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Attributes | |
ACN | 1041733 |
Time | |
Date | 201210 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Make Model Name | B737-700 |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Flight Plan | IFR |
Component | |
Aircraft Component | Engine Air Starter |
Person 1 | |
Function | First Officer |
Experience | Flight Crew Last 90 Days 64 |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy Deviation - Procedural Maintenance Flight Deck / Cabin / Aircraft Event Other / Unknown |
Narrative:
Approximately five minutes prior to the scheduled push time; I started the APU and placed the aircraft electronics on the APU generator. The APU bleed was switched to on after operating for greater than a minute. Shortly thereafter; a ground crew member asked if we had been cleared to start an engine; then stated an engine was turning; and there was no anti-collision light on. Both pilots responded 'no' to his question. I then saw the number two engine start switch was in the ground position and immediately moved it to the off position. The ground crew member exited the cockpit.maintenance had been performed on the number two thrust reverser prior to the arrival of the originating flight crew. Both pilots reviewed the preflight flows in the aom; but found no requirement for either pilot to ensure the correct position of the start switches prior to starting and using the APU. I could find no requirement for checking the position of the start switches until the after engine start flows.
Original NASA ASRS Text
Title: Maintenance personnel failed to ensure the right engine start switch was correctly positioned after performing maintenance on the thrust reverser. The engine began to motor when the First Officer started the APU and opened the APU bleed five minutes prior to scheduled departure.
Narrative: Approximately five minutes prior to the scheduled push time; I started the APU and placed the aircraft electronics on the APU generator. The APU Bleed was switched to on after operating for greater than a minute. Shortly thereafter; a Ground Crew Member asked if we had been cleared to start an engine; then stated an engine was turning; and there was no anti-collision light on. Both pilots responded 'no' to his question. I then saw the number two engine start switch was in the GND position and immediately moved it to the off position. The Ground Crew Member exited the cockpit.Maintenance had been performed on the number two thrust reverser prior to the arrival of the originating flight crew. Both pilots reviewed the preflight flows in the AOM; but found no requirement for either pilot to ensure the correct position of the start switches prior to starting and using the APU. I could find no requirement for checking the position of the start switches until the after engine start flows.
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.