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时间:2010-05-22 22:34来源:蓝天飞行翻译 作者:admin
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take-off into low and high speed.
· Below 100 kts, it is possible to reject for any reason.
· Above 100 kts, and approaching V1, be "go-minded" unless major failures or ECAM
warnings occur.
· Once above V1, the take-off must be continued as it may be impossible to stop the aircraft
on the runway remaining.
Remember to bring the airplane to a complete stop, not slowed, stopped. Set the Parking
Brake. When the airplane is stopped identify/confirm failure. If ENG FIRE, it is
recommended to use the QRH as ECAM will normally be lost on second engine shut down
(APU not normally running). In other cases where evacuation is considered necessary use
the ON GROUND EMER/EVAC checklist. The ENG FIRE ON GROUND checklist includes
the possibility of emergency evacuation, therefore there is no need to use the
EMER/EVACUATION checklist when this checklist is being used.
Use ATC, fire service and cabin staff to gain as much information as possible to assist in
making a decision on whether to evacuate or not. Remember that the simplest way to
confirm an engine fire, on the ground, is to open the cockpit window and look out.
If no evacuation is necessary, clear the runway if safe to do so.
06 - COMPLETION STANDARDS
· Makes appropriate decision before V1.
· Carries out correct actions to ensure a safe stop on runway centerline.
07 - COMMON ERRORS
· Disarming of autobrake due to instinctive manual braking.
· ATC and/or Cabin crew not informed.
· Reversers thrust remains engaged after aircraft stop.
· Omitting to select parking brake on.
· Non respect of task-sharing during emergency procedure.
· Failure to have QRH available.
· Confusion over use of ON GROUND EMER/EVACUATION or ENG FIRE ON GROUND
checklist.
· Inability to use mechanical seat controls.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.10 Page 2
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
OPERATING TECHNIQUES
CHAP03\10
ENGINE FAILURE OR FIRE AFTER V1
01 - TRAINING OBJECTIVE
· To recognize engine failure and/or fire warning.
· Take correct actions to maintain a safe trajectory.
· To perform correct engine fail or fire after V1procedure.
02 - SCHEDULE
Briefing duration : 20 minutes
03 - EQUIPMENT
DOC references :
· QRH 2.19 (Engine stall)
· QRH 2.21 (Overweight landing)
· FCOM 1.27.20 (Sideslip target)
· FCOM 3.02.10 (Operating techniques)
· FCOM 3.02.26 (Engine fire)
· FCOM 3.02.70 (Engine fail)
· FCOM 4.04.30 (EOSID) if applicable
· FCOM 4.05.30 (Engine Out Procedure)
04 - INSTRUCTOR’S ACTIONS
Briefing of the following key points :
MAIN
· GO/STOP decision making.
· Aircraft control on the ground and at rotation.
· Roll control, sideslip target and "Fly by wire" characteristics.
· Pitch attitude and speed control.
· Specific task sharing procedures.
· Confirmation of non-reversible items with ECAM actions.
· Engine-out profile.
SECONDARY
· A/P engagement / Rudder trim.
· EOSID activation.
· Availability and use of TOGA.
· FD roll limit below green dot speed.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.10 Page 3
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
OPERATING TECHNIQUES
CHAP03\10
ENGINE FAILURE OR FIRE AFTER V1 (CONT’D)
05 - TRAINEES’ ACTIONS
ENGINE FAILURE
After detecting an engine failure, PNF is to call "engine failure", without identifying which
engine has failed.
TOGA power is available, but should only be applied when required by PF. This is because
the increase in power may cause directional control difficulties when at light weights and low
speeds.
PF should maintain runway centerline with rudder, visually or with assistance of the PFD yaw
bar (if available). At VR, rotate smoothly to 12°5 nose up and centralize blue b target (see
below for explanatory note) with rudder. Adjust pitch attitude and monitor speed trend arrow
(minimum speed V2) until SRS has stabilized. The change over from yellow side slip index
to blue b target may not occur instantaneously. Use rudder trim to neutralize rudder pedal
pressure. When a positive climb has been achieved, call for retraction of the gear. Use
autopilot if it is available.
PNF should closely monitor the aircraft’s flight path, cancel warnings and identify the failure
when appropriate. Note when a positive climb has been established and announce
 
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