1

L’A380 pour Air France

2

A3XX / A3XX-F

79.8 m

73 m

24.1 m

SPAN

LENGTH

HEIGHT

A3XX dimensionsA3XX dimensions

3

Caractéristiques de Caractéristiques de l’A380l’A380

277 t / 293.1 t *

38 LD3s or 13 palettes 18 LD3s* and 5 palettes*

8,000 nm / 6700 nm*560 t

302 kN

A380

386 t361 t

84 t / 67.9 t *310 000 l

OWE (masse de base)

Capacité fret

Rayon d’action (max pax)

MDTOWMLWMZFW

Charge marchande Capacité carburantPoussée moteur (slst)

Capacité passager

* Configuration Air France

555/559*

4

Rayon d’action autour de Rayon d’action autour de Paris A380/GP7200Paris A380/GP7200

CDG

LAX

BKK

NRT

HKG

SIN

Rayon d’action avec charge marchande maximale passager (559pax) 548t/560t: 6398nm/6731nmVents les plus défavorables- probabilité annuelle de 85%ISAMarge de 3% sur le rayon d’action

5

L’ économie de l’ L’ économie de l’ avionavion

Ref :747-400, 416 sièges,

Prix catalogue : 180 m$ 2000

A380-800, 555 sièges,

Prix catalogue: 216 m$ 2000

Prix/siègeCoût direct

d'opération/siège*

L’A380 : un avion économiquement attractif

-10%-13.5%

Coût carburant /siège*

-15%

*Comparaison basée sur un secteur de 6000 nm - coûts d ’opération standards Airbus

Nose Fuselage DimensionsNose Fuselage Dimensions

A380A340

A320

7

Plus grand dehors Plus grand dehors

Plus grand dedans

L’A380 : capacité et espace

747-400747-400 +35 % de capacité supplémentaire+35 % de capacité supplémentaire 2 cabines distinctes (ponts principal 2 cabines distinctes (ponts principal

et supérieur)et supérieur)

Un confort et Un confort et

flexibilité grâce à deux flexibilité grâce à deux

très larges cabinestrès larges cabines

160’’160’’

241’’241’’

233’’Fuselage large

259’’Fuselage large

8

La réponse A380La réponse A380

DU CONFORT POUR DU CONFORT POUR

LE PASSAGER LE PASSAGER

… … ET DE LA CAPACITE ET DE LA CAPACITE

CARGOCARGO

De 4 à 9 de frontDe 4 à 9 de front

De 4 à 11 de frontDe 4 à 11 de front

Poste de repos Poste de repos et toilettes en soutes et toilettes en soutes optionnelsoptionnels

PalettesPalettes

2 palettes2 palettes

LD3s et/ou palettesLD3s et/ou palettes

9

Configuration A380 Air France :559 sièges

Pont supérieur

Pont principal

16 P, pas 82”

78J, pas 48”

330 Y, pas 31”

135 Y, pas 31”

AFR923 up

AFR923main

10

Les prochaines étapes du programme

Jan.Jan.9999

DurantDurant20002000

Gel de laGel de la ConfigurationConfiguration

Gel de laGel de la ConfigurationConfiguration

AutorisationAutorisationcommercialecommercialeAutorisationAutorisationcommercialecommerciale

Clients Clients de lancementde lancement

Clients Clients de lancementde lancement

MiMi20002000

MiMi20042004

Premier Premier volvol

Premier Premier volvol

DébutDébut20062006

Mise en Mise en serviceservice

Mise en Mise en serviceservice

FinFin20012001

Définition Définition terminéeterminée

Définition Définition terminéeterminée

11

Principales Principales innovationsinnovations

•2 Packs ( BP et HP )

•PA intégré au CDV

•Génération électrique : fréquence variable.

•CDV : concept EHA et EBHA

•Fuel : optimisation du CG de l’ avion lors du remplissage.

•Hydraulique : 5000 Psi.

•LDG : 22 roues / aide au management de configuration.

•Oxygéne : Systéme OBOGS ?

•OIS / OMS : avion communicant / informations embarquées…..

