37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
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Attributes | |
ACN | 1065030 |
Time | |
Date | 201301 |
Local Time Of Day | 0001-0600 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Night |
Aircraft 1 | |
Make Model Name | Airbus Industrie Undifferentiated or Other Model |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Component | |
Aircraft Component | Minimum Equipment List (MEL) |
Person 1 | |
Function | Technician |
Qualification | Maintenance Airframe Maintenance Powerplant |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural FAR Deviation - Procedural Published Material / Policy |
Narrative:
Airbus aircraft had CF6-80a3 engines and I referenced MEL 36-11-03 that referenced CF6-90c2 engines for high pressure (hp) valve inoperative (inop). If the aircraft had CF6-80c2 engines; the MEL would apply. However; it did not have CF6-80c2 engines; which would not require a lock-out of the thrust reverser (T/right). Because of this error; the thrust reverser was locked-out when it was not required; nor documented as such. Pilot tried to use the T/right when landing and the number 2 T/right was locked-out with no documentation. When I looked up the engine type for this aircraft under aircraft component control; I [had] looked at the engine type incorrectly by two letters; so an error was made. [Recommend] slow down and double check the documents.
Original NASA ASRS Text
Title: A Line Mechanic reports an incorrect MEL had been applied to an Airbus aircraft with CF6-80A3 engines. Number Two Engine Thrust Reverser (T/R) had been locked out when it was not required and was not documented. Pilot had tried to use the T/R on landing.
Narrative: Airbus aircraft had CF6-80A3 engines and I referenced MEL 36-11-03 that referenced CF6-90C2 engines for High Pressure (HP) Valve inoperative (inop). If the aircraft had CF6-80C2 engines; the MEL would apply. However; it did not have CF6-80C2 engines; which would not require a lock-out of the Thrust Reverser (T/R). Because of this error; the Thrust Reverser was locked-out when it was not required; nor documented as such. Pilot tried to use the T/R when landing and the Number 2 T/R was locked-out with no documentation. When I looked up the Engine type for this aircraft under Aircraft Component Control; I [had] looked at the engine type incorrectly by two letters; so an error was made. [Recommend] slow down and double check the documents.
Data retrieved from NASA's ASRS site as of July 2013 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.