7Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
3527
2829
3031
3233
3436
3738
3940
4142
4344
4546
47
3533
3129
2725
3739
4143
4547
49%
MA
C
AIRCRAFT WEIGHT (kg x 1000)
L_MF_010700_1_0050101_01_00
TAKE−OFF
MA
X. L
AN
DIN
G W
EIG
HT
= 3
91 0
00kg
MA
X. Z
ER
O F
UE
L W
EIG
HT
= 3
66 0
00kg
MA
X. T
AK
E−
OF
F W
EIG
HT
= 5
69 0
00kg
FLIGHT TAKE−OFF/LANDIN
G
LANDING
TAKE−OFF/LANDING
FLIGHT
Center of Gravity LimitsMTOW 569000 kg - A380-800 Models
1-7Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
3527
2829
3031
3233
3436
3738
3940
4142
4344
4546
47
3533
3129
2725
3739
4143
4547
49%
MA
C
AIRCRAFT WEIGHT (kg x 1000)
MA
X. L
AN
DIN
G W
EIG
HT
= 4
27 0
00kg
FLIGHT
TAKE−OFF/LANDING
TAKE−OFF
MA
X. T
AK
E−
OF
F W
EIG
HT
= 5
90 0
00kg
MA
X. Z
ER
O F
UE
L W
EIG
HT
= 4
02 0
00kg LANDING
FLIGHT
TAKE−OFF/LANDING
L_MF_010700_1_0030101_01_00
Center of Gravity LimitsMTOW 590000 kg - A380-800F Models
1-7Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
260
280
300
320
340
360
380
400
420
440
460
480
500
520
540
560
580
3527
2829
3031
3233
3436
3738
3940
4142
4344
4546
47
3533
3129
2725
3739
4143
4547
49%
MA
C
AIRCRAFT WEIGHT (kg x 1000)
L_MF_010700_1_0060101_01_00
MA
X. L
AN
DIN
G W
EIG
HT
= 4
27 0
00kg
MA
X. Z
ER
O F
UE
L W
EIG
HT
= 3
79 0
00kg
FLIGHT TAKE−OFF/LANDIN
G
TAKE−OFF
MA
X. T
AK
E−
OF
F W
EIG
HT
= 6
00 0
00kg
LANDING
FLIGHT
TAKE−OFF/LANDING
Center of Gravity LimitsMTOW 600000 kg - A380-800F Models
1-7Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-8 Airplane Attitude
**ON A/C A380-800 Models A380-800F Models
Airplane Attitude
1. GeneralThis section contains the graphs that show the approximate deflections of:- the tires- the Nose Landing Gear shock absorbers- the Wing Landing Gear shock absorbers- the Body Landing Gear shock absorbers.When different combinations of deflated tires are considered, the figures are approximate.
NOTE : These aircraft have radial or bias ply tires installed. They are required to have the samestatic loaded radius. There are many manufacturers of radial and bias ply tires, each makeof tire could give different deflections. The graphs that follow are for Michelin radial plytires:
Tires DimensionsA380-800 A380-800F
NLG 1270 x 455R22 32PR 50 x 20R22 34PRWLG 1400 x 530R23 40PR 1400 x 530R23 42PRBLG 1400 x 530R23 40PR 1400 x 530R23 42PR
1-8Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0010101_01_01
300
320
340
360
380
400
420
440
460
480
500
520
540
560
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
mm
)
11.8
12.8
13.8
14.8
15.8
16.8
17.8
18.8
19.8
20.8
21.8
120011001000900800700600
(x1000 kg)
(x1000 lb)
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
in )
CG POSITION29 % mac37.5 % mac41 % mac43 % mac
NLG Shock-Absorber DeflectionNLG Shock-Absorber Deflection - A380-800 Models
1-8Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0020101_01_01
300
320
340
360
380
400
420
440
460
480
500
520
540
560
260 300 340 380 420 460 500 540 580 620
AIRCRAFT GROSS WEIGHT
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
mm
)
11.8
12.8
13.8
14.8
15.8
16.8
17.8
18.8
19.8
20.8
21.8
1300120011001000900800700600
(x1000 kg)
(x1000 lb)
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
in )
CG POSITION29 % mac36 % mac40 % mac43 % mac
NLG Shock-Absorber DeflectionNLG Shock-Absorber Deflection - A380-800F Models
1-8Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0030101_01_01
CG POSITION29 % mac33 % mac37.5 % mac41 % mac43 % mac
1270 x 455R22 32PR TIRESTIRE PRESSURE CONSTANT AT 14.1 bar (205 psi)
30
40
50
60
70
80
90
100
110
120
130
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
1.2
1.5
1.8
2.1
2.4
2.7
3.0
3.3
3.6
3.9
4.2
4.5
4.8
5.1
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)ALL TIRES INFLATED
50 % SHOCK−ABSORBERLOAD ON TIRE
NLG Tire Deflection 50 % LoadNLG Tire Deflection 50 % Load - A380-800 Models
1-8Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0040101_01_01
1270 x 455R22 32PR TIRESTIRE PRESSURE CONSTANT AT 14.1 bar (205 psi)
60
80
100
120
140
160
180
200
220
240
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
2.4
2.9
3.4
3.9
4.4
4.9
5.4
5.9
6.4
6.9
7.4
7.9
8.4
8.9
9.4
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
CG POSITION 29 % mac 33 % mac 37.5 % mac 41 % mac 43 % mac
ONE TIRE DEFLATED100 % SHOCK−ABSORBER
LOAD ON TIRE
NLG Tire Deflection 100 % LoadNLG Tire Deflection 100 % Load - A380-800 Models
1-8Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0050101_01_01
50 x 20R22 34PR TIRESTIRE PRESSURE CONSTANT AT 14.9 bar (216 psi)
30
40
50
60
70
80
90
100
110
120
130
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
1.2
1.5
1.8
2.1
2.4
2.7
3.0
3.3
3.6
3.9
4.2
4.5
4.8
5.1
600 700 800 900 1000 1100 1200 1300
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
CG POSITION29 % mac33 % mac36 % mac40 % mac43 % mac
ALL TIRES INFLATED 50 % SHOCK−ABSORBER
LOAD ON TIRE
NLG Tire Deflection 50 % LoadNLG Tire Deflection 50 % Load - A380-800F Models
1-8Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0060101_01_01
60
80
100
120
140
160
180
200
220
240
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
2.4
2.9
3.4
3.9
4.4
4.9
5.4
5.9
6.4
6.9
7.4
7.9
8.4
8.9
9.4
600 700 800 900 1000 1100 1200 1300
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
50 x 20R22 34PR TIRESTIRE PRESSURE CONSTANT AT 14.9 bar (216 psi)
29 % mac33 % mac36 % mac40 % mac43 % mac
CG POSITION
ONE TIRE DEFLATED 100 % SHOCK−ABSORBER
LOAD ON TIRE
NLG Tire Deflection 100 % LoadNLG Tire Deflection 100 % Load - A380-800F Models
1-8Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0070101_01_01
345
360
375
390
405
420
435
450
465
480
495
510
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
mm
)
13.6
14.6
15.6
16.6
17.6
18.6
19.6
120011001000900800700600
(x1000 kg)
(x1000 lb)
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
in )
CG POSITION29 % mac37.5 % mac43 % mac
WLG Shock-Absorber DeflectionWLG Shock-Absorber Deflection - A380-800 Models
1-8Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0080101_01_01
290
310
330
350
370
390
410
430
450
470
490
260 300 340 380 420 460 500 540 580 620
AIRCRAFT GROSS WEIGHT
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
mm
)
11.4
12.4
13.4
14.4
15.4
16.4
17.4
18.4
1300120011001000900800700600
(x1000 kg)
(x1000 lb)
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
in )
CG POSITION29 % mac36 % mac43 % mac
WLG Shock-Absorber DeflectionWLG Shock-Absorber Deflection - A380-800F Models
1-8Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0090101_01_01
50
55
60
65
70
75
80
85
90
95
100
105
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.4
3.6
3.8
4.0
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 40PRTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
CG POSITION 29 % mac 33 % mac 37.5 % mac 43 % mac
ALL TIRES INFLATED25 % SHOCK−ABSORBER
LOAD ON TIRE
WLG Tire Deflection 25 % LoadWLG Tire Deflection 25 % Load - A380-800 Models
1-8Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0100101_01_01
90
100
110
120
130
140
150
160
170
180
190
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
3.5
3.8
4.1
4.4
4.7
5.0
5.3
5.6
5.9
6.2
6.5
6.8
7.1
7.4
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 40PRTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
CG POSITION 29 % mac 33 % mac 37.5 % mac 43 % mac
ONE TIRE DEFLATED50 % SHOCK−ABSORBER
LOAD ON TIRE
WLG Tire Deflection 50 % LoadWLG Tire Deflection 50 % Load - A380-800 Models
1-8Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0110101_01_01
45
50
55
60
65
70
75
80
85
90
95
100
105
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
1.8
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.4
3.6
3.8
4.0
600 700 800 900 1000 1100 1200 1300
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 42 PRTIRE PRESSURE CONSTANT AT 16.1 bar (234 psi)
ALL TIRES INFLATED 25 % SHOCK−ABSORBER
LOAD ON TIRE
CG POSITION 29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
WLG Tire Deflection 25 % LoadWLG Tire Deflection 25 % Load - A380-800F Models
1-8Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0120101_01_01
85
95
105
115
125
135
145
155
165
175
185
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
3.3
3.6
3.9
4.2
4.5
4.8
5.1
5.4
5.7
6.0
6.3
6.6
6.9
7.2
600 700 800 900 1000 1100 1200 1300
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 42 PRTIRE PRESSURE CONSTANT AT 16.1 bar (234 psi)
CG POSITION 29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
ONE TIRE DEFLATED 50 % SHOCK−ABSORBER
LOAD ON TIRE
WLG Tire Deflection 50 % LoadWLG Tire Deflection 50 % Load - A380-800F Models
1-8Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0130101_01_01
350
370
390
410
430
450
470
490
510
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
mm
)
13.8
14.8
15.8
16.8
17.8
18.8
19.8
120011001000900800700600
(x1000 kg)
(x1000 lb)
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
in )
CG POSITION29 % mac37.5 % mac43 % mac
BLG Shock-Absorber DeflectionBLG Shock-Absorber Deflection - A380-800 Models
1-8Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0140101_01_01
320
340
360
380
400
420
440
460
480
500
260 300 340 380 420 460 500 540 580 620
AIRCRAFT GROSS WEIGHT
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
mm
)
12.6
13.6
14.6
15.6
16.6
17.6
18.6
19.6
1300120011001000900800700600
(x1000 kg)
(x1000 lb)
SH
OC
K−
AB
SO
RB
ER
DE
FLE
CT
ION
S (
in )
CG POSITION29 % mac36 % mac43 % mac
BLG Shock-Absorber DeflectionBLG Shock-Absorber Deflection - A380-800F Models
1-8Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
50
55
60
65
70
75
80
85
90
95
100
105
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.4
3.6
3.8
4.0
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 40 PRTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
CG POSITION 29 % mac 33 % mac 37.5 % mac 43 % mac
ALL TIRES INFLATED16.7 % SHOCK−ABSORBER
LOAD ON TIRE
L_MF_010800_1_0150101_01_01
BLG Tire Deflection 16.7 % LoadBLG Tire Deflection 16.7 % Load - A380-800 Models
1-8Page 16
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0160101_01_01
70
80
90
100
110
120
130
140
150
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
2.8
3.1
3.4
3.7
4.0
4.3
4.6
4.9
5.2
5.5
5.8
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 40PRTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
TWO TIRES DEFLATED25 % SHOCK−ABSORBER
LOAD ON TIRE
CG POSITION29 % mac33 % mac37.5 % mac43 % mac
BLG Tire Deflection 25 % LoadBLG Tire Deflection 25 % Load - A380-800 Models
1-8Page 17
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0170101_01_01
90
100
110
120
130
140
150
160
170
180
190
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
3.5
3.8
4.1
4.4
4.7
5.0
5.3
5.6
5.9
6.2
6.5
6.8
7.1
7.4
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 40 PRTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
ONE TIRE DEFLATED33.3 % SHOCK−ABSORBER
LOAD ON TIRE
CG POSITION29 % mac33 % mac37.5 % mac43 % mac
BLG Tire Deflection 33.3 % LoadBLG Tire Deflection 33.3 % Load - A380-800 Models
1-8Page 18
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_010800_1_0180101_01_01
120
140
160
180
200
220
240
260
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
4.7
5.2
5.7
6.2
6.7
7.2
7.7
8.2
8.7
9.2
9.7
10.2
120011001000900800700600
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 40 PRTIRE PRESSURE CONSTANT AT 15 bar (218 psi)
CG POSITION 29 % mac 33 % mac 37.5 % mac 43 % mac
FOUR TIRES DEFLATED50 % SHOCK−ABSORBER
LOAD ON TIRE
BLG Tire Deflection 50 % LoadBLG Tire Deflection 50 % Load - A380-800 Models
1-8Page 19
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0190101_01_01
45
50
55
60
65
70
75
80
85
90
95
100
105
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
1.8
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.4
3.6
3.8
4.0
600 700 800 900 1000 1100 1200 1300
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 42 PRTIRE PRESSURE CONSTANT AT 16.1 bar (234 psi)
CG POSITION 29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
ALL TIRES INFLATED 16.7 % SHOCK−ABSORBER
LOAD ON TIRE
BLG Tire Deflection 16.7 % LoadBLG Tire Deflection 16.7 % Load - A380-800F Models
1-8Page 20
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0200101_01_01
65
75
85
95
105
115
125
135
145
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
2.6
2.9
3.2
3.5
3.8
4.1
4.4
4.7
5.0
5.3
5.6
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 42 PRTIRE PRESSURE CONSTANT AT 16.1 bar (234 psi)
600 700 800 900 1000 1100 1200 1300
CG POSITION 29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
TWO TIRES DEFLATED 25 % SHOCK−ABSORBER
LOAD ON TIRE
BLG Tire Deflection 25 % LoadBLG Tire Deflection 25 % Load - A380-800F Models
1-8Page 21
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0210101_01_01
85
95
105
115
125
135
145
155
165
175
185
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
3.3
3.6
3.9
4.2
4.5
4.8
5.1
5.4
5.7
6.0
6.3
6.6
6.9
7.2
600 700 800 900 1000 1100 1200 1300
(x1000 kg)
(x1000 lb)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 42 PRTIRE PRESSURE CONSTANT AT 16.1 bar (234 psi)
ONE TIRE DEFLATED 33.3 % SHOCK−ABSORBER
LOAD ON TIRE
CG POSITION 29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
BLG Tire Deflection 33.3 % LoadBLG Tire Deflection 33.3 % Load - A380-800F Models
1-8Page 22
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_010800_1_0220101_01_01
120
130
140
150
160
170
180
190
200
210
220
230
240
250
260
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
TIR
E D
EF
LEC
TIO
NS
( m
m )
4.7
5.2
5.7
6.2
6.7
7.2
7.7
8.2
8.7
9.2
9.7
10.2
600 700 800 900 1000 1100 1200 1300
(x1000 kg)
TIR
E D
EF
LEC
TIO
NS
( in
)
1400 x 530R23 42 PRTIRE PRESSURE CONSTANT AT 16.1 bar (234 psi)
(x1000 lb)
CG POSITION 29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
FOUR TIRES DEFLATED 50 % SHOCK−ABSORBER
LOAD ON TIRE
BLG Tire Deflection 50 % LoadBLG Tire Deflection 50 % Load - A380-800F Models
1-8Page 23
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CONDITION AXLE ALL TIRES INFLATED, 25% OF GEAR LOAD ON EACH TIRE.HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (25% LOAD).HEIGHT OF AXLE B ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (25% LOAD).
A
B
1
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (50% LOAD).HEIGHT OF AXLE B ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (25% LOAD).
A
B
2
= TIRE RADIUS − TIRE DEFLECTION (50% LOAD).HEIGHT OF AXLE B ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (50% LOAD).
A
B
3
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (25% LOAD).HEIGHT OF AXLE B ABOVE GROUND= RIM OUTER FLANGE RADIUS.
A
B
4
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (50% LOAD).HEIGHT OF AXLE B ABOVE GROUND= RIM OUTER FLANGE RADIUS.
A
B
5
25% 25%
25% 25%
50% 0%
25% 25%
50% 0%
50% 0%
25% 25%
25% 25%
50% 0%
25% 25%
ONE TIRE DEFLATED ON ONE AXLE, 50% OF GEAR LOADON INFLATED TIRE, 0% ON THE DEFLATED TIRE.
ONE TIRE DEFLATED ON BOTH AXLES, 50% OF GEAR LOADON BOTH INFLATED TIRES, 0% ON THE DEFLATED TIRES.
TWO TIRES DEFLATED ON ONE AXLE, 25% OF GEAR LOAD ON EACHINFLATED TIRE, 25% ON THE RIMS OF EACH DEFLATED TIRE.
THE RIMS OF EACH DEFLATED TIRE ON AXLE B.
THREE TIRES DEFLATED, 50% OF GEAR LOAD ON THE INFLATEDTIRE, 0% ON THE DEFLATED TIRE ON THE SAME AXLE, 25% ON
TIRE SIZE 1400 X 530 R23 40PR
NOTE:
MAXIMUM GROWN TIRE (UNLOADED) RADIUS = 722 mm (28.4 in).RIM OUTER FLANGE RADIUS = 356 mm (14 in).
TWO EXAMPLES OF HOW TO USE THE TIRE INFLATED/DEFLATED GRAPHS AS SHOWN.ASSUME AN AIRCRAFT WEIGHT OF 510 000 kg (1 124 360 lb) WITH THE CG AT 37.4% MAC.
EXAMPLE 2
FROM THE GRAPHS,
EXAMPLE 1FOR CONDITION 2,HEIGHT OF AXLE A ABOVE GROUND = 722 −165 = 557 mm (21.9 in).HEIGHT OF AXLE B ABOVE GROUND = 722 −92 = 630 mm (24.8 in).
FOR CONDITION 5,HEIGHT OF AXLE A ABOVE GROUND = 722 −165 = 557 mm (21.9 in).HEIGHT OF AXLE B ABOVE GROUND = 356 mm (14 in) (RIM OUTER FLANGE RADIUS).
A TIRE THAT CARRIES 25% OF THE WLG LOADS DEFLECTS 92 mm (3.6 in).A TIRE THAT CARRIES 50% OF THE WLG LOADS DEFLECTS 165 mm (6.5 in).
HEIGHT OF AXLE A ABOVE GROUND
CONDITIONS 1 TO 5 SHOW POSSIBLE DAMAGE SITUATIONS FOR TIRES ON WLG BOGIE.
L_MF_010800_1_0230101_01_00
WLG Tire Deflection NotesWLG Tire Deflection
1-8Page 24
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CONDITION AXLE ALL TIRES INFLATED, 16.7% OF GEAR LOAD ON EACH TIRE.HEIGHT OF AXLES A, B, C ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (16.7% LOAD).
A
B1
C
16.7%
16.7%
16.7%
16.7%
16.7%
16.7%
A
B2
C
33.3%
16.7%
16.7%
0%
16.7%
16.7%
A
B3
C
33.3%
33.3%
16.7%
0%
0%
16.7%
A
B4
C
33.3%
33.3%
33.3%
0%
0%
0%
THEN FOR CONDITION 2,HEIGHT OF AXLE A ABOVE GROUND = 722 −165 = 557 mm (21.9 in).HEIGHT OF AXLE C ABOVE GROUND = 722 −92 = 630 mm (24.8 in).
FROM THE GRAPHS, A TIRE THAT CARRIES 16.7% OF THE BLG LOADS DEFLECTS 92 mm (3.6 in).A TIRE THAT CARRIES 25% OF THE BLG LOADS DEFLECTS 129 mm (5.1 in).A TIRE THAT CARRIES 33.3% OF THE BLG LOADS DEFLECTS 165 mm (6.5 in).
EXAMPLE OF HOW TO USE THE TIRE INFLATED/DEFLATED GRAPHS AS SHOWN.ASSUME AN AIRCRAFT WEIGHT IS 510 000 kg (1 124 360 lb) WITH THE CG AT 37.4% MAC.
CONDITIONS 1 TO 4 SHOW POSSIBLE DAMAGE SITUATIONS FOR TIRES ON BLG BOGIE.NOTE:TIRE SIZE 1400 X 530 R23 40PRMAXIMUM GROWN TIRE (UNLOADED) RADIUS = 722 mm (28.4 in).RIM OUTER FLANGE RADIUS = 356 mm (14 in).
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (33.3% LOAD).
HEIGHT OF AXLE C ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (16.7% LOAD).
ONE TIRE DEFLATED ON ONE AXLE, 33.3% OF GEAR LOAD ONINFLATED TIRE, 0% ON THE DEFLATED TIRE.
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (33.3% LOAD).
HEIGHT OF AXLE C ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (33.3% LOAD).
ONE TIRE DEFLATED ON THREE AXLES, 33.3% OF GEAR LOAD ONEACH INFLATED TIRE, 0% ON THE DEFLATED TIRES.
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (33.3% LOAD).
HEIGHT OF AXLE C ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (33.3% LOAD)
ONE TIRE DEFLATED ON TWO AXLES, 33.3% OF GEAR LOAD ONEACH INFLATED TIRE, 0% ON THE DEFLATED TIRE.
L_MF_010800_1_0240101_01_00
BLG Tire Deflection NotesBLG Tire Deflection
1-8Page 25
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CONDITION AXLE FOUR TIRES DEFLATED, 50% OF GEAR LOAD ON EACHINFLATED TIRE, 0% ON THE DEFLATED TIRES.A
B5
C
50%
50%
0%
0%
0%
0%
A
B6
C
50%
0%
25%
0%
0%
25%
A
B7
C
25%
0%
25%
25%
0%
25%
A
B8
C
25%
0%
25%
25%
0%
25%
THEN FOR CONDITION 8,HEIGHT OF AXLE A ABOVE GROUND = 722 −129 = 593 mm (23.3 in).HEIGHT OF AXLE C ABOVE GROUND = 356 mm (14 in) (RIM OUTER FLANGE RADIUS).
FROM THE GRAPHS, A TIRE THAT CARRIES 16.7% OF THE BLG LOADS DEFLECTS 92 mm (3.6 in).A TIRE THAT CARRIES 25% OF THE BLG LOADS DEFLECTS 129 mm (5.1 in).A TIRE THAT CARRIES 33.3% OF THE BLG LOADS DEFLECTS 165 mm (6.5 in).
EXAMPLE OF HOW TO USE THE TIRE INFLATED/DEFLATED GRAPHS AS SHOWN.ASSUME AN AIRCRAFT WEIGHT IS 510 000 kg (1 124 360 lb) WITH THE CG AT 37.4% MAC.
CONDITIONS 5 TO 8 SHOW POSSIBLE DAMAGE SITUATIONS FOR TIRES ON BLG BOGIE.NOTE:TIRE SIZE 1400 X 530 R23 40PRMAXIMUM GROWN TIRE (UNLOADED) RADIUS = 722 mm (28.4 in).RIM OUTER FLANGE RADIUS = 356 mm (14 in).
AXLE C. HEIGHT OF AXLE A ABOVE GROUND
HEIGHT OF AXLE C ABOVE GROUND= RIM OUTER FLANGE RADIUS.
FIVE TIRES DEFLATED, 50% OF GEAR LOAD ON INFLATED TIRE,0% ON THE DEFLATED TIRE ON THE SAME AXLE.
HEIGHT OF AXLE C ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (50% LOAD).
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (50% LOAD).
25% OF GEAR LOAD ON THE RIMS OF THE DEFLATED TIRES ON
HEIGHT OF AXLE A ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (25% LOAD).
HEIGHT OF AXLE C ABOVE GROUND= TIRE RADIUS − TIRE DEFLECTION (25% LOAD).
TWO TIRES DEFLATED ON CENTER AXLE, 25% OF GEAR LOAD ONEACH INFLATED TIRE.
AXLE C.HEIGHT OF AXLE A ABOVE GROUND
HEIGHT OF AXLE C ABOVE GROUND= RIM OUTER FLANGE RADIUS.
FOUR TIRES DEFLATED, 25% OF GEAR LOAD ONEACH INFLATED TIRE.25% OF GEAR LOAD ON THE RIMS OF THE DEFLATED TIRES ON
= TIRE RADIUS − TIRE DEFLECTION (50% LOAD).
= TIRE RADIUS − TIRE DEFLECTION (25% LOAD).
L_MF_010800_1_0250101_01_00
BLG Tire Deflection Notes
1-8Page 26
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-9 Ground Clearances
**ON A/C A380-800 Models A380-800F Models
Ground Clearances
1. General
This section gives the heights of various points of the aircraft, above the ground, for different aircraftconfigurations. Dimensions in the tables are approximate and will vary with tire type and conditions.
1-9Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
D
C1F1
E1
F3F2C2
E2
H G
K2 K1
L2
L3 L4 L5 L6 J2 J1
M1M2M3M5 M4 U1U2U3
NOTE: MAXIMUM JACKING WEIGHT = 333 700 kg
C3
L_MF_010900_1_0010102_01_01
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
1-9Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
260tMID 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_MF_010900_1_0020102_01_00
Ground ClearancesA380-800F Models
1-9Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
A B CD E F GH J K L
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
3.95 12.9 3.98 13.0 4.15 13.6 4.10 13.4DN1 INBDEND
DN1/DN2 4.60 15.1 4.62 15.2 4.82 15.8 4.78 15.7DN2 OUTBD
END5.12 16.8 5.13 16.8 5.35 17.5 5.32 17.5
SLAT 2 INBDEND
5.12 16.8 5.13 16.8
5.34 17.5 5.35 17.6 5.62 18.4
17.6 5.35 17.5
SLAT 2/3SLAT 3/4 5.53 18.1 5.53 18.1 5.84 19.2 5.85 19.2
SLAT 4 OUTBDEND
5.65 18.5 5.65 18.5 6.02 19.8 6.04 19.8
SLAT 5 INBDEND
5.78 19.0 5.77 18.9 6.18 20.3 6.21 20.4
SLAT 5/6SLAT 6/7
SLAT 7 OUTBDEND
5.895.986.05
19.319.619.8
5.875.966.02
19.319.619.7
6.356.526.67
20.821.421.9
6.406.586.75
21.021.622.1
A
BC
D
EFG
H
JKL
A380−800 LEADING EDGE SLATS EXTENDED
18.45.61
3.36
L_MF_010900_1_0030103_01_00
Ground ClearancesLeading Edge Slats - Extended - A380-800 Models
1-9Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
12.9 13.0 13.6DN1 INBDEND
DN1/DN2DN2 OUTBD
END16.8 17.5
SLAT 2 INBDEND
16.8
17.5
17.6
SLAT 2/3SLAT 3/4 18.1 5.84 19.2
SLAT 4 OUTBDEND
18.5 18.5
SLAT 5 INBDEND
18.9
SLAT 5/6SLAT 6/7
SLAT 7 OUTBDEND
19.319.619.8 19.7
20.821.421.9
A
BC
D
EFG
H
JKL
3.92 3.95 4.14 4.12 13.5
4.57 15.0 4.60 15.1 4.81 15.8 4.80 15.85.09 16.7 5.11 5.34 5.35 17.6
5.09 16.7 5.11 5.36 5.37 17.6
5.32 5.33 17.5 5.61 18.4 5.64 18.55.50 18.1 5.50 5.88 19.35.63 5.62 6.01 19.7 6.07 19.9
5.76 18.9 5.75 6.17 20.2 6.24 20.5
5.87 5.85 19.2 6.35 6.43 21.15.97 5.94 19.5 6.51 6.61 21.76.03 5.99 6.66 6.78 22.2
A380−800F LEADING EDGE SLATS EXTENDED
A B CD E F GH J K L
L_MF_010900_1_0040102_01_00
Ground ClearancesLeading Edge Slats - Extended - A380-800F Models
1-9Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
AB
1.54 5.0 1.53 5.0 1.68 5.5 1.71 5.63.43 11.3 3.42 11.2 3.62 11.9 3.66 12.0
CD
4.56 15.0 4.54 14.9 4.86 16.0 4.92 16.25.11 16.8 5.08 16.7 5.53 18.1 5.61 18.4
INNER ENDINNER/MIDMID OUTEROUTER END
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
AB
5.0 5.511.9
CD 18.1
INNER ENDINNER/MIDMID OUTEROUTER END
1.52 1.50 4.9 1.67 1.74 5.73.41 11.2 3.39 11.1 3.61 3.70 12.14.54 14.9 4.52 14.8 4.86 15.9 4.96 16.35.10 16.7 5.06 16.6 5.52 5.64 18.5
ABCD
A380−800 FLAPS EXTENDED
A380−800F FLAPS EXTENDED
L_MF_010900_1_0050102_01_00
Ground ClearancesTrailing Edge Flaps - Extended
1-9Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABC
DEFGHJK
SPOILER 1 INBDSPOILER 1/2SPOILER 2
OUTBD ENDSPOILER 3
SPOILER 3/4SPOILER 4/5SPOILER 5/6SPOILER 6/7SPOILER 7/8SPOILER 8
OUTBD END
4.98 16.3 4.97 16.3 5.12 16.8 5.17 17.05.62 18.4 5.61 18.4 5.76 18.9 5.81 19.16.09 20.0 6.08 19.9 6.23 20.4 6.31 20.7
6.32 20.7 6.31 20.7 6.46 21.2 6.55 21.56.56 21.5 6.55 21.5 6.70 22.0 6.80 22.36.79 22.3 6.78 22.2 6.93 22.7 7.07 23.26.94 22.8 6.93 22.7 7.08 23.2 7.25 23.87.02 23.0 7.00 23.0 7.14 23.4 7.36 24.17.02 23.0 7.00 23.0 7.14 23.4 7.42 24.37.00 23.0 6.98 22.9 7.12 23.4 7.45 24.5
ABCDEFGHJK
A380−800 SPOILERS EXTENDED
L_MF_010900_1_0060102_01_00
Ground ClearancesSpoilers - Extended - A380-800 Models
1-9Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
ABCDEFGHJK
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABC
DEFGHJK
SPOILER 1 INBDSPOILER 1/2SPOILER 2
OUTBD ENDSPOILER 3
SPOILER 3/4SPOILER 4/5SPOILER 5/6SPOILER 6/7SPOILER 7/8SPOILER 8
OUTBD END
16.318.4
20.721.5
22.2
23.023.0
4.96 4.95 16.2 5.14 16.9 5.20 17.15.60 5.59 18.3 5.78 19.0 5.84 19.26.07 19.9 6.05 19.9 6.27 20.6 6.34 20.8
6.30 6.29 20.6 6.51 21.4 6.58 21.66.54 6.53 21.4 6.76 22.26.77 22.2 6.76 7.02 23.0 7.10 23.36.93 22.7 6.91 7.20 23.6 7.28 23.97.00 6.97 22.9
22.7
22.97.31 24.0 7.39 24.3
24.424.6
7.01 6.98 7.35 24.1 7.456.98 22.9 6.95 22.8 7.38 24.2 7.49
A380−800F SPOILERS EXTENDED
22.46.83
L_MF_010900_1_0070102_01_00
Ground ClearancesSpoilers - Extended - A380-800F Models
1-9Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
D C B A
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABCD
INNER ENDINNER/MIDMID OUTEROUTER END
5.83 19.1 5.80 19.0 6.24 20.5 6.32 20.75.90 19.4 5.87 19.2 6.35 20.8 6.43 21.15.99 19.7 5.96 19.5 6.49 21.3 6.58 21.66.12 20.1 6.08 19.9 6.69 21.9 6.78 22.3
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABCD
INNER ENDINNER/MIDMID OUTEROUTER END
5.815.885.986.10
19.119.319.620.0
5.775.845.936.05
18.919.219.519.9
6.236.356.496.68
20.520.821.321.9
6.356.476.616.82
20.821.221.722.4
A380−800 AILERONS DOWN
A380−800F AILERONS DOWN
L_MF_010900_1_0080102_01_00
Ground ClearancesAilerons - Down
1-9Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
D C B A
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABCD
INNER ENDINNER/MIDMID OUTEROUTER END
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABCD
INNER ENDINNER/MIDMID OUTEROUTER END
6.386.416.456.50
20.921.021.221.3
6.356.386.416.46
20.820.921.021.2
6.806.876.957.07
22.322.522.823.2
6.876.947.047.17
22.522.823.123.5
6.366.756.846.97
20.922.122.422.9
6.646.716.806.92
21.822.022.322.7
6.796.866.957.06 23.2
22.522.8
6.906.987.077.20
22.722.923.223.6
22.3
A380−800F AILERONS UP
A380−800 AILERONS UP
L_MF_010900_1_0090102_01_00
Ground ClearancesAilerons - Up
1-9Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
DE C
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABCD
TRACK 2TRACK 3TRACK 4TRACK 5TRACK 6 E
2.172.873.083.483.86
7.19.410.111.412.7
2.152.853.063.453.82
7.19.310.011.312.5
2.333.083.353.824.27
7.710.111.012.514.0
2.373.123.423.894.35
7.810.211.212.814.3
m ft m ft m ft m ft
MRWAFT CG
MRWFWD CG
300TAFT CG
OWEMID
DESCRIPTION
ABCDE
2.152.853.073.463.84
7.09.310.111.412.6
2.132.823.033.433.80
7.09.310.011.212.5
2.333.073.343.814.26
7.610.1
14.012.511.0
2.413.153.453.934.38
7.910.411.312.914.4
TRACK 2TRACK 3TRACK 4TRACK 5TRACK 6
B
A
A380−800F FLAP TRACKS EXTENDED
A380−800 FLAP TRACKS EXTENDED
L_MF_010900_1_0100102_01_00
Ground ClearancesFlap Tracks - Extended
1-9Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_010900_1_0110102_01_00
Ground ClearancesForward Nose Landing Gear Doors
1-9Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_010900_1_0120102_01_00
Ground ClearancesAft Nose Landing Gear Doors
1-9Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_010900_1_0130102_01_00
Ground ClearancesWing Landing Gear Doors
1-9Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_010900_1_0140102_01_00
Ground ClearancesBody Landing Gear Doors - Sheet 1/2
1-9Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_010900_1_0150102_01_00
Ground ClearancesBody Landing Gear Doors - Sheet 2/2
1-9Page 16
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
FR117FR112
* DEPENDING ON CG POSITION AND AIRCRAFT WEIGHT
GROUND LINE
MAX 5.52 (18.10 ft)MIN 5.49 (18.00 ft)
MAX 6.66 m (21.84 ft)MIN 6.63 m (21.74 ft)
FUSELAGE DATUM LINE
**
L_MF_010900_1_0160102_01_00
Ground ClearancesAPU Doors
1-9Page 17
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-10 Door Clearances
**ON A/C A380-800 Models A380-800F Models
Door Clearances
1. General
This section gives the identification/location, dimensions and clearances of :- passenger/crew doors (passenger A/C)- courier/crew doors (freighter A/C)- cargo compartment doors- emergency exit doors.
