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Emergency Landing All Engine Failure презентация
Содержание
- 1. Emergency Landing All Engine Failure
- 2. Contents Page
- 3. Background Require manufacturer of turbine powered
- 4. New Procedure Create new procedure EMERGENCY LANDING:
- 5. ALL ENGINE FAILURE procedure Main Steps Initial
- 6. Creation “EMERGENCY LANDING” Scope Total thrust loss
- 7. When to apply the different
- 8. When to apply the different procedures Enhanced procedures THRUST LOSS Engine Operative Page
- 9. When to apply the different
- 10. When to apply the different procedures Engine Operative Page
- 11. When to apply the different
- 12. When to apply the different
- 13. When to apply the different
- 14. When to apply the different
- 15. When to apply the different procedures Thrust loss BANG Page
- 16. Emergency Landing - Procedure Provides the minimum
- 17. Emergency Landing - Procedure OLM 2012 - Emergency Landing / All Engine Failure Page
- 18. Emergency Landing - Procedure
- 19. Emergency Landing - Procedure Page
- 20. Emergency Landing - Procedure Page
- 21. Emergency Landing - Procedure Elec Page
- 22. Emergency Landing - Procedure
- 23. Emergency Landing - Procedure Cabin Page
- 24. Emergency Landing - Procedure Mini V/S Pitch Page
- 25. Emergency Landing - Procedure
- 26. Contents Page
- 27. Conclusion EMERGENCY LANDING
- 28. © AIRBUS S.A.S. All rights reserved. Confidential
Contents Page
Слайд 3Background
Require manufacturer of turbine powered aircraft
to develop checklist and procedure for
dual engine failure occurring at low altitude.
NTSB Safety Recommendation :
Hudson event:
Bird strike
Thrust Loss at 3000 ft AGL
Touchdown 3 minutes later
All 155 persons on-board safely evacuated
Page
Слайд 4New Procedure
Create new procedure
EMERGENCY LANDING:
To configure for landing
when no time to
relight
Airbus Answer
Require manufacturer of turbine powered aircraft
to develop checklist and procedure for
dual engine failure occurring at low altitude.
Page
Слайд 5ALL ENGINE FAILURE procedure
Main Steps
Initial Descent
Starter Assisted Relight
Approach
Forced landing - Ditching
Windmilling Relight
Descent at Green Dot
OLM 2012 - Emergency Landing / All Engine Failure
Page
Слайд 6Creation “EMERGENCY LANDING”
Scope
Total thrust loss very close to the ground -
No time to relight
Remaining time to touchdown must be used to configure the aircraft for touchdown.
Remaining time to touchdown must be used to configure the aircraft for touchdown.
Page
Слайд 12
When to apply the different procedures
Thrust loss
No longer possible to
maintain level flight
Not always associated with the ECAM Alert:
ENG DUAL FAILURE
Not always associated with the ECAM Alert:
ENG DUAL FAILURE
Apply QRH proc even if not prompted by ECAM
Page
Слайд 13
When to apply the different procedures
Thrust loss
Close to the ground
?
Is touchdown imminent ?
Time to relight ?
Not only a matter of altitude but rather a matter of:
Time to touchdown
Flight crew workload:
Pilot judgment will determine what can be attempted to recover
Environmental conditions
(weather, day/night, terrain, ...)
Is touchdown imminent ?
Time to relight ?
Not only a matter of altitude but rather a matter of:
Time to touchdown
Flight crew workload:
Pilot judgment will determine what can be attempted to recover
Environmental conditions
(weather, day/night, terrain, ...)
Page
Слайд 16Emergency Landing - Procedure
Provides the minimum steps to land:
APU Start /
Landing Gear / Flaps / Speed target
Main steps of “Forced landing” or “Ditching” procedure of the All Engine Failure procedure.
Compromise:
Main steps of “Forced landing” or “Ditching” procedure of the All Engine Failure procedure.
Compromise:
Short
Straight Forward
Easy to apply
Covering
as many cases
as possible
Page
Слайд 18Emergency Landing - Procedure
Electrical Power Supply
Gear - Flaps - Speed
Securing the
Aircraft
EMER EVAC PROC APPLY
EMER EVAC PROC APPLY
Pitch - minimize Vertical Speed
“Brace for Impact”
Page
Слайд 27
Conclusion
EMERGENCY LANDING
ALL ENG FAILURE
Immediately accessible
To configure the aircraft
When no
time to relight
New Procedure
Page
Слайд 28© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document. This
document and all information contained herein is the sole property of AIRBUS S.A.S. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof.
AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.
AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks.
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