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Attributes | |
ACN | 1190561 |
Time | |
Date | 201407 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.ARTCC |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | A320 |
Operating Under FAR Part | Part 121 |
Flight Phase | Descent |
Flight Plan | IFR |
Component | |
Aircraft Component | Fan Reverser |
Person 1 | |
Function | Pilot Not Flying Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe |
Narrative:
Descending thru FL180; checking status page on descent flow we observed:'ENG2 at idle on grd''ENG2 max pwr idle'inop system:'reverser 2''ENG2 thr'[there was; however; no ECAM message; no immediate action; no ECAM exception; no QRH procedure or guidance in the qrhi asked a jumpseating captain to see if there was something in the ECAM supplemental guide for supportive information. [Although I understand the] ECAM supplemental is for actual ECAM and crew awareness [and that] we never received an ECAM [however it appeared] we had a possible situation with the number 2 reverser. The guide did provide some insight into what could be wrong. We discerned that a probable reason is there could be a disagreement relating to the fadec and thrust lever position. Nevertheless; we figured this had to with reverser door position with the sts/inop system messages.the ECAM supplemental guide under 'engine reverser pressurized' explains...'reverse thrust system pressurized without reverse deployment order'action: 'thr lvr 2..... Idle' 'if flight conditions permit; reduce thrust lever of affected engine to idle as a precautionary measure'.what we didn't know was if the reverser was pressurized or not. What we did know [is] if the reverser sleeve/door opened it would not be good.landing distance [decrement was] quickly checked and verified with 25% increase. We were in a position to land [while] on base leg when I made the decision to bring the thrust lever to idle as a precautionary measure. We briefed and used both reversers on touchdown. Landing and rollout were normal with both thrust reversers operating. Sts messages and inoperative system cleared.after shutdown; a maintenance message: ENG2 fadec [was displayed][an MEL:] 'reverser inop' was added for next flight.
Original NASA ASRS Text
Title: Odd Status page messages--observed during completion of the Descent Checklist--regarding the right engine reverser but which had not triggered an ECAM message/resolution presented a quandary to the flight crew of an A320.
Narrative: Descending thru FL180; checking Status Page on Descent flow we observed:'ENG2 at Idle on GRD''ENG2 Max Pwr Idle'INOP SYS:'REVERSER 2''ENG2 THR'[There was; however; no ECAM message; No Immediate Action; No ECAM Exception; No QRH Procedure or guidance in the QRHI asked a jumpseating Captain to see if there was something in the ECAM Supplemental Guide for supportive information. [Although I understand the] ECAM Supplemental is for actual ECAM and Crew Awareness [and that] we never received an ECAM [however it appeared] we had a possible situation with the Number 2 Reverser. The guide did provide some insight into what COULD be wrong. We discerned that a probable reason is there could be a disagreement relating to the FADEC and Thrust Lever Position. Nevertheless; we figured this had to with Reverser Door position with the STS/Inop SYS messages.The ECAM Supplemental Guide under 'ENG REVERSER PRESSURIZED' explains...'Reverse Thrust System Pressurized Without Reverse Deployment order'ACTION: 'THR LVR 2..... Idle' 'If flight conditions permit; reduce thrust lever of affected engine to IDLE as a precautionary measure'.What we didn't know was if the reverser was pressurized or not. What we DID know [is] if the reverser sleeve/door opened it would not be good.Landing distance [decrement was] quickly checked and verified with 25% increase. We were in a position to land [while] on base leg when I made the decision to bring the Thrust Lever to IDLE as a PRECAUTIONARY measure. We briefed and used BOTH reversers on touchdown. Landing and rollout were normal with BOTH thrust reversers operating. STS messages and INOP SYS cleared.After shutdown; a Maintenance Message: ENG2 FADEC [was displayed][An MEL:] 'Reverser Inop' was added for next flight.
Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.