NOTE : For ground clearances of door stills, refer to Section 1-9.
1-10Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_011000_1_0010101_01_00
Door ClearancesDoor Location (Sheet 1) - A380-800 Models
1-10Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_011000_1_0020101_01_00
Door ClearancesDoor Location (Sheet 2) - A380-800 Models
1-10Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_011000_1_0030101_01_00
Door ClearancesDoor Location (Sheet 1) - A380-800F Models
1-10Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_011000_1_0040101_01_00
Door ClearancesDoor Location (Sheet 2) - A380-800F Models
1-10Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
SEECHAPTER
1−9
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_MF_011000_1_0050101_01_00
Door ClearancesForward Doors
1-10Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
1−9MEASURED 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
1−9
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_MF_011000_1_0060101_01_00
Door ClearancesMain and Upper Deck Doors - A380-800 Models
1-10Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
A−A
SEECHAPTER
1−9
UPPER DECK DOORU1R
FWD
A
A
545 mm(214.57 in)
1080 mm(425.20 in)
L_MF_011000_1_0070101_01_00
Door ClearancesUpper Deck Doors - A380-800F Models
1-10Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
SEECHAPTER
1−9
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_MF_011000_1_0080101_01_00
Door ClearancesAft Doors - A380-800 Models
1-10Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
SEECHAPTER
1−9
45 mm(1.77 in)
MEASURED FROM THE EXTERNAL POINT OFTHE SCUFF PLATE AND THE MOSTEXTERNAL POINT OF THE DOOR SKIN
01NOTE:
2138 mm(84.2 in)
1883 mm(74.1 in)
FREE AISLE
2124 mm(83.6 in)
1067 mm
2453 mm
1091 mm
(96.6 in)
(42 in)
(43 in)
FWD
MAIN DECK DOORM5L
FREE AISLE 01
955 mm(37.6 in)
01
1262 mm(49.7 in)
L_MF_011000_1_0090101_01_00
Door ClearancesAft Doors - A380-800F Models
1-10Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
SEECHAPTER
1−9
SEECHAPTER
1−9
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 (121 in) AT FR81A2945 mm (116 in) AT FR85
FWD
1130 mm(44.49 in)
2794 mm(110 in)
GROUND LINE
2008 mm(79.05 in)
B
B
A AB BL_MF_011000_1_0100101_01_02
A
A
Door ClearancesAft Cargo Compartment Doors - A380-800 Models
1-10Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
SEECHAPTER
1−9
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_MF_011000_1_0110101_01_00
Door ClearancesMain Deck Cargo Door - A380-800F Models
1-10Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
SEECHAPTER
1−9
SEECHAPTER
1−9
1752 mm(68.98 in)
2090 mm(82.28 in)
6420 mm(252.76 in) 991 mm
(39.02 in)
1402 mm(55 in)
FWD
1130 mm(44.49 in)
2794 mm(110 in)
GROUND LINE
2008 mm(79.05 in)
A
A
B
B
A AB BL_MF_011000_1_0120101_01_02
3071 mm (121 in) AT FR81A2945 mm (116 in) AT FR85
Door ClearancesLower Deck Aft Cargo Doors - A380-800F Models
1-10Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
SEECHAPTER
1−9
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_MF_011000_1_0130101_01_01
Door ClearancesForward Cargo Compartment Doors - A380-800 Models
1-10Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
A−A
SEECHAPTER
1−9
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_MF_011000_1_0140101_01_02
Door ClearancesUpper Deck Cargo Door - A380-800F Models
1-10Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
SEECHAPTER
1−9
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_MF_011000_1_0150101_01_02
Door ClearancesLower Deck Forward Cargo Door - A380-800F Models
1-10Page 16
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-11 Fuselage Cross-sections
**ON A/C A380-800 Models A380-800F Models
Fuselage Cross-sections
1. General
This section gives fuselage cross-sections.
1-11Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
Z=1063.9
Z=−1561.1
FRAME 0STA8170.2
Z=1533.3
Z=−1868.2
FRAME 5STA8789.2
FRAME 6STA9114.2
Z=1694.4
FRAME 7STA9437.2
Z=1998.7
Z
YY
Z
Y
Z
Y 00
0
Z
0
Z=−1985 Z=−2080
L_MF_011100_1_0010101_01_00
Fuselage Cross-SectionSection 11/12 - FR0 to FR7
1-11Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
FRAME 8STA9760.2
Z=2320.6
Z=−2158.8
Z=2621.9
Z=−2225.4
FRAME 9STA10083.2
FRAME 10STA10406.2
Z=−2282.8
FRAME 11STA10805.2
Z=3176.4
Z=2339.3
Z
Z
Y
Z
Y
Y
Z
Y
00
00
Z=2897.2
L_MF_011100_1_0020101_01_00
Fuselage Cross-SectionSection 11/12 - FR8 to FR11
1-11Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
Z=3428.4
Z=−2390.2
FRAME 12STA11128.2
FRAME 13STA11453.2
Z=3634.0
Z=−2432.7
FRAME 14STA11778.2
FRAME 15STA12053.2
Z=3820.9 Z=3965.2
Z
Y
Z
Y
Z
Y
00
0
Z
Y0
Z=−2470.9 Z=−2500
L_MF_011100_1_0030101_01_00
Fuselage Cross-SectionSection 11/12 - FR12 to FR15
1-11Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
Z=−70.4
MAIN DECKDOOR 1
Z=2056.8
FRAME 17BSTA13073.2
Z=4404.7
FRAME 15ASTA12355.2
Z=4110.1
Z=−2529.0
FRAME 16STA12657.2
Z=4242.1
Z=−2555.3
Z=−2587.6
FRAME 17CSTA13429.2
Z
Y
Z
Y
Z
Y
00
0
Z
Y0
Z=4528.5
Z=−2612.0
L_MF_011100_1_0040101_01_00
Fuselage Cross-SectionSection 11/12 - FR15A to FR17C
1-11Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
Z=−70.4
MAIN DECKDOOR 1
FRAME 18ASTA13824.2
Z=4651.4
Z=2057.1
Z=−2636.2
FRAME 19BSTA14351.2
Z=4795.7
Z=−2664.1
Z
Y
Z
Y
L_MF_011100_1_0050101_01_00
Fuselage Cross-SectionSection 11/12 - FR18A to FR19B
1-11Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
Z=5064
Z=−2713.4
Z=−5176.5
Z=−2732.2
Z=4934.1
Z=−2690.1
FRAME 21STA15570.2
FRAME 22STA16205.2
FRAME 20STA14935.2
Z
Y
Z
Y
Z
Y
L_MF_011100_1_0060101_01_00
Fuselage Cross-SectionSection 11/12 - FR20 to FR22
1-11Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
FRAME 24STA17475.2
FRAME 25STA18110.2
FRAME 26STA18745.2
Z=5274.3
Z=−2747.2
Z=5358.9
Z=−2759
Z=5431.1
FRAME 23STA16840.2
Z
Y
Z
Y
ZZ
Y
a: FORWARD CARGO COMPARTMENT DOOR
a a
Z=−2429.6
Z=−2768.1
Z=−2432.2
Z=−660
0 0
Y0
Z=5491.5
Z=−2775
Z=−66
L_MF_011100_1_0070101_01_00
Fuselage Cross-SectionSection 13 - FR23 to FR26 - A380-800 Models
1-11Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 23STA16840.2
Z
Y
Z
Y
0SCALE (mm)
1000 2000 a: FORWARD CARGO COMPARTMENT DOOR
DOORM1L
Z=−2747.2
Z=5274.3
0
Z=−2759
0
Z Z
Y Y
FRAME 25STA18110.2
FRAME 26STA18745.2
Z=−2768.1Z=−2429.6Z=−2429.6
Z=−66 Z=−66
Z=−2775
Z=5491.5Z=5431.1
Z=2688.5
Z=4788.5
aa
0 0
FRAME 24STA17475.2
Z=5358.9
Z=−2432.2
L_MF_011100_1_0080101_01_00
Fuselage Cross-SectionSection 13 - FR23 to FR26 - A380-800F Models
1-11Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z
Z=−2780
Z=5540.3
FORWARDCARGO
COMPARTMENTDOOR
FORWARDCARGO
COMPARTMENTDOOR
FRAME 28STA20015.2
FRAME 27STA19380.2
Z=−2434.1
Z=−66
Z=−2435.4
Z=−66
0
0
Y
Z=5577.7
Z=−2783
L_MF_011100_1_0090101_01_00
Fuselage Cross-SectionSection 13 - FR27 to FR28 - A380-800 Models
1-11Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 27STA19380.2
Y
Y
Z
Z
FRAME 28STA20015.2
Z=5540.3
Z=−2780
Z=5577.7
Z=−2783Z=−2435.4
Z=−66
Z=−2434.1
Z=−66
FORWARD CARGOCOMPARTMENT DOOR
FORWARD CARGOCOMPARTMENT DOOR
0
0
0SCALE (mm)
1000 2000
L_MF_011100_1_0100101_01_00
Fuselage Cross-SectionSection 13 - FR27 to FR28 - A380-800F Models
1-11Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z
Y
FRAME 29STA20650.2
FRAME 30STA21285.2
Z=5604.2
Z=5619.8
0
0
Z=−2785.3
Z=−2784.8
L_MF_011100_1_0110101_01_00
Fuselage Cross-SectionSection 13 - FR29 to FR30 - A380-800 Models
1-11Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
0SCALE (mm)
1000 2000
Z=5604.2
Z=−2784.8
Z=5619.8
Z=−2785.3
FRAME 29STA20650.2
FRAME 30STA21285.2
Y
Z
Y
Z
0
0
L_MF_011100_1_0120101_01_00
Fuselage Cross-SectionSection 13 - FR29 to FR30 - A380-800F Models
1-11Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y0
FRAME 31STA21920.2
Z=5624.7
Z=−2785.3
Z
Y0
Z=5624.7
Z=−2785.3
FRAME 32STA22555.2
L_MF_011100_1_0130101_01_00
Fuselage Cross-SectionSection 13 - FR31 to FR32 - A380-800 Models
1-11Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 31STA21920.2
FRAME 32STA22555.2
Z=5624.7
0SCALE (mm)
1000 2000
Z=5233.1
Z=2556.3
Z=−2785.3
Z=5624.7
Z=−2785.3
Z=5233.1
Z=2556.3
UPPER DECKCARGO DOOR
UPPER DECKCARGO DOOR
0
Y
Z
Y
Z
0
L_MF_011100_1_0140101_01_00
Fuselage Cross-SectionSection 13 - FR31 to FR32 - A380-800F Models
1-11Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z
Y
Z=−2785.3
0
FRAME 33STA23190.2
Z=−2785.3
0
FRAME 34STA23825.2
MAIN DECKDOOR 2
Z=2054
Z=−70.4
Z=5624.7
Z=5624.7
L_MF_011100_1_0150101_01_00
Fuselage Cross-SectionSection 13 - FR33 to FR34 - A380-800 Models
1-11Page 16
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 33STA23190.2
Z=5233.1
Z=2556.3
Z
Y
UPPER DECKCARGO DOOR
Z=−2785.3
Z=5624.7
FRAME 34STA23825.2
Z
Y
Z=5233.1
Z=2556.3
Z=−2785.3
Z=5624.7
UPPER DECKCARGO DOOR
0SCALE (mm)
1000 2000
0
0
L_MF_011100_1_0160101_01_00
Fuselage Cross-SectionSection 13 - FR33 to FR34 - A380-800F Models
1-11Page 17
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z
Y
FRAME 36STA25095.2
FRAME 35STA24460.2
Z=5624.7
Z=−2785.3
0
0
Z=5624.7
Z=−2785.3
L_MF_011100_1_0170101_01_00
Fuselage Cross-SectionSection 13 - FR35 to FR36 - A380-800 Models
1-11Page 18
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
0
Z=5233.1
Y
Z
UPPER DECKCARGO DOOR
Z=2556.3
Z=−2785.3
Y
Z
Z=−2785.3
FRAME 35STA24480.2
FRAME 36STA25095.2
0SCALE (mm)
1000 2000
0
L_MF_011100_1_0180101_01_00
Fuselage Cross-SectionSection 13 - FR35 to FR36 - A380-800F Models
1-11Page 19
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z=−2785.3
FRAME 37STA25730.2
FRAME 38STA26365.2
0
Z
Y
Z=5624.7
Z=−2785.3
0
L_MF_011100_1_0190101_01_00
Fuselage Cross-SectionSection 13 - FR37 to FR38 - A380-800 Models
1-11Page 20
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 37STA25790.2
FRAME 38STA26365.2
Z=5624.7
0
0
Y
Z
Y
Z
0SCALE (mm)
1000 2000
Z=−2785.3
Z=5624.7
Z=−2833.2
L_MF_011100_1_0200101_01_00
Fuselage Cross-SectionSection 13 - FR37 to FR38 - A380-800F Models
1-11Page 21
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
FRAME 39STA27000.2
FRAME 40STA27635.2
0
Z=−2985.3
Z=5624.7
Z=−2911.8
Z=5624.7Z
Y0
L_MF_011100_1_0210101_01_00
Fuselage Cross-SectionSection 15/21 - FR39 to FR40 - A380-800 Models
1-11Page 22
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 39STA27000.2
Z
Z=5624.7
Z=−2911.8
0
FRAME 40STA27685.2
Z
Z=5624.7
Z=−2985.3
Y
0SCALE (mm)
1000 2000
0
Y
L_MF_011100_1_0220101_01_00
Fuselage Cross-SectionSection 15/21 - FR39 to FR40 - A380-800F Models
1-11Page 23
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z
Y
Z=5624.7
0
0
UPPER DECKDOOR 7
FRAME 41STA28270.2
FRAME 42STA28905.2
Z=4775.5
Z=1753.4
Z=−3053.1
Z=−3115.5
Z=−3053.1
Z=5624.7Z=5624.7
L_MF_011100_1_0230101_01_00
Fuselage Cross-SectionSection 15/21 - FR41 to FR42 - A380-800 Models
1-11Page 24
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 41STA28270.2
Z
FRAME 42STA28905.2
Z
Z=5624.7
Z=−3053.1
Z=5624.7
Z=−3115.5
0SCALE (mm)
1000 2000
Y
Y
0
0
L_MF_011100_1_0240101_01_00
Fuselage Cross-SectionSection 15/21 - FR41 to FR42 - A380-800F Models
1-11Page 25
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
FRAME 43STA29540.2
FRAME 44STA30175.2
Z
Y
Z
Y
0
0
Z=5624.7
Z=5624.7
Z=−3224.3
Z=−3172.5
L_MF_011100_1_0250101_01_00
Fuselage Cross-SectionSection 15/21 - FR43 to FR44 - A380-800 Models
1-11Page 26
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z=−3172.5
FRAME 43STA29540.2
Z=5624.7
FRAME 44STA30175.2
Z=−3224.3
Z
Y0
0
L_MF_011100_1_0260101_01_00
Fuselage Cross-SectionSection 15/21 - FR43 to FR44 - A380-800F Models
1-11Page 27
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z=5624.7
Z
Y
Z=5624.7
Z
Y
Z=5624.7
Z=−3272.5
0
Z=−3315.5
FRAME 45STA30835.6
FRAME 46STA31496
FRAME 47STA32156.4
FRAME 48STA32816.8
Z=−3353.7
0
00
Z=−3387.2
L_MF_011100_1_0270101_01_00
Fuselage Cross-SectionSection 15/21 - FR45 to FR48 - A380-800 Models
1-11Page 28
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 45STA30835.6
FRAME 47STA32156.4
FRAME 48X=32816.8
FRAME 46STA31496
0SCALE (mm)
1000 2000
0 0
0 0
Z Z
Z Z
Y
YY
Z=5624.7
Z=−3272.5
Z=5624.7
Z=−3353.7
Z=5624.7
Z=−3315.5
Z=5624.7
Z=−3387.2
Y
L_MF_011100_1_0280101_01_00
Fuselage Cross-SectionSection 15/21 - FR45 to FR48 - A380-800F Models
1-11Page 29
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z=5624.7
0
FRAME 49STA33477.2
Z=−3416.5
Z=−3441.8
FRAME 50STA34137.6
0
L_MF_011100_1_0290101_01_00
Fuselage Cross-SectionSection 15/21 - FR49 to FR50 - A380-800 Models
1-11Page 30
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 49STA33477.2
FRAME 50STA34137.6
Z=5624.7
Z=5624.7
Z=−3416.5
Z=−3441.8
0
0
0SCALE (mm)
1000 2000
Z
Y
Z
Y
L_MF_011100_1_0300101_01_00
Fuselage Cross-SectionSection 15/21 - FR49 to FR50 - A380-800F Models
1-11Page 31
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
FRAME 51STA34798
FRAME 53STA36118.8
Z Z
ZZ
Y Y
YY
0 0
0 0
0SCALE (mm)
1000 2000
FRAME 52STA35458.4
FRAME 54STA36779.2
Z=−3463.2
Z=5624.7
Z=−3495.8 Z=−3507.4
Z=−3481.2
Z=5624.7
Z=5624.7Z=5624.7
L_MF_011100_1_0310101_01_00
Fuselage Cross-SectionSection 15/21 - FR51 to FR54 - A380-800 Models
1-11Page 32
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 51STA34798
FRAME 53STA36118.8
Z Z
ZZ
Y Y
YY
0 0
0 0
0SCALE (mm)
1000 2000
FRAME 52STA35458.4
FRAME 54STA36779.2
Z=−3463.2
Z=5624.7
Z=−3495.8 Z=−3507.4
Z=−3481.2
Z=5624.7
Z=5624.7Z=5624.7
L_MF_011100_1_0320101_01_00
Fuselage Cross-SectionSection 15/21 - FR51 to FR54 - A380-800F Models
1-11Page 33
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z=5624.7
Z
Y
Z=5624.7
Y
Z=5624.7Z
Z=−3515.9
FRAME 55STA37439.6
0 0
Z=−3521.7
FRAME 56STA38100
0
Z=−3524.7
FRAME 57STA38735
FRAME 58STA39370
Z=−3525.5
0
L_MF_011100_1_0330101_01_00
Fuselage Cross-SectionSection 15/21 - FR55 to FR58 - A380-800 Models
1-11Page 34
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 55STA37439.6
Z
Y0
Z=5624.7
Z=−3515.9
Z=5624.7
Z=−3521.7
FRAME 56STA38100
Z
Y0
FRAME 57STA38735
Z
FRAME 58STA39370
Z
Z=5624.7
Z=−3524.7
Z=5624.7
Z=−3525.5
0SCALE (mm)
1000 2000
0 0Y Y
L_MF_011100_1_0340101_01_00
Fuselage Cross-SectionSection 15/21 - FR55 to FR58 - A380-800F Models
1-11Page 35
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z=5624.7
0
0
MAIN DECKDOOR 3
Z=−3520.7
Z=−3524.2
FRAME 60STA40640
FRAME 59STA40005
Z=2054
Z=−65
L_MF_011100_1_0350101_01_00
Fuselage Cross-SectionSection 15/21 - FR59 to FR60 - A380-800 Models
1-11Page 36
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 59
0
0
Z=5624.7
Z=−3524.2
Z=5624.7
Z=−3520.7
STA40005
FRAME 60STA40640
0SCALE (mm)
1000 2000
Z
Y
Z
Y
L_MF_011100_1_0360101_01_00
Fuselage Cross-SectionSection 15/21 - FR59 to FR60 - A380-800F Models
1-11Page 37
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z
Y
Z=5624.7
Z=5624.7
0 0
Z=−3506
FRAME 61STA41275
FRAME 62STA41910
0
FRAME 63STA42545
Z=−3479.5
FRAME 64STA43180
Z=−3494.3
Z=5624.7
Z=−3514.7
Z
Y0
L_MF_011100_1_0370101_01_00
Fuselage Cross-SectionSection 15/21 - FR61 to FR64 - A380-800 Models
1-11Page 38
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 61STA41275
Y
Z=5624.7 Z=5624
Z=5624.7
Z=−3506Z=−3514.7
FRAME 62STA41910
Y0
Y
FRAME 63STA42545
FRAME 64STA43180
Y
Z=5624.7
Z=−3494.3 Z=−3479.5
0
0SCALE (mm)
1000 2000
0
0
Z Z
Z Z
L_MF_011100_1_0380101_01_00
Fuselage Cross-SectionSection 15/21 - FR61 to FR64 - A380-800F Models
1-11Page 39
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z
Y
Y
Z
0 0
FRAME 65STA43815
FRAME 66STA44450
FRAME 67STA45085
0
FRAME 68STA45720
Z=5624.7
Z=5624.7
Z=5624.7
Z=5624.7
Z=−3461.6
Z=−3388.3Z=−3416
Z=−3440.4
Z
Y0
L_MF_011100_1_0390101_01_00
Fuselage Cross-SectionSection 15/21 - FR65 to FR68 - A380-800 Models
1-11Page 40
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 65STA43815
FRAME 66STA44450
FRAME 68STA45720
FRAME 67STA45085
0SCALE (mm)
1000 2000
Z=5624.7 Z=5624.7
Z=−3461.6 Z=−3440.4
Z=5624.7 Z=5624.7
Z=−3416 Z=−3388.3
Z Z
ZZ
Y
YY
Y0 0
0 0
L_MF_011100_1_0400101_01_00
Fuselage Cross-SectionSection 15/21 - FR65 to FR68 - A380-800F Models
1-11Page 41
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z=5624.7
0
Z=−3322.9
FRAME 70STA46990
0
FRAME 69STA46255
Z=−3357.4
L_MF_011100_1_0410101_01_00
Fuselage Cross-SectionSection 15/21 - FR69 to FR70 - A380-800 Models
1-11Page 42
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 65STA43815
FRAME 66STA44450
FRAME 68STA45720
FRAME 67STA45085
0SCALE (mm)
1000 2000
Z=5624.7 Z=5624.7
Z=−3461.6 Z=−3440.4
Z=5624.7 Z=5624.7
Z=−3416 Z=−3388.3
Z Z
ZZ
Y
YY
Y0 0
0 0
L_MF_011100_1_0420101_01_00
Fuselage Cross-SectionSection 15/21 - FR65 to FR68 - A380-800F Models
1-11Page 43
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z=5624.7
0
Z=−3284.6
FRAME 71STA47625
UPPER DECKDOOR 8
0
Z=−3242
FRAME 71STA48260
Z=4775.5
Z=1753.4
L_MF_011100_1_0430101_01_00
Fuselage Cross-SectionSection 15/21 - FR71 to FR72 - A380-800 Models
1-11Page 44
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
Z=5624.7
Z=−3284.6
Z=5624.7
Z=−3242
0
0
0SCALE (mm)
1000 2000
FRAME 71STA47625
Z
FRAME 72STA48260
Z
Y
Y
L_MF_011100_1_0440101_01_00
Fuselage Cross-SectionSection 15/21 - FR71 to FR72 - A380-800F Models
1-11Page 45
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z
Y
Z=5624.7
Z
Y
Z=5624.7
0
Z=−3143.1
FRAME 74STA49530
FRAME 73STA48895
Z=−3194.9
0
L_MF_011100_1_0450101_01_00
Fuselage Cross-SectionSection 15/21 - FR73 to FR74 - A380-800 Models
1-11Page 46
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
0SCALE (mm)
1000 2000
FRAME 73STA48895
FRAME 74STA49530
Z=5624.7
Z=−3194.9
Z=5624.7
Z=−3143.1
Z
Y
Z
Y
0
0
L_MF_011100_1_0460101_01_00
Fuselage Cross-SectionSection 15/21 - FR73 to FR74 - A380-800F Models
1-11Page 47
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
FRAME 75STA50165
1000 2000
FRAME 77STA51435
FRAME 76STA50800
FRAME 78STA52070
Z=5624.7
Z=5624.7
Z=5624.7
Z=−3086.5 Z=−3025
Z=−2932.7Z=−2958.6
MAINDECK
DOOR 4
Z=5624.7
Z=2054
Z=−70.4
Z
Y
Z
Y
Z
Y
Z
Y
0
0
0
0
L_MF_011100_1_0470101_01_00
Fuselage Cross-SectionSection 18 - FR75 to FR78 - A380-800 Models
1-11Page 48
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
Z Z
Z Z
Y Y
Y Y
0 0
0 0
FRAME 75
0SCALE (mm)
1000 2000
Z=5624.7
Z=5624.7 Z=5624.7
Z=−3086.5 Z=−3025
Z=−2958.6 Z=−2932.7
FRAME 75STA50165
FRAME 76FRAME 75STA50800
FRAME 77STA51435
FRAME 78STA52070
Z=5624.7
L_MF_011100_1_0480101_01_00
Fuselage Cross-SectionSection 18 - FR75 to FR78 - A380-800F Models
1-11Page 49
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
FRAME 79STA52705
Z=5624.7Z=5624.7
Z=−2932.7 Z=−2912.3
FRAME 81STA53975
Z
Y
Z
Y
Z
Y
00
0
Z=5624.7
Z=−2850.9
FRAME 80STA53340
L_MF_011100_1_0490101_01_00
Fuselage Cross-SectionSection 18 - FR79 to FR81 - A380-800 Models
1-11Page 50
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z=5624.7
Z=5624.7
Z=−2683.4
FRAME 82STA54610
FRAME 83STA55245
Z=−2771
Z=−68
AFTCARGODOOR
Z
Y
Z
Y
0
0Z=−68
Z=−2532.5
AFTCARGODOOR
Z=−2497.9
L_MF_011100_1_0510101_01_00
Fuselage Cross-SectionSection 18 - FR82 to FR83 - A380-800 Models
1-11Page 51
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 82STA54610
FRAME 83STA55245
Z=5624.7
Z=−2771
Z=5624.7
Z=−2683.4
Z=−452.2
Z=2597.8
Z=2597.8
Z=−452.2
Z=−2497.9
Z=−68
Z=−68
Z=−2532.5
LOWER DECKAFT CARGO
DOOR
MAIN DECKCARGO DOOR
MAIN DECKCARGO DOOR
LOWER DECKAFT CARGO
DOOR
0
0
0SCALE (mm)
1000 2000
Z
Y
Z
Y
L_MF_011100_1_0520101_01_00
Fuselage Cross-SectionSection 18 - FR82 to FR83 - A380-800F Models
1-11Page 52
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Z=5624.7
FRAME 84STA55880
FRAME 85STA56515
Z=5624.7
Z=−2589.8
Z=−2492.1
UPPERDECK
DOOR 9
Z=4775.5
Z=1753.4
Z
Y
Z
Y
0
0Z=−68
AFTCARGODOOR
Z=−68
AFTCARGODOOR
Z=−2382.5
Z=−2448.3
L_MF_011100_1_0530101_01_00
Fuselage Cross-SectionSection 18 - FR84 to FR85 - A380-800 Models
1-11Page 53
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
0SCALE (mm)
1000 2000
Z=−2448.3
Z=−68
LOWER DECKAFT CARGO
FRAME 84STA55880
Z
0
Z=5624.7
Y
MAIN DECKCARGO DOOR
Z=2597.8
Z=−452.2
FRAME 85STA58515
Z
Z=5624.7
Z=−2589.8
Z=−68
Z=−2382.5
DOOR
LOWER DECKAFT CARGO
DOOR
MAIN DECKCARGO DOOR
Z=2597.8
Z=−452.2
Z=−2492.1
Y0
L_MF_011100_1_0540101_01_00
Fuselage Cross-SectionSection 18 - FR84 to FR85 - A380-800F Models
1-11Page 54
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)1000 2000
Z
Y
Y Y
Z
Y
0
0
0
0
Z=5624.7 Z=5622.4
FRAME 86STA57150
FRAME 87STA57785
Z=−2286.1Z=−2390.7
FRAME 88STA58420
Z=5615.1
Z
FRAME 89STA59055
Z=5802.7
Z
Z=−2178.7 Z=−2068.4
BULKCARGODOOR
Z=−1956.9
Z=−1330.9
L_MF_011100_1_0550101_01_00
Fuselage Cross-SectionSection 18 - FR86 to FR89 - A380-800 Models
1-11Page 55
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
Z=5624.7
Z=−2390.7
Z=5615.1
Z=−2178.7
Z=−2286.1
Z=5622.4
Z=−452.2
Z=2597.8
a
b
Z=−1330.9
Z=−1956.9
FRAME 86STA57150
0SCALE (mm)
1000 2000
FRAME 88STA58420
FRAME 89STA59055
FRAME 87STA57785
a: MAIN DECK CARGO DOOR
b: BULK DOOR
0 0
0 0
Z
Y
Z
Y
Z
Y
Z
Y
Z=5602.7
Z=−2068.4
L_MF_011100_1_0560101_01_00
Fuselage Cross-SectionSection 18 - FR86 to FR89 - A380-800F Models
1-11Page 56
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
FRAME 90STA59690
Z=5585.3
Z=−1955.3
FRAME 91STA60325
Z=5562.9
Z=−1839.3
FRAME 92STA60960
Z=−1720.2
Z=2054
Z=5535.3Z=5535.3Z=5535.3
MAIN DECKDOOR 5
Z=−70.4
Z
Y
Z
Z
Y
Y
00
0
L_MF_011100_1_0570101_01_00
Fuselage Cross-SectionSection 18 - FR90 to FR92 - A380-800 Models
1-11Page 57
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 90STA59690
Z=5585.3
Z=−1955.3
Z=5562.9
Z=−1839.3
Z=5535.3
Z=−1720.2
Z=−117.8
Z=2042.2
DOOR M5L
Z
0
Z
Y
Z
FRAME 91STA60325
FRAME 92STA60960
0 0
0SCALE (mm)
1000 2000
Y Y
L_MF_011100_1_0580101_01_00
Fuselage Cross-SectionSection 18 - FR90 to FR92 - A380-800F Models
1-11Page 58
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0SCALE (mm)
1000 2000
Y0
Z
Y0
Z
Y0
FRAME 95STA62865
Z
FRAME 93STA61595
FRAME 94STA62230
Z=5502.8
Z=−1597.7
Z=5465.2
Z=−1471
Z=5422.4
Z=−1339.2
L_MF_011100_1_0590101_01_00
Fuselage Cross-SectionSection 18 - FR93 to FR95 - A380-800 Models
1-11Page 59
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FRAME 93STA61595
Z=5502.8
Z=−1597.7
Z=5465.2
Z=−1471
Z=5422.4
Z=−1339.2
FRAME 94STA62230
FRAME 95STA62865
0SCALE (mm)
1000 2000
Y
Z
Y
Z
Y
Z
0 0
0
L_MF_011100_1_0600101_01_00
Fuselage Cross-SectionSection 18 - FR93 to FR95 - A380-800F Models
1-11Page 60
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
Z
Y0
Z
Y0
Z
Y0
FRAME 98STA64770
Z=5263.8
Z=−932.3
FRAME 96STA63500
FRAME 97STA64135
Z=5374.7 Z=5321.8
Z=−1204.1 Z=−1068.4
L_MF_011100_1_0610101_01_00
Fuselage Cross-SectionSection 19 - FR96 to FR98
1-11Page 61
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
FRAME 99STA65405
FRAME 100STA66040
FRAME 101STA66675
FRAME 102STA67310
Z=5200.8 Z=5132.6
Z=−795.5 Z=−658
Z=5059.2 Z=4980.8
Z=−519.6 Z=−380.1
Z
Y
Z
Y
Z
Y
Z
Y
0
0
0
0
L_MF_011100_1_0620101_01_00
Fuselage Cross-SectionSection 19 - FR99 to FR102
1-11Page 62
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
FRAME 103STA67945
FRAME 104STA68580
FRAME 105STA69260
FRAME 106STA69640
Z=4897.2 Z=4814.6
Z=−239.4 Z=−97
Z=4731.9 Z=4655
Z=57.6 Z=215.2
Z
Y
Z
Y
Z
Y
Z
Y
0
0
0
0
L_MF_011100_1_0630101_01_00
Fuselage Cross-SectionSection 19 - FR103 to FR106
1-11Page 63
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
FRAME 107STA70620
FRAME 108STA71300
FRAME 109STA71810
FRAME 110STA72320
Z=4584.1
Z=542.7
Z=4519
Z=4473.5 Z=4424.8
Z=671.5 Z=804.6
Z=376.5
Z
Y
Z
Y
Z
Y
Z
Y
0
0
0
0
L_MF_011100_1_0640101_01_00
Fuselage Cross-SectionSection 19 - FR107 to FR110
1-11Page 64
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
FRAME 111STA72354
FRAME 112STA72922
FRAME 113STA73462
FRAME 114STA74002
Z=4421.4 Z=4359.5
Z=4297.8 Z=4236.1
Z=813.4 Z=974.9
Z=1134.4 Z=1293.9
Z
Y
Z
Y
Z
Y
Z
Y
0
0
0
0
L_MF_011100_1_0650101_01_00
Fuselage Cross-SectionSection 19 - FR111 to FR114
1-11Page 65
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0SCALE (mm)
