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|
Attributes | |
ACN | 1688291 |
Time | |
Date | 201909 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | FO |
Aircraft 1 | |
Make Model Name | B767-300 and 300 ER |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Component | |
Aircraft Component | Leading Edge Slat |
Person 1 | |
Function | Technician |
Qualification | Maintenance Powerplant Maintenance Airframe |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Deviation - Procedural Published Material / Policy Deviation - Procedural MEL Deviation - Procedural Maintenance |
Narrative:
Aircraft X was in ZZZ when they discovered a dent on #1 slat. Their evaluation of the dent was accomplished with what appears to be tape? [Engineering department] was notified and an [engineering order] was issued and item was placed on dip to be repaired in 1 fc. Once in ZZZ1 the dent was re-evaluated prior to permanent repair being performed