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标题: Blocked AOA Probes Temporary procedure for aircraft equipped with conic cover [打印本页]

作者: 航空 时间: 2014-12-17 13:25:56 标题: Blocked AOA Probes Temporary procedure for aircraft equipped with conic cover

作者: 航空 时间: 2014-12-17 13:26:14

Blocked AOA Probes
Temporary procedure for aircraft equipped with conic cover plates
Presented by
Pierre-Henri REVERBEL –Senior Flight Operations Engineer
Flight Operations Web conference –December 2012
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
December 2012
Flight Operations Webconf
AGENDA
1. The conic AOA cover plates2. One in-service event: facts3. Temporary Procedures : OEB-45•A330/A340 Temporary Procedure•A320 Family Temporary Procedure
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
December 2012
Flight Operations Webconf
AGENDA
1. The conic AOA cover plates2. One in-service event: facts3. Temporary Procedures : OEB-45•A330/A340 Temporary Procedure•A320 Family Temporary Procedure
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
Conic AOA Cover Plates
•
The conic AOA cover plates aim at protecting the AOA root from the ice crystals phenomenon.
•
Installation of conic cover plates started in February 2012:
•
170 A330/A340 aircraft
•
520 A320 family aircraft
•
One equipped aircraft had an in-service event
December 2012
Flight Operations Webconf
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
December 2012
Flight Operations Webconf
AGENDA
1. The conic AOA cover plates2. One in-service event: facts3. Temporary Procedures : OEB-45•A330/A340 Temporary Procedure•A320 Family Temporary Procedure
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
In-service event
•
4 minutes after Take-off , reaching FL113 with TAT=-12°C, 3 AOA recorded at a constant value of 5°for about 1 hour
•
Flight Crew reported: passing FL250, both PFD’s ValphaProt rising up toward SEL SPD 260kts
•
Flight Crew decided to troubleshoot at FL310
•
When reaching FL310, AP automatically disconnected due to AOA protection activation.
•
Just after AP disconnection, with sidestickfree, Alpha Prot Law commanded pitch down order to target alpha prot(4°)
December 2012
Flight Operations Webconf
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
In-service event
•
With pitch attitude continuously decreasing, PF reacted by applying permanent (for about 20s) sidestickorder in the full backward position.
•
Pitch angle continued to decrease and AC to descend
•
A/THR reduced the thrust due to Speed increase (Selected Speed 305kts)
•
The flight crew elected to switch ADRs to OFF
•
With reversion to alternate law, the High Angle-of-Attack protection was no longer available.
•
Pitch attitude was recovered.
•
Flight crew diverted and performed an uneventful landing.
December 2012
Flight Operations Webconf
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
December 2012
Flight Operations Webconf
AGENDA
1. The conic AOA cover plates2. One in-service event: facts3. Temporary Procedures : OEB-45•A330/A340 Temporary Procedure•A320 Family Temporary Procedure
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
OEB 45 / AFM TR286-A320 / AFM TR293-A330 / AFM TR294-A340
•
Airbus decided to provide, as a precautionary measure (root cause of the in-service event still under investigation), the operators with temporary procedures for aircraft equipped with conic AOA cover plates.
•
Goals:
1.
Provide cockpit effects to detect two or three AOAs sending same constant values
2.
Provide procedure to revert to alternate law
December 2012
Flight Operations Webconf
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
December 2012
Flight Operations Webconf
AGENDA
1. The conic AOA cover plates2. One in-service event: facts3. Temporary Procedures : OEB-45•A330/A340 Temporary Procedure•A320 Family Temporary Procedure
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A330/A340 Procedure
•
Procedure entry points -cockpit effects:
􀂾
In stabilized flight path (Nz=1), Alpha Prot strip increases and permanently hides the VLS strip:
December 2012
Flight Operations Webconf
Increase in Mach
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A330/A340 Procedure
•
Procedure entry points -cockpit effects:
􀂾
A LOCK message remaining displayed even with speed increase to VFE CONF1 –10kt:
December 2012
Flight Operations Webconf
FLAP 0
Selection
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A330/A340 Procedure
•
At anytime, if the aircraft goes to an unmanageable pitch down attitude, even with sidestickin full backward position: reversion to alternate law: 2 ADRs….OFF
December 2012
Flight Operations Webconf
IMMEDIATELY
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A330/A340 Procedure
•
Procedure steps:
•
Stop accelerating
•
Stop climbing
•
Revert to Alternate law
December 2012
Flight Operations Webconf
Prevent increase in Mach number
Prevent Alpha Prot activation
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
December 2012
Flight Operations Webconf
AGENDA
1. The conic AOA cover plates2. One in-service event: facts3. Temporary Procedures : OEB-45•A330/A340 Temporary Procedure•A320 Family Temporary Procedure
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A320 Family Procedure
•
Procedure entry points -cockpit effects:
􀂾
In stabilized flight path (Nz=1), Alpha Max strip increases and hides completely the Alpha Prot strip:
December 2012
Flight Operations Webconf
Increase in Mach
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A320 Family Procedure
•
Procedure entry points -cockpit effects:
􀂾
With AP ON and increase in load factor (Nz>1), Alpha Prot strip moves by more than 30kt
December 2012
Flight Operations Webconf
Increase in load factor
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A320 Family Procedure
•
Procedure entry points -cockpit effects:
􀂾
A LOCK message remaining displayed even with speed increase to VFE CONF1:
December 2012
Flight Operations Webconf
FLAP 0
Selection
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A320 Family Procedure
•
At anytime, if the aircraft goes to an unmanageable pitch down attitude, even with sidestickin full backward position: reversion to alternate law: 2 ADRs….OFF
December 2012
Flight Operations Webconf
IMMEDIATELY
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
A320 Family Procedure
•
Procedure steps:
•
Stop accelerating
•
Stop climbing
•
Revert to Alternate law
December 2012
Flight Operations Webconf
Prevent increase in Mach number
Prevent Alpha Prot activation
© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.
December 2012
Flight Operations Webconf
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