•Station de maintenance : face au pylone + possibilité d’ interrogation à distance par terminaux sans fil.

•Structures : CFRP / Glare

•Portes : électriques

•Moteurs : surveillance enrichie ( analyse des gaz en sortie ….. )

12

2 multi-functions keyboards2 multi-functions keyboards

8 identical potentially interactive displays8 identical potentially interactive displays

Control and Display SystemControl and Display System

2 multi-functionsCursor Control Devices

2 multi-functionsCursor Control Devices

13

Maintenance Maintenance station station

14

To be examined in the mock-up To be examined in the mock-up

Rear Fuselage

Same ladder in different positions

16

Air Air Generation Generation pack concept pack concept - redundancy- redundancy

3 3 3 3+3* 4 2 4 4+2* *for HX-mode

ConventionalTechnology

AdvancedTechnology

FCV RHX RDA ACM

BPV

FCV RHX RDA ACM

BPV

FCV RHX RDA ACM

BPV

RHXHP -ACM

BPV

LP -ACM

RHXHP -ACM

BPV

LP -ACM

No. of Components

RDA

RDA

RDA

RDA

FCV1

FCV2

FCV1

FCV2

Components:FCV: Flow Control ValveRHX: Ram Heat ExchangerRDA: Ram Door ActuatorBPV: Bypass ValveACM: Air Cycle Machine

Conventional: Most single failures result in loss of complete pack.Advanced: No cooling degradation due to most single failures.

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115 V AC network confirmed

Suppliers involved• TRW-LUCAS : 120 KVA variable

frequency generator on test. • HONEYWELL-ALLIED : 150 kVA

generator in lab. in Feb 2001• HAMILTON SUNDSTRAND:

150 kVA gen. in lab. in Feb 2001

Network characterization under process

with EUROCAE and RTCA (DO160 update)

Variable frequency network Variable frequency network Objectives :• Significant improvement of the ATA24 DMC and operational reliability• Reduction of the aircraft systems DMC• Re-open industrial competition

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AC1 AC2 AC4AC3

Galley3Galley 2Galley1 Galley4

Engine 1 Engine 2 Engine 3 Engine 4APU

<<Ext 1 <<Ext 2 Ext 3>> Ext 4>>

AC network general AC network general architecturearchitecture

4x90kVA ext. connections

4x150kVA VFG

2x120kVACF gen

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•Gauging technology under evaluation•Refueling procedure under review with the airlines

Fuel system provides

Protection of fuel volume following

engine rotor failure (FAR 25.903(d)(1))

Provision of wing bending relief and CG

management

Embodiment of TWA800 accident

recommendations

Fuel SystemFuel System

Trim Tank

Aft CenterTank

Outer Engine

Feed Tank

Outer Transfer Tank

Inner EngineFeed Tank

Vent Tanks

Inner TransferTank

Aft center tank- 42 400 litres (-800 R and -900 only)Inner feed Tank - 28500 litresInner Transfer Tank - 84400 litresOuter Eng Feed Tank - 28400 litresOuter Transfer Tank - 10600 litresTrim tank - 24 000 litres

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Increased hydraulic pressure 5000 psi

Trade-off study (PDR)

Hydraulic fluid analysis

Initial actions

Review with the airlines - system workshop 26/28 Oct 1999

Kick-off (1998) :current experiencepotential show stopperscriteria for trade-offaction list

Final decision : 8 November 1999+ follow-up actions

Airline questionnaire2 Hyd. benches for enduranceDefinition of standardsAdditional benches in suppliers

• System weight : - 1200 kg• Feasibility confirmed

• Technical risk on Hydraulic system reduced

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2H/2E 2H/2E Architecture Architecture SchematicSchematic

Body Gear Brakes

1, 3, 5, 7 (L &R)

Upper & Lower

LIB & RIB

Flaps

Body Gears

Body Gears

Yellow System

PMF

EDP EDP EDP EDP

Alt. Ener

Pitch trim 2PMV

EMP

Eng. 3 Eng. 4

L & R i/b & o/b

PV

Eng. 1

AileronsSpoilersRudderElevatorsTHSSlats/Flaps

Gear actuationSteering

Braking

EDP EDP

L & R o/b & m/b

2, 4, 6, 8 (L&R)

