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|
Attributes | |
ACN | 575244 |
Time | |
Date | 200302 |
Day | Tue |
Local Time Of Day | 0001 To 0600 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | agl single value : 0 |
Environment | |
Flight Conditions | IMC |
Weather Elements | Snow |
Light | Night |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | DC-10 10 |
Operating Under FAR Part | Part 121 |
Flight Phase | climbout : takeoff ground : takeoff roll |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp pilot : commercial pilot : flight engineer pilot : instrument pilot : multi engine |
Experience | flight time last 90 days : 250 flight time total : 14000 flight time type : 3000 |
ASRS Report | 575244 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : non compliance with mel non adherence : far non adherence : published procedure |
Independent Detector | aircraft equipment other aircraft equipment : #2 n1 indicator other flight crewa other flight crewb other other : 3 |
Resolutory Action | none taken : detected after the fact |
Consequence | other |
Factors | |
Maintenance | contributing factor : manuals contributing factor : schedule pressure performance deficiency : logbook entry performance deficiency : testing performance deficiency : fault isolation |
Supplementary | |
Problem Areas | Maintenance Human Performance Aircraft Flight Crew Human Performance Chart Or Publication |
Primary Problem | Maintenance Human Performance |
Narrative:
We had a deferred #2 engine N1 gauge. Procedurally, this requires some different procedures for engine start, but all other system are supposed to be normal. It was snowing, which necessitated deicing. We finally taxied out for takeoff on runway 18L. On takeoff roll, we added power and began the takeoff roll. Frequently we get an engine fail light due to the engines spooling up at different rates, but they soon extinguish. The lights remained on, but all engine instruments remained normal. The takeoff and subsequent flight were uneventful, and we went to our destination. As it turns out, the airplane was deferred on the incorrect MEL. Rather than an inoperative gauge, the sensor was inoperative. This will cause the engine fail light to illuminate and also requires a weight limitation -- which we were below. I felt the safest course of action was to continue the takeoff rather than abort, but safety could have been compromised.
Original NASA ASRS Text
Title: A DC10-10 WAS DISPATCHED WITH #2 ENG N1 INDICATOR DEFERRED AS INOP PER THE MEL, BUT ACTUALLY HAD THE ENG FAIL SYS INOP.
Narrative: WE HAD A DEFERRED #2 ENG N1 GAUGE. PROCEDURALLY, THIS REQUIRES SOME DIFFERENT PROCS FOR ENG START, BUT ALL OTHER SYS ARE SUPPOSED TO BE NORMAL. IT WAS SNOWING, WHICH NECESSITATED DEICING. WE FINALLY TAXIED OUT FOR TKOF ON RWY 18L. ON TKOF ROLL, WE ADDED PWR AND BEGAN THE TKOF ROLL. FREQUENTLY WE GET AN ENG FAIL LIGHT DUE TO THE ENGS SPOOLING UP AT DIFFERENT RATES, BUT THEY SOON EXTINGUISH. THE LIGHTS REMAINED ON, BUT ALL ENG INSTS REMAINED NORMAL. THE TKOF AND SUBSEQUENT FLT WERE UNEVENTFUL, AND WE WENT TO OUR DEST. AS IT TURNS OUT, THE AIRPLANE WAS DEFERRED ON THE INCORRECT MEL. RATHER THAN AN INOP GAUGE, THE SENSOR WAS INOP. THIS WILL CAUSE THE ENG FAIL LIGHT TO ILLUMINATE AND ALSO REQUIRES A WT LIMITATION -- WHICH WE WERE BELOW. I FELT THE SAFEST COURSE OF ACTION WAS TO CONTINUE THE TKOF RATHER THAN ABORT, BUT SAFETY COULD HAVE BEEN COMPROMISED.
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.