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|
Attributes | |
ACN | 449642 |
Time | |
Date | 199909 |
Day | Sun |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | agl single value : 0 |
Environment | |
Light | Daylight |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | B737-500 |
Operating Under FAR Part | Part 121 |
Flight Phase | ground : parked ground : maintenance |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | maintenance : technician |
Qualification | technician : powerplant technician : airframe |
Experience | maintenance technician : 27 |
ASRS Report | 449642 |
Person 2 | |
Affiliation | company : air carrier |
Function | oversight : supervisor |
Qualification | technician : airframe technician : powerplant |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : improper maintenance non adherence : published procedure |
Independent Detector | other other : 1 |
Resolutory Action | none taken : unable |
Consequence | other other |
Factors | |
Maintenance | performance deficiency : non compliance with legal requirements |
Supplementary | |
Problem Areas | Maintenance Human Performance Company Aircraft |
Primary Problem | Maintenance Human Performance |
Narrative:
During operations check of flaps/slats, flaps were lowered on to a ladder causing a 2 inch dent/crack on left inboard trailing edge flap, the honeycomb material was sealed with pro seal and hi speed tape installed per maintenance control and srm 57. I was not sure that the above temperature repair was legal, but followed maintenance control's instruction by installing the high speed tape, the aircraft was released for positioning flight.
Original NASA ASRS Text
Title: A B737-500 INCURRED DAMAGE TO THE L INBOARD TRAILING EDGE FLAP DURING AN OPS CHK WHEN LOWERED ONTO A LADDER.
Narrative: DURING OPS CHK OF FLAPS/SLATS, FLAPS WERE LOWERED ON TO A LADDER CAUSING A 2 INCH DENT/CRACK ON L INBOARD TRAILING EDGE FLAP, THE HONEYCOMB MATERIAL WAS SEALED WITH PRO SEAL AND HI SPD TAPE INSTALLED PER MAINT CTL AND SRM 57. I WAS NOT SURE THAT THE ABOVE TEMP REPAIR WAS LEGAL, BUT FOLLOWED MAINT CTL'S INSTRUCTION BY INSTALLING THE HIGH SPD TAPE, THE ACFT WAS RELEASED FOR POSITIONING FLT.
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.