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|
Attributes | |
ACN | 530959 |
Time | |
Date | 200111 |
Day | Thu |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : enl.airport |
State Reference | IL |
Altitude | msl single value : 27000 |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Controlling Facilities | artcc : zid.artcc |
Operator | common carrier : air carrier |
Operating Under FAR Part | Part 121 |
Flight Phase | cruise : level |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : second officer |
Qualification | pilot : instrument pilot : multi engine pilot : flight engineer pilot : atp pilot : cfi pilot : commercial |
Experience | flight time last 90 days : 95 flight time total : 2000 flight time type : 3300 |
ASRS Report | 530959 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Events | |
Anomaly | aircraft equipment problem : critical non adherence : company policies non adherence : published procedure other anomaly other |
Independent Detector | aircraft equipment other aircraft equipment : eng inst other flight crewa other flight crewb other other : 3 fo |
Resolutory Action | controller : provided flight assist flight crew : overcame equipment problem |
Supplementary | |
Problem Areas | Aircraft Flight Crew Human Performance |
Primary Problem | Flight Crew Human Performance |
Narrative:
#2 engine failed and was noticed spooling down by both captain and first officer. Speed started to dissipate, so a request to descend was approved to FL240. Captain and flight engineer conducted the engine shutdown checklist during which time it was determined that the #2 engine fuel valve shutoff switch was in the closed position. After realizing the cause for the failure, and determining normal engine parameters, and in-flight start was accomplished, and the flight continued to the destination routinely. The fuel valve shutoff switch had been inadvertently closed by me, I believe, while rotating tank boost pressure light caps to the dim night position. A possible corrective action would be to install more positive guarded caps over the shutoff valve switches. I, in the future will be much more guarded, when I move light caps of other switches in proximity to the engine fuel shutoff switches.
Original NASA ASRS Text
Title: A B727 CREW, DURING CRUISE AT FL270, EXPERIENCED A SPOOL DOWN OF #2 ENG, SELF INDUCED BY THE INADVERTENT CLOSING OF THE ENG FUEL VALVE.
Narrative: #2 ENG FAILED AND WAS NOTICED SPOOLING DOWN BY BOTH CAPT AND FO. SPD STARTED TO DISSIPATE, SO A REQUEST TO DSND WAS APPROVED TO FL240. CAPT AND FE CONDUCTED THE ENG SHUTDOWN CHKLIST DURING WHICH TIME IT WAS DETERMINED THAT THE #2 ENG FUEL VALVE SHUTOFF SWITCH WAS IN THE CLOSED POS. AFTER REALIZING THE CAUSE FOR THE FAILURE, AND DETERMINING NORMAL ENG PARAMETERS, AND INFLT START WAS ACCOMPLISHED, AND THE FLT CONTINUED TO THE DEST ROUTINELY. THE FUEL VALVE SHUTOFF SWITCH HAD BEEN INADVERTENTLY CLOSED BY ME, I BELIEVE, WHILE ROTATING TANK BOOST PRESSURE LIGHT CAPS TO THE DIM NIGHT POS. A POSSIBLE CORRECTIVE ACTION WOULD BE TO INSTALL MORE POSITIVE GUARDED CAPS OVER THE SHUTOFF VALVE SWITCHES. I, IN THE FUTURE WILL BE MUCH MORE GUARDED, WHEN I MOVE LIGHT CAPS OF OTHER SWITCHES IN PROX TO THE ENG FUEL SHUTOFF SWITCHES.
Data retrieved from NASA's ASRS site as of July 2007 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.