Take Off and landing: better then 747-400 ○ Altitude The “Airbus Cockpit Philosophy”, results of customers feed-back, •camera/video, taxiing aids
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A380: Challenges for the FutureA380: Challenges for the Future
Capt. Jacques DRAPPIER
Senior Director Training Programmes
The A380 : Flagship of the 21st Century The A380 : Flagship of the 21st CenturyLaunch Variants
Launch Variants
A380555 seats
8,000 nm
14,800 km
EIS 1Q06
Launch
variantLaunch
variant 150 t330,000 lb
5,600 nm
10,400 km
EIS 2Q08
A380-F
A380 general arrangementA380 general arrangement
The 80x80m box compliance for better airport integration The 80x80m box compliance for better airport integrationA380-800 / A380-800F
261 ft 10 in / 79.8 m
239 ft 6 in / 73.0 m
79 ft 1 in / 24.1 mSPAN
LENGTH
HEIGHT
General PerformanceGeneral Performance
Taxi constraints : better then actual 747 or 777
Take Off and landing: better then 747-400
Altitude capability: FL 330 at Max To Weight
Vortex generation: better then 747
CONCLUSION : the A380 will not create piloting
challenges different from actual wide body airplanesNew TechnologyNew Technology
Structure:
•Laser welding •G L A R E •Carbon fiber panels •CFRP Wing RibsElectrical generation:
•Variable frequency generatorsHydraulics:
•Self contained Electro Hydraulic actuatorsThe cockpitThe cockpit
The "Airbus Cockpit Philosophy", results of customers feed-back, experience, and research on new technology The "Airbus Cockpit Philosophy", results of customers feed-back, experience, and research on new technologyThe cockpitThe cockpit
Common features with the A320 and A340 families:
•Overall cockpit layout (screens and controls arrangement, dark cockpit, symbology and color coding ....) •Flight envelope protection •Side sticks •Non back-driven thrust levers •FMS functions base line is FMS 2nd generation Cockpit improvements are driven by Flight safety enhancements, Lessons learnt from airlinesand product added values: •take-off acceleration monitoring, •on-board Information System •thrust indication •vertical situation awareness, collision avoidance •enhanced crew rest•camera/video, taxiing aids •larger & interactive displays, •FMS interface, •enhanced ECAM, •navigation on airports,The cockpitThe cockpit
8 identical potentially interactive displays 8 identical potentially interactive displays 2 KCCU:Keyboard and Cursor Control Units
2 KCCU:Keyboard and Cursor Control Units
Control and Display SystemControl and Display System track-ballwheel validation functional short cuts back-up CCD numeric pad spare keys screen cursor allocation alphabeticQWERTY pad
Keyboard and Cursor Control DeviceKeyboard and Cursor Control DeviceAll FMS functions accessible
through this interactive MFD with KCCUAll FMS functions accessible
through this interactive MFD with KCCULateral Flight Plan revisions graphically on ND with KCCULateral Flight Plan revisions
graphically on ND with KCCUFMSFMS
Memos,limitations
abnormal procedures, normal check-lists on WD through dedicated controlsMemos,limitations
abnormal procedures, normal check-lists on WD through dedicated controlsA/C configuration,
some memos and limitations below PFDA/C configuration,
some memos and limitations below PFDECP:Dedicated ECAM controls (keys and pointer)
ECP:Dedicated ECAM controls (keys and pointer)
System pages, status
accessible on the SD through dedicated controlsSystem pages, status
accessible on the SD through dedicated controlsECAMECAM
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XXXX102. 6 4. 6 102. 6 102. 6N1
458158
458
458EGT
°C 102.6 458
CL 88.
6 % THR 10566.
2 0 105
66.
2 0 105
66.
2 0 105
66.
2 0
SEAT BELTS
NO SMOKINGECAMECAM
Cockpit Thrust indicationCockpit Thrust indicationACUTE - Airbus Cockpit Universal Thrust Emulator
•THR will replace N1 (or EPR/TPR) as cockpit thrust control / monitoring parameter (providing enhanced cockpit commonality). •Engine manufacturers will select the thrust control / monitoring parameter (N1/EPR/TPR) at engine level -converted to THR thrust indication via the FADEC •Meaningful thrust indications are displayed as "percentage thrust" using straightforward reference levels: -100% THR = maximum available thrust in actual flight conditions without air bleed e.g. Max Take-off thrust in the take-off flight envelopeMax Cont thrust outside take-off flight envelope
-0% THR = engine shutdown (windmilling) •Improves readability and improves scale significance •Fan speed will remain as primary indication (E/WD) and N2 (and N3 forR-R) will be available as secondary indications
THR Cockpit Indication THR Cockpit Indication --draftdraft THRCLB78.
0%Engine 1
Engine 2
Engine 3
Engine 4
0 59.0 5 10 0 59.
0 5 10 0 59.
0 5 10 0 59.
0 5 10