1000 2000
FRAME 115STA74542
FRAME 116STA75082
Z=4112.6Z=4174.4
Z=1453.4 Z=1612.9
FRAME 117STA75622
Z=4050.9
FRAME 118STA75983
Z=4009.7
Z=1879
FRAME 119STA76149.5
Z=3990.6
Z=1928.2
Z
Y
Z
Y
Z
Y0
0
0
Y0
Z
Y0
Z
Z=1772.4
L_MF_011100_1_0660101_01_00
Fuselage Cross-SectionSection 19.1 - FR115 to FR119
1-11Page 66
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-12 Nose Contours
**ON A/C A380-800 Models A380-800F Models
Nose Contours
1. GeneralThis section gives the Nose Contours.
1-12Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
X=1
490
FR0
X=2
757
FR
7
X=4
773
FR13
X=7
144
FR18
A
X=2
0650
FR
29
X=1
7475
FR
24
EV
OLU
TIV
E S
HA
PE
LIM
IT X
=145
75
A
B
C
D
E
F
Z=4150
Z=2703.5
Z=778
Z=−50
Z=−1000
Z=−2128
UPPER DECKFLOOR LEVEL
COCKPITFLOOR LEVELMAIN DECKFLOOR LEVEL
CARGOFLOOR LEVEL
A
B
C
D
E
F
L_MF_011200_1_0010102_01_00
Nose ContoursLevel Positions - A380-800 Models
1-12Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
X=8
170.
2 FR
0
X=9
437.
2 F
R7
X=1
1453
.2 F
R13
X=1
3824
.2 F
R18
A
X=2
0650
FR
29
X=1
7475
.2 F
R24
EV
OLU
TIV
E S
HA
PE
LIM
IT X
=145
75
A
B
C
D
E
F
Z=4150
Z=2770.6
Z=778
Z=−97.4
Z=−1000
Z=−2128
UPPER DECKFLOOR LEVEL
COCKPITFLOOR LEVELMAIN DECKFLOOR LEVEL
CARGOFLOOR LEVEL
A
B
C
D
E
FX
=187
45.2
FR
26
L_MF_011200_1_0020102_01_00
Nose ContoursLevel Positions - A380-800F Models
1-12Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
NOSE CONTOUR POINTS A380−800
POINTS X (mm) Y (mm) Z (mm)
8170.2FR0
P1 633.7 7788170.2P2 1136 −508170.2P3 1038.9 −10009427.2P4 1507.4 7789427.2P5 1843.1 −509427.2P6 1751.5 −1000
11453.2P7 1430.6 2703.511453.2P8 2393.7
−5011453.2P9 2520.2778
11453.2P10 2381.7 −100011453.2P11 1471.6 −212813824.2P12 1317.2 415013824.2P13 2422.5 2703.513824.2P14 2978.1 77813824.2P15 2979.9 −5013824.2P16 2783.5 −100013824.2P17 1911.9 −212817475.2P18 2372.3 415017475.2P19 3135.4 2703.517475.2P20 3420.6 77817475.2P21 3314.6 −5017475.2P22 2993.6 −100017475.2P23 2013.7 −212820650.2P24 2717.9 415020650.2P25 3537.8 2703.520650.2P26 3377.8 77820650.2P27 3381.1 −5020650.2P28 3015.7 −100020650.2P29 2019 −2128
FR7
FR13
FR18A
FR24
FR29
FR
0
FR
7
FR
13
FR
18A
FR
24
FR
29
P1
P2
P3
P4
P5
P6 P10
P9
P8
P11 P17
P16
P7 P13
P12 P18
P19
P20
P21
P25
P24
P29
P28
P27
P26P14
P22
P23
L_MF_011200_1_0030102_01_02
P15
Nose ContoursContour Points at Frame Positions - A380-800 Models
1-12Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
NOSE CONTOUR POINTS A380−800F
POINTS X (mm) Y (mm) Z (mm)
8170.2FR0
P1 633.7 7788170.2P2 1150.1 −97.48170.2P3 1038.9 −10009427.2P4 1507.4 7789427.2P5 1852.2 −97.49427.2P6 1751.5 −1000
11453.2P7 1376.2 2770.611453.2P8 2393.7
−97.411453.2P9 2520778
11453.2P10 2381.7 −100011453.2P11 1471.6 −212813824.2P12 1317.2 415013824.2P13 2389.9 2770.613824.2P14 2978.1 77813824.2P15 2976.1 −97.413824.2P16 2783.5 −100013824.2P17 1911.9 −212817475.2P18 2372.3 415017475.2P19 3110.3 2770.617475.2P20 3420.6 77817475.2P21 3304.3 −97.417475.2P22 2993.6 −100017475.2P23 2013.7 −212820650.2P24 2717.9 415020650.2P25 3358.2 2770.620650.2P26 3537.8 77820650.2P27 3367.8 −97.420650.2P28 3015.7 −100020650.2P29 2019 −2128
FR7
FR13
FR18A
FR24
FR29
FR
0
FR
7
FR
13
FR
18A
FR
24
FR
29
P1
P2
P3
P4
P5
P6 P10
P9
P8
P11 P17
P16
P7 P13
P12 P18
P19
P20
P21
P25
P24
P29
P28
P27
P26P14
P22
P23
L_MF_011200_1_0040102_01_01
P15
Nose ContoursContour Points at Frame Positions - A380-800F Models
1-12Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
ABC
X=
1747
5
X=
2065
0
D
E
F
X=
1490
X=
2757
X=
4773
X=
7144
UPPER NOSE CONTOUR
LOWER NOSE CONTOUR
L_MF_011200_1_0050102_01_00
Nose ContoursUpper and Lower Contours - A380-800 Models
1-12Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
ABC
X=
1747
5.2
X=
2065
0.2
D
E
F
X=
8170
.2
X=
9437
.2
X=
1145
3.2
X=
1382
4.2
X=
1874
5.2
UPPER NOSE CONTOUR
LOWER NOSE CONTOUR
L_MF_011200_1_0060102_01_00
Nose ContoursUpper and Lower Contours - A380-800F Models
1-12Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-13 Vertical Stabilizer Contours
**ON A/C A380-800 Models A380-800F Models
Vertical Stabilizer Contours
1. GeneralThis section gives Vertical Stabilizer contours.Vertical stabilizer contours shown in this section have been selected to assist in designing stands orequipment. These levels provide access to important maintenance areas such as servo controls, rudderhinges, leading edge, trailing edge, HF and VOR antennas.The contours given are on the surface of body skin ; clearance space allowances will have to be madeas required.Ground clearances will depend on whether the airplane is on jacks or on wheels and in this case whatthe CG and weight conditions are.
1-13Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Z
4320 mm
A
Z=0
1000 mm (39.37 in)
2000 mm (78.74 in)
3000 mm (118.11 in)
4000 mm (157.48 in)
6000 mm (236.22 in)
7000 mm (275.59 in)
9000 mm (354.33 in)
10000 mm (393.70 in)
11000 mm (433.07 in)
12000 mm (472.44 in)
13000 mm (511.81 in)
14000 mm (551.18 in)
(170.08 in)
B
8000 mm (314.96 in)
5000 mm (196.85 in)
L_MF_011300_1_0010101_01_00
Vertical Stabilizer ContoursLevel Positions
1-13Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
AZ
BB
BB
BB
BB
BB
BB
BB
BB
BB
BB
BB
B
L_MF_011300_1_0020101_01_01
Vertical Stabilizer Contours
1-13Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-14 Horizontal Stabilizer Contours
**ON A/C A380-800 Models A380-800F Models
Horizontal Stabilizer Contours
1. GeneralThis section gives Horizontal Stabilizer contours.Horizontal stabilizer contours shown in this subject have been selected to assist in designing stands orequipment. These levels provide access to important maintenance areas such as servo controls,elevator hinges, trimmable horizontal stabilizer hinges, leading edge, trailing edge.The contours given are on the surface of body skin ; clearance space allowances will have to be madeas required.Ground clearance will depend on whether the airplane is on jacks or on wheels and in this case whatthe CG and weight conditions are.
1-14Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
X
(Z=0)
Z1
Z2
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
Y X
250098.433500
137.804500177.175500
216.546500
255.917500
295.288500
334.659500
374.0210500413.3911500
452.7612500492.1313500531.50
00
Z1 Z2 Z1 Z2 Z1 Z2 Z1 Z22671
105.142782
109.552894113.923003118.223108
122.373213
126.513319
130.653424
134.803529
138.943634
143.083739
147.223825
150.60
2671105.142782
109.552894113.923003118.223108
122.373213
126.513319
130.653424
134.803529
138.943634
143.083739
147.223825
150.60
75029.53
2957116.403030119.303107
122.333187
125.473281
129.163376
132.933472
136.693567
140.423661
144.143755
147.833848151.503923
154.45
222187.46229090.15250398.532635
103.752755
108.452872113.072989117.693107
122.323225
126.95
131.593460
136.233567
140.42
225088.58
2983117.433051120.113123
122.953199
125.963289
129.493380
133.083471
136.653561
140.183649
143.673737147.123823150.513891
153.20
211483.23223788.08240894.812546
100.252670105.112791
109.872912
114.643033119.423155
124.213277
129.003399133.813514
138.35
2970 2060116.923036119.533107
122.343184
125.343270
128.743357132.153442
135.523526
138.843609
142.083689
145.243767
148.293825
150.57
81.10220486.78236292.98250398.552630
103.552755
108.452879113.363005118.303131
123.263257
128.243385
133.263511
138.23
in
in
in
in
in
in
in
in
in
in
in
in
150059.06
3342
L_MF_011400_1_0010101_01_00
Horizontal Stabilizer ContoursHorizontal Stabilizer Contours (Sheet 1)
1-14Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
mm
Y X
250098.433500
137.804500177.175500
216.546500
255.917500
295.288500
334.659500
374.0210500413.3911500
452.7612500492.1313500531.50
3000 3750 4500 5250118.11 147.64 177.17 206.69
Z1 Z2 Z1 Z2 Z1 Z2 Z1 Z22931115.412998118.033071
120.903148
123.953230127.183312
130.383391
133.493468
136.523542
139.443613
142.263684
145.043743
147.35
203980.29219586.43234692.37249098.052621
103.202750
108.272880113.383010
118.523142
123.713275
128.933408134.193544
139.52
2875113.182943115.863016
118.763093121.793170
124.813245
127.743318
130.613390
133.473464
136.403539
139.343614
142.283676
144.74
204680.55221387.14235792.80250498.592640
103.922774
109.202909114.523045119.873181
125.233317
130.593452
135.893588141.28
2807110.512876113.212948116.063022118.983097121.913172
124.893249
127.903326
130.933402
133.953477136.913550
139.76− − −− − − − − − − − − − − −
− − − − − − − − −− − −− − −− − −− − −− − −
− − −− − −− − −
207781.79226489.12239294.172541
100.062681
105.552819
110.982957116.423095121.843231
127.213366
132.523499
137.74
2735107.682805110.432880113.372957116.423035119.503114
122.603192
125.683269
128.703343131.63
213083.84236493.07244596.262595102.152735
107.702874113.163012
118.593149
123.973284
129.29
X
(Z=0)
Z1
Z2
in
in
in
in
in
in
in
in
in
in
in
in
in
L_MF_011400_1_0020101_01_00
Horizontal Stabilizer ContoursHorizontal Stabilizer Contours (Sheet 2)
1-14Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
L_MF_011400_0_AAM0_01_00
Y10500
Y11500
Y12500
Y13500
Y0
Y2500
Y3500
Y4500
Y5500
Y6500
Y7500
Y8500
Y9500
L_MF_011400_1_0030101_01_00
Horizontal Stabilizer ContoursLevel Positions
1-14Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-15 Tail Contours
**ON A/C A380-800 Models A380-800F Models
Tail Contours
1. General
This section gives Tail contours.Tail contours shown in this section have been selected to assist in designing stands or equipment.The levels provide access to maintenance areas such as APU, aft passenger/crew doors.The contours given are on the surface of body skin ; clearance allowances will have to be made asrequired.Ground clearances will depend on whether the airplane is on jacks or on wheels in this last case whatthe C.G and weight conditions are.
1-15Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
FR95/STA62865
FR96/STA63500
FR97/STA64135
FR98/STA64770
FR99/STA65405
FR100/STA66040
FR101/STA66675
FR102/STA67310
FR103/STA67945
FR104/STA68580
FR105/STA69260
FR106/STA69940
FR107/STA70620
FR108/STA71300
FR109/STA71810
FR110/STA72320FR111/STA72354FR112/STA72922
FR114/STA74002
FR117/STA75622
FR120/STA77204.5
FR119/STA76677
FR118/STA76149.5
FR116/STA75132
FR115/STA74592
FR113/STA73462
L_MF_011500_1_0010101_01_00
Tail Contours
1-15Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Y=
0.0
1155.4 mm
2233.2 mm
2899.2 mm
3423.9 mm
3873 mm
4268.5 mm
4614.6 mm
4923.7 mm
5203.7 mm
5459.3 mm
STA72320/FR110
STA71810/FR109
STA71300/FR108
(114.141 in)
(134.799 in)
(152.480 in)
(168.051 in)
(181.677 in)
(193.846 in)
(204.870 in)
(214.933 in)
(45.488 in)
(87.921 in)
STA70620/FR107
STA69640/FR106
STA69260/FR105
STA68580/FR104
STA67945/FR103
STA67310/FR102
STA66675/FR101
STA66040/FR100
STA65450/FR99
STA64770/FR98
STA64135/FR97
STA63500/FR96
STA62865/FR95
3164.3 mm
3371.2 mm
3521.1 mm
3557.9 mm
3625.8 mm
3732.1 mm
3877.5 mm
4048.4 mm
4252.6 mm
4489.7 mm
4758.7 mm
5057.2 mm
5375.4 mm
5687.9 mm
5974.2 mm
6170.8 mm
(124.578 in)
(132.724 in)
(138.625 in)
(140.074 in)
(142.748 in)
(146.933 in)
(152.657 in)
(159.385 in)
(167.425 in)
(176.759 in)
(187.350 in)
(199.102 in)
(211.629 in)
(223.933 in)
(235.204 in)
(242.944 in)
L_MF_011500_1_0020101_01_00
Tail ContoursLevel Positions
1-15Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-16 Wing Profile
**ON A/C A380-800 Models A380-800F Models
General
1. This section gives the Wing Profile.Positions and dimensions of the wing ribs, from the centerline of the aircraft are given in Figures 1and 2.Figure 2 also shows a typical aerofoil cross-section with dimensions for Y and Z.The selection of these rib positions along the wing is to give the aircraft operator the necessaryheights to make aircraft servicing stands, supports or trestles.The dimensions for the wing profiles (dimensions Y and Z) at each of the rib positions are given inpara. 2. to 9. All the dimensions for the profiles are taken from the local datum position (at the wingleading edge, with the slats retracted) and from the horizontal datum VZO.These dimensions (when plotted from datum VZO) give the shape of the aerofoil cross-section andfull slope of the wing from wingtip to wingroot.All the dimensions for the profiles are taken from the local datum position (at the wing leading edge,with the slats retracted) and from the horizontal datum VZO.
2. RIB 7Intersection of Front Spar and rib 7.Source of Local datum for rib 7.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in2746.23 108.12 -- 228.28 -- 8.99 03056.71 120.34 -- 295.96 -- 11.65 03367.68 132.59 -- 361.41 -- 14.23 03679.15 144.85 -- 424.45 -- 16.71 03991.12 157.13 -- 484.90 --19.09 04303.61 169.43 -- 542.68 -- 21.37 04616.57 181.75 -- 597.79 -- 23.54 04929.98 194.09 -- 650.33 -- 25.60 05243.77 206.45 -- 700.49 -- 27.58 05557.90 218.81 -- 748.55 -- 29.47 05872.30 231.19 -- 794.74 -- 31.29 06186.95 243.58 -- 839.27 -- 33.04 06501.81 255.98 -- 882.23 -- 34.73 06816.89 268.38 -- 923.59 -- 36.36 07132.19 280.79 -- 963.20 -- 37.92 07447.74 293.22 -- 1000.79 -- 39.40 07763.55 305.65 -- 1036.09 -- 40.79 08079.64 318.10 -- 1068.81 -- 42.08 08396.00 330.55 -- 1098.80 -- 43.26 0
1-16Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in8712.61 343.02 -- 1126.08 - 44.33 0
3. RIB 14Intersection of Front Spar and rib 14.Source of Local datum for rib 14.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in1357.81 53.46 974.01 38.35 01672.93 65.86 917.43 36.12 01988.25 78.28 861.91 33.93 02303.97 90.71 808.69 31.84 02620.15 103.16 758.35 29.86 02936.75 115.62 710.65 27.98 03253.66 128.1 665.07 26.18 03570.82 140.58 621.31 24.46 03888.24 153.08 579.46 22.81 04205.98 165.59 540.05 21.26 04524.09 178.11 503.88 19.84 04842.65 190.66 471.76 18.57 05161.63 203.21 444.34 17.49 05481.01 215.79 421.92 16.61 05800.70 228.37 404.52 15.93 06120.61 240.97 391.71 15.42 06440.66 253.57 382.90 15.07 06760.78 266.17 377.46 14.86 07080.94 278.78 374.54 14.75 07401.10 291.38 373.01 14.69 0
4. RIB 19Intersection of Front Spar and rib 19.Source of Local datum for rib 19.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in1208.34 47.57 1430.76 56.33 01490.67 58.69 1384.62 54.51 01773.38 69.82 1340.85 52.79 02056.60 80.97 1300.54 51.2 0
1-16Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in2340.38 92.14 1264.43 49.78 02624.70 103.33 1232.80 48.54 02909.48 114.55 1205.61 47.46 03194.63 125.77 1182.68 46.56 03480.08 137.01 1163.72 45.82 03765.74 148.26 1148.42 45.21 04051.57 159.51 1136.49 44.74 04337.51 170.77 1127.69 44.4 04623.53 182.03 1121.98 44.17 04909.59 193.29 1119.41 44.07 05195.66 204.55 1120.16 44.1 05481.71 215.82 1124.09 44.26 05767.72 227.08 1130.67 44.51 06053.68 238.33 1138.95 44.84 06339.62 249.59 1147.76 45.19 06625.58 260.85 1155.96 45.51 0
5. RIB 26Intersection of Front Spar and rib 26.Source of Local datum for rib 26.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in1078.37 42.46 1926.80 75.86 01342.52 52.86 1888.34 74.34 01607.23 63.28 1853.93 72.99 01872.47 73.72 1823.99 71.81 02138.20 84.18 1798.63 70.81 02404.32 94.66 1777.83 69.99 02670.76 105.15 1761.59 69.35 02937.44 115.65 1750.03 68.9 03204.29 126.15 1743.34 68.64 03471.22 136.66 1741.76 68.57 03738.13 147.17 1745.42 68.72 04004.91 157.67 1754.31 69.07 04803.74 189.12 1768.29 69.62 04271.48 168.17 1787.01 70.35 04537.75 178.65 1809.53 71.24 05069.53 199.59 1834.22 72.21 0
1-16Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in5335.34 210.05 1858.72 73.18 05601.37 220.53 1880.68 74.04 0
6. RIB 29Intersection of Front Spar and rib 29.Source of Local datum for rib 29.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in1023.63 40.3 2111.24 83.12 01317.16 51.86 2069.15 81.46 01611.41 63.44 2032.40 80.02 01906.44 75.06 2002.66 78.84 02202.15 86.7 1980.57 77.98 02498.30 98.36 1965.59 77.39 02794.70 110.03 1956.84 77.04 03091.22 121.7 1953.66 76.92 03387.74 133.38 1955.80 77.00 03684.18 145.05 1963.33 77.3 03980.43 156.71 1976.28 77.81 04276.40 168.36 1994.49 78.52 04572.05 180.00 2017.36 79.42 04867.48 191.63 2043.06 80.44 05162.95 203.27 2068.22 81.43 0
7. RIB 36Intersection of Front Spar and rib 36.Source of Local datum for rib 36.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in905.61 35.65 2510.61 98.84 01139.12 44.85 2479.20 97.61 01372.92 54.05 2450.08 96.46 01607.16 63.27 2424.69 95.46 01841.91 72.52 2404.70 94.67 02077.11 81.78 2390.91 94.13 02312.59 91.05 2383.03 93.82 02548.18 100.32 2380.19 93.71 0
1-16Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in2783.78 109.6 2381.50 93.76 03019.34 118.87 2386.46 93.96 03254.81 128.14 2394.74 94.28 03490.16 137.41 2405.81 94.72 03725.40 146.67 2418.94 95.23 03960.57 155.93 2433.33 95.8 04195.75 165.19 2447.71 96.37 0
8. RIB 42Intersection of Front Spar and rib 42.Source of Local datum for rib 42.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in799.38 31.47 2862.47 112.7 01076.17 42.37 2831.00 111.46 01353.12 53.27 2801.03 110.28 01630.57 64.2 2776.08 109.29 01908.64 75.14 2759.57 108.64 02187.13 86.11 2753.27 108.40 02465.66 97.07 2756.86 108.54 02743.96 108.03 2769.03 109.02 03021.90 118.97 2787.73 109.75 03299.67 129.91 2808.93 110.59 0
9. RIB 48Intersection of Front Spar and rib 48.Source of Local datum for rib 48.
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in698.44 27.5 3158.68 124.36 0889.44 35.02 3139.88 123.62 01080.60 42.54 3122.74 122.94 01272.02 50.08 3109.03 122.4 01463.74 57.63 3100.28 122.06 01655.63 65.18 3097.23 121.94 01847.53 72.74 3099.73 122.04 02039.29 80.29 3107.32 122.34 0
1-16Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
SKIN PROFILE POINTS TO LOCAL DATUMX X Y Y Z
mm in mm in2230.84 87.83 3119.28 122.81 02422.17 95.36 3134.28 123.4 0
1-16Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
RIB7
RIB14
RIB19
RIB26
RIB29
RIB36
RIB42
RIB48
A
AL_MF_011600_1_0010101_01_00
Wing ProfileRib Locations
1-16Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
RIB
7R
IB14
RIB
19R
IB26
RIB
29R
IB36
RIB
42R
IB48
AIR
CR
AF
TC
EN
TE
R−
LIN
E
5582
.7(2
19.8
)10
631.
6(4
18.6
)14
424.
2(5
67)
1982
3.3
(780
.4)
2214
7.1
(872
)
2729
2.5
(107
4.5)
3207
6.2
(126
2.8)
3677
7.8
(144
7.9)
8203
.4(3
23)
1333
6(5
25)
1684
5.7
(663
.2)
2185
9.2
(860
.6)
2401
0.3
(945
.3)
2877
1.2
(113
2.7)
3319
9.5
(130
7)37
553.
2(1
478.
5)
DIM
EN
SIO
N F
RO
M A
IRC
RA
FT
CE
NT
ER
−LI
NE
TO
TH
E R
IB/R
EA
R S
PA
R IN
TE
RS
EC
TIO
ND
IME
NS
ION
S IN
mm
(in
IN B
RA
CK
ET
S)
DIM
EN
SIO
N F
RO
M A
IRC
RA
FT
CE
NT
ER
−LI
NE
TO
TH
E R
IB/F
RO
NT
SP
AR
INT
ER
SE
CT
ION
DIM
EN
SIO
NS
IN m
m (
in IN
BR
AC
KE
TS
)
L_MF_011600_1_0020101_01_00
Wing ProfileRib Positions
1-16Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
FRONTSPAR
REARSPAR
VZO
VIEW ON LOCAL DATUMRIB 7
y
z zz
LOCAL DATUMSOURCE
Z
VIEW ON LOCAL DATUMRIBS 14, 19, 29, 36, 42 AND 48
LOCAL DATUMSOURCE
Z
FRONTSPAR REAR
SPAR
VZO
y
z z z
L_MF_011600_1_0030101_01_00
Wing Profile
1-16Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
1-17 Nacelle Contours
**ON A/C A380-800 Models A380-800F Models
Nacelle Contours
1. General
Nacelle contours shown in this section have been selected to assist in designing stands or equipment.These levels provide access to important maintenance areas.The contours given are on the surface of body skin ; clearance space allowances will have to be madeas required.Ground clearances will depend on whether the airplane is on jacks or on wheels and in this case whatthe CG and weight conditions are.
1-17Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Z=1906,53
Z=−1989,67
Y=−1936,62Y=1936,62
X=−165 X=3640,5 (TOP)
DISTANCE FROM THE NOSE
INBOARDENGINE
22.228 m(72.92 ft)
DISTANCE FROMTHE NOSE
Y=0
Z=0
29.943 m(98.23 ft)
FWD
OUTBOARDENGINE
A
X=167,95 X=1466,67 X=3642 (BOTT) X=6501,83X=8221,27
X=6028,9
X=6873,20
X=6769,73
PLUG
PRIMARY NUZZLE
THRUST REVERSER
FAN COWL
NOSE COWL
AL_MF_011700_1_0010102_01_00
Nacelle ContoursNacelle Contours - TRENT 900 Engines
1-17Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
X=175.62X=1341.77 X=3519.98 X=6036.19
X=6364.77X=6960.47
X=8134.4
PLUG
PRIMARY NOZZLE
THRUST REVERSERFAN COWL
NOSE COWL
X=−157.69
X=0
IVGOVG
X=3443.44 X=3595.64
A
X=6996.85
Z=0
Y=0
Y=1938.18
Z=1889.531
Z=1989.64
Y=1938.18
AL_MF_011700_1_0020101_01_00
Nacelle ContoursNacelle Contours - GP 7200 Engines
1-17Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
TERMINAL AND RAMP
2-1 Airplane Servicing Arrangement
**ON A/C A380-800 Models A380-800F Models
Airplane Servicing Arrangement
1. General
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 2-2.
2-1Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020100_1_0010102_01_00
Typical Ramp Layout -- Two BridgesServicing Via Main and Upper Decks
2-1Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020100_1_0020102_01_00
Typical Ramp Layout -- Two BridgesServicing Via Main Deck
2-1Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020100_1_0030102_01_00
Opportunities of Direct Upper Deck Accessfor Airport and Airlines
2-1Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FUEL
FUEL
G.P
.UG
.P.U
TOW
PL
PL
CO
NV
EY
OR
WV
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
L_MF_020100_1_0040102_01_00
Typical Ramp Layout
2-1Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-2 Turnaround Stations
**ON A/C A380-800 Models A380-800F Models
Turnaround Stations
1. General
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 2-1.
2. Assumed Turn-Round Time Parameters For A380-800
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 :- dedicated door-galley = 1.5 min/FSTE- cart circulation (1 seat zone) = + 0.5 min/FSTE- cart circulation (> 1 seat zone) = + 1.0 min/FSTE- via lift :dedicated door to single lift = 2.0 min/FSTE
F. GROUND HANDLING/SERVICING- start of operations :
2-2Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
- bridges = t0 = 0others = 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
3. 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.
2-2Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020200_1_0010102_01_00
Baseline Turn-Round Time -- Two BridgesServicing Via Main and Upper Decks
2-2Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020200_1_0020102_01_00
Typical Turn-Round Time -- Two BridgesServicing Via Main Deck
2-2Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-3 Ground Service Connections and Locations
**ON A/C A380-800 Models A380-800F Models
Ground Service Connections and Locations
1. General
This section gives the ground service connections and locations.
2-3Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
15
15
15 − POTABLE WATER DRAIN PANEL
L_MF_020300_1_0010102_01_00
Ground Service Connections LayoutA380-800 Models
2-3Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
1
3
4
3
4
L_MF_020300_1_0020102_01_00
Ground Service Connections LayoutA380-800F Models
2-3Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Hydraulic System
1. Doors Location
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDGreen hydraulic groundconnectors :(Access door 469FL)
34.67 (113.7) 14.90 (48.88) 5.08(16.67)
Yellow hydraulic groundconnector :(Access door 479FL)
34.67 (113.7) 14.90 (48.88) 5.08 (16.67)
Hydraulic Reservoir ServicingPanel :(Access door 197CB)
31.89 (104.63) 2.34 (7.68) 1.71 (5.61)
A. Reservoir pressurization- one connector ETRTO V0.09.6, 1/4 in.
B. Reservoir filling- One connector AE96993E, 1/4 in.
2-3Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
B
RESERVOIRPRESSURIZATION
CONNECTOR
RESERVOIR FILLINGCONNECTOR
Z190
A
B
L_MF_020300_1_0270101_01_00
Ground Service ConnectionsHydraulic Reservoir Servicing Panel
2-3Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0300101_01_00
Ground Service ConnectionsHydraulic Ground Connections
2-3Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Electrical System
1. Electrical System for A380-800 Models.
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDRight side access door :134AR
5.99 (19.65) 0.45 (1.48) 2.59 (8.49)
Left side access door : 133AL 5.99 (19.65) 0.45 (1.48) 2.59 (8.49)
A. External Power Receptacles :- Four standard ISO R461 receptacles - 90 KVA each.
B. Power supply :- Three phase, 115V, 400 Hz.
C. Electrical connectors for servicing :- AC outlets : HUBBEL 5258- DC outlets : HUBBEL 7472- Vacuum cleaner outlets : HUBBEL 5258
2. Electrical System for A380-800F Models.
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUNDAccess door : TBD 5.99 (19.65) 0.45 (1.48) 2.59 (8.49)
A. External Power Receptacles :- Two standard ISO R461 receptacles - 90 KVA each.
B. Power supply :- Three phase, 115V, 400 Hz.
C. Electrical connectors for servicing :- AC outlets : HUBBEL 5258- DC outlets : HUBBEL 7472
2-3Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
A
B
A
B
EXTERNAL POWER RECEPTABLES
EXTERNAL POWER RECEPTABLES
L_MF_020300_1_0280101_01_00
Ground Service ConnectionsElectrical Service Panel - A380-800 Models
2-3Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
A
EXTERNAL POWER RECEPTABLES
A
L_MF_020300_1_0290101_01_00
Ground Service ConnectionsElectrical Service Panel - A380-800F Models
2-3Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Fuel System
1. Ground Service Panel
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROM
GROUND
Refuel/Defuel control panel: (Access door 199KB)
41.55 (136.31) 0.68 (2.23) 1.98 (6.50)
2. Refuel/Defuel connectors
Refuel/defuel coupling, left(Access door 522GB)
31.89 (104.63) 17.97 (58.96)MAX 5.94(19.49)
Refuel/defuel coupling,right (Access door 622GB)
31.89 (104.63) 17.97 (58.96)MAX 5.94(19.49)
A. Refuel/Defuel couplings :- Standard ISO R45, 2.5 in., two per wing
B. Refuel pressure :- Max. pressure : 3.45 bar (50 psi)
2-3Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0310101_01_00
Ground Service ConnectionsRefuel/Defuel Control Panel
2-3Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0320101_01_00
Ground Service ConnectionsPressure Refuel Connectors
2-3Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Pneumatic System
1. Low Pressure Air Connectors for Preconditioned Air :
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF NOSER SIDE L SIDE
MEAN HEIGHTFROM GROUND
Access doors 191GB, 21.85 (71.69) 1.24 (4.07) 2.08 (6.82)
Access doors 191JB 22.36 (73.36) 1.76 (5.77) 2.08 (6.82)
Access doors 192HB 21.85 (71.69) 1.24 (4.07) 2.08 (6.82)
Access doors 192KB 22.36 (73.36) 1.76 (5.77) 2.08 (6.82)
A. Connectors :- Four standard MS33562 (ISO1034), 8 in.
2. High Pressure Air Connectors for Cabin Heating, Cooling and Engine Starting :
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF NOSE
R SIDE L SIDE
MEAN HEIGHTFROM GROUND
Access doors 193BB 25.37 (83.23) 0.2 (0.66) 1.78 (5.84)
A. Connectors :- three standard MS33740 (ISO2026), 3 in.
2-3Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
LOW PRESSURE AIR CONNECTOR
Z190
BB
B
BA
A
B
L_MF_020300_1_0330101_01_00
Ground Service ConnectionsLow Pressure Preconditioned Air
2-3Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
HIGH PRESSURE AIR CONNECTORS
Z190
BA
A
B
L_MF_020300_1_0340101_01_00
Ground Service ConnectionsHigh Pressure Preconditioned Air
2-3Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Potable Water System
1. Potable Water Ground Service Panel for A380-800 Models:
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
Potable water groundservice panel (access door199NB)
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 :- Fill/Drain Nipple, 3/4 in.
B. Capacity :- Standard configuration - six tanks : 1700 l (449 USgal)- Optional : 2266 l (598 USgal)
C. Filling pressure :- Max Filling Pressure: 8.6 bar (125 psi)
2. Potable Water Ground Service Panel for A380-800F Models :
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
Access door TBD 5.99 (19.65) 0.45 (1.48) 2.59 (8.49)
A. Connectors :- Fill/Drain Nipple, 3/4 in.
B. Capacity :- Standard configuration - one tank : 80 l (21 USgal)- Option available for reservoir of 160 l (42 USgal)
C. Filling pressure :- Max Filling Pressure: 8.6 bar (125 psi)
2-3Page 16
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0350101_01_00
Ground Service ConnectionsPotable Water Ground Service Panel - A380-800 Models
2-3Page 17
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
SWITCH FOR PANEL CLOSING FILL/DRAIN NIPPLE TANK FULL INDICATOR
OVERFLOW NIPPLEHANDLE
C
O
A
A
L_MF_020300_1_0360101_01_00
Ground Service ConnectionsPotable Water Ground Service Panel - A380-800F Models
2-3Page 18
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
ACCESS DOOR
DRAIN NIPPLE
FWD CARGOFWD CARGOCOMPARTMENTDOOR
DRAIN VALVECONTROL HANDLE
Z130A
B
B
A
FR23
FR24
FR23
FR24
L_MF_020300_1_0370101_01_00
Ground Service ConnectionsPotable Water Drain Panel
2-3Page 19
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Engine Oil Servicing
1. Engine Oil Servicing (TRENT 900 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
Engine 1 (access door416BR)
32.65 (107.12) 23.58 (77.36) 4.24 (13.91)
Engine 2 (access door426BR)
24.98 (81.96) 12.74 (41.79) 3.83 (12.56)
Engine 3 (access door436BR)
24.98 (81.96) 16.61 (54.49) 3.83 (12.56)
Engine 4 (access door446BR)
32.65 (107.12) 27.45 (90.05) 4.24 (13.91)
2. Engine Oil Servicing (GP 7200 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
Engine 1 (access door415CL)
33.03 (108.37) 27.42 (89.96) 4.4 (14.44)
Engine 2 (access door425CL)
25.35 (83.17) 16.62 (54.53) 3.13 (10.27)
Engine 3 (access door435CL)
25.35 (83.17) 12.78 (41.93) 3.13 (10.27)
Engine 4 (access door445CL)
33.03 (108.37) 23.62 (77.49) 4.4 (14.44)
2-3Page 20
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
OIL TANK
OIL FILLER CAP
OIL LEVELSIGHT GLASS
A
L_MF_020300_1_0380101_01_00
Ground Service ConnectionsEngine Oil Servicing - TRENT 900 Engines
2-3Page 21
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0390101_01_01
Ground Service ConnectionsEngine Oil Servicing - GP 7200 Engines
2-3Page 22
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
VFG Oil Servicing
1. VFG oil servicing (TRENT 900 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
Engine 1 (access door415CL)
33.17 (108.83) 26.14 (85.76) 2.56 (8.39)
Engine 2 (access door425CL)
25.57 (83.89) 15.31 (50.22) 1.33 (4.36)
Engine 3 (access door435CL)
25.57 (83.89) 13.93 (45.70) 1.33 (4.36)
Engine 4 (access door445CL)
33.17 (108.83) 24.90 (81.69) 2.56 (8.39)
2. VFG oil servicing (GP 7200 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
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 (GP 7200 Engines), open:- Fan Exhaust Cowl (engine 1 - 4)- Thrust Reverser Cowl (engine 2 -3)
2-3Page 23
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0400101_01_01
Ground Service ConnectionsVFG Oil Servicing - TRENT 900 Engines
2-3Page 24
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0420101_01_01
Ground Service ConnectionsVFG Oil Servicing - GP 7200 Engines
2-3Page 25
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Starter Oil Servicing
1. Starter Oil Servicing (TRENT 900 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
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 (GP 7200 Engines)
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
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
2-3Page 26
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
OIL FILL PLUG
OILSIGHTGLASS
A
L_MF_020300_1_0430101_01_00
Ground Service ConnectionsStarter Oil Servicing - TRENT 900 Engines
2-3Page 27
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0440101_01_01
Ground Service ConnectionsStarter Oil Servicing - GP 7200 Engines
2-3Page 28
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
MEANHEIGHTFROMGROUND
Access door 315BL 67.55 (217.36) 0.44 (1.44) 6.83 (22.40)
A. Capacity:- 18.13L (4.85 US gal)
2-3Page 29
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0450101_01_00
Ground Service ConnectionsAPU Oil Servicing
2-3Page 30
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Vacuum Toilet System
1. Vacuum Toilet System For A380-800 Models
DISTANCE : Meters (ft)
FROM AIRPLANE CENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
Access door 171AL 53.31 (174.90) 0.26 (0.85) 3.40 (11.15)
A. Connectors :- Flushing and filling : 1 in.- 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
2. Vacuum Toilet System For A380-800F Models
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINEAFT OF NOSER SIDE L SIDE
MEAN HEIGHTFROM GROUND
Access door TBD 11.11 (36.45) 2.48 (8.14) 3.51 (11.52)
A. Connectors :- Flushing and filling : 1 in.- Draining : 4 in.
B. Capacity : 80l
C. Operating pressure for the waste tank rinsing process: 50 psi (max 125 psi)
D. Flow rate : 40 l/min
2-3Page 31
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020300_1_0460101_01_00
Ground Service ConnectionsVacuum Toilet System - A380-800 Models
2-3Page 32
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
Z130 A
FR22
FR38
CONTROL LEVERWASTE DRAIN
FILL AND RINSE
CONNECTION
CONNECTION
B
B
A
FWD
L_MF_020300_1_0470101_01_00
Ground Service ConnectionsVacuum Toilet System - A380-800F Models
2-3Page 33
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Oxygen System
1. Door Location
DISTANCE : Meters (ft)
FROM AIRPLANECENTERLINE
AFT OF NOSER SIDE L SIDE
MEANHEIGHTFROMGROUND
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
2-3Page 34
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
AL_MF_020300_1_0480101_01_00
Ground Service ConnectionsOxygen System
2-3Page 35
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-4 Interior Arrangements
**ON A/C A380-800 Models A380-800F Models
Interior Arrangements
1. General
This section gives standard interior arrangements.
2-4Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020400_1_0010102_01_00
Interior Arrangements - Plan ViewStandard Configuration - Upper Deck
2-4Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020400_1_0020102_01_00
Interior Arrangements - Plan ViewStandard Configuration - Main Deck
2-4Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020400_1_0030102_01_00
Interior Arrangements - Plan ViewStandard Configuration - Cargo Compartments
2-4Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020400_1_0040102_01_00
Interior Arrangements - Cross-sectionTypical Configuration - Upper Deck
2-4Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020400_1_0050102_01_00
Interior Arrangements - Cross-sectionTypical Configuration - Main Deck
2-4Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
UPPER DECKCARGO COMPARTMENT
MAIN DECKCARGO COMPARTMENT
LOWER DECKCARGO COMPARTMENT
UPPER DECKCOURIER AREA
L_MF_020400_1_0060102_01_00
Interior Arrangements - Cross-sectionTypical Configuration
2-4Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-5 Escape Slides
**ON A/C A380-800 Models
Escape Slides
1. General
This section gives location of cabin escape facilities and related clearances.
2. Location
A. A380-800 ModelsEscape facilities are provided at the following locations :
(1) Upper deck evacuation :- one slide-raft at each passenger/crew door (total six)
(2) Main deck evacuation :- one slide-raft at each passenger/crew door (total eight)- one slide for each emergency exit door (total two). The slides are housed in the belly
fairing for off-the-wing evacuation.
2-5Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
OFFWING SLIDE
MAIN DECK SLIDE
UPPER DECK SLIDE
MAIN DECK SLIDE
UPPER DECK SLIDEMAIN DECK SLIDE
MAIN DECK SLIDE
UPPER DECKSLIDE
L_MF_020500_1_0010101_01_00
Escape Slides/RaftsLocation
2-5Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
0
3
EMERGENCY EVACUATION
GRID EQUALS 1m IN REALITY
6
9
12
15
18
21
24
27
30
33
36
39
L_MF_020500_1_0020101_01_00
Escape Slides/RaftsDimensions
2-5Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-6 Galley
**ON A/C A380-800 Models
Galley
1. General
This section gives information on Galleys Location and General Layout.
2-6Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
MA
IN D
EC
K
UP
PE
R D
EC
K
FLEXIBLE INSTALLATION ZONES FOR TRANSVERSAL GALLEYS
MA
XF
LEX
AR
EA
LAT
ER
AL
MA
XF
LEX
AR
EA
LAT
ER
AL
MA
XF
LEX
AR
EA
CE
NT
ER
MA
XF
LEX
AR
EA
CE
NT
ER
L_MF_020600_1_0010101_01_00
General Location of Transversal Galleys
2-6Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
TRANSVERSAL GALLEY MODULE
L_MF_020600_1_0020101_01_00
General LayoutTransversal Galley (Sheet 1)
2-6Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
TRANSVERSAL GALLEY MODULE
L_MF_020600_1_0030101_01_00
General LayoutTransversal Galley (Sheet 2)
2-6Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
MA
IN D
EC
K
UP
PE
R D
EC
K
FLEXIBLE INSTALLATION ZONES FOR LONGITUDINAL GALLEYS
MA
XFL
EX
AR
EA
LAT
ER
AL
MA
XFL
EX
AR
EA
LAT
ER
AL
MA
XFL
EX
AR
EA
CE
NT
ER
MA
XFL
EX
AR
EA
CE
NT
ER
L_MF_020600_1_0040101_01_00
General LocationLongitudinal Galleys
2-6Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
LONGITUDINAL GALLEY MODULE
L_MF_020600_1_0050101_01_00
General LayoutLongitudinal Galleys (Sheet 1)
2-6Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
LONGITUDINAL GALLEY MODULE
L_MF_020600_1_0060101_01_00
General LayoutLongitudinal Galleys (Sheet 2)
2-6Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-7 Cargo
**ON A/C A380-800 Models A380-800F Models
Cargo
1. General
This section gives information related to cargo compartment location/dimensions and loading.
NOTE : For cargo door clearances, refer to Section 1-10.
A. Arrangements
(1) A380-800 ModelsThere are three cargo compartments (forward, aft and bulk), all located on the lower deck.
(2) A380-800F ModelsThere are five cargo compartments as follows :- three lower deck cargo compartments (forward, aft and bulk),- one main deck cargo compartment,- one upper deck cargo compartment.
B. Loading/UnloadingAll the cargo compartments can be used independently within the overall weight andperformance limitations of the aircraft.All the cargo compartments (except the lower deck bulk cargo compartment) are equipped forsemi-automatic power assisted cargo handling.
(1) Lower deck forward and aft cargo compartments (A380-800/800F Models)These compartments can accommodate the following Unit Load Devices (ULDs) :- Half-size containers,- Full-size containers,- 60.4 in x 61.5 in pallets,- 60.4 in x 125 in pallets,- 88 in x 125 in pallets,- 96 in x 125 in pallets.
(2) Lower deck bulk cargo compartment (A380-800/800F Models)This compartment can accommodate bulk cargo and/or be used for the transportation oflive animals (as limited by the compartment’s characteristics and conditions).The usable volume is approximately 18.4 m3 (650 ft3) for the A380-800F model, and 14.3m3 (505 ft3) for the A380-800 model.
(3) Main and upper deck cargo compartments (A380-800F Models)These compartments can accommodate the following Unit Load Devices (ULDs) :- 96 in x 125 in containers,- 96 in x 125 in pallets.
2-7Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020700_1_0010101_01_00
Cargo CompartmentsLocation and Dimensions - A380-800 Models
2-7Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020700_1_0020101_01_00
Cargo CompartmentsLocation and Dimensions - A380-800F Models (Sheet 1)
2-7Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
2.7 m(108 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_MF_020700_1_0030101_01_00
Cargo CompartmentsLocation and Dimensions - A380-800F Models (Sheet 2)
2-7Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
ST
AN
DA
RD
: 20
LD−
3 O
R 7
PA
LLA
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
LLA
TS
88
in /
96 in
X 1
25 in
OP
TIO
N: 6
PA
LLE
TS
88
in /
96 in
X 1
25 in
ST
AN
DA
RD
: 20
LD−
3 O
R 7
PA
LLA
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
LLA
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_MF_020700_1_0040101_01_00
Cargo CompartmentsLoading Combinations - A380-800 Models
2-7Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020700_1_0050101_01_00
Cargo CompartmentsLoading Combinations - A380-800F Models (Sheet 1)
2-7Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020700_1_0060101_01_00
Cargo CompartmentsLoading Combinations - A380-800F Models (Sheet 2)
2-7Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-8 Towing
**ON A/C A380-800 Models A380-800F Models
Towing
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).
2-8Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
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.)).
2-8Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
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
L_MF_020800_1_0010102_01_01
Ground Towing RequirementsGround Towing Requirements A380-800 Models
2-8Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020800_1_0020102_01_01
Ground Towing RequirementsTypical Tow Bar configuration 1
2-8Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020800_1_0030102_01_01
Ground Towing RequirementsTypical Tow Bar configuration 2
2-8Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
0.200 m(7.9 in)
A
0.555 m(21.85 in)
L_MF_020800_1_0040101_01_02
Ground Towing RequirementsNose Gear Towing Fittings
2-8Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020800_1_0050101_01_00
Ground Towing RequirementsMaximum Extension of the NLG Shock Absorber
2-8Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-9 Ground Maneuvering
**ON A/C A380-800 Models A380-800F Models
Ground Maneuvering
1. General
This section provides information on 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 throughout the world. Variations from standard aircraft operatingpatterns may be necessary to satisfy physical constraints within the maneuvering area, such asadverse grades, limited area or high risk of jet blast damage. For these reasons, ground maneuveringrequirements should be coordinated with the using airlines prior to layout planning.
2-9Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
R4
R3
R5
R6
55°
60°
65°
SEE PAGE 3 FOR DIMENSIONS
29.83 m (97.9 ft)
70°
NOTE:
L_MF_020900_1_0010101_01_00
Turning RadiiTurning Radii (Sheet 1)
2-9Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
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.
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
THE TURN.
L_MF_020900_1_0020101_01_00
Turning RadiiTurning Radii (Sheet 2)
2-9Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
R4
R3
R5
Y
R6
(TU
RN
ING
WID
TH
)
NOTE: SEE PAGE 5 FOR DIMENSIONS
65°
29.83 m (97.9 ft)
L_MF_020900_1_0030101_01_01
CL
Minimum Turning Radii(Sheet 1)
2-9Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020900_1_0040101_01_00
Minimum Turning Radii(Sheet 2)
2-9Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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)
4.99 m (16.4 ft)
R 25.9 m (85 ft)
6.62 m (21.7 ft)
7 m (23 ft)
22.9 m (75 ft)
L_MF_020900_1_0050101_01_00
135˚ Turn - Runway to Taxiway135˚ Turn - Runway to Taxiway (Sheet 1)
2-9Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020900_1_0110101_01_00
135˚ Turn - Runway to Taxiway135˚ Turn - Runway to Taxiway (Sheet 2)
2-9Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
NOTE:
NLG PATH
COCKPIT TRACKPARALLEL TOGUIDELINE
TAXIWAYGUIDELINE
WLG PATH
FAA GROUP V JUDGEMENTAL OVERSTEER METHOD
45.7 m(150 ft)
4.94 m (16.2 ft)
R 45.7 m (150 ft)
R 25.9 m (85 ft)
9.21 m(30.2 ft)
22.9 m (75 ft)
7 m (23 ft)
L_MF_020900_1_0060101_01_00
90˚ Turn - Runway to Taxiway90˚ Turn - Runway to Taxiway (Sheet 1)
2-9Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020900_1_0130101_01_00
90˚ Turn - Runway to Taxiway90˚ Turn - Runway to Taxiway (Sheet 2)
2-9Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020900_1_0070101_01_00
180˚ Turn on a Runway
2-9Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
NOTE:
COCKPIT TRACKPARALLEL TOGUIDELINE
NLG PATH
TAXIWAYGUIDELINE
NOMINAL OFFSET
WLG PATH
FAA GROUP V JUDGEMENTAL OVERSTEER METHOD
22.9 m
(75 ft)
4.94 m
(16.2 ft)
8.85 m
(29 ft)
22.9 m
(75 ft)
R 25.9 m (85 ft)
R 45.7 m (150 ft)
7 m (23 ft)
L_MF_020900_1_0080101_01_00
90˚ Turn - Taxiway to Taxiway90˚ Turn - Taxiway to Taxiway (Sheet 1)
2-9Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020900_1_0140101_01_00
90˚ Turn - Taxiway to Taxiway90˚ Turn - Taxiway to Taxiway (Sheet 2)
2-9Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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)
R 45.7 m (150 ft)
R 25.9 m (85 ft)8.47 m(27.8 ft)
(23 ft)
4.99 m (16.4 ft)
22.9 m(75 ft)
7 m
L_MF_020900_1_0090101_01_00
135˚ Turn - Taxiway to Taxiway135˚ Turn - Taxiway to Taxiway (Sheet 1)
2-9Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_020900_1_0120101_01_00
135˚ Turn - Taxiway to Taxiway135˚ Turn - Taxiway to Taxiway (Sheet 2)
2-9Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
NOTE:
(360 ft)
109.7 m
6.1 m
(20 ft)
12.2 m
(40 ft)
6.1 m
(20 ft)
COORDINATE WITH USING AIRLINE FOR SPECIFIC PLANNED OPERATING PROCEDURE
L_MF_020900_1_0100101_01_00
Runway Holding Bay (Apron)
2-9Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-10 Airplane Parking
**ON A/C A380-800 Models A380-800F Models
Airplane Parking
1. General
This section gives information on Aircraft Parking.The following figures and charts show the rectangular space required for parking against the terminalbuilding :- Steering Geometry- Minimum Parking Space Requirements
2-10Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
PARKINGSTRAIGHT ENTRY PUSH BACK
PARKING45° ENTRY PUSH OUT
70.3
1 m
(23
0.7
ft)77
.07
m (
252.
9 ft)
80.81 m (265.1 ft)
94.64 m (310.5 ft)
L_MF_021000_1_0010101_01_00
Airplane ParkingSteering Geometry
2-10Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
0 10 20 30 40 50 60 70 80 90 100 110 120
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
DISTANCEOUT
FROM TERMINAL
DISTANCE ALONG TERMINAL (m)
DISTANCE ALONG TERMINAL (ft)
(m)(ft)
45° ENTRY PUSH OUT
STRAIGHT ENTRY PUSH BACK
10
L_MF_021000_1_0020101_01_00
Airplane ParkingSteering Geometry - Minimum Parking Space Requirements
2-10Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-11 Operating Conditions
**ON A/C A380-800 Models A380-800F Models
Operating Conditions
1. Jet Engine Exhaust Velocities and Temperatures
This 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 900The 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 140 ˚F (60˚C).
B. Data from Engine Alliance’s GP7200The estimated efflux data are presented at ISA+15 ˚C (30 ˚C), Sea Level Static with 20-knotheadwind. It also assumed ground plane and proximity effects.Velocity contours are presented at 35 MPH (15 m/s), 65 MPH (30 m/s) and 105 MPH (46m/s), while temperature contours are presented at 122 ˚F (50 ˚C), 212 ˚F (100 ˚C) and 392˚F (200 ˚C).Engine Alliance strongly recommends that jet blast studies using their contours include theeffect of a 20-knot headwind.
2. 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.
2-11Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
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.
2-11Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0010102_01_00
Engine Exhaust VelocitiesGround Idle Power - TRENT 900 Engines
2-11Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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)
NOTE:
L_MF_021100_1_0020102_01_01
Engine Exhaust VelocitiesGround Idle Power - GP 7200 Engines
2-11Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0030102_01_01
GROUND IDLE POWER
Engine Exhaust TemperaturesGround Idle Power -- TRENT 900 Engines
2-11Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0040102_01_01
Engine Exhaust TemperaturesGround Idle Power -- GP 7200 Engines
2-11Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0050102_01_00
Engine Exhaust VelocitiesBreakaway Power -- TRENT 900 Engines
2-11Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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:
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)
L_MF_021100_1_0060102_01_01
Engine Exhaust VelocitiesBreakaway Power -- GP 7200 Engines
2-11Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0070102_01_01
BREAKAWAY POWER(11% MAX TAKE−OFF THRUST)
Engine Exhaust TemperaturesBreakaway Power -- TRENT 900 Engines
2-11Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0080102_01_00
Engine Exhaust TemperatureBreakaway Power -- GP 7200 Engines
2-11Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0090102_01_00
Engine Exhaust VelocitiesMax. Take-Off Power -- TRENT 900 Engines
2-11Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
−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)
L_MF_021100_1_0100102_01_01
Engine Exhaust VelocitiesMax. Take-Off Power -- GP 7200 Engines
2-11Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0110102_01_01
MAX TAKE−OFF POWER
Engine Exhaust TemperaturesMax. Take-Off Power -- TRENT 900 Engines
2-11Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0120102_01_00
Engine Exhaust TemperaturesMax. Take-Off Power -- GP 7200 Engines
2-11Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0130102_01_00
APU Exhaust Velocities and TemperaturesMax. ECS Conditions
2-11Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0140102_01_00
APU Exhaust Velocities and TemperaturesMES Conditions
2-11Page 16
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
DESCRIPTION OF TEST CONDITIONS
THE ARC OF CIRCLE ( RADIUS = 60 m (196.85 ft)), WITH MICROPHONES 1.2 m (3.94 ft) HIGH,IS CENTERED ON THE POSITION OF THE NOISE REFERENCE POINT.A.P.U.: OFF ; E.C.S.: PACKS OFF.
− TEMPERATURE: 32° C (89.6° F)− RELATIVE HUMIDITY: 31 %− ATMOSPHERIC PRESSURE (QFE): 996 hPa (144.45 PSI)− WIND SPEED: NEGLIGIBLE− NO RAIN
L_MF_021100_1_0300101_01_01
MAX THRUST POSSIBLEON BRAKES
4 ENGINES RUNNING
GROUND IDLE4 ENGINES RUNNING
Airport and Community Noise DataTRENT 900 Engines
2-11Page 17
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0150102_01_01
DESCRIPTION OF TEST CONDITIONS
THE ARC OF CIRCLE (RADIUS = 60 m (196.85 ft)), WITH MICROPHONES 1.2 m (3.94 ft) HIGH,IS CENTERED ON THE POSITION OF THE NOISE REFERENCE POINT.A.P.U.: OFF ; E.C.S.: PACKS OFF.
− TEMPERATURE: 12° C (53.6° F)− RELATIVE HUMIDITY: 90 %− ATHMOSPHERIC PRESSURE (QFE): 1015 hPa (147.21 PSI)− WIND SPEED: NEGLIGIBLE− NO RAIN
Airport and Community Noise DataGP 7200 Engines
2-11Page 18
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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)
L_MF_021100_1_0160102_01_00
30TO 70 m (230 ft) AFT OF EXHAUST NOZZLES
Danger Areas of the EnginesGround Idle Power - TRENT 900 Engines
2-11Page 19
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0170102_01_01
Danger Areas of the EnginesGround Idle Power - GP7200 Engines
2-11Page 20
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0180102_01_00
Danger Areas of the EnginesMax Take-Off Power - TRENT 900 Engines
2-11Page 21
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0190102_01_01
Danger Areas of the EnginesMax. Take-Off Power - GP 7200 Engines
2-11Page 22
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0200102_01_00
Danger Areas of the EnginesBreakaway Power - TRENT 900 Engines
2-11Page 23
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021100_1_0210102_01_02
Danger Areas of the EnginesBreakaway Power - GP 7200 Engines
2-11Page 24
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
2-12 Airplane Mooring
**ON A/C A380-800 Models A380-800F Models
Airplane Mooring
1. General
This section provides information on airplane mooring.
2-12Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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_MF_021200_1_0010101_01_00
Airplane Mooring
2-12Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
LINE MAINTENANCE AND HANGAR
3-1 Airplane Maintenance Jacking
**ON A/C A380-800 Models A380-800F Models
Airplane Maintenance Jacking
1. Aircraft Jacking Points for Maintenance
A. General
(1) The A380 aircraft can be jacked :- at not more than the maximum permitted aircraft weight for jacking,- within the limits of the permissible wind speed when the aircraft is jacked outside a
closed environment.
B. Primary jacking Points
(1) The aircraft are provided with three primary jacking points :- one located under the forward fuselage,- two located under the wings (one under each wing).
(2) Three jack adapters (ground equipment) are used as intermediary parts between theaircraft jacking points and the jacks :- one male spherical jack adapter at the forward fuselage,- two female jack pad adapters at the wings (one at each wing).
C. Auxiliary stabilizing Point (Safety point)
(1) When the aircraft is on jacks, a safety stay is installed under the aft fuselage (Ref. Fig.Jacking point location) to prevent tail tipping caused by accidental displacement of theaircraft center of gravity.
(2) The safety point must not be used for lifting the aircraft.
(3) One male spherical stay adapter (ground equipment) is used as intermediary part betweenthe aircraft safety point and the stay.
2. Jacks and Safety Stay
A. Jacks Specifications
The Maximum Eligible Static Load (Ref. Fig. Jacking Point Location) given in graph are themaximum loads applicable on jack fittings.
(1) In fully retracted position (jack stroke at minimum), the height of the jacks is such thatthey may be placed beneath the airplane under the most adverse conditions, namely, tiresdeflated and chock absorbers depressurized and, in addition, with a sufficient clearancebetween the aircraft jacking point and the jack upper end.
3-1Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
(2) The jacks stroke enables the aircraft to be jacked up so that the Fuselage Datum Line(FDL) may be positioned up to 7300 mm (23.95 ft) from the ground to allow all requiredmaintenance procedure and in particular, the Landing Gear shock absorbersremoval/installation.
B. Safety stay
(1) The stay stroke enables the aircraft tail to be supported up to the Fuselage Datum Line(FDL) positioned at 7300 mm (23.95 ft) from the ground.
3-1Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
JACKINGPOINT
JACKINGPOINT
SAFETYSTAY
Y
JACKINGPOINT
X
7.33 m(24.04 ft)
X =
0
L_MF_030100_1_0010102_01_02
A
B
B’
C
NOTE: SAFETY STAY IS NOT USE FOR JACKING
SAFETY STAY
WING JACKINGPOINT
C
B’
B
FORWARD FUSELAGEJACKING POINT A
7.28 23.91 0
12.22
−12.22
0
0
40.10
−40.10
0
MAXIMUMLOAD ELIGIBLE
m ft daN
YX
m ft
35.23
35.23
59.34
115.58
115.58
194.70
34 011
157 480
157 480
4 500
Jacking Points Location
3-1Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
LN
AIRCRAFT ON WHEELS WITH STANDARD TIRES, MAX.JACKWEIGHT 333700kg (735683lb)
AIRCRAFT ON WHEELS, SHOCK ABSORBERS DEFLATED ANDTIRES FLAT
AIRCRAFT ON WHEELS, NOSE LANDING GEAR SHOCKABSORBERS DEFLATED AND TIRES FLAT
AIRCRAFT ON WHEELS, LEFT WING AND BODY LANDINGGEARS SHOCK ABORBERS DEFLATED AND TIRES FLAT (SAMEDATA FOR RIGHT SIDE CONDITIONS)
AIRCRAFT ON WHEELS, WING AND BODY LANDING GEARSSHOCK ABSORBERS DEFLATED AND TIRES FLAT
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 6350 mm (250 in) FOR LANDINGGEARS EXTENSION/RETRACTION
2472 mm97.32 in
2259 mm88.94 in
2296 mm90.39 in
2474 mm97.4 in
2391mm94.13 in
3673 mm144.61 in
5112 mm201.26 in
4788 mm188.5 in
5117 mm201.46 in
4523 mm178.07 in
4803 mm189.09 in
6158 mm242.44 in
4707 mm185.31 in
4462 mm175.67 in
5044 mm198.59 in
4257 mm167.6 in
4291 mm168.94 in
5830 mm229.53 in
(M left)
AIRCRAFT ON JACKS, FUSELAGE DATUM LINEPARALLEL TO GROUND AT 7200 mm (283.46 in) FOR LANDINGGEARS REMOVAL/INSTALLATION
L M N
4523 mm178.07 in
7008 mm275.9 in
6680 mm262.99 in
FUSELAGE DATUM LINE
M
L_MF_030100_1_0020102_01_01
Jacking Dimensions
3-1Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
FR20 RIB16 1
B
2
3
4
C
FR101
5
A
BA
B
CRIB16
L_MF_030100_1_0030102_01_00
Jacks and Safety Stay Adapter
3-1Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-2 Landing Gear Jacking for Wheel Change
**ON A/C A380-800 Models A380-800F Models
Landing Gear Jacking for Wheel Change
1. To replace a wheel or wheel brake assembly on any of the landing gears it is necessary to lift thelanding gear with a jack. The landing gear can be lifted by a pillar jack or with a cantilever jack.
A. Nose Landing Gear (NLG)The nose gear can be lifted with a pillar jack or a cantilever jack. The NLG has a dome shapedjacking adaptor at the base of the shock absorber strut. The adapter is 31.75 mm (1.25 in) indiameter.Important dimensions of the NLG when lifted are shown in Fig. 001.The reaction loads at the jacking positions for the A380-800 are shown in Figs. 004 to 009.
NOTE : The load at each jacking position is the load required to give a 25.5 mm (1 in)clearance between the ground and the tire.
B. Wing Landing Gear (WLG)An adapter at the front and rear of each bogie is fitted to make sure that the jack is locatedcorrectly. The adapter is 31.75 mm (1.25 in) in diameter. The wheels and brake units can bereplaced on the end of the bogie beam that is lifted.The forward and aft ends of the bogie can be lifted at the same time. When lifting both ends atthe same time the bogie beam must always be kept level to prevent damage.If a WLG has all four tires deflated or shredded, replace the wheel assemblies in this sequence :
(1) Replace the wheel assemblies on the aft axle.
(2) Replace the wheel assemblies on the forward axle.Important dimensions of the WLG when lifted are shown in Fig. 002.The reaction loads at the jacking position for the A380-800 are shown in Figs. 004 to 009.
NOTE : The load at each jacking position is the load required to give a 25.5 mm (1 in)clearance between the ground and the tire.
C. Body Landing Gear (BLG)An adapter at the front and at the rear of each bogie is fitted to make sure that the jack islocated correctly. The adapter is 31.75 mm (1.25 in) in diameter. Both wheels and brake unitscan be replaced on the end of the bogie beam that is lifted.For a center wheel change only, the forward and aft ends of the bogie can be lifted at the sametime. When lifting both ends at the same time the bogie beam must always be kept level toprevent damage.If a BLG has all six tires deflated or shredded, replace the wheel assemblies in this sequence :
(1) Replace the wheel assemblies on the aft axle.
(2) Replace the wheel assemblies on the center axle.
3-2Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
(3) Replace the wheel assemblies on the forward axle.Important dimensions of the WLG when lifted are shown in FIG. 003.The reaction loads at the jacking position for the A380-800 are shown in Figs. 004 to 009.
NOTE : The load at each jacking position is the load required to give a 25.5 mm (1 in)clearance between the ground and the tire.
3-2Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
DATA FOR 1270X455R22 TIRES
MRW = 562 000 kg (1 238 989 lb)MLW = 386 000 kg (850 984 lb)
VIEW LOOKING INBOARD LHS(LH WHEEL NOT SHOWN)
A
B
CONFIGURATION WEIGHT CG%
MRW 43
MRW 43
MLW−PAX
44
DIM. B
2 INFLATED TIRES 400 (15.75)
DIM. A
541 (21.3)
1 INFLATED TIRE 353 (13.9) 530 (20.87)
2 DEFLATED TIRES +50%RIM DAMAGE
29 134 (5.28) 519 (20.43)
2 DEFLATED TIRESNO RIM DAMAGE
2 DEFLATED TIRES +50%RIM DAMAGE
136 (5.35) 519 (20.43)
519 (20.43)29 164 (6.46)
N/A N/A
N/A N/A
MAXIMUM JACKINGHEIGHT TO CHANGEWHEELS
N/A 506 (19.92) N/A
168 (6.61)
137 (5.34)
166 (6.54) 519 (20.43)
519 (20.43)
519 (20.43)
2 DEFLATED TIRESNO RIM DAMAGE
MLW−PAX
MLW−PAX
MLW−PAX
NOTE: DIMENSIONS IN MILIMETERS (INCHES IN BRACKETS)
44
20 DEFLATED TIRES+50%RIM DAMAGE
20 DEFLATED TIRESNO RIM DAMAGE
N/A
L_MF_030200_1_0010101_01_00
Nose Landing Gear Jacking Point HeightsA380-800 Models
3-2Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
NOTE: DIMENSIONS IN MILIMETERS (INCHES IN BRACKETS)MRW = 562 000 kg (1 238 989 lb)MLW = 386 000 kg (850 984 lb)
A A
B
CONFIGURATION WEIGHT CG% DIM. A
FWD
DIM. A
AFT
DIM. B DIM. C
ALL 4 TIRES SERVICEABLE
MRW 43 347 (13.7) 347 (13.7) 750 (25.9) 364 (14.3)
1 FWD TIRE DEFLATED
MRW 43 264 (10.4) 353 (13.9) 718 (28.3) 364 (14.3)
1 AFT TIRE DEFLATED
MRW 43 353 (13.9 ) 264 (10.4) 718 (28.3) 364 (14.3)
2 DEFLATED FWD TIRES +50% RIM DAMAGE
MLW
− PAX
44 93 (3.7) 406 (16) 686 (27) 364 (14.3)
2 DEFLATED AFT TIRES +50% RIM DAMAGE
MLW
− PAX
44 406 (16) 93 (3.7) 686 (27) 364 (14.3)
+50% RIM DAMAGE
MLW
− PAX
44 93 (3.7) 93 (3.7) 686 (27) 364 (14.3)
FWD TIRE CHANGE MAX. GROWN TIRE
MRW 43 513 (20.2) 331 (13) 795 (31.3) 364 (14.3)
AFT TIRE CHANGE MAX. GROWN TIRE
MRW 43 331 (13) 513 (20.2) 795 (31.3) 364 (14.3)
20 FLAT TIRES+50% RIM DAMAGE
N/A N/A 83 (3.3) 83 (3.3) 686 (27) 364 (14.3)
DATA FOR 1400X530R23 TIRES
C
4 TIRES DEFLATED
L_MF_030200_1_0020101_01_00
Wing Landing Gear Jacking Point HeightsA380-800 Models
3-2Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
MLW = 386 000 kg (850 984 lb)
C
B
A A
NOTE: DIMENSIONS IN MILIMETERS (INCHES IN BRACKETS)MRW = 562 000 kg (1 238 989 lb)
CONFIGURATION WEIGHT CG%
MRW 43
MRW 43
DIM. A
DATA FOR 1400X530R23 TIRES
N/A N/A
DIM. A DIM. B DIM. C DIM. CFWD AFT FWD AFT
ALL 6 TIRESSERVICABLE
347 (13.7) 312 (12.3) 930 (36.6) 460 (18.1) 432 (17)
1 FWD TIREUNSERVICEABLE 295 (11.6) 328 (12.9) 898 (35.4) 460 (18.1) 432 (17)
MRW 43 898 (35.4) 460 (18.1) 432 (17)
460 (18.1) 432 (17)
MRW 43 460 (18.1) 432 (17)
MRW 43 460 (18.1) 432 (17)
43 898 (35.4) 460 (18.1) 432 (17)
MLW−PAX
460 (18.1) 432 (17)
MLW−PAX
460 (18.1) 432 (17)
MLW−PAX
460 (18.1) 432 (17)
43 460 (18.1) 432 (17)
1 CENTER TIREUNSERVICEABLE
MRW 334 (13.1) 299 (11.8)
1 AFT TIREUNSERVICEABLE
363 (14.3) 260 (10.2)
2 FWD TIRESDEFLATED +50%RIM DAMAGE
44 74 (2.9) 505 (19.9) 866 (34.1)
2 CENTER TIRESDEFLATED
44 358 (14.1) 323 (12.7) 866 (34.1)MLW−PAX
2 AFT TIRESDEFLATED +50%RIM DAMAGE
44 540 (21.1) 40 (1.6) 866 (34.1)
6 TIRES DEFLATED+50% RIMDAMAGE
44 74 (2.9) 39 (1.5) 866 (34.1)
FWD TIRE CHANGEMAX. GROWN TIRE
496 (19.5) 264 (10.4) 975 (38.4)
CTR TIRE CHANGEPOSITIONMAX. GROWN TIRE
MRW 496 (19.5) 461 (18.2) 975 (38.4)
AFT TIRE CHANGEMAX. GROWN TIRE
299 (11.8) 461 (18.2) 975 (38.4)
20 DEFLATEDTIRES +50% RIMDAMAGE
102 (4) 67 (2.6) 866 (34.1) 460 (18.1) 432 (17)
L_MF_030200_1_0030101_01_00
Body Landing Gear Jacking Point HeightsA380-800 Models
3-2Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_030200_1_0040101_01_01
10
15
20
25
30
35
40
45
50
55
60
260 300 340 380 420 460 500 540 580
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 k
g ]
22
32
42
52
62
72
82
92
102
112
122
132
(x1000 kg)
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 lb
]
AIRCRAFT GROSS WEIGHT
120011001000900800700600
(x1000 lb)
CG POSITION 29 % mac 33 % mac 37.5 % mac 41 % mac 43 % mac
Nose Landing Gear Jacking Point LoadsA380-800 Models
3-2Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_030200_1_0050101_01_01
10
15
20
25
30
35
40
45
50
55
60
65
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 k
g ]
22
32
42
52
62
72
82
92
102
112
122
132
142
1300120011001000900800700600
(x1000 kg)
(x1000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 lb
]
CG POSITION29 % mac33 % mac36 % mac40 % mac43 % mac
Nose Landing Gear Jacking Point LoadsA380-800F Models
3-2Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_030200_1_0060101_01_01
23
27
31
35
39
43
47
51
55
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 k
g ]
51
56
61
66
71
76
81
86
91
96
101
106
111
116
121
120011001000900800700600
(x1000 kg)
(x1000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 lb
]
CG POSITION 29 % mac 33 % mac 37.5 % mac 41 % mac 43 % mac
Wing Landing Gear Jacking Point LoadsA380-800 Models
3-2Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
22
26
30
34
38
42
46
50
54
58
260 290 320 350 380 410 440 470 500 530 560 590 620
AIRCRAFT GROSS WEIGHT
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 k
g ]
49
54
59
64
69
74
79
84
89
94
99
104
109
114
119
124
1300120011001000900800700600
(x1000 kg)
(x1000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 lb
]
29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
CG POSITION
L_MF_030200_1_0070101_01_01
Wing Landing Gear Jacking Point LoadsA380-800F Models
3-2Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
L_MF_030200_1_0080101_01_01
34
38
42
46
50
54
58
62
66
70
74
78
82
260 300 340 380 420 460 500 540 580
AIRCRAFT GROSS WEIGHT
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 k
g ]
75
85
95
105
115
125
135
145
155
165
175
120011001000900800700600
(x1000 kg)
(x1000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 lb
]
CG POSITION 29 % mac 33 % mac 37.5 % mac 41 % mac 43 % mac
Body Landing Gear Jacking Point LoadsA380-800 Models
3-2Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
L_MF_030200_1_0090101_01_01
AIRCRAFT GROSS WEIGHT
34
38
42
46
50
54
58
62
66
70
74
78
82
86
260 290 320 350 380 410 440 470 500 530 560 590 620
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 k
g ]
75
85
95
105
115
125
135
145
155
165
175
185
1300120011001000900800700600
(x1000 kg)
(x1000 lb)
LOA
D A
T J
AC
KIN
G P
OIN
T [
x 10
00 lb
]
CG POSITION 29 % mac 33 % mac 36 % mac 40 % mac 43 % mac
Body Landing Gear Jacking Point LoadsA380-800F Models
3-2Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-3 Leveling, Symmetry and Alignment
**ON A/C A380-800 Models A380-800F Models
Leveling, Symmetry and Alignment
1. Quick LevelingThere are three alternative procedures to level the aircraft:- Quick leveling procedure with Air Data / Inertial Reference System (ADIRS).- Quick leveling procedure with a spirit level in the upper or main deck passenger compartment.- Quick leveling procedure with a spirit level in the FWD cargo compartment.
2. Precise LevelingFor precise leveling, it is necessary to install sighting rods in the receptacles located under thefuselage (points 11 and 16 for longitudinal leveling) and under the wings (points 1R and 1L for lateralleveling) and use a sighting tube. With the aircraft on jacks, adjust the jacks until the referencemarks on the sighting rods are aligned in the sighting plane (aircraft level).
3. Symmetry and Alignment CheckPossible deformation of the aircraft is measured by photogrametry.
3-3Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
FR35
FR36
FR88
FR89
RIB6
RIB6
16
11
1L
1R
L_MF_030300_1_0010102_01_00
Location of Leveling Points
3-3Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-4 De-icing and Washing
**ON A/C A380-800 Models A380-800F Models
De-icing and Washing
1. De-Icing and Washing on GroundThe mobile equipment for aircraft de-icing and washing must be capable of reaching heights up toapproximately 25 meters (82 ft). For use on the ramp, it must have a de-icing liquid storage tankwith means for heating the liquid to the required temperature. Inside the hangar, the same mobileunit or fixed equipment may be used. Impingement pressure of the de-icing or washing liquid is about5 psi (0.35 bar) except for wing root fillet and various other fairings where it will be 1.5 psi (0.10bar).At major airports, a substantial saving in manpower and aircraft time can be achieved if a de-icing/washing hangar, especially one with a mechanized and automated facility, is provided for use byall airlines.
2. Wetted Area for the Complete Aircraft
A380m2 ft2
Fuselage 1490 16038
Belly fairing 384 4133
Wing (3) 1454 15651
Vertical Stabilizer 232 2497Horizontal Stabilizer 346 3724Nacelles and Pylons 390 4198
TOTAL 4296 46241
3. Liquid- Anti/De-Icing fluid type I - AMS 1424 (Material 10-001)- Anti/De-icing fluid type II - AMS 1428 (Material 10-003)- Anti/De-Icing fluid type IV - AMS 1428C (Material 10-004)
3-4Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-5 Air Conditioning
**ON A/C A380-800 Models A380-800F Models
Air Conditioning
1. Air conditioningThe air conditioning system controls the airflow in the cockpit, the two cabin decks and the lowerdeck cargo compartments. The air conditioning system keeps the air in the pressurized fuselagecompartments at the correct pressure, temperature and freshness.The bleed air system supplies compressed air to the air conditioning system from:- the main engine compressor,- the APU compressor,- three high pressure ground connectionsThe air conditioning system cools and conditions the hot compressed air. Then it sends the air to thefuselage compartments. From there, the hot air flows through ducts and goes overboard through avalve.Four low-pressure ground connections can also supply the conditioned air to the distribution system.In a double failure case during flight operations, two emergency ram air inlets open automatically andsupply the distribution system with air from outside.The conditioned air is supplied to the cabin and the cockpit. The cockpit and the cabin zones havean independent temperature control. The temperature of the cabin zones and the cockpit arenormally controlled to between 18˚C and 30˚C (65˚ and 86˚F). An automatic control keeps the airtemperature at the selected value in each cabin zone and in the cockpit.
2. PressurizationThe Cabin Pressure Control System (CPCS) controls the pressure in the fuselage during flight andground operations.The CPCS controls the rate of change of the cabin pressure and the cabin differential pressure.It gives the best possible comfort and safety for the passengers and the crew.The operation of the CPCS is fully automatic under all operating conditions.
3. Ventilation
A. Unpressurized Compartment Ventilation SystemThe function of the unpressurized compartments ventilation system is to supply air to theunpressurized compartments ventilation in the belly fairing.The unpressurized compartments have two main zones:- Zone A is in the forward belly fairing and includes the Air Generation Units (AGU) 1 and 2
and the hot air ducts.
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@A380MAINTENANCE FACILITY PLANNING
- Zone B is under the wing center box, in the belly fairing. The unpressurized compartmentsventilation system supplies a correct quantity of ventilation air on each zone (A and B), toremove heat from the AGUs and fuel vapors. It also keeps, on the ground or in flight, amean temperature of 80˚C in the unpressurized compartment with an external temperatureof 55˚C. This temperature is compatible with the structure constraints in the unpressurizedcompartments. The unpressurized compartments ventilation-system operates without aircraftelectrical power.
B. Avionics Equipment Ventilation SystemThe avionics equipment ventilation system supplies cooling to the components with airflowthrough the racks in the compartment. The supplemental cooling system supplies cooled air tothe compartment. An extraction fan moves the hot air to the under floor area and lateroverboard through the outflow valve.
4. AGU Dimensions
Length 1645.9 mm (64.8 in.)
Width 1818.6 mm (71.6 in.)
Height 1535.3 mm (60.5 in.)
Weight 403.3 kg (889.0 lb)
3-5Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
BU
LK
HE
AT
ER
AF
T C
AR
GO
BLE
ED
AIR
UP
PE
R D
EC
K (
SE
VE
N T
EM
P Z
ON
ES
)
MA
IN D
EC
K (
EIG
HT
TE
MP
ZO
NE
S)
WIN
GG
EA
R
LOC
AL
MIX
ING
UN
IT
2’’ L
P G
RO
UN
D
OZ
ON
CO
NV
ER
TE
RS
FLO
W C
ON
TR
OL
VA
LVE
ST
RIM
AIR
SY
ST
EM
2’’ L
P G
RO
UN
DC
ON
NE
CT
OR
EM
ER
GE
NC
YR
AM
AIR
CO
NN
EC
TO
R
EM
ER
GE
NC
YR
AM
AIR
FW
D C
AR
GO
OU
TF
LOW
VA
LVE
RE
CIR
CU
LAT
ION
FA
NS
TR
IM A
IRV
ALV
ES
VA
LVE
OU
TF
LOW
TR
IM A
IR S
YS
TE
M
0201
0202
0202
0101
0101
LOC
AL
MIX
ING
UN
IT
PR
E M
IXIN
G U
NIT LO
CA
L M
IXIN
GU
NIT
4
LOC
AL
MIX
ING
UN
IT
AIR
GE
NE
RA
TIO
NS
YS
TE
M
MIX
ER
UN
IT
L_MF_030500_1_0010102_01_00
Air ConditioningGeneral Layout
3-5Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
RH FANINLET PLENUM
LH PLENUM HEADER
CONDENSER
LH ACM
LH TURBINEBYPASS VALVE
RH TURBINE BYPASS VALVE
RH ACM
RH PLENUM HEADER
ACMISOLATION VALVE
A
A
LH DUALHEAT EXCHANGER
LH TEMPCONTROL VALVE
LH TEMPCONTROL VALVE
RH DUALHEAT EXCHANGER
AL_MF_030500_1_0020102_01_00
Air ConditioningAir Generation Unit (AGU)
3-5Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-6 Communications
**ON A/C A380-800 Models A380-800F Models
Communications
1. GeneralThe communications system has these functions:- Speech communication inside and outside the aircraft by the crew members- Data transmission with the ground stations- Radio and audio management- Audio and video monitoring and intercommunication.
For the protection of the communications system, static dischargers are installed on the aircraft.The A380-800 basic aircraft is equipped with:
A. Speech Communication
(1) High Frequency (HF) systemThe HF system is used for all long-distance voice and data
(2) Very High Frequency (VHF) systemThe VHF system is used for short-range voice and data communications.
B. Interphone
(1) Cockpit-to-ground crew call systemThe cockpit to ground crew call system enables cockpit crew-to-ground mechanic calls orground mechanic-to-cockpit crew calls.
(2) Service interphoneThis system provides a means of telephone communication on the ground between theflight crew and the ground service personnel.
C. Radio and Audio Management
(1) Audio IntegratingThe audio integrating system integrates and manages all audio signals supplied by and sentto the radio communication and radio navigation systems. Also, it has SELCAL and flightinterphone functions.
(2) Radio Frequencies and Satellite Channels TuningThrough this function, the frequencies of all radio communication equipment are controlledby the Radio and Audio Management Panel (RMP). The RMP also controls thefrequencies of radio navigation equipment as a back-up solution.
D. Static DischargingStatic dischargers protect the communications system from interference caused by staticelectricity.
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E. Audio and Video Monitoring and Intercommunication
(1) Cockpit Voice Recorder (CVR)The CVR records in-flight and on-ground conversations and communications in solid-statememories.
(2) External Video System (ETACS)The External and Taxiing Aid Camera System (ETACS) is an aid to the crew duringtaxiing of the aircraft.
3-6Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
SATCOM2−TOP
HF ANTENNA
HPA1−TOP TWLU
LEO−MEO
VHF−2
VHF−3VHF−1
SATCOM1−TOP
FR22FR38 FR74
FR95
14RJ13RJ
8RJ
AFT CARGO
AIR CONDITIONINGBAY
AFT AVIONICSCOMPARTMENT
LANDINGGEAR
FWD CARGOCOMPARTMENT
FWD AVIONICSCOMPARTMENT
EMERGENCYAVIONICS
COMPARTMENT
HYDRAULICSCOMPARTMENT
NOSE 7RJ
INTERPHONE JACKS
APUTHS ACTUATOR
BULK CARGODOOR
COMPARTMENT
10RJREFUEL PANEL
9RJ
6RJ5RJ
23RJ
2RJ
22RJ
24RJ
L_MF_030600_1_0010102_01_02
CommunicationsLocation of Antennas
3-6Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-7 Electrical Power
**ON A/C A380-800 Models A380-800F Models
Electrical Power
1. General
The electrical system generates and distributes electrical power to all the aircraft systems throughthese networks.A 115VAC normal network with variable frequency. Power is supplied to this network from :- Four Variable Frequency Generators (VFG) or,- Two auxiliary generators (APU generators) with constant frequency or,- Four external power units (through four external-power receptacles).A 28VDC normal network with the No Break Power Transfer (NBPT) function. Power is supplied tothis network from :- Two Transformer Rectifier Units (TRU)- One Transformer Rectifier (TR) 2- Two batteries (1 and 2).A 115VAC and 28VDC emergency network which is segregated from the normal network.Power is supplied to the AC emergency network from :- The normal AC network (if available) or,- An electrical Ram Air Turbine (RAT) with variable frequency or,- Battery 1 and the essential battery through the static inverter. Power is supplied to the DC
emergency network from :- The AC emergency network through the essential TRU or,- Battery 1 and the essential battery (during extension of the RAT and after landing in emergency
electrical configuration).An APU network, supplied by busbar 200XP4. This network has a TR, a battery and the relatedcontactors and protection devices. The APU network is used to start the APU.
2. AC Generation (Ref. Fig. 001)
A. Variable Frequency Generator (VFG)Each of the four engines drives its related VFG through the accessory gearbox.The VFG is an oil-cooled generator with a nominal 115V, 150KVA, three-phase, 370-770 Hzoutput.Each VFG has two pushbutton switches on ICP 1225VM (overhead panel), one for mechanicaldisconnection of the VFG, the other for electrical connection and disconnection of the VFG.The Generator and Ground Power Control Unit (CCPCU) 1(2,3,4) control and monitor the VFG1(2,3,4).
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@A380MAINTENANCE FACILITY PLANNING
B. APU GeneratorThe APU drives two APU generators at a constant frequency. The APU generator is an oil-cooled generator with a nominal output of 115V, 120KVA, three-phase, 400Hz. Each APUgenerator has a pushbutton switch on the overhead panel for electrical connection anddisconnection.
C. External powerThe external power supply is the AC power source used on the ground when the VFGs and theAPU generators are not available. Four external power receptacles are used to supply power tothe aircraft network.Each external power receptacle supplies 90KVA with a constant frequency of 400Hz.The GGPCU 1(2,3,4) controls and monitors the external power unit 1(2,3,4) that is connectedto the receptacles.
D. Electrical RATThe electrical RAT supplies electrical power if the main power source is unserviceable. It drivesan AC emergency generator at a variable frequency. The generator is an air-cooled generatorwith a nominal 115V, 70KVA, three-phase, 360-800 Hz output.The generator is mechanically connected to the RAT. A Generator Control Unit (GCU) controlsand monitors the RAT. The RAT extends automatically but it is possible to control the RATmanually by means of a pushbutton switch on the overhead panel.
E. Transfer circuitThe transfer circuit reconfigures the electrical network to keep the busbars supplied according tothe availability of the power sources. The primary main distribution reconfigures the network ifthere is connection and disconnection of the AC main power source.The transfer contactors close to obey the priority and segregation rules. If two VFGs of a sameside are not available (without external power supply or APU supply) :- The outer serviceable VFG supplies the busbar of the outer unserviceable VFG.- The inner serviceable generator supplies the busbar of the inner unserviceable VFG.
3. DC Generation (Ref. Fig. 001)
A. TRUsEach TRU has these functions :- It controls the charge of the batteries- It monitors the batteries to DC network.
B. TR 2TR 2 is used if TRU 2 is unserviceable. It has these functions :- It changes 115VAC into 28VDC.- It controls the charge of the batteries.- It monitors the batteries.
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@A380MAINTENANCE FACILITY PLANNING
C. APU TRThe APU TR is supplied by the APU DC busbar and is used to start the APU with or withoutthe battery.The APU TR :- Controls the charge of the batteries.- Monitors the batteries and the DC network.
D. BatteriesThe primary functions of the batteries are the NBPT function and the supply of the DCnetwork in some conditions.
4. AC and DC Distribution (Ref. Fig. 002)The electrical distribution system :- Connects and disconnects the power source.- Reconfigures the electrical network.- Gives maximum availability of the busbar.- Gives electrical protection to prevent paralleling and protection faults.- Prevents short circuits.
The distribution system has three sub-systems segregated on two electrical sides.- The primary main distribution- The secondary main distribution- The emergency distribution.
A. Primary main distributionThe components for the primary main distribution are in the PEPDC. The PEPDC supplies115VAC variable-frequency and 28VDC to all the electrical users of the aircraft. It alsoconfigures the electrical network architecture.
B. Secondary main distributionThe secondary main distribution is installed in the SEPDCs and in the SPDRs. It supplies115VAC variable frequency and 28VDC electrical power. The secondary main distributionincludes the AC and DC secondary technical -- system and commercial-system busbars andrelated protection devices. The SEPDCs and the SPDBs use the SSPC technology for AC andDC rating. The secondary main distribution has these items :- Two SEPDCs which include all the circuit breakers (SSPCs) that supply all the AC and DC
low-power loads.- Eight SPDBs which include all the circuit breakers (SSPCs) that supply the cabin and cargo
electrical system.
C. Emergency distributionThe emergency distribution is installed in the emergency power center. The emergency powercenter is segregated from the PEPDC. In normal electrical configuration, the AC emergencybusbar is supplied by busbar 100XP1 or 200XP4 (see primary main distribution). The DCessential busbars are supplied by the essential TRU. If the essential TRU is unserviceable, TRU1 supplies busbar 400PP.
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@A380MAINTENANCE FACILITY PLANNING
In emergency electrical configuration (power supplied from the RAT), the electrical RATgenerator supplies the emergency busbars 400XP and 491XP. Busbar 247XP (EHA busbar) issupplied if the hydraulic system is unserviceable (TEFO configuration). Essential TRU suppliesthe DC essential busbars. In emergency electrical configuration (power supplied from thebatteries), the batteries supply busbar 400PP and the static inverter supplies busbar 491XP.
3-7Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
BA
T 1
LC
709
PP
AP
UT
R
BA
T 1
ES
S B
AT
ELC
1
IBLC
1
ES
S B
CR
ULC
ES
SB
AT
LC
EH
AC
EH
AC
2
BA
T 2
LC
ES
SIB
LC
IBLC
2B
CR
ULC
BA
T 2
AP
U B
AT
BC
RU
2LC
TR
2LC
BT
C 6
BT
C 5
3XC
BT
C 2B
TC 1
BT
C 3B
TC 4
SIC
HO
T B
US
1 7
05 P
P
GE
N1
EX
T P
WR
RC
PT
1
GE
N2
EX
T P
WR
RC
PT
2
GE
N1
RA
TG
EN
AP
U
EX
T P
WR
RC
PT
3
EP
C 1G
LC 1E
PC 2
GLC 2
AP
UG
LC1
GLC 3
EP
C 3G
LC 4E
PC 4
AP
UG
LC2
AC
BU
S 1
−2
100X
P2
AC
BU
S 1
−1
100X
P1
AC
BU
S 2
−4
200X
P4
AC
BU
S 2
−3
200X
P3
EX
T P
WR
RC
PT
4
TR
U 1
DC
BU
S 1
100
PP
DC
ES
S B
US
400
PP
ES
S H
OT
BU
S 7
03 P
P
HO
T B
US
2 7
02 P
P
DC
EH
A24
7 P
P
DC
BU
S 2
200
PP
AP
US
TA
RT
ING
SY
ST
EM
AP
U S
TA
RT
ING
DC
BU
S
DC
BU
S 6
260P
P
TR
U2
TR 2
ST
AT
INV
ES
SB
CR
U
AC
ES
S 4
91 X
PA
C E
SS
SH
ED
400
XP
AC
EH
A24
7 X
P
GE
N2
AP
UG
EN
3G
EN
4
GG
PC
U3
GG
PC
U2
GG
PC
U5
GC
UG
GP
CU
6G
GP
CU
4G
GP
CU
1
L_MF_030700_1_0010102_01_01
Electrical PowerGeneral Schematic
3-7Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
PE
PD
C
CP
IOM
−E
1&2
AIR
CR
AF
T L
OA
DS
SE
PD
S
EM
ER
GE
NC
Y E
LEC
TR
ICA
LP
OW
ER
DIS
TR
IBU
TIO
NC
EN
TE
R(E
EP
DC
)
ELE
CT
RIC
AL
PO
WE
R G
EN
ER
AT
ION
SY
ST
EM
PE
PD
C: P
RIM
AR
Y E
LEC
TR
ICA
LP
OW
ER
DIS
TR
IBU
TIO
N C
EN
TE
RS
EP
DS
: SE
CO
ND
AR
Y E
LEC
TR
ICA
LP
OW
ER
DIS
TR
IBU
TIO
N S
YS
TE
MC
PIO
M−
E: C
OR
E P
RO
CE
SS
OR
INP
UT
OU
TP
UT
MO
DU
LE E
NE
RG
Y
ELE
CT
RIC
AL
LOA
DM
AN
AG
ME
NT
FU
NC
TIO
N(E
LMF
)
CIR
CU
IT B
RE
AK
ER
MO
NIT
OR
ING
FU
NC
TIO
N(C
BM
F)
ES
SE
NT
IAL
LOA
DH
IGH
T A
CP
OW
ER
LO
AD
TE
CH
NIC
AL
LOA
DC
OM
ME
RC
IAL
LOA
D
SE
CO
ND
AR
YP
OW
ER
DIS
TR
IBU
TIO
NB
OX
1&
2(S
PD
B)
SE
CO
ND
AR
YE
LEC
TR
ICA
LP
OW
ER
DIS
TR
IBU
TIO
NC
EN
TE
R 1
&2
(SE
PD
C)
AC
AN
D D
CB
US
BA
RS
CIR
CU
IT B
RE
AK
ER
S(C
/BS
)
RE
MO
TE
CO
NT
RO
LC
IRC
UIT
BR
EA
KE
RS
(RC
CB
S)
AC
AN
D D
CC
ON
TA
CT
OR
S
L_MF_030700_1_0020102_01_00
Electrical PowerAC and DC Distribution
3-7Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
VFG4
VFG3
SPDB2
SPDB4
SPDB6 APU
SPDB5SPDB1SEPDC1
SEPDC2
RAT
VFG2
VFG1
SPDB7
EXTERNAL POWERRECEPTACLE
PEPDC
SPDB3
EQUIPMENT LOCATION
SPDB8
EMER PWR CTR
L_MF_030700_1_0030102_01_00
Electrical PowerComponent Location
3-7Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-8 Flight Controls
**ON A/C A380-800 Models A380-800F Models
Flight Controls
1. There are two types of flight controls :- the Primary controls- the Secondary controls.
A. Primary Controls
(1) The roll control is achieved on each wing by the inner and outer aileron complementedwith six spoilers.
(2) The yaw control is achieved by a rudder attached to the vertical stabilizer with a hinge.
(3) The pitch control is achieved by two elevators attached to the Trimmable HorizontalStabilizer (THS) (trim function) with hinges.
B. Secondary ControlsThe lift augmenting is achieved by the surfaces on each wing as follows :- two trailing edge flaps- seven leading edge slats- two ailerons which droop when the flaps are extended.
2. Operation
A. Roll ControlHydraulic servo controls, which receive electrical signals and are independently supplied, operatethe spoilers and ailerons.Two servo controls are on each aileron and one on each spoiler. Signals by the side stickcontrollers are analyzed by the electrical control computers which give the calculated controlsurface position.
B. Yaw ControlsThe rudder is operated by three independently supplied hydraulic servo-controls. The servo-controls receive signals through interconnected pedals by a single cable. The single cable runs upto a spring-loaded artificial feed unit. Yaw trim is signalled from a switch located on the centerpedestal and analyzed by the flight augmentation computers which control the rudder trimactuator.
C. Pitch ControlThe two elevators are operated by independent hydraulic servo controls. The servo controls areoperated hydraulically and controlled electrically with hydraulic pressure. Two servo controls areinstalled on each elevator.Pitch trim is provided by adjustment of the Trimmable Horizontal Stabilizer (THS). Control ofthe THS position can be achieved automatically in the normal (electrical) operating mode, viathe elevator and the Aileron computer, or mechanically by operation of the interconnectedhandwheels located on the center pedestal.
3-8Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
D. Lift AugmentationEach trailing edge flap moves by means of the carriages. The flaps are actuated by a powercontrol unit which has two hydraulic motors that drive the rotary actuator by means of atransmission shaft.Each leading edge slat moves by means of the tracks. The slats are actuated by a power controlunit which has two hydraulic motors. The two hydraulic motors drive the rotary actuator bymeans of a transmission shaft.
3-8Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
30
30
A
A A−−B B
Z= 0
(574.49 in)
4320 mm(170.08 in)
(25.73 in)
660.27 mm(25.99 in)
1691.1 mm(66.58 in)
1684.27 mm(66.31 in)
12056.5 mm(474.67 in)
4700 mm(104.61 in)
1314.1 mm(51.74 in) 3366.71 mm
(132.55 in)
30
30
32.1
24.75
ARUDDER HINGELINE 67%
653.57 mm
14592 mm
B
B
L_MF_030800_1_0010101_01_00
Control Surface TravelRudder (Sheet 1)
3-8Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
30
30
30
DIM mm in
DIMENSION CODESAND CONVERSIONS
XC
XD
XE
806.97
1162.86
1518.76
31.77
45.78
59.79
Z:
Z:
Z:
−−
−
C
D
E E
C
E E
D
17000 mm(669.29 in)
12000 mm(472.44 in)
7000 mm(275.59 in)
XC
XE
XD
Z= 0
DC
C
D
L_MF_030800_1_0020101_01_00
Control Surface TravelRudder (Sheet 2)
3-8Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
6
19.92 25.62
ELEVATORHINGE AXIS 70%
1527.19 mm(60.13 in)
A
A
B
B
C
C
L_MF_030800_1_0030101_01_00
Control Surface TravelTrimmable Horizontal Stabilizer and Elevator (Sheet 1)
3-8Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
ELEVATOR HINGE AXIS
THS CHORD PLANE
THS REAR SPAR
THS CHORD PLANE
THS HINGE AXIS
ELEVATOR HINGE AXIS
THS HINGE AXIS
THS CHORD PLANE
10
2
30
10
20
20
2
10
1425.53 mm(56.12 in)
1800.70 mm(70.89 in)
375.17 mm(14.75 in)
2832.09 mm(111.50 in)
1786.84 mm(70.35 in)
191.33 mm(7.53 in) 1045.25 mm
(41.15 in)
1906.44 mm(75.06 in)
1338.82 mm(52.71 in)
358.57 mm(14.12 in)
750.78 mm(29.56 in)
A A−
−B B
−C C
THS HINGE AXIS
580.39 mm(22.85 in)
2657.22mm104.61(in)
30
2
ELEVATORFRONT SPAR
L_MF_030800_1_0040101_01_00
Control Surface TravelTrimmable Horizontal Stabilizer and Elevator (Sheet 2)
3-8Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-9 Hydraulic Power
**ON A/C A380-800 Models A380-800F Models
Hydraulic Power
1. General
The hydraulic power system supplies the applicable hydraulic flow and pressure to the consumers.It supplies hydraulic fluid to the consumers in normal operation and for ground maintenance whenthe engines are not in operation. The indicating system monitors the system continuously. It giveswarning and cautions, and shows messages as applicable.Two hydraulic power systems operate independently :- The Green system- The Yellow system.
NOTE : There is no Blue system.The primary flight controls of the aircraft are supplied through :- The hydraulic system that operates the servo-controls,- The electrical system that supplies the Electro-Hydrostatic Actuators (EHA) and the Electrical
Back-up Hydraulic Actuators (EBHA).
2. GenerationIn normal operation, the engine hydraulic pumps get the hydraulic fluid from the applicable reservoirby suction. Then, the hydraulic pumps supply the fluid to the consumers at a nominal pressure of 345bar (5000 psi). The consumers receive the fluid flow and pressure that is necessary for theiroperation.The fluid is depressurized through the consumers and goes back to the applicable reservoir at apressure of 70 bar (1015 psi). The electrical motor pumps supply the hydraulic power for groundmaintenance operations only.The main consumers are :- The flight control system- The landing gear system- The cargo door system- The retraction system of the Ram Air Turbine (RAT)
3. Distribution
A. Green Main Hydraulic PowerThe Green main hydraulic system is one of the two systems that supply the aircraft withhydraulic power.The Green system is mechanically and hydraulically isolated from the Yellow system. In normaloperation, four engine hydraulic pumps pressurize the High-Pressure (HP) system at a nominalpressure of 345 bar (5004 psi).For the ground maintenance, it is also possible to pressurize the system with a HP hydraulicground-cart.
3-9Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
The Green hydraulic system supplies :
(1) The flight control system- The primary and secondary flight controls with one slat and one flap motor- The flap wing-tip brakes (WTB)- An actuator of the Trimmable Horizontal Stabilizer (THS).The primary flight controls of the aircraft are supplied through :- The hydraulic system that operates the servo-controls.- The electrical system that supplies the Electro-Hydrostatic Actuators (EHA) and the
Electrical Back-up Hydraulic Actuators (EBHA).
(2) The landing gear system and specially :- The nose landing-gear system (extension/retraction)- The wing landing-gear system (extension/retraction)- The nose-wheel steering system- The normal braking system
(3) The retraction system of the Ram Air Turbine (RAT)
B. Yellow Main Hydraulic PowerThe Yellow main hydraulic system is one of the two systems that supply the aircraft withhydraulic power.The Yellow system is mechanically and hydraulically isolated from the Green system. In normaloperation, four engine hydraulic pumps pressurize the High-Pressure (HP) system at a nominalpressure of 345 bar (5004 psi).For the ground maintenance, it is also possible to pressurize the system with a HP hydraulicground-cart. The Yellow hydraulic system supplies :
(1) Flight control system specially :- Primary and secondary flight controls (one flap motor)- Flap Wing-tip brakes (WTB)- An actuator of the Trimmable Horizontal Stabilizer (THS).The primary flight controls of the aircraft are supplied through :- The hydraulic system that operates the servo-controls- The electrical system that supplies the Electro-Hydrostatic Actuators (EHA) and the
Electrical Back-up Hydraulic Actuators (EBHA).
(2) Landing gear system and specially :- Body landing-gear system (extension/retraction)- Body wheel-steering system (extension/retraction)- Normal braking system
3-9Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4. Particulars
A. Engine Driven Pump :- Eight Engine Driven Pumps to provide main hydaulic power. Two EDP are fixed to the
accessory gearbox on the bottom of each gearbox. Each EDP supplies fluid to the system ata nominal pressure of 345 bars (5004 psi) with 0 flow, and a flow of 160 l/mn at a pressureof 330 bars.
- The nominal EDP speed for RR engine at take-off is 3775 rpm (max = 3841 rpm). Duringthe flight, descent, approach, the minimum speed can reach 2204 rpm.
- The Maximum EDP speed for EA engine at take-off is 4070 rpm. During the flight, descent,approach, the minimum speed can reach 2205 rpm.
- A clutch which is integrated into the EDP may disconnect in flight the EDP from theengine. This function is controlled by the crew, or may be used on ground by maintenancecrew for dispatch purpose (MMEL).
B. Electric Motor Pump :- Four Electric Motor Pumps (EMP) to supply auxiliary hydraulic power only on ground. The
electrical motor is a three phase AC induction motor (dual winding stator) using the A/C115 volts, 400 Hz electrical power supply. The electrical motor turns at 7580 rpm. Ahydraulic pump is fixed to the electrical motor through a shaft. This hydraulic pump is avariable displacement pump with 9 pistons and supplies fluid to the system at a nominalpressure of 345 bars (5004 psi) with 0 flow, a flow of 22.5 l/mn at 330 bars, and a flow of37.5 l/mn at 200 bars. Two EMPs are dedicated to each system and are located within eachinner pylon.
3-9Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
PMV
S
M
F
S
HP
M
P
Pr
H
ELECTRIC PUMP
ENGINE PUMP
RAM AIR TURBINE (RAT)
HAND PUMP
ELECTRICALLY OPERATED
GROUND CONNECTOR
SELF SEALING COUPLING
PRESSURE RELIEF VALVE
CHECK VALVE
FILTER
PRESSURE TRANSMITTER
PRESSURE SWITCH
SOLENOID VALVE
HYDRAULIC ACTUATOR
HYDRAULIC MOTOR
PRIORITY VALVE
TEMPERATURE SENSOR
PRESSURE ACCUMULATOR
SHUT OFF VALVE
HYDRAULIC SAFETY VALVE(FUSE)
PRESSURE MAINTAININGVALVE
HYDRAULIC OPERATEDSELECTOR VALVE
HIGHT PRESSUREREMANIFOLD
L_MF_030900_1_0010102_01_00
Hydraulic Power SystemSymbols
3-9Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
P P
P P
P P
P
SS
SS
SS
SS
CA
RG
O D
OO
RS
AC
TU
AT
ION
RA
T A
CT
UA
TO
R R
ET
RA
CT
ION
NO
SE
WH
EE
L S
TE
ER
ING
NO
SE
& W
ING
GE
AR
S
WIN
G G
EA
RS
BR
AK
ES
SLA
TS
& F
LAP
S
BA
CK
UP
PO
WE
R S
UP
PLY
THS
− P
ITC
H T
RIM
1
ELE
VA
TO
RS
LH
OU
TB
D &
LH
INB
D
RU
DD
ER
S U
PP
ER
& L
OW
ER
SP
OIL
ER
S 2
, 4, 6
, 8 (
LH &
RH
)
AIL
ER
ON
S L
H O
UT
BD
& R
H O
UT
BD
,LH
INB
D &
RH
INB
D
HA
ND
PU
MP
LEH
GS
LEH
GS
EN
GIN
E 2
TH
RU
ST
RE
VE
RS
ER
SLA
TS
ELE
VA
TO
RS
LH
INB
D&
RH
OU
TB
D
RU
DD
ER
S U
PP
ER
& L
OW
ER
SP
OIL
ER
S 6
(LH
& R
H)
AIL
ER
ON
S L
H M
ED
& R
H M
ED
RU
DD
ER
LOW
ER
EN
GIN
E 3
TH
RU
ST
RE
VE
RS
ER
TH
S −
PIT
CH
TR
IM 3
ELE
VA
TO
RS
LH
OU
TB
D&
RH
INB
D
RU
DD
ER
UP
PE
R
SP
OIL
ER
S 5
(LH
& R
H)
AIL
ER
ON
S L
H IN
BD
& R
H IN
BD
LEH
GS
BO
DY
WH
EE
L S
TE
ER
ING
BO
DY
GE
AR
S
BO
DY
GE
AR
BR
AK
ES
FLA
PS
BA
CK
UP
PO
WE
R S
UP
PLY
TH
S −
PIT
CH
TR
IM 2
ELE
VA
TO
RS
RH
OU
TB
D&
RH
INB
D
RU
DD
ER
S U
PP
ER
& L
OW
ER
SP
OIL
ER
S 1
, 3, 5
, 7 (
LH &
RH
)
AIL
ER
ON
S L
H O
UT
BD
& R
H O
UT
BD
,LH
ME
D &
RH
ME
D
ELE
CT
RIC
PU
MP
GE
N 1
GE
N 2
EN
GIN
E 1
EN
GIN
EP
UM
P
EN
GIN
E 2
EN
GIN
EP
UM
PE
NG
INE
PU
MP
GE
N
GE
N
RA
T
AP
U
HP
GR
OU
ND
CO
NN
EC
TO
R
GE
NG
EN
3G
EN
4
EN
GIN
E 3
EN
GIN
E 4
EN
GIN
EP
UM
PE
NG
INE
PU
MP
EN
GIN
EP
UM
PE
NG
INE
PU
MP
ELE
CT
RIC
PU
MP
115
VA
C
L_MF_030900_1_0020102_01_00
Main Hydraulic Power SystemArchitecture
3-9Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
SS
SS
M
RE
LIE
FV
ALV
E
HP
FIL
TE
RH
PF
ILT
ER
GN
D C
NC
TR
DE
LIV
ER
Y
FS
OV
HY
DF
ILT
ER
HY
DF
ILT
ER
AIR
/HY
DC
OO
LER
AIR
/HY
D H
XH
YD
FA
N
TE
MP
ER
AT
UR
E T
RA
NS
MIT
TE
R
TO
FE
ED
TA
NK
FR
OM
FE
ED
TA
NK
FU
EL/
HY
D H
X
FU
EL
SH
UT
OF
VA
LVE
FR
OM
US
ER
S
TE
MP
ER
AT
UR
ET
RA
NS
MIT
TE
R
LOW
LE
VE
LT
RA
NS
MIT
TE
RQ
UA
NT
ITY
TR
AN
SM
ITT
ER
PR
ES
SU
RE
TR
AN
SM
ITT
ER
AC
CU
MU
LAT
OR
AIR
/HY
D H
XH
YD
FA
N
SA
MP
LIN
GV
ALV
E
RE
LIE
FV
ALV
E
HP
FIL
TE
RH
PF
ILT
ER
FS
OV
HY
DF
ILT
ER
HY
DF
ILT
ER
AIR
/HY
D H
XH
YD
FA
NA
IR/H
YD
CO
OLE
R
GR
EE
N H
PM
AN
IFO
LD F
ILT
ER
(14
00 J
G)
EN
GIN
EP
UM
P 1
.1E
NG
INE
PU
MP
1.2
GR
EE
NR
ES
ER
VO
IR
GR
EE
N L
P M
AN
IFO
LD(1
300
JG)
GR
EE
N C
DM
AN
IFO
LD(1
600
JG)
EN
GIN
EP
UM
P 2
.1E
NG
INE
PU
MP
2.2
GR
EE
N H
PM
AN
IFO
LD F
ILT
ER
(17
00 J
G)
FLT
/CT
LLH
WIN
G
−R
UD
DE
R−
TH
S−
ELE
VA
TO
RS
−F
LAP
S
−W
ING
S L
/GB
RA
KE
S
−F
LT/C
TL
RH
WIN
G−
BP
S
−W
ING
S L
/GS
YS
TE
M
−S
LAT
S−
NO
SE
L/G
SY
ST
EM
GR
EE
N H
P B
ELL
YF
AIR
ING
MA
NIF
OLD
(110
0 JG
)
MM
Pr
L_MF_030900_1_0030102_01_00
Green Hydraulic SystemGeneral
3-9Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
SS
SS
M
RE
LIE
FV
ALV
E
YE
LLO
W H
PM
AN
IFO
LD F
ILT
ER
(17
00 J
Y)
HP
FILT
ER
HP
FILT
ER
GN
D C
NC
TR
DE
LIV
ER
Y
EN
GIN
EP
UM
P 3
.1E
NG
INE
PU
MP
3.2
FS
OV
HY
DFI
LTE
RH
YD
FILT
ER
YE
LLO
W C
DM
AN
IFO
LD(1
600
JY)
AIR
/HY
DC
OO
LER
AIR
/HY
D H
XH
YD
FA
N
TE
MP
ER
AT
UR
E T
RA
NS
MIT
TE
R
TO
FE
ED
TA
NK
FR
OM
FE
ED
TA
NK
FU
EL/
HY
D H
X
FU
EL
SH
UT
OF
VA
LVE
FR
OM
US
ER
S
TE
MP
ER
AT
UR
ET
RA
NS
MIT
TE
R
LOW
LE
VE
LT
RA
NS
MIT
TE
R
YE
LLO
WR
ES
ER
VO
IRQ
UA
NT
ITY
TR
AN
SM
ITT
ER
FLT
/CT
LLH
WIN
G
BO
DY
L/G
SY
STE
M
PR
ES
SU
RE
TR
AN
SM
ITT
ER
AC
CU
MU
LAT
OR
AIR
/HY
D H
XH
YD
FA
NF
LT/C
TL
RH
WIN
G SA
MP
LIN
GV
ALV
E
BR
AK
ES
SY
STE
M
−FLA
PS
−RU
DD
ER
−ELE
VA
TOR
S−T
HS
YE
LLO
W L
P M
AN
IFO
LD(1
300
JY)
YE
LLO
W H
PM
AN
IFO
LD F
ILT
ER
(14
00 J
Y)
RE
LIE
FV
ALV
E
HP
FILT
ER
HP
FILT
ER
EN
GIN
EP
UM
P 4
.1E
NG
INE
PU
MP
4.2
FS
OV
HY
DFI
LTE
RH
YD
FILT
ER
AIR
/HY
D H
XH
YD
FA
NA
IR/H
YD
CO
OLE
R
MM
Pr
L_MF_030900_1_0040102_01_00
Yellow Hydraulic SystemGeneral
3-9Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
SP
EE
D B
RA
KE
S, G
RO
UN
D S
PO
ILE
RS
RO
LL S
UR
FA
CE
S
SP
EE
D B
RA
KE
S, G
RO
UN
D S
PO
ILE
RS
RO
LL S
UR
FA
CE
S
O/B
ME
D
AIL
ER
ON
S8
76
54
32
1
SP
OIL
ER
S
SLA
TS
FLA
PS
12
34
56
78
SP
OIL
ER
S
ME
DO
/B
AIL
ER
ON
S
TH
S A
TH
S
O/B
I/BI/B
O/B
ELE
VA
TO
RS
ELE
VA
TO
RS
UP
PE
RR
UD
DE
R
LOW
ER
RU
DD
ER
VE
RT
ICA
LS
TA
BIL
IZE
R
GY
YG
GY
GY
GY
GY
G
GY
GY
GG
YY
GG
GG
YY
YY
GG
YY
Y G YG
CO
NV
EN
TIO
NA
L H
YD
RA
ULI
C S
ER
VO
CO
NT
RO
L
G Y
GR
EE
N H
YD
RA
ULI
C S
YS
TE
M
YE
LLO
W H
YD
RA
ULI
C S
YS
TE
M
I/BI/B
L_MF_030900_1_0050102_01_00
Hydraulic PowerDistribution
3-9Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-10 Landing Gear
**ON A/C A380-800 Models A380-800F Models
Landing Gear
1. The aircraft has:- two Wing Landing Gears (WLG) and related doors- two Body Landing Gears (BLG) and related doors- a Nose Landing Gear (NLG) and related doors.The Landing Gear (L/G) System includes:- a number of control devices in the cockpit- a number of computers in the avionics compartment- a number of L/Gs and their related doors- an extension and retraction system for the gears and doors- a system of brakes and related systems- a tire pressure indicating system- an oleo pressure monitoring system- a steering system.The control devices in the cockpit let the flight crew make the necessary inputs to the computers.These inputs tell the computers how to control the L/G functions that follow :- extension and retraction- braking- steering.The landing gears support the aircraft on the ground and include oleo-pneumatic shock absorbersthat absorb taxi, take-off and landing loads. During flight the L/Gs are retracted into bays.Mechanically and hydraulically operated doors close to make the aerodynamic contours of thefuselage when the L/G retracts. The hydraulically operated doors also close after the L/G is extended.The extension and retraction system extends and retracts the L/G. A normal extension and retractionsystem is usually used for this function. If the normal extension and retraction system is not available,an emergency (free fall) extension system lets each L/G extend.
2. Nose Gear and Doors (Fig. 001 and 002)The nose landing gear (NLG) includes a single-stage direct acting oleo-pneumatic shock absorber andretracts forward into a bay in the fuselage. A two-piece drag-stay assembly with a lock-stay,mechanically locks the leg in the extended position. The leg includes a hydraulically operated steeringmechanism.Four doors close the NLG bay. These are:- two hydraulically operated forward doors- two mechanically operated rear doors.An electrically operated ground door opening mechanism (for maintenance personnel) lets the forwarddoors be opened for access to the NLG bay when the aircraft is on the ground.
3. Wing Gear and Doors (Fig. 003 and 004)Each wing landing gear has a leg assembly and a four-wheel bogie beam. The WLG leg includes abogie trim actuator (BTA) and an oleo-pneumatic shock absorber.
3-10Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
The shock absorber is a single piece main cylinder with a sliding piston (slider) inside. Torque linksare attached on the rear of the leg between the shock absorber cylinder and the slider. The lower endof the slider is in the shape of a fork to which the bogie beam is attached with a pivot-pin.The BTA is mounted between the forward side of the slider and the bogie beam. The BTA keeps thebogie beam in the correct position in relation to the slider when the weight is off the landing gearduring:- take-off- retraction- and landing.A two-piece side-stay assembly holds the WLG in the extended position. A lock-stay keeps the side-stay assembly stable in the locked down position.Four doors close each WLG bay. These are:- a hydraulically-operated main door- two mechanically-operated hinged doors- a fixed fairing door attached to the WLG leg.
4. Body Landing Gear and Doors (Fig. 005 and 006)The two body landing gears have a six-wheel bogie beam and a leg assembly that includes an oleo-pneumatic shock absorber. The landing gear retracts aft into a bay in the fuselage. A two-piece drag-stay assembly mechanically locks the leg in the extended position. A bogie-trim-actuator (BTA) keepsthe bogie beam in the correct position in relation to the slider when the weight is off the landing gearduring:- take-off- retraction- and landing.The aft axle of the bogie beam can be steered.Four doors close the BLG bay. These are:- three hydraulically-operated doors- a driven fairing door attached to the inner door.An electrically operated ground door opening mechanism open the door for maintenance access to theBLG bay when the aircraft is on the ground.
5. Landing Gear Extension and Retraction SystemsTwo independent systems can be used to extend the landing gear.The Normal system is hydraulically operated and computer controlled. The hydraulic piping andelectrical harness runs are contained in a combination of rigid and flexible hoses/conduits. Theconduit routing gives protection from damage that runway debris and birdstrikes can cause. Theconduit routing also gives the maximum separation of the two systems.The Emergency Extension System (Free Fall) This system will extend the wing, body and nose gears.The system includes switches and electric actuators. When selected, the actuators operate to openthe gear and door up-locks and hydraulic valves. This lets gravity extend the gears.The L/G control lever mechanism has a baulk device. This device is a solenoid-controlled valve thatprevents selection to the UP position until:- the NLG, WLG and BLG shock absorbers are fully extended
3-10Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
- the nose wheel steering is centered.
6. SteeringThe Steering System is a computer controlled electro-hydraulic system used to change the directionof the aircraft when it moves on the ground with engine power. The system uses nose wheel steering(NWS) and body wheel steering (BWS).Pressure for the hydraulic components in the system is supplied from the:- Green Hydraulic Power system for the NWS- Yellow Hydraulic System for the BWS.The hydraulic components operate a steering mechanism which changes the direction of the NLGwheels.The core processing input/output module (CPIOM) is the computer that controls and monitors theoperation of the system. Two hand-wheel transmitters in the cockpit supply the primary steeringinputs to the CPIOM. The rudder pedals and the autopilot supply secondary steering inputs to theCPIOM through the Flight Control Primary Computers (FCPC)The system operation can be:- cancelled to let the nose wheels castor during aircraft movement on the ground- isolated from the rudder pedal inputs during the pre-flight check.
7. Tire Pressure Indicating System (TPIS)The TPIS automatically monitors the tire pressures and shows these values on Test Equipment(BITE) and also supplies other data and warnings on the WHEEL page of the Systems Display (SD).The TPIS includes Built In Test Equipment.
8. Built In Test Equipment (BITE)The BITE has these functions, it:- continuously monitors its system for failures- sends failure data (maintenance and warnings) to other systems in the aircraft- keeps a record of the failures- automatically does specified tests of the system, or part of the system, at specified times- lets specified tests be done during maintenance procedures.The BITE for the following systems is described in these chapters:- the Brakes and Steering,- the TPIS,- the Landing Gear.
3-10Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
TOWINGADAPTER
NWSACTUATOR
NWSACTUATOR
LOCK STAY
DOORACTUATOR
FORWARDDOOR RETRACTION
ACTUATOR
DRAG STAYASSEMBLY
DOWNLOCKACTUATOR
REARDOOR
STEERINGMECHANISM
L_MF_031000_1_0010101_01_00
Landing GearNose Gear and Doors
3-10Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
JACKINGPOINT
GROUNDINGPOINT
OIL DRAINVALVE
MAINTENANCE SERVICEPANEL
NITROGEN AND OILCHARGING VALVE
SEAL CHANGEOVERVALVE (COV)
STEERINGDISCONNECT
PANEL
TIRE INFLATIONADAPTER
L_MF_031000_1_0020101_01_00
Landing GearNose Gear Servicing Points
3-10Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
MAIN DOOR(HYDRAULICALLY
OPERATED)
AUXILIARY DOOR
DOOR ACTUATOR
HINGED DOORFAIRING DOOR
L_MF_031000_1_0030101_01_00
Landing GearWing Gear and Doors
3-10Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CHECK/FILLVALVE (OIL)
SEAL CHANGEOVERVALVE (COV)
GROUND POINT
CHARGE VALVE(NITROGEN)
A
B
C
C
B
A
TIRE INFLATION ADAPTER(TYPICAL)
L_MF_031000_1_0040101_01_00
Landing GearWing Gear Servicing Points
3-10Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
INNER DOOR
AUXILIARY DOOR
INNER DOOR OUTER DOOR
INNER DOORACTUATOR
BLG LEGASSEMBLY
RETRACTION ACTUATOR CENTER DOORACTUATOR
DRAG BRACE ASSEMBLY
OUTER DOOR ACTUATOR
CENTER DOOR
A
A
L_MF_031000_1_0050101_01_00
Landing GearBody Gear and Doors
3-10Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CHARGING VALVE(NITROGEN)
DRAINVALVE
SEAL CHANGEOVERVALVE (COV)
GROUNDINGPOINTS
(RIGHT ONE SHOWN LEFT ONE SIMILAR)
C
A
B
C
TIRE INFLATION ADAPTOR(TYPICAL)
A
B
L_MF_031000_1_0060101_01_00
Landing GearBody Gear Servicing Points
3-10Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE
BODY GEAR TIRE SIZE
BODY GEAR TIRE PRESSURE
562 000 kg (1 239 000 lb)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
1270 x 455R22 32PR
14.1 bar (205 psi)
15 bar (218 psi)
1400 x 530R23 40PR
1400 x 530R23 40PR
15 bar (218 psi)
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)
L_MF_031000_1_0070101_01_00
Landing GearLanding Gear Footprint - A380-800 Models
3-10Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**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
MAXIMUM RAMP WEIGHT
WING GEAR TIRE SIZE
WING GEAR TIRE PRESSURE
BODY GEAR TIRE SIZE
BODY GEAR TIRE PRESSURE
14.7 bar (213 psi)
15 bar (218 psi)
15 bar (218 psi)
592 000 kg (1 305 125 lb)
NOSE GEAR TIRE SIZE
NOSE GEAR TIRE PRESSURE
50 x 20R22 34PR
1400 x 530R23 42PR
1400 x 530R23 42PR
1 700 mm(66.9 in)
1 700 mm(66.9 in)
14 336 mm(47.03 ft)
7 344 mm(24.1 ft)
L_MF_031000_1_0080101_01_00
Landing GearLanding Gear Footprint - A380-800F Models
3-10Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-11 Exterior Lighting
**ON A/C A380-800 Models A380-800F Models
Exterior Lighting
1. This section gives the location of the aircraft exterior lighting.
3-11Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
BEACON LIGHT
BEACON LIGHTS
OBSTRUCTION LIGHT
WING STROBE LIGHT
WING TIP NAVIGATION LIGHT
OBSTRUCTION LIGHT
WING STROBE LIGHT
WING TIP NAVIGATION LIGHT
REAR STROBE LIGHT
REAR NAVIGATION LIGHT
TAXI CAMERA LIGHTS
TAXI CAMERA LIGHTS
A
LOGO LIGHTS
WING / ENGINESCAN LIGHTS (LH/RH)
L_MF_031100_1_0010101_01_00
Exterior LightingExterior Lighting Available in Flight (Sheet 1)
3-11Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
TAXI LIGHTS (WING LEADING EDGE)
TAKE OFF LIGHTS
RUNWAY TURN OFF LIGHTS(NOSE LANDING GEAR)
TAKE OFF LANDING LIGHTS
(SYMMETRICAL ON RH WING)
(SYMMETRICAL ON RH WING)
L_MF_031100_1_0020101_01_00
Exterior LightingExterior Lighting Available in Flight (Sheet 2)
3-11Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
FORWARD LANDINGWHEEL WELL LIGHT
FORWARD CARGO COMPARTMENTLOADING AREA LIGHT
RIGHT AND LEFTLANDING WHEEL
WELL LIGHTS
AFT CARGO COMPARTMENTLOADING AREA LIGHT
L_MF_031100_1_0030101_01_00
Exterior LightingExterior Lighting for Ground Use - A380-800 Models
3-11Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
FORWARD LANDINGWHEEL WELL LIGHT
UPPER DECK CARGO COMPARTMENTLOADING AREA LIGHT
MAIN DECK CARGO COMPARTMENTLOADING AREA LIGHT
AFT CARGO COMPARTMENTLOADING AREA LIGHT
FORWARD LANDING WHEELWELL LIGHT
FORWARD CARGO COMPARTMENTLOADING AREA LIGHT
RIGHT LANDING WHEELWELL LIGHT
LEFT LANDING WHEELWELL LIGHT
L_MF_031100_1_0040101_01_00
Exterior LightingExterior Lighting for Ground Use - A380-800F Models
3-11Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-12 Navigation
**ON A/C A380-800 Models A380-800F Models
Navigation
1. Air Data/Inertial Reference System (ADIRS)
A. A triplicated ADIRS shall be installed to provide main air data, inertial reference informationGPS position and GPIRS position and integrity, to cockpit instruments and other systems. Thesystem shall consist of three sets of air data probes and three Air. Data and Inertial ReferenceUnits (ADIRU), which combine air data and inertial reference systems.Each air data probe set shall consist of a pair of static probes, a sideslip probe and a multifunction probe which groups pitot, total temperature and angle of attack sensors.All probes shall be de-iced.
B. Standby navigation systemThe following standby indications shall be displayed on two Integrated.Standby Instrument Systems (ISIS) :- Altimeter scales in feet or if selected in feet and meters- Baro setting in hPa or in Hg- Airspeed- Attitude- Landing System deviations upon crew selection.
A standby magnetic compass shall be installed in a position visible to both pilots.
2. Landing and Taxiing aids
A. Two Multi-Mode Receivers (MMR)The primary function of the MMR is to process signals received from the Localizer, the GLIDEand the Global Positioning System antennas. The MMR includes two main functions :- ILS function
The ILS provides the crew and airborne system users with the aircraft position during thelanding phase with respect to a predetermined descent path.
- GPS functionThe GPS is a radio aid to worldwide navigation, which provides the crew and the airbornesystem user (FMGEC) with a readout of accurate navigation information.
- FLS functionThe FLS function enables the pilot to fly the current published non precision approaches(RNAV, VOR, VOR/DME, NDB, NDB/DME, GPS) in a way similar to precisionapproaches.
3. Independent Position Determining
A. Aircraft Environment Surveillance System (AESS)Three distinct systems of the AESS :
3-12Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
- Two weather radar system. This system enables detection and localization of theatmospheric disturbances in the area defined by the antenna scanning and displays them onthe Navigation-Display (ND) with different colors according to the level of disturbance.
- One Traffic Collision Avoidance System (TCAS). This system enables detection and displayof aircraft in the immediate vicinity and gives corrective vertical deviation in case of collisionthreat.
- GPWS system One Enhanced Ground Proximity Warning System (Enhanced GPWS). Thissystem provides the flight crew with visual and aural alerts when potentially hazardousconditions are met with the terrain.
B. Two radio altimetersThis system provides, below 2500 feet, the crew and the airborne system users with the radioheight data, which is the main landing gear wheels height above the ground. Radio altimeterinformation is displayed on the PFDs.
4. Dependent Position Determining
A. Two Distance Measuring Equipment (DME) systemsThis system provides the crew and the airborne user systems with a digital readout of the slantrange distance of the aircraft from a selected ground station with audio and possible digitalidentification of the selected ground station.
B. Two Air Traffic Control (ATC) systemsThis system gives aircraft identification to the ground and other aircraft and enables effectiveground surveillance of the air traffic.
C. One Automatic Direction Finder (ADF) systemThis system provides an indication of the relative bearing of the aircraft to a selected groundstation with aural identification of the ground station and decoding of the Morse identification.
D. Two VOR/MARKER systemsThis system comprises two independent systems :
(1) VOR system for the radio navigation.This system provides the crew with aircraft position with respect to the ground station andaircraft angular deviation from the selected course.
(2) MARKER (MKR) system for the landing approach phase.This system determines the distance between the aircraft and the runway and providesaural and visual indications of the passage of the aircraft over the marker transmitterlocated on the runway.
3-12Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
VO
R A
NT
EN
NA
AD
F 1
AD
F 2
TC
AS
TO
P 2
TC
AS
TO
P 1
GP
S2
GPS
1
WE
AT
HE
RR
AD
AR
GLI
DE
CA
PTU
RE G
LID
ET
RA
CK
TC
AS
BO
TT
OM
2 DM
E 1
TC
AS
BO
TT
OM
1
DM
E 2MA
RK
ER
L_MF_031200_1_0010102_01_01
NavigationLocation of Antennas
3-12Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-13 Auxiliary Power Unit
**ON A/C A380-800 Models A380-800F Models
Auxiliary Power Unit
1. DescriptionThe Auxiliary Power Unit (APU) PW980 is a twin-spool gas turbine engine used to provide auxiliaryelectrical and pneumatic power to the aircraft. The APU supplies bleed air power to the aircraft forthe Environmental Control System (ECS) and for Main Engine Starting (MES), and it also supplieselectrical power for the Electrical System through two A/C generators. The APU is a self-containedunit which makes the aircraft independent of external pneumatic or electrical power supply, mainlyfor on ground use. Anyway, during the take-off the APU supplies bleed air to the ECS (thus avoidinga reduction in engine thrust) and in flight it backs up both electrical and air conditioning systems.The APU obtains power for self-starting from the aircraft batteries, or in combination with theexternal power, ground service, or normal aircraft supply. lThe APU system has four different subsystems:- the APU engine system,- the APU fuel system,- the APU oil system,- the APU air system.The APU Engine architecture splits in five sections:- the load gearbox section,- the load compressor section,- the accessory gearbox section,- the engine section,- the exhaust section.
2. Installation- The APU is installed in the tail cone, at the rear part of the fuselage (section 19.1), inside a
fireproof compartment (between frames 112 and 117).- The Air Intake System is located on top of the APU and crosses the space between the APU
plenum chamber and the aircraft outside (upper right side position). The Air Intake Housing islocated between frames 111 and 113, and the Air Intake Duct is located in the space betweenframes 113 and 115.
- The Exhaust Muffler is located at the end of the tail cone, aligned with the APU, and crossesthree different zones, from frame 116 to the rear fairing.
- The Electronic Control Box (ECB) is installed in an electronic cooled rack, closed to frame 95,within the pressurized fuselage.
3-13Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3. APU PW980The APU PW980 is a double-shaft gas generator. Air from outside the aircraft enters through the airintake to the APU inlet, where it is delivered to both the engine and load compressor. The enginecompressor (High Pressure Compressor) compresses the air and delivers it to the reverse-flowcombustor chamber where fuel is added and burned. The high pressure/high temperature gas expandsthrough the engine turbine (High Pressure Turbine) providing the energy to drive the enginecompressor and the Accessory Gearbox (AGB). The gas further expands through the power turbine,which provides the energy to drive the load compressor and the electrical generators through theLoad Gearbox (LGB). The low energy gas expands through the exhaust diffuser from where it isdelivered to the aircraft mounted exhaust muffler. The power spool and the gas generator spoolrotate about a common axis.
4. Control CircuitThe Elecronic Control Box (ECB) initiates and automatically executes an APU start sequence uponreceipt of a start command from the aircraft flight deck. The ECB continually monitors APUoperation in order to maintain optimal performance. It also provides automatic fault shutdowns.
5. Controls and IndicationPrimary APU controls and indications are installed in the cockpit, mainly in the overhead panel,center pedestal panel and forward center panel. Additionally, two external emergency shutoff controlsare installed on the Nose Landing Gear panel and on the Refuel/Defuel panel.
3-13Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
L_MF_031300_0_AAM0_01_00
THE DISTANCE FROM FR94, FR98, FR100 BOTTOMCENTERLINE TO FUSELAGE DATUM (FD) AS FOLLOWSFR112 TO FD= 974.9 mm (38.38 in)FR117 TO FD= 1772.4 mm (69.78 in)FR120 TO FD= 2239.8 mm (88.18 in)
NOTE:
A
STA73713 FR117/
STA72922 FR112/
STA72310 FR110/
315BL
315AL315AR
313AB
317AB
313AZ
A
L_MF_031300_1_0010101_01_00
Auxiliary Power UnitAPU Access Doors
3-13Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
EXHAUSTMUFFLER
FIREWALL
FIRE EXTINGUISHERBOTTLE
FIREWALL
AIR INTAKEDUCT ASSEMBLY
COOLING AIR DUCT
BLEEDLINE
Z317
Z313Z315
FR112
FR110
FR117
L_MF_031300_1_0020101_01_00
Auxiliary Power UnitGeneral Layout
3-13Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-14 Power Plant
**ON A/C A380-800 Models A380-800F Models
Power Plant
1. DimensionsThis section contains data necessary for determining the platforms and associated facilities requiredfor power plant handling.
3-14Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
AT
W−
MM
−05
16−
A
INBOARD POSITION
OUTBOARD POSITION
8495 mm(334.45 in)
6194 mm(243.86 in)
10565 mm(415.94 in)
3808 mm(149.92 in)
1311 mm(51.81 in) 2333 mm
(91.85 in)
L_MF_031400_1_0010102_01_01
3899 mm(153.5 in)
Engine DimensionsGP 7200 Engines
3-14Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
INBOARD
OUTBOARD
7194 mm(283.2 in)
6178 mm(243.2 in)
8360 mm(329 in)
3873 mm(152.5 in)
INSTALLATION
INSTALLATION
2376 mm(93.5 in)
1178 mm(46.3 in)
3896 mm(153.4 in)
L_MF_031400_1_0020102_01_00
Engine DimensionsTRENT 900 Engines
3-14Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
OPEN POSITIONS:INITIAL: 40°FULL: 50°
40°50°
OPENPOSITION INBOARD ENG. OUTBOARD ENG. INBOARD ENG. OUTBOARD ENG. ALL ENG.
DIM. B DIM. C DIM. A
40°
50°
6.95 m1.30 m(4.2 ft)1.30 m
2.27 m(7.4 ft)2.27 m(7.4 ft)
A
C
B
2.0 m(6.6 ft)2.4 m(7.8 ft)
3.0 m(9.7 ft)
3.4 m(11.2 ft)
7.3 m(23.9 ft)(4.2 ft)
(22.8 ft)
L_MF_031400_1_0040101_01_01
A
A
Fan CowlsTRENT 900 Engines
3-14Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
45°
C
B
ALL ENGINES
6.80
22.3045°
m
ft
A
MIN MAX
A
ENGINE 1−4
2.64
8.6645°
m
ft
B
3.14
10.30
MIN MAX
ENGINE 2−3
1.86
6.10
2.16
7.08
C
SEE MFP SECTION1−9
NOTE:
AA
A
A
: FAN COWL
1 1
B AND C DEPENDING ON AIRCRAFT CONFIGURATION.
1 A
L_MF_031400_1_0060101_01_01
Fan Cowls - Engine 1-2-3-4GP 7200 Engines
3-14Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
6.30
20.6645°
m
ft
AMIN MAX
2.64
8.6645°
m
ft
3.14
10.30
SEE MFP SECTION1−9
NOTE:
A
A
5.70
18.7035°
m
ft
2.30
7.5435°
m
ft
2.80
9.18
C
45°35°C B C
B
A A11
1 1
: FAN EXHAUST COWL1
B AND C DEPENDING ON AIRCRAFT CONFIGURATION.
A
B
L_MF_031400_1_0070101_01_01
Fan Exhaust Cowls - Engine 1-4GP 7200 Engines
3-14Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
A
6.30
20.6645°
m
ft
AMIN MAX
1.86
6.1045°
m
ft
B
2.16
7.08
SEE MFP SECTION1−9
NOTE:
5.80
19.0235°
m
ft
1.52
4.9835°
m
ft
1.82
5.97
C
: TRUST REVERSER1
B AND C DEPENDING ON AIRCRAFT CONFIGURATION.
A
L_MF_031400_1_0080101_01_00
45°35°C B C
B
A A11
1 1
Thrust Reverser - Engine 2-3GP 7200 Engines
3-14Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-15 Component Sizes and Weights
**ON A/C A380-800 Models A380-800F Models
Component Sizes and Weights
1. General
This topic details the weights of the primary removable components on the A380 aircraft for models-800 and -800F. Weights in para. A are for components fitted to each wingAll weights are approximate values and are given in kg (lb.).
A. Wing
SLATS
Model -800/ Model -800F
Droop Nose 1 219 kg (482 lb.) /221 kg (487 lb.)
Droop Nose 2 200 kg (441 lb.) /202 kg (445 lb.)
Slat 2 148 kg (326 lb.) /149 kg (328 lb.)
Slat 3 145 kg (319 lb.) /146 kg (322 lb.)
Slat 4 150 kg (330 lb.) /152 kg (335 lb.)
Slat 5 131 kg (288 lb.) /132 kg (291 lb.)
Slat 6 115 kg (253 lb.) /116 kg (255 lb.)
Slat 7 108 kg (238 lb.) /109 kg (240 lb.)
FLAPS
Model -800/ Model -800F
Inner 656 kg (1446 lb.) /687 kg (1514 lb.)
Midboard 681 kg (1501 lb.) /709 kg (1563 lb.)
Outer 395 kg ( 870 lb.) /410 kg ( 904 lb.)
FLAP TRACKS
Model -800/ Model -800F
Equipped Track 1 212 kg ( 467 lb.) /229 kg ( 505 lb)
Equipped Track 2 455 kg (1003 lb.) /478 kg (1053 lb)
Equipped Track 3 366 kg ( 807 lb.) /383 kg ( 844 lb)
Equipped Track 4 343 kg ( 756 lb.) /360 kg ( 793 lb)
Equipped Track 5 334 kg ( 736 lb.) /350 kg ( 771 lb)
Equipped Track 6 192 kg ( 423 lb.) /198 kg ( 436 lb)
3-15Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
FLAP TRACKS
Model -800/ Model -800F
Flap Track Fairing 2 (LH wing) <1> 209 kg (460 lb.)
Flap Track Fairing 2 (RH wing) 179 kg (394 lb.)
Flap Track Fairing 3 139 kg (306 lb.)
Flap Track Fairing 4 149 kg (328 lb.)
Flap Track Fairing 5 139 kg (306 lb.)
Flap Track Fairing 6 89 kg (196 lb.)
<1> RAT installed.
AILERONS
Model -800/ Model -800F
Inner 215 kg (474 lb.)
Midboard 235 kg (518 lb.)
Outer 256 kg (564 lb.)
SPOILERS
Model -800/ Model -800F
Spoiler 1 96 kg (211 lb.)
Spoiler 2 91 kg (200 lb.)
Spoiler 3 77 kg (169 lb.)
Spoiler 4 84 kg (185 lb.)
Spoiler 5 77 kg (169 lb.)
Spoiler 6 85 kg (187 lb.)
Spoiler 7 79 kg (174 lb.)
Spoiler 8 78 kg (172 lb.)
B. Landing gear
BODY LANDING GEAR (BLG)
Model -800/ Model -800F
BLG 5847 kg (12890 lb.)
BLG Dragbrace assembly 462 kg (1018 lb.)
BLG Shock absorber assembly 2111 kg (4654 lb.)
BLG Actuator retraction assembly 91 kg (201 lb.)
BLG Actuator bogie trim assembly 71 kg (157 lb.)
3-15Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
BODY LANDING GEAR (BLG)
Model -800/ Model -800F
BLG wheels 873 kg (1925 lb.)
BLG Brakes 443 kg (977 lb.)
BLG Tires 701 kg (1545 lb.)
BLG Door actuator centre 18 kg (40 lb.)
BLG Door actuator inner 20 kg (44 lb.)
BLG Door actuator outer 38 kg (84 lb.)
WING LANDING GEAR (WLG)
Model -800/ Model -800F
WLG 4014 kg (8849 lb)
WLG Sidestay assembly 238 kg (525 lb)
WLG Shock absorber assembly 1598 kg (3523 lb)
WLG Actuator retraction assembly 117 kg (258 lb)
WLG Actuator bogie trim assembly 9 kg (20 lb)
WLG Wheels 606 kg (1336 lb)
WLG Brakes 443 kg (977 lb)
WLG Tires 467 kg (1030 lb)
Wing gear door actuator 30 kg (66 lb)
NOSE LANDING GEAR
Model -800/ Model -800F
NLG 1909 kg (4209 lb.)
NLG Leg 1215 kg (2679 lb.)
NLG Upper panel equiped 226 kg (498 lb.)
NLG Retraction actuator equiped 69 kg (152 lb.)
NLG Wheels 176 kg (388 lb.)
NLG Tires 182 kg (401 lb.)
Nose gear door actuator 27 kg (60 lb.)
3-15Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
C. Fuselage
NOSE FUSELAGE
Model -800/ Model -800F
Radome 60 kg (132 lb.)
Windshield panel 36 kg ( 79 lb.)
Lateral Sliding Window panel 21 kg ( 46 lb.)
(including mechanism) 46 kg (101 lb.)
Lateral Fixed Window panel 21 kg ( 46 lb.)
PASSENGER DOORS AND ASSOCIATED SLIDES (MAIN DECK)
Model -800Door n˚ M2 + Slide 125 kg (275 lb.) + 102 kg (225 lb.)
Door n˚ M3 + Slide 122 kg (269 lb.) + 96 kg (216 lb.)
Door n˚ M4 + Slide 118 kg (260 lb.) + 85 kg (187 lb.)
Door n˚ M5 + Slide 122 kg (269 lb.) + 88 kg (194 lb.)
Door n˚ M6 + Slide 124 kg (273 lb.) + 88 kg (194 lb.)
PASSENGER DOORS AND ASSOCIATED SLIDES (UPPER DECK)
Model -800Door n˚ U1 + Slide 125 kg (275 lb.) + 136 kg (299 lb.)
Door n˚ U2 + Slide 125 kg (275 lb.) + 134 kg (295 lb.)
Door n˚ U3 + Slide 125 kg (275 lb.) + 134 kg (295 lb.)
CARGO DOORSModel -800
Forward Cargo Door 300 kg ( 661 lb.)
Aft Cargo Door 270 kg ( 595 lb.)
Bulk Cargo Door 40 kg ( 88 lb.)
Upper Deck Cargo Door 410 kg ( 904 lb.)
Main Deck Cargo Door 470 kg (1036 lb.)
REAR FUSELAGE SECTION 19.1
Model -800/ Model -800F
Structure 433 kg (955 lb)
3-15Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
REAR FUSELAGE SECTION 19.1
Model -800/ Model -800F
Systems 236 kg (520 lb.)
MISCELLANEAOUS
Model -800/ Model -800F
Nose Landing gear doors:-- forward (each)-- rear (each)
167 kg (368 lb.)58 kg (128 lb.)25.5 kg ( 56 lb.)
Body Landing gear doors:-- Outer door-- Centre door-- Inner door-- Auxiliary door
388.2 kg (856 lb)103.3 kg (228 lb)167.8 kg (370 lb)10.1 kg (22 lb)
Wing Landing gear doors-- Main door-- Auxiliary door
369.4 kg (814 lb)31.6 kg (70 lb)
Control Units:-- Flaps-- Slats
55 kg (121 lb.)34 kg (75 lb.)
Air Conditioning Pack (one side) 397 kg (875 lb.)
APU access door:-- right-- left
25 kg (55 lb.)27 kg (60 lb.)
APU exhaust 96 kg (211 lb.)
APU electrical system 49 kg (108 lb.)
D. Stabilizers
VERTICAL TAIL
Model -800/ Model -800F
Box (equipped without rudder) 2491 kg (5491 lb)
Rudder 693 kg (1527 lb)
Leading edge 171 kg ( 377 lb)
Dorsal fin 25 kg ( 55 lb)
Tip 30 kg ( 66 lb)
Fuselage fairing 62 kg ( 136 lb)
3-15Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
HORIZONTAL TAIL
Model -800/ Model -800F
Box 3982 kg (8778 lb.)
Outer elevator 388 kg ( 855 lb.)
Inner elevator 508 kg (1119 lb.)
Leading edge 467 kg (1029 lb.)
Trailing edge 688 kg (1516 lb.)
Tip 100 kg ( 220 lb.)
Miscellaneous 114 kg ( 251 lb.)
Systems 241 kg ( 531 lb.)
E. Miscellaneous
MISCELLANEAOUS
Model -800/ Model -800F
Ram air turbine assembly 185.2 kg ( 408 lb.)
Battery 41.9 kg ( 92 lb.)
Engine fire extinguisher bottle 21.8 kg ( 48 lb.)
F. Engine and nacelle
ENGINE AND NACELLE TRENT 900
Model -800/ Model -800F
Engine (Excluding mounting and BFE) 6469 kg (14262 lb)
Fan Cowl 198 kg (437 lb.) / nacelle
Thrust Reverser 650 kg (1433 lb.) / nacelle
Fan Exhaust Cowl 900 kg (1984 lb.) / nacelle
BFE 139 kg (306 lb.)
Air Inlet 351 kg (774 lb.) / nacelle
Pylon (structure + systems) 1230 kg (2712 lb)
ENGINE AND NACELLE GP 7200
Model -800/ Model -800F
Engine 6123 kg (13499 lb)
Fan Cowl 240 kg (529 lb) / nacelle
Thrust Reverser Unit 1381 kg (3045 lb) / nacelle
Fan Exhaust Cowl 918 kg (2024 lb) / nacelle
3-15Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
ENGINE AND NACELLE GP 7200
Model -800/ Model -800F
BFE-EBU 710 kg (1565 lb)
Air Inlet 358 kg (789 lb)
Pylon (structure + systems) 1240 kg (2734 lb)
3-15Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-16 Component Handling
**ON A/C A380-800 Models A380-800F Models
Component Handling
1. General
Section 3-16 gives the information on dimensions and on the Center of Gravity (C.G.) locations of thevarious control surfaces. All the dimensions are in millimeters and inches.
3-16Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
DROOP NOSE 1
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
CG
HOISTINGPOINT
742 (29.2)2127 (83.7)
3511 (138.2)
4325 (170.3)
323(12.7)
328(12.9)
363(14.3)
FWD
OTBD
L_MF_031600_1_0010101_01_00
Droop Nose 1CG Location
3-16Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
DROOP NOSE 2
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
CG
HOISTINGPOINT
4383 (172.5)
3843 (151.3)2240 (88.1)
720 (28.3)
320(12.6)
338(13.3)
372(14.6)
FWD
OTBD
L_MF_031600_1_0020101_01_00
Droop Nose 2CG Location
3-16Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTINGPOINT
SLAT 2
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
3724 (146.6)
2575 (101.4)
1802 (70.9)
883 (34.7)
315(12.4)
352(13.9)
438(17.3)
FWD
OTBD
L_MF_031600_1_0030101_01_00
Slat 2CG Location
3-16Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTINGPOINT
SLAT 3
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
3854 (151.7)
2919 (114.9)
1937 (76.3)
999 (39.3)
361(14.2)
375(14.8)
395(15.5)
FWD
OTBD
L_MF_031600_1_0040101_01_00
Slat 3CG Location
3-16Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTINGPOINT
SLAT 4
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
3871 (152.4)
2892 (113.9)
1892 (74.5)
1056 (41.6)
344(13.5)
327(12.9)
348(13.7)
FWD
OTBD
L_MF_031600_1_0050101_01_00
Slat 4CG Location
3-16Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTINGPOINT
SLAT 5
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
4786 (188.4)
3424 (134.8)4786 (188.4)
2398 (94.4)
231(9.1)
278(11)
300(11.8)
FWD
OTBD
L_MF_031600_1_0060101_01_00
Slat 5CG Location
3-16Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTINGPOINT
SLAT 6
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
4534 (178.5)3423 (134.8)
2317 (91.2)1143 (45)
215(8.5)
270(10.6)
317(12.5)
FWD
OTBD
L_MF_031600_1_0070101_01_00
Slat 6CG Location
3-16Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTINGPOINT
SLAT 7
NOTE: DIMENSIONS IN MILLIMETRES (INCHES IN BRACKETS)
5234 (206)
4338 (170.8)2688 (105.8)
920 (36.2)
212(8.4)
218(8.6)
236(9.3)
FWD
OTBD
L_MF_031600_1_0080101_01_00
Slat 7CG Location
3-16Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
L_MF_031600_1_0130101_01_00
FWD
OUTBOARD
HINGELINE
2252 (88.7)
2074 (81.6)
1196 (47.1)
956 (37.6)
379(14.9)
277(10.9)
292(11.5)
256(10.1)
885(34.8)
CG
HOISTING POINT
INBOARD AILERON
Inboard AileronCG Location
3-16Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
MID AILERON
FWD
OUTBOARD
HINGELINE
2923 (115.1)
2455 (96.6)
1377 (54.2)
1201 (47.3)
417(16.4)
261(10.3)
299(11.8)
823(32.4) 258
(10.1)
L_MF_031600_1_0140101_01_00
Mid AileronCG Location
3-16Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
OUTBOARD AILERON
FWD
OUTBOARD
HINGELINE
4090 (161.0)
4026 (158.5)
2232 (87.9)
1911 (75.2)
652(25.7)
250(9.8)
226809
780(30.7)
271(10.7)
L_MF_031600_1_0150101_01_00
Outboard AileronCG Location
3-16Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 1
L_MF_031600_1_0160101_01_00
FWD
OUTBOARD
2517 (99.1)
2186 (86.1)
1273 (50.1)
596(23.5)
252(9.9)
50(1.9)
50(1.9)
Spoiler 1CG Location
3-16Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 2
L_MF_031600_1_0170101_01_00
FWD
OUTBOARD
2236 (88.0)
2021 (79.6)
1108 (43.6)
431(17.0)
235(9.2)
50(1.9)
50(1.9)
Spoiler 2CG Location
3-16Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 3
L_MF_031600_1_0180101_01_00
FWD
OUTBOARD
2311 (91.0)
2039 (80.3)
1037 (40.8)
299(11.8)
239(9.4)
50(1.9)
50(1.9)
Spoiler 3CG Location
3-16Page 15
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 4
L_MF_031600_1_0190101_01_00
FWD
OUTBOARD
2206 (86.8)
1966 (77.4)
1103 (43.4)
226(8.9)
248(9.8)
50(1.9)
50(1.9)
Spoiler 4CG Location
3-16Page 16
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 5
L_MF_031600_1_0200101_01_00
FWD
OUTBOARD
2089 (82.2)
1898 (74.7)
1047 (41.2)
308(12.1)
234(9.2)
50(1.9)
50(1.9)
Spoiler 5CG Location
3-16Page 17
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 6
L_MF_031600_1_0210101_01_00
FWD
OUTBOARD
2610 (102.7)
1942 (76.5)
1318 (51.9)
352(13.9)
196(7.7)
50(1.9)
50(1.9)
Spoiler 6CG Location
3-16Page 18
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 7
L_MF_031600_1_0220101_01_00
FWD
OUTBOARD
2716 (106.9)
2287 (90.0)
1370 (53.9)
697(27.4)
190(7.5)
50(1.9)
50(1.9)
Spoiler 7CG Location
3-16Page 19
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG
HOISTING POINT
SPOILER 8
FWD
OUTBOARD
2872 (113.1)
2183 (85.9)
1427 (56.2)
593(23.3)
154(6.1)
50(1.9)
50(1.9)
L_MF_031600_1_0230101_01_00
Spoiler 8CG Location
3-16Page 20
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
15 mm(0.6 in)
11896 mm(468.3 in)
1. CG POSITION OF HORIZONTAL STABILIZER WITHOUT THE ELEVATORS2. CG POSITION OF THE INNER ELEVATOR3. CG POSITION OF THE OUTER ELEVATOR
2 CG
3 CG
3293 mm(129.6 in)
9030 mm(355.5 in)
9356 mm(368.3 in)
1 CG
6864 mm(270.2 in) 3293 mm
(129.6 in)
L_MF_031600_1_0090101_01_00
Horizontal StabilizerCG Location
3-16Page 21
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
CG POSITION OF THE VERTICAL STABILIZER WITH THE RUDDER AND WITH THE DORSAL FIN
5912 mm(232.8 in)
9950 mm(391.7 in)
VTX0
VTZ0
CG
L_MF_031600_1_0100101_01_00
Vertical Stabilizer and RudderCG Location (Sheet 1)
3-16Page 22
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
2777 mm(109.3 in)
VTZ0
VTX0
1 CG
2 CG
3 CG
9027 mm(355.4 in)
5894 mm(232.0 in)
9320 mm(366.9 in)
14660 mm(577.2 in)
11021 mm(433.9 in)
1. CG POSITION OF THE VERTICAL STABILIZER WITHOUT THE RUDDER AND DORSAL FIN2. CG POSITION OF THE UPPER RUDER3. CG POSITION OF THE LOWER RUDDER
L_MF_031600_1_0110101_01_00
Vertical Stabilizer and RudderCG Location (Sheet 2)
3-16Page 23
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
Y
X
STA77204.5/FR120
STA72320/FR110
CG
WITHAPU GENERATOR
WITHOUTAPU GENERATOR
mm mm
XYZ
206622
2420 95.280.87
81.34 214635
2609 102.721.38
84.49
in in
Z
CL
STA74592/FR115
STA74002/FR114
L_MF_031600_1_0120101_01_00
Tail coneCG Location
3-16Page 24
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-17 Suggested Hangar Arrangement
**ON A/C A380-800 Models A380-800F Models
Suggested Hangar Arrangement
1. General
The purpose of a maintenance hangar is to provide a weather-safe space for aircraft servicing,maintenance and repair activities. It may also include space for aircraft component workshops,support equipment and administrative facilities.Maintenance hangar planning should take the following factors into consideration :- level of maintenance to be performed,- capacity including storage space,
NOTE : The number of hangar bays depends on :- fleet size,- aircraft utilization,- maintenance check intervals,- number of aircraft requiring maintenance action at the same time,- maintenance check elapsed time,- working hours available.- local labor regulations,- clearances : external (e.g. hangar doors) and internal (e.g. for aircraft jacking),- tractor drive-through capability,- special features (see paragraph A.),- ground support equipment (see paragraph B.),- environmental control (lighting/heating/air conditioning) : temperature (hot or cold climate),
dust or humidity, prevailing winds,
NOTE : Hangar lighting levels should be 75 footcandles (800 lm/m2).- structural materials/design (the roof is the most expensive part of the hangar),- security,- safety equipment and fire protection (see paragraph C.),- local building codes,- site location with respect to aprons, taxiways, runways and electromagnetic constraints.- geotechnical investigation,- extension capability.
2. Special Features :- Cranes,- landing gear maintenance pits,- mezzanine,- fixed work stands,- aircraft cleaning, stripping and painting capabilities,- drainage,
3-17Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
- ventilation (work in fuel tank),- pneumatic, electrical and hydraulic connections,- computer system (aircraft maintenance and planning).
3. Ground Support Equipment :- Air conditioning unit,- nitrogen cart,- oxygen cart,- hydraulic rig,- air starter unit,- air compressor,- electrical ground power unit,- fuel tank ventilation unit,- lavatory service unit, -- tractor,- tow bars,- engine cradles and trolleys (engine Removal/Installation),- mobile maintenance docks/platforms,- jacks,- elevating platforms,- stairways,- access steps,- mobile scissor platform,- weighing devices,- storage racks.
4. Safety Equipment and Fire Equipment :- safety harnesses with damping device,- explosive atmosphere detection devices,- sprinkler network using a mixture of water and emulsifying agent,
NOTE : Quantity required is 10 l/m2 per minute minimum. Water storage tanks should haveenough capacity for one hour’s use.
- foam spray gun(s) using same mixture as the sprinkler system,
NOTE : Minimum flow rage : 200 m3/h.- portable fire-fighting devices using dry chemical (powder), water or CO2.
3-17Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
16 m(50.50 ft)
29.5 m(96.78 ft)5 m (16.40 ft)
5 m(16.40 ft)
29.5 m(96.78 ft)
L_MF_031700_1_0010102_01_00
Suggested Hangar ArrangementNose--in Position (Sheet 1)
3-17Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
15 m *(49.21 ft)*
10 m(32.80 ft)
10 m(32.80 ft)
10 m(32.80 ft)
98 m (321.52 ft)
100
m (
328.
08 ft
)
* : MINIMUM NECESSARY DISTANCE TO MOVE AWAY A TRACTOR WITH A TOW BAR
L_MF_031700_1_0020102_01_00
Suggested Hangar ArrangementNose--in Position (Sheet 2)
3-17Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
5 m(16.40 ft)
29.5 m(96.78 ft)
L_MF_031700_1_0030102_01_00
Suggested Hangar ArrangementTail--in Position (Sheet 1)
3-17Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
10 m(32.80 ft)
10 m(32.80 ft)
10 m(32.80 ft)
100
m(3
28.0
8 ft)
10 m(32.80 ft)
93 m (305.11 ft)
L_MF_031700_1_0040102_01_00
Suggested Hangar ArrangementTail--in Position (Sheet 2)
3-17Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-18 Landing Gear Maintenance Pits
**ON A/C A380-800 Models A380-800F Models
Landing Gear Maintenance Pits
1. General
The maintenance pit envelopes for the landing gear shock absorber maintenance are shown in Figs.001 thru 004. The three envelopes show the minimum dimensions for these maintenance operations :- extension and retraction- gear removal- piston removal.All dimensions shown are minimum dimensions with zero clearances. The dimensions for the pits havebeen determined as follows :- The length and width of the pits allow the gear to rotate as the weight is taken off the landing
gear.- The landing gear is in the max. grown condition.- The WLG and BLG bogie beams are removed before the piston is removed.- The NLG wheels are removed before the piston is removed.- All pistons are removed vertically.Dimensions for elevators and associated mechanisms must be added to those in Figs 001 thru 003.
A. ElevatorsThese can be either mechanical or hydraulic. They are used to :
(1) Permit easy movement of persons and equipment around the landing gears.
(2) To lift remove landing gear assemblies out of the pits.
B. JackingThe airplane must be in position over the pits to put the gear on the elevators. Jacks must beinstalled and engaged with all the jacking points, Ref. Section 3-1 for airplane maintenancejacking. Jacks must support the total airplane weight, i.e. when the landing gears do not touchthe elevators on retraction/extension tests.When tripod support jacks are used the tripod-base circle radius must be limited because thelocations required for positioning the columns are close to the sides of the pits.
3-18Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
2 59
8
(102
.3)
5 62
5.5
(221
.5)
1 66
3
(65.
5)
FRONT OF NOSE RADOME
1 52
6
(60.
1) 763
(30)
NLG
EX
TE
NS
ION
/RE
TR
AC
TIO
N P
IT O
UT
LIN
E
FW
D J
AC
KIN
G P
OIN
T 33 6
59(1
325
.1)
AIR
CR
AF
T C
EN
TE
R L
INE
WLG
RE
MO
VA
L P
IT O
UT
LIN
E
WLG
PIS
TO
N R
EM
OV
AL
PIT
OU
TLI
NE
WLG
EX
TE
NS
ION
RE
TR
AC
T P
IT O
UT
LIN
E
WIN
G J
AC
KIN
G P
OIN
T
LH W
ING
SH
OW
N R
H S
IMIL
AR
BLG
EX
TE
NS
ION
RE
TR
AC
T P
IT O
UT
LIN
E
BLG
RE
MO
VA
L P
IT O
UT
LIN
E
BLG
PIS
TO
N R
EM
OV
AL
PIT
OU
TLI
NE
4 506
(177.4)
DIM
EN
SIO
NS
IN m
m(I
NC
HE
S IN
BR
AC
KE
TS
)M
INIM
UM
DIM
EN
SIO
NS
, ZE
RO
CLE
AR
AN
CE
S S
HO
WN
L_MF_031800_1_0010101_01_00
Maintenance PitsMaintenance Pit Envelopes
3-18Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
576
(22.
7)
709
(29.
9)
1 72
5(6
7.9)
804
(31.
7)1
127
(44.
4)
1 97
7
(77.
8)
802
(31.
6)
1 24
3(4
8.9)
1 98
9
(78.
3)
NLG EXTENSION/RETRACTION
NLG REMOVAL/INSTALLATION
NLG PISTON REMOVAL −INSTALLATION
WLG EXTENSION/RETRACTION
WLG PISTON REMOVAL −INSTALLATION
WLG REMOVAL/INSTALLATION
BLG REMOVAL/INSTALLATION
BLG PISTON REMOVAL/INSTALLATION
BLG EXTENSION/RETRACTION
DIMENSIONS IN mm(INCHES IN BRACKETS)
MINIMUM DIMENSIONS, ZERO CLEARANCES SHOWN
L_MF_031800_1_0020101_01_00
Maintenance PitsNecessary Depths
3-18Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
3 560(140.2)
513(20.2)
2 79
1(1
09.9
)
WLG
PIS
TO
N R
EM
OV
AL
PIT
OU
TLI
NE
972
(38.
3)
3 15
8(1
24.3
)
3 71
1(1
46.1
)
7 13
4(2
80.9
)
4 12
6(1
62.4
)
1 92
9(7
5.9)
1 490(58.7)
2 58
5(1
01.8
)
952(37.5)
2 368(93.2)
1 067(42)
6 228(245.2)
WLG
EX
TE
NS
ION
/RE
TR
AC
TIO
NP
IT O
UT
LIN
E
WLG
RE
MO
VA
LP
IT O
UT
LIN
E
BLG
EX
TE
NS
ION
/RE
TR
AC
TIO
NP
IT O
UT
LIN
E
AIR
CR
AF
T C
EN
TE
R L
INE
DIMENSIONS IN mm(INCHES IN BRACKETS)
MINIMUM DIMENSIONS, ZERO CLEARANCES SHOWN L_MF_031800_1_0030101_01_00
Maintenance PitsMaintenance Pit Envelopes - WLG Pit Dimensions
3-18Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
AIR
CR
AF
T C
EN
TE
R L
INE
1 68
0(6
6.1)
DIMENSIONS IN mm(INCHES IN BRACKETS)
1 025(40.4)
2 105(82.9)
1 490(58.6)
133
(5.2
)
4 85
6(1
91.2
)3
188
(125
.5)
7 13
4(2
80.9
)
1 168(46)
2 632(103.6)
BLG
PIS
TO
N R
EM
OV
AL
BLG
RE
MO
VA
LP
IT O
UT
LIN
E
WLG
RE
MO
VA
L A
ND
EX
TE
NS
ION
/RE
TR
AC
TIO
NP
IT O
UT
LIN
E
BLG
EX
TE
NS
ION
/RE
TR
AC
TIO
NP
IT O
UT
LIN
E
PIT
OU
TLI
NE
MINIMUM DIMENSIONS, ZERO CLEARANCES SHOWN L_MF_031800_1_0040101_01_01
Maintenance PitsMaintenance Pit Envelopes - BLG Pit Dimensions
3-18Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
3-19 Suggested Workstands
**ON A/C A380-800 Models A380-800F Models
Suggested Workstands
1. GeneralThe essential aspects that affect a decision to build a fixed dock or a movable dock are :- the fleet size of one type of aircraft,- the different types of aircraft in operation which demand the same hangar facilities,- the hangar facilities must comply for both light maintenance or major maintenance.It would appear logical to build a fixed dock facility where the fleet size of one type of aircraftprovides for an adequate workload. This therefore implies that the fixed dock is in use most of thetime.When the fleet size is small or adaptability is required, movable workstands are more economic andproficient. Movable workstands are a facility that can be used for different types of aircraft.Illustrations which show the movable workstands have been incorporated to help develop basefacilities.
Summary of Recommended Movable Workstands Aircraft on Wheels A380-800 Models
Item No. of Description Access to
1 4Cargo CompartmentPlatform
Cargo Compartments
2 4 Engine Platform Engine/Pylon/Radome Nose LandingGear
3 1WLG/BLG CompartmentPlatform
Wing and Body Landing GearCompartments
4 1 Rear Fuselage Platform Rear Fuselage
5 1 Hydraulic Platform-GiraffeVertical/Horizontal Stabilizer/APUCompartment/Fuselage
6 6Pax Door Platform -- Mainand Upper Decks
Passenger Doors/Cabin/Flight Deck
7 1 Fuselage Platform Fuselage
8 2 Inner Wing Platform Wing Root and Flap/Slat System
9/10 4 Outer Wing Platform Flap/Slat and Spoiler System
Summary of Recommended Movable Workstands Aircraft on Wheels A380-800F Models
Item No. of Description Access to
1 4 Cargo Compartment Platform Cargo Compartments
2 4 Engine Platform Engine/Pylon/Radome Nose LandingGear
3-19Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
Summary of Recommended Movable Workstands Aircraft on Wheels A380-800F Models
Item No. of Description Access to
3 1WLG/BLG CompartmentPlatform
Wing and Body Landing GearCompartments
4 1 Rear Fuselage Platform Rear Fuselage
5 1 Hydraulic Platform-GiraffeVertical/Horizontal Stabilizer/APUCompartment/Fuselage
6 6Pax Door Platform -- Mainand Upper Decks
Passenger Doors/Cabin/Flight Deck
7 1 Fuselage Platform Fuselage
8 2 Inner Wing Platform Wing Root and Flap/Slat System
9/10 4 Outer Wing Platform Flap/Slat and Spoiler System
3-19Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
6 14 66 1
66
6 6
6 5
5 6
66 7
6 65
32910 8 9 9
L_MF_031900_1_0010101_01_01
General Arrangement(Sheet 1)
3-19Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
1
1
5
5
4 17
61 56
1
1 6
32910 8 9 9
L_MF_031900_1_0020101_01_01
General Arrangement(Sheet 2)
3-19Page 4
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models
A
ASEE
CHAPTER1−9
L_MF_031900_1_0030101_01_00
Cargo Compartment Platform(Sheet 1)
3-19Page 5
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800F Models
A
A
EXAMPLE
FWD AND AFT CARGO DOORS
CARGO COMPARTMENT PLATFORM
EXAMPLE FOR MAIN DECK ANDUPPER DECK CARGO DOORS
A
SEECHAPTER
1−9
FWD FWD
L_MF_031900_1_0040101_01_00
Cargo Compartment Platform(Sheet 2)
3-19Page 6
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
ACCESS TO PYLONS AND ENGINES
A
A
EXAMPLEENGINE PLATFORM
SEE CHAPTER 1−9SEE CHAPTER 1−9
L_MF_031900_1_0050101_01_00
Engine Platform
3-19Page 7
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A
A
BLG/WLG COMPARTMENT PLATFORM
SEECHAPTER
1−9
L_MF_031900_1_0060101_01_00
WLG/BLG Compartment Platform
3-19Page 8
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
ADJUSTABLE STAIRS
A
A
REAR FUSELAGE PLATFORM
SEECHAPTER
1−9
L_MF_031900_1_0070101_01_00
Rear Fuselage Platform
3-19Page 9
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
(137.8 in)3500 mm
SEECHAPTER
1−9
L_MF_031900_1_0080101_01_00
Hydraulic Platform -- Giraffe
3-19Page 10
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
A B
BB
MAIN DECK UPPER DECK
EXAMPLE
A
2400 mm
900 mm(35.4 in)
1200 mm(47.2 in)(94.5 in)
SEECHAPTER
1−9
SEECHAPTER
1−9
A
L_MF_031900_1_0090101_01_00
Pax Door Platform -- Main and Upper Decks
3-19Page 11
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
(197 in)5 m 8 m
(315 in)
A
A
FUSELAGE PLATFORM
L_MF_031900_1_0100101_01_00
Fuselage Platform
3-19Page 12
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
INNER WING PLATFORM
A
9.17 m(361.02 in)
L_MF_031900_1_0110101_01_01
SEE CHAPTER1−9
A
Inner Wing Platform
3-19Page 13
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
**ON A/C A380-800 Models A380-800F Models
OUTER WING PLATFORM
TYPICAL
SEECHAPTER
1−9
SEECHAPTER
1−9
SEECHAPTER
1−9
6.95 m(273.62 in)
12.23 m(481.59 in)
A
B
A
BL_MF_031900_1_0120101_01_00
Outer Wing Platform
3-19Page 14
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
COMPONENT REPAIR/OVERHAUL AND FUNCTIONAL TEST
4-1 Batteries Shop
**ON A/C A380-800 Models A380-800F Models
Batteries Shop
1. GeneralThe workshops should be located as close as possible to the maintenance hangar. Certain supportshops are closely associated with on-aircraft maintenance.They should be designed to allow future extension of the Airline fleet and to accept test and repair ofcomponents coming from other Airlines. The capability and consequently the size of the shops willdepend on the level of on and off-aircraft maintenance that they support.They should be located in the same area and arrangement should consider the following:- Rapid transit between hangar floor, workshops and stores.- Minimal movement and minimal administrative tracking.- Bring aircraft maintenance activities and workshops services ″to the aircraft″.They could be divided/regrouped in three main activities:
A. Aircraft Maintenance- Interior equipment shop.- Life jacket, slide/raft equipment shop.- Metal shop.- Machine shop.- Composite repair shop.- Tube repair shop.- Electrical wire marking shop.
B. Aircraft Components and Engines
(1) Avionic- Battery shop.- VFG Generator shop.- Electrical accessories shop.- I.E.R.A. (Instrument, Electric, Radio and navigation, Avionic) shop.
(2) Hydro/mechanic- Engine and APU shop.- Fuel components shop.- Hydraulic components shop.- Pneumatic components shop.- Tire/wheel and brake shop.
C. Aircraft Support- Laboratory test of fluids/metallurgical.- Painting shop.- Surface and heat treatment shop.
4-1Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
They should be at different floor level e.g.: wheel and brake, machine tool, surface protection...at ground level, cabin interior, safety equipment... at first floor.Stores and offices should be air conditioned. Shop lighting should be 50 foot-candles (800lumens/m2) with a 100 foot-candle local task lighting for inspection or detailed work. Nondestructive test, composite repair, avionic shops and safety equipment shop should be equippedwith air moisture and temperature control device.
4-1Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-2 VFG Generator Shop
**ON A/C A380-800 Models A380-800F Models
VFG Generator Shop
1. GeneralThe shop is dedicated to overhaul, test and repair all components of electrical generation system.- VFG generator test stand- VFG governor test stand- Flushing cart VFG cooling system- Standard and specific adapters- Standard tools
4-2Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-3 Composite Repair Shop
**ON A/C A380-800 Models A380-800F Models
Composite Repair Shop
1. GeneralThe shop is dedicated to composite and fibreglass repair according to SRM procedures.- The room or surrounding temperature has to remain between 18˚C and 30˚C (64-86˚F) during
the repair.- The preparation area has to be dust cleaned (air filtration = 10 micron m) and dry.- The relative humidity has not to be greater than 75 %.- Condensation on the repair area has to be avoided.- Environmental data: temperature and humidity, have to be recorded.
2. Paint Removal/cleaning
A. Scraper
B. Cutter
C. Abrasive rotating disk
D. Abrasive paper
E. ″Scotch brite″ brown
F. Ethyl acetate
G. Demineralized water
H. Tweezers
3. Machining/specific Tooling
A. Polymerized material
(1) Fibreglass/carbon- Drills has or carbide- Diamante shark cutters: spot face cutter, rose countersink, cone countersink, circular
saw cutter...- Countersink micro stop 100˚ adjustable drive- Pneumatic drilling machine- Pneumatic router equipped with vacuum system- Specific adaptors.
(2) Kevlar- Specific twist cutter or alternate teeth carbide cutter- Cutter- Abrasive disk/paper.
(3) Honeycomb- Diamante shark cutter- Cutter
4-3Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
- Metal saw- Abrasive disk/paper- Adhesive tape double face
B. Prepreg/dry fabric
(1) Fibreglass/carbon- Scissors standard- Cutter- Templates
(2) Kevlar- Specific ceramic scissors
(3) GLARE
4. Standard Tools
A. Spatula
B. High precision weighing device
C. Squeegee
D. Containers (for resin)
E. Glass rods
F. Plastic film
G. Bottles
H. Spring pin type clamps
J. Clamp
K. Adhesive tape
L. Syringe with hypodermic needle
M. Gloves (rubber and cotton)
N. Mask
P. Pair of glasses
Q. Sanding block
R. White ink ″rotring″S. Riveting machine for blind rivets
5. Heating and Pressure Equipment
A. Hot bonding and vacuum control unit
B. Heating blankets
C. Anti humidity heat blankets or radiant panels
4-3Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
D. Nylon vacuum bag films (3 grades)
E. Breather fabrics
F. Peel/bleed fabric
G. Shrink tapes
H. Perforated plastic film I. Mosite J. Sealant tape
J. Oven L. Autoclave (1 m dia x 2.5 m)*
6. Test Equipment
A. Ultra sonic test equipment
B. Tool for tap test
C. Compression/traction and peeling testers**
D. Lamp
E. Inspection mirror
4-3Page 3
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-4 Electrical Accessories Shop
**ON A/C A380-800 Models A380-800F Models
Electrical Accessories Shop
1. GeneralThe shop is dedicated to the overhaul, test and repair of all aircraft electrical accessories.
A. General test stand ac/dc power requirements
B. Amplifier control test
C. Test stand for lights
D. Test stand coffee makers and refrigerators
E. Functional test stand for linear actuators and control dampers
F. Functional test stand for rotary actuators
G. Test set static inverters
4-4Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-5 Electrical Wire Marking Shop
**ON A/C A380-800 Models A380-800F Models
Electrical Wire Marking Shop
1. GeneralDedicated to mark the electrical wires used for electrical harnesses repair.The wires authorized for use on Airbus aircraft are those listed in AWM/AWL Chapter 20-41. Ingeneral Airbus have nickel plated cores and American spec. wires have tin plated cores. We do notuse extruded x- linked Tefzel insulation (e.g. Raychem 55) for Airbus general airframe wires (exceptin specific areas like the U/C).- U.V. laser machine
or- Co2 laser machine
NOTE : ink-jet system is not generally used for Airbus aircraft.Airbus wire are marked with either UV laser or CO2 laser technology depending on the origin of theharness but CO2 may be phased out in the future with all wires being marked with UV laser. It wouldappear that UV laser technology is being accepted as the industry standard internationally.CO2 markable wire cannot be UV laser marked and vice versa.
4-5Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-6 Engine and APU Shop
**ON A/C A380-800 Models A380-800F Models
Engine and APU Shop
1. GeneralThe shop is dedicated to disassembly/assembly (modules exchange) and repair engines and APU.
A. Overhead cranes
B. Press
C. Standard hand tools
D. Balancing machine: static and dynamic balance
E. Grinding machine
F. Plasma spray and welding machines
4-6Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-7 Fuel Component Shop
**ON A/C A380-800 Models A380-800F Models
Fuel Component Shop
1. GeneralThe shop is dedicated to overhaul, test and repair all fuel system components.
A. Universal main engine fuel control/accessories test stand
B. Test stand
(1) Fuel boost
(2) Fuel pump
C. Standard adapters and tools
D. Low flow fuel accessory test stand
4-7Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-8 Hydraulic Component Shop
**ON A/C A380-800 Models A380-800F Models
Hydraulic Component Shop
1. GeneralThe shop is dedicated to test bench capabilities for hydraulic fluids-Working and static tests-Overhaul, inspection and component replacement of most hydraulic actuators and accumulators.
A. Hydraulic generation and accessory test bench
B. Pump hydraulic test stand
C. Servo valves and actuators test stand
D. Standard adapters and tools
4-8Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-9 I.E.R.A. Shop
**ON A/C A380-800 Models A380-800F Models
I.E.R.A. Shop
1. GeneralThe I.E.R.A. shop is dedicated to the overhaul and repair of all Instruments, Electric components,Radio and Avionic equipments.
A. Test bench radio
B. Test bench VOR/ILS
C. Test bench dme
D. Test bench adf
E. Test bench SATCOM
F. Test bench Weather Radar
G. Automatic Test Equipment
H. Dedicated test equipment
J. Personal computers
K. Oscilloscopes
L. Arinc reader/generators
M. Magnetic tapes/disc/cassettes eraser (TBC)
N. Data loaders
4-9Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-10 Interior Equipment Shop
**ON A/C A380-800 Models A380-800F Models
Interior Equipment Shop
1. GeneralThe shop is dedicated to carpet, seats and cabin panels and partitions repair and fabrication.
A. Cabin Interior
(1) Drilling machine
(2) Painting booth
(3) Washing booth
(4) Vaccum cleaner
(5) Binding machine
(6) Engraving machine
(7) Sewing machine
(8) Press, heat/vacuum pressure equipment
(9) Polishing windows machine
(10) Shear bench
(11) Oven
(12) Freezer
(13) Hand grinder
(14) Circular saw
(15) Sander belt
(16) Kevlar driller
(17) Cutting tools
(18) Work bench
(19) Standard hand tools.
B. Seats
(1) Sewing machine
(2) Drilling machine
(3) Bending machine
(4) Grinding wheel
(5) Belt grinder
(6) Circular saw
4-10Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
(7) Riveting gun
(8) Riveting block
(9) Work bench
(10) Standard hand tools.No special tools or specific equipment are required for maintenance or overhaul work to becarried out on the passenger seats. Standard tools are sufficient for these operations.In addition to standard tools, only few specific tools or equipment are required formaintenance and overhaul work to be carried out on the pilot seats. (Refer to relevantCMM)
4-10Page 2
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-11 Laboratory Test of Fluids
**ON A/C A380-800 Models A380-800F Models
Laboratory Test of Fluids
1. GeneralThe laboratory is dedicated to analyse all fluids used on aircraft.
A. Hydraulic fluid - fire resistant - phosphoric ester basedReference documents
(1) NSA307110
(2) AMM A380
(3) CHAPTER 12.32.28
(4) SAE ARP 598
(5) SAE ARP 785
(6) NF T 60-100
(7) NF T 60-101
(8) NF T 60-112 (ASTM D974)
(9) NF T 20-052 (ASTM D1744)
(10) NAS 1638
B. The values below represent the max. Allowable limits of the fluid in service. These limits are alsospecified in the aircraft maintenance manual.
(1) Viscosity
(2) Water content
(3) Density . Acidity
(4) Chlorine content
(5) Conductivity
(6) Particles fluid contamination
4-11Page 1
Oct 01/09
@A380MAINTENANCE FACILITY PLANNING
4-12 Metal Shop
**ON A/C A380-800 Models A380-800F Models
Metal Shop
1. GeneralFabrication of all metallic parts involving milling boring and turning. All welding processes for allaircraft metals and alloys.
A. Universal lathe 1.5 x 2 x 2
B. Milling machine 1.6 x 0.4
C. Boring machine 0.75 x 0.75 x 0.6
D. Centerless grinding machine
E. Cylindrical grinding machine
F. Universal drilling machine
G. Radial drilling machine
H. Grinders
J. Circular saws
K. Hydraulic press (3 t)
L. Drilling machines set
M. Standard hand tools set
N. Benches
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4-13 Painting Shop
**ON A/C A380-800 Models A380-800F Models
Painting Shop
1. GeneralThe shop is dedicated for painting aircraft parts and components.
A. Surface treatment rooms- Sand blasting- Washing- Decreasing- Phosphating cleaning- Drying
B. PaintingClosed spray booth with downdraft ventilation- With multiple wording zones in line- With ventilation zones- With drying device + oven- Open booth with dry filter- Open ″waterscreen″ spray booth- Painting guns- Air compressed sources- Special room for product storage- Special room for paint preparation- Safety equipment: masks, gloves, gas detectors, fire extinguishers.
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4-14 Pneumatic Component Shop
**ON A/C A380-800 Models A380-800F Models
Pneumatic Component Shop
1. GeneralThe shop is dedicate to overhaul, test and repair all pneumatic components.Workshop test conditions:Atmospheric ambient pressure : TBDAmbient temperature : TBDRelative ambient humidity : TBDDust : normal protection (conventional dust cleaning at regular intervals)Air source :Capable of supplying clean, dry : CONTACT RELATED VENDORS FOR SPECIFICATIONS
NOTE : Hot air source: TBD.
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4-15 Life Jacket, Escape Slide / Raft Shop
**ON A/C A380-800 Models A380-800F Models
Life Jacket, Escape Slide / Raft Shop
1. GeneralThe shop is dedicated to the periodic tests and repair of the on-board safety devices.THE SHOP AREA MUST BE CLEAN AND COVERED WITH A TARPAULIN, CARPETING OROTHER PROTECTIVE COVERING. DO NOT WALK ON THE EQUIPMENT. USE SPECIFICSHOES.
A. Cleaning
(1) Moderate duty : simple liquid detergent
(2) Heavy duty : toluene (C6H5CH3) and isopropyl alcohol (according to vendor equipmentspec.)
(3) Dry cleaning solvent for metal parts
(4) Stiff bristle brush
(5) Soft bristle brush
(6) Brush paint
(7) Gloves - Rubber
B. Testing
(1) Compressed air source (oil and moisture free, 20 micron filter) with pressure regulator.
(2) Leak test solution, Ivory clear, Mild liquid detergent.
(3) Soft bristle brush.
(4) Barometer, Scale increments not more than 0.10 inches.
(5) Thermometer, Scale increments not more than 1˚.
(6) Push/pull gage 0-50 lbs O.5 Lbs graduations.
(7) Stopwatch, plain timer, 1/10 Seconds graduations.
(8) Manometer (water). 0-0.5 psi.
(9) Manometer (meriam fluid). 0-6.4 psig. (0.01 graduation).
(10) Manometer (digital pressure). 0-20 psi.
(11) Test set slide raft batteries.
(12) Tester inertia reels.
(13) Weighing devices for bottles and cylinders.
C. Disassembly/assembly/repair
(1) Neoprene strap
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(2) Cotton clothes
(3) Scour cloth
(4) Talc or powdered soapstone
(5) Sealer heat poly bags
(6) Wrench open end set
(7) Crowfoot wrench set
(8) Hex key set
(9) Torque wrench. 0-80 in.Lb
(10) Strap wrench
(11) Crescent pliers
(12) Scissors
(13) 5 inch blunt nose, plated
(14) Spatula (pusher)
(15) Hand roller
(16) Vacuum cleaner. Household type
(17) Chain vise
(18) High pressure cap (AN929-4)
(19) Cap filler valve (MS20813-1)
(20) Valve core extraction/insertion tools (Specific. Vendor equipment items)
(21) O-ring installation tools (specific. Vendor equipment items)
(22) Heat gun
(23) Fixture check maximum envelope
(24) Sewing machine
D. Ingredients
(1) Refer to vendor equipment recommendation.
E. Reconditioning
(1) Refer to reconditioning method described in relevant CMM.
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4-16 Surface Heat Treatment Shop
**ON A/C A380-800 Models A380-800F Models
Surface Heat Treatment Shop
1. GeneralThis shop is dedicated to surface and heat treatment.
A. Surface TreatmentChemical cleaning baths
(1) Acid
(2) Alkaline descaler
(3) Alkaline permanganate
(4) Caustic cleaner
(5) Corrosion inhibitor
(6) EmulsionHot water rinse bathCold water rinse bathChemical plating bath
(7) Cadmium
(8) Nickel
(9) Chromium
(10) Salt nitriding
(11) Alodine
(12) Chromate
(13) Phosphating
(14) Passivation
(15) Sulphuric/chromic acid anodisinShot peening equipmentSand blasting
B. Heat TreatmentOvenBathsFreezerStandard toolsLiquid effluent decontamination systemExtracted effluvium washing system.
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4-17 Tube Repair Shop
**ON A/C A380-800 Models A380-800F Models
Tube Repair Shop
1. Rigid tubes
A. Bending machineBending machines with internal mandrels shall be used. For each nominal diameter there mustbe several mandrels. For titanium pipes it is recommended to use plastic mandrels.
B. Tube end forming device
C. Cutting, facing and deburingStandard hacksaw, band saw, circular saw and conical milling cutter can be used.
D. Cleaning and degreasingStandard equipment: compressed air, perchloroethylene vapour bath....
E. Test equipment
(1) Pressure testStandard pressure test bench with capacity of TBD min. (Pressure test with gas and withliquid).
(2) Dimensions and shape checkStandard equipment + master, template....
F. Tube repair equipmentRefer to AMM chapter 20-23-11 for permaswage repair kit and harrison/sierracin fittingsinstallation.
2. Flexible hosesDue to very specific equipment necessary to manufacture or repair flexible hoses it is suggested tocontact directly the vendors mentioned hereafter.
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4-18 Tire/Wheel and Brake Shop
**ON A/C A380-800 Models A380-800F Models
Tire/Wheel and Brake Shop
1. 1. Tire Shop
A. Nitrogen bottles
B. Pressure gauge
C. Inflating gauge
D. Inflating/deflating adapters
E. Safety cage for tire pressure tests
F. Storage racks
2. Wheel Shop″Dirty″ work on wheel overhaul consists of disassembly of the wheel and rim-cleaning. Cleaning canbe done manually: hot water high pressure washing device, combined with semi-automatic devices:solvent baths including treatment bath + rinsing bath + drying bath or with a ″tunnel″ typemachine. Cleaning of small parts like bearings or bolts can be done using an ultrasonic washingmodule or a vertical agitation and total turbulence machine.″Clean″ procedures for wheels start NDT for crack detection. Eddy Current and ultrasonic testingdevices can be used for this purpose.
NOTE : Complete process of wheel cleaning may include paint stripping which can be done usingmedia plastic blasting equipment or solvent baths.
A. Standard equipment
(1) Tire bead breaker universal
(2) High pressure washing device and
(3) Ultrasonic bath or vertical agitation machine for wheel bearing cleaning
(4) Hydraulic press
(5) Hand tool set
(6) Torque wrench
(7) Wheel support
(8) Trolley crane
B. Specific toolsAccording to the relevant CMM.
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3. Brake shop″Dirty″ work on brake overhaul includes disassembly and cleaning of the brake. An intensive cleaningis necessary to avoid damages of the piston bearing, as the remaining dirt can create a leak when thepistons are repressed.″Clean″ procedures follow after the brakes has been visually inspected. Cleaning can be done usingultrasonic bath or vertical agitation and total turbulence machine.The brake pistons are returned to their original position. When it has been accomplished, test for leakare performed.
A. Standard equipment
(1) Bath solvent cleaning
(2) Trolley crane
(3) Hydraulic test bench (315 bars)
(4) Dummy body for functioning test
(5) Tester brake unit spring tension
(6) Press for resetting the brake piston to the zero, position
(7) Hardness test machine.Carbon brake disk repairSubcontracted to specialized repair centre
B. Specific toolsAccording to the relevant CMM.
4. StorageAircraft tire storage conditions are determined by the tire manufacturers. There is no Airbusdocument dealing with this subject.Tires should be stored in a cool, dry environment and protected from direct sunlight. Particular careshould be taken to store tires away from fluorescent lights, electrical motor, battery chargers, electricwelding equipment, electric generator since they all create ozone which cause a rapid ageing ofrubber.The store room temperature should be comprised between 0 and 40˚C. Tires should be storevertically in a suitable rack, away from oil, grease, hydraulic fluid or other contaminants.
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VENDORS LIST
5-1 Vendors Information
**ON A/C A380-800 Models A380-800F Models
General
1. VENDORS INFORMATIONThe vendors information is contained in the Vendors Information Manual (VIM) and in the VendorsInformation Manual/Ground Support Equipment (VIM/GSE).The Vendor Information Manual (VIM) gives contact names and addresses of AIRBUS equipmentvendors and their product support organizations. This manual covers all aircraft types.In addition the VIM/GSE gives contact names and addresses of Ground Support Equipment Vendorswhich fabricate market facilities or maintenance equipment to test or to overhaul the aircraft. Itcontains also the Vendors product support organizations. This manual covers all aircraft types.
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