A380-800
2 mar. 2006 Note: The Nose Landing Gear is equipped with 2 radial 1 270 x 455 x R22 tires. 1.6. Page 13. STL 945.1380/05 Issue 2. Flight Deck and Systems ...
Video compression of airplane cockpit screens content
3 jul. 2022 real example of a cockpit of A380 airplane. Other instrumentation technologies are integrated such as Head-Up Displays (HUD). Video ...
A350-900 Flight Deck and Systems Briefing for Pilots - SmartCockpit
Takeoff Performance and Initial Cruise Altitude Capability aircraft video sources and transmits these signals to the CDS. The different video sources ...
TRAINEES BOOKLET (FCTP extracts) A380 This document must be
5 feb. 2009 The takeoff data and session syllabus based on Airbus Airport ... of aircraft type to another based on common cockpit and flight ...
FLIGHT CREW TRAINING PROGRAM (FCTP) TABLE OF
A380. 00.00. PAGE LEFT INTENTIONALLY BLANK. FLIGHT CREW TRAINING PROGRAM Cockpit Preparation + Before Start / After Start + Taxi / Before Takeoff + ...
A/STAB
Airbus Integrated Management/Cockpit Resource Management. AIM-FANS Concentrator and Multiplexer for Video ... Continuous Safe Flight/Landing.
Airbus A380-800 Report of the FCL/OPS Subgroup Report Revision
18 jul. 2011 EASA Operational Evaluation Board Airbus A380 – FCL & OPS Subgroup ... and that the Ground courseware on CBT/Video/Transparencies is.
B-01 SC & IM: Stalling and scheduled operating speeds
2 may. 2002 The A380 is equipped with a low speed protection system providing a ... maintain level flight at a speed of 1.5 Vsr1 at maximum landing ...
A350 XWB - training for the future
Subset below PFD. System Display. System synoptic and Status. Cockpit door Cabin
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
FORWARD
THR REV5 10 0 Max 3. 0 5 10 0 3. 0 5 10 0 REV5 10 0 MaxREVERSE
CLRAPUENG
BLEED PRESS COND EL/AC EL/DC FUEL F/CTL HYD WHEEL C/B ALL RCL T.O.CONFIG
EMER CANC C/ L ABN NORM STS BACK OXY VIDEO DOORS SYS PROC MOREECAMECAMControlControlPanelPanel
SF 333.5 %
NOSE UP NOSE DN Pitch trim control and displayPitch trim control and displayVertical displayVertical display
A380 AFS FCU Backup PrincipleA380 AFS FCU Backup PrincipleAFS Backup AFS Backup
On both
On both MFDsMFDsAFS Backup AFS Backup
On one of the
On one of theMFDsMFDs
Both channel failureBoth channel failure
or Voluntary disconnect or Voluntary disconnectATC full page (access from FMS page
or with direct function key on keyboard)ATC full page (access from FMS page
or with direct function key on keyboard)Attention getter
Attention getter
Permanent ATC Mail box
Permanent ATC Mail box
ATC data linkATC data link
ATCATC
ATC Communication full page on MFDATC permanent mail box below SD3 dedicated
Radio and Audio
management panels3 dedicated
Radio and Audio
management panelsVoice communicationVoice communication
RAMPRAMP
AESS control page
(access from FMS page or with direct function key on keyboard)AESS control page
(access from FMS page or with direct function key on keyboard)Dedicated control panelDedicated control panel
SurveillanceSurveillance
AESS control panel on pedestal
AESS page on MFD
AESSAESS
Cabin/Passenger services
IFECabin operation
Maintenance
Cockpit operation
The Aircraft becomes a node on:The Aircraft becomes a node on: -Air traffic networkAir traffic network -Airline networkAirline network A380 Onboard Information SystemA380 Onboard Information SystemOIS objectivesOIS objectives
- Offer cost-effective capability for implementing tools which improve A/L operations in three domains: cockpit, cabin & maintenance by: • Reducing paper usequotesdbs_dbs14.pdfusesText_20[PDF] a380 cockpit takeoff and landing
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