Upper & Lower

LOB & ROB

Pitch trim 1

Slats Flaps

Nose & Wing

Nose

Wing Gear Brakes

Green System

PV

PMV

PMF

EDP EDP

T/REMP

Eng. 2

Alt. Ener

Alt. Ener

Electric System 1 Electric System 2

RAT

6 (L & R)

Upper & Lower

LIB & RIB

Pitch trim

Slats

4 (L & R)

Upper & Lower

LOB & ROB

L & R i/b L & R o/b

Eng. 2 T/R Eng. 3 T/R

Gen

Gen Gen

APUGen

Isolation GenGen Gen Gen

22F

ram

e 1

0

Fra

me

11

Fra

me

12

STATUS 14STATUS 14

100

15

0

STATUS 11STATUS 11

Nose gear & fuselage studies

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Main Gear Group

560t & 590t MTOW

growth

• 4 post main gear group for 560 & 590 t• 4 wheel Wing gear

• 6 wheel Body gear

• 5 post main gear group for growth

• bay gives extra cargo volume with good central fuselage structure

• compatible with pavement loading (being demonstrated by PEP)

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AFDX Ethernet Network

Ethernetnetwork

Avionics for A380Avionics for A380

fuel&LG

Cabin

energy

FCGCFCSC SFCC

Flightcontrol

ADIRU MMR

R/A

FADEC

ACAS, TAWS, W/R

FWFCDC

Avionicsserver

CVR, DFDR

IOM

HFDR, VDR, SATCOM

SELCAL, RAMP, AMU...

OMT AWLU

WACSSATCOMLEO/MEO

connectors

NCR

Utilities

GCUAPUGCU

ELMCBMHSyM

PHCECMFQI/FuM

FQI/FuM

LGBCSCTP

LGBCSCTP

IRDCLG

CockpitFM ATC

cockpit

Sensors

.

..Air Gene-

ration /Temp

Contr .

CabinPressure /VentalationContr .

Air Gener.Temp ctl

Bleed mon.Overheat detect.

..

Cabin PressureVentil. Ctl

Avioncs cooling.

VOR DME

Engines

Ctrl & Displays

std by

AFDX network

Ethernet network

Radio comm.

Recorders

SurveillanceACRSCI

TACS : cameras, video switches

ACMFFDIF

WHC

.

.

Cabin Intercom Data -CIDS

Smoke detect.Water/waste ctl

. .

.

LRU Cabin server

IFE

• Charts and Maps• Weather• Electronic Library• Electronic log book

IFE

Passenger Terminals

• FMS Nav Data Base• Operational S/W

Loading• Fault Correction Guide• Quick Access Recorder

FS Router

Gate Link

Crew Station

Flight Deck Info Cabin Services Maintenance Apps• Direct TV• Internet

IFE• Passenger Manifest• Consumables Tracking• Financial Transactions• Cabin Logbook, Checklist

On Board Information On Board Information

VHF

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A3XX Onboard A3XX Onboard Maintenance System Maintenance System

conceptconcept

BITEA/C Systems and engines

Ops.data

Maintenance Electronic

documentation

Consultation

Link

Recording PrintingUplink

Downlink

TerminalsCockpit, cabin, Portable

Onboard Information Network

Control, reporting display, customisation programming

Centralized Maintenance

Aircraft Condition Monitoring

Data Loading

Fault acquisitionTests activation

Acquisition and processing

S/W and data bases loading

27

A3XX Scenario for A3XX Scenario for Advanced MaterialsAdvanced Materials

Upper Fuselage Panels:Fibre Laminates (GLARE)

Upper Floor Beams:CFRP for Pax version,Aluminium for freighter version

Center Wing Box:CFRP Fixed Wing Leading Edge:

Thermoplastic J-Nose

Rear Pressure Bulkhead:CFRP

Empennage:CFRP

Outer Wing:Metal bonded

Lower Fuselage Panels:Laser Beam Welded aluminium alloys

Wing Panels:Advanced aluminium alloys