AIRBUS - SmartCockpit

1 STL Issue 4 AIRBUSA330 Flight deck and systemsbriefing for pilotsTHIS BROCHURE IS PROVIDEDFOR INFORMATION PURPOSES ONLYAND ITS CONTENTSWILL NOT BE MUST NOT BE USED AS AN OFFICIAL TECHNICAL DATA OR OPERATIONAL PROCEDURES,PLEASE REFER TO THERELEVANT AIRBUS DOCUMENTATIONM arch 1999 STL issue 4 STL Issue 4 STL Issue Flight deck layout3. Electrical system4. Hydraulic system5. Flight controls6. Landing gear7. Fuel system8. Engine controls9. Auxiliary power unit10.

2 Automatic flight system11. Environmental control system12. Electronic instrument system13. Radio management and communication14. Central Maintenance Issue 4 STL Issue 41. Issue 4A330 m191ft m83ft m208ft cabinzTrue widebodyspaciousness andadaptabilityLower cargo holdszLarge, efficient, fullycompatible with existingworldwide air general cabin layout256 seatsA330-20018 sleeperette(62 in pitch)42 Business(40 in pitch)196 Economy(32 in pitch)295 seatsA330-30018 sleeperette(62 in pitch)49 Business(40 in pitch)228 Economy(32 in pitch)

3 A330 fuselage cross-sectionSTL Issue 4A330 General The medium to long-range A330 is an all-new, wide-body, twin-engine, twin-aisle aircraft. The design combines high technology developed for the A320 and A340 with the wide experience gained from the A300 and A310 aircraft currently in world-wide two-man crew operation with CRT displays- electrically signalled flight controls- sidestick controllers- full authority digital engine control (FADEC)- centralized maintenance system. Since it s introduction in December 1993 the aircraft is the most advanced medium to long-range airliner offering a major stride forward in airline profitability.

4 Certification basis includes :- JAR 25 at change 13- JAR AWO at change 1 for CAT II and CAT III and ICAO annex 16 chapter 3 for noise. MTOW*MLWMZFWMax fuel capacityMax operating altitudePowerplantsDesign speedsVmo/MmoUnderfloor cargo230 000 kg180 000 kg168 000 kg139 090 lit41 100 ftGE CF6-80E1A470 000 lbRR Trent 77271 100 lbPW 416868 000 lb330 kt 27LD3 to 3LD3 + 8 pallets+ bulk m3217 000 kg179 000 kg169 000 kg97 170lit41 100 ftGE CF6-80E1A267 500 lbRR Trent 768 / 77267 500 lb / 71 100 lbPW 4164 / 416864 000 lb / 68 000 lb330 kt pallets+ bulk m3A330-300A330-200* Max ramp weight 900 kg higher than MTOWB asic with the A319, A320.

5 A321 and A340, it will incorporate all of the following features :STL Issue 4A330 design specifications1. Design weights (see page )2. Design speedsVMO= 330 kt CASMMO= 365 kt CASMD= 260 kt CASMB= (landing gear) extensionretractionVLE(Landing gear extended)3. Slat and flap design speeds250 kt CAS01123 FullClimb/cruise/holdingHoldingTake-offA pproachTake-offTake-off/approachLanding0 11 + F1* speedVFEkt (CAS)4. Structural life (design aims)The objectives for primary structure fatigue life are as follows based on average block time of 4 hours :- design life goal.

6 20000 flights- threshold for initial inspection .. 8 750 flights5. Landing gearThe design aim is 25000 cycles safe life operation in accordance with FAR and Cabin pressureMax nominal operationaldifferential pressureActuating cabin pressureof discharge valveMax relief valve overpressureMax negative differentialpressure574 mb 7 mb610 mb 7 mb638 mb-70 psi psi psiSTL Issue 4A330 GeneralAircraft design specifications11 09511 0959649641 64610 98036 7458. Pavement strengthMax ramp weight and max aft A6156 Cat B6661 Cat C7771 Cat D10595 Cat A5248 Cat B6155 Cat C7365 Cat D8576 Rigid pavementFlexible pavementACNT yres radial- main gear 1400 mm x 530 mm x R23- nose gear 1050 mm x 395 mm x tank LHInner tank RHOuter tank LHOuter tank RHCenter tankTrim tankTotal42 00042 0003 6503 6506 23041 560139 090 LitresUS gallonsLitresUS gallons7.

7 Fuel capacityA330-300A330-20041 90441 9043 6243 6246 230-97 28611 07011 0709579571 646-25 700 STL Issue 4A330 GeneralWeight and balanceA330-200 CG limitsA330-300 CG Issue 4A330 turning radiusTowingThe A330 can be towed or pushed up to a nosewheel angle of 78 from the aircraft centre line at all weights up to maximum ramp weight without disconnecting the turning radii (with tyre slip) and minimum pavement width for 180 turn are as (Feet) (Feet) of turn 2 Effective turn Type of turn 1 Effective turn angle78 X = m / ftType of turn 1 : Asymmetric thrust differential braking (pivoting on one main gear)Type of turn 2 : Symmetric thrust no brakingA330-200X = m / ftYAR3R4R5R6(Feet) (Feet) of turn 2 Effective turn Type of turn 1 Effective turn maneuvre capabilityR6 Outside face of tireMin.

8 Turning width for 180 turnEffective turn angle10,684mAYR4R5R3 STL Issue 4 STL Issue 42. Flight deck Issue 4A330 flight deck As the A330 is a medium long-range aircraft the cockpit offers full provision for a 3rd occupant seat as well as a folding 4th occupant provisionsCaptain's sidestickSliding window(Emergencyevacuation)Captain's seatCaptain's briefcaseDocumentationstowageCoat room/suitcasestowageRear consoleFourthoccupant seatThird occupantseatFirst officer'sbriefcaseFirst officer'sseatSliding window(Emergency evacuation)

9 First officer's sidestickSTL Issue 4A330 flight deck layoutForward outletAssist handle Ceiling lightSliding tablesFO boomset stowageFO boomset jack panelReading lightWindow controlhandleLoudspeakersNose wheelsteering CTLC hecklist stowageOxygen maskAir conditioningoutletWaste binNormal checkliststorageBriefcase stowageWindow outletsFlash lightChecklist stowageFlight documentsstowageWaste binOxygen maskRoller sunblindAshtrayHand microphoneSidestickEscape rope stowageSTL Issue 4A330 flight deck view : right aft cornerRear view : left aft corner RAIN REPELLENT BOTTLE(OPTION)OXY MASKLIFE VEST3rdOCCUPANTCONSOLEOXY MASKLIFE VESTJACK PANELHEADSETBOOMSET4th OCCUPANTCONSOLEAXESTL Issue 4A330 flight deck layoutVisibility Windows are designed to meet or exceed the Aerospace standard.

10 Geometry :- windshield panels : flat glass- lateral windows: curved vision 130 120 110 100 90 80 70 60 50 40 30 20 100 10 20 30 40 50 50 403020100 102030 Wingtip visiblePilot s axisDownward visibility in the pilot axis : 20 Aerospace standard 580 BBinocular visionPilots field of visionSTL Issue 4A330 flight deck field of visionPilot s eye position25 19 20 7ft aft visionwith head rotatedabout spinal column111 135 115 135 Pilot s eye position62 42 30 36 42 62 30 36 1ft headmoved 5 inchesoutboardSTL Issue 4A330 flight deck field of vision - landingconfiguration CAT II DH = 100 ft This geometry improves external aircraft monitoring, thereby increasing safety Downward visibility in the pilot axis is 20.