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|
Attributes | |
ACN | 133837 |
Time | |
Date | 199001 |
Day | Fri |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : ase |
State Reference | CO |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | Medium Transport |
Flight Phase | climbout : takeoff ground other : taxi |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Experience | flight time last 90 days : 150 flight time total : 5000 flight time type : 2000 |
ASRS Report | 133837 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp |
Experience | flight time last 90 days : 155 flight time total : 2700 flight time type : 160 |
ASRS Report | 134466 |
Events | |
Anomaly | aircraft equipment problem : less severe non adherence : published procedure |
Independent Detector | aircraft equipment other aircraft equipment : unspecified |
Resolutory Action | none taken : anomaly accepted |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | Pilot Deviation |
Narrative:
Taxiing for departure in aspen, the #3 AC gen hot caution light illuminated. After consulting the MEL and the afm, the gen was switched off-line, deferring and the flight proceeded uneventfully. Reviewing the incident on arrival and after a closer look at the MEL, I found the gen had been deferring in error. MEL did not include a crew procedure for deferring on aircraft gen when only 1 was inoperative, but did include a crew deferrable procedure with 2 inoperative. The aircraft flight manual also contains a procedure to resolve an AC gen hot caution light indication. AC gens with mod XXXX (all our mdt aircraft AC gens have this mod) have a bearing wear detector in addition to a heat detector. Both can turn on the AC gen hot caution light. The procedure determined our situation to be preliminary bearing wear and the gen need not be removed until the end of the flying day. The MEL does not mention the afm procedure. Having gotten involved with the afm procedure, I lost track of the MEL's lack of a crew procedure to defer an AC gen. The mle appears to conflict with itself and is not in agreement with the flight manual.
Original NASA ASRS Text
Title: COMMUTER MDT FAILED TO COMPLY WITH MINIMUM EQUIPMENT LIST REQUIREMENT.
Narrative: TAXIING FOR DEP IN ASPEN, THE #3 AC GEN HOT CAUTION LIGHT ILLUMINATED. AFTER CONSULTING THE MEL AND THE AFM, THE GEN WAS SWITCHED OFF-LINE, DEFERRING AND THE FLT PROCEEDED UNEVENTFULLY. REVIEWING THE INCIDENT ON ARR AND AFTER A CLOSER LOOK AT THE MEL, I FOUND THE GEN HAD BEEN DEFERRING IN ERROR. MEL DID NOT INCLUDE A CREW PROC FOR DEFERRING ON ACFT GEN WHEN ONLY 1 WAS INOP, BUT DID INCLUDE A CREW DEFERRABLE PROC WITH 2 INOP. THE ACFT FLT MANUAL ALSO CONTAINS A PROC TO RESOLVE AN AC GEN HOT CAUTION LIGHT INDICATION. AC GENS WITH MOD XXXX (ALL OUR MDT ACFT AC GENS HAVE THIS MOD) HAVE A BEARING WEAR DETECTOR IN ADDITION TO A HEAT DETECTOR. BOTH CAN TURN ON THE AC GEN HOT CAUTION LIGHT. THE PROC DETERMINED OUR SITUATION TO BE PRELIMINARY BEARING WEAR AND THE GEN NEED NOT BE REMOVED UNTIL THE END OF THE FLYING DAY. THE MEL DOES NOT MENTION THE AFM PROC. HAVING GOTTEN INVOLVED WITH THE AFM PROC, I LOST TRACK OF THE MEL'S LACK OF A CREW PROC TO DEFER AN AC GEN. THE MLE APPEARS TO CONFLICT WITH ITSELF AND IS NOT IN AGREEMENT WITH THE FLT MANUAL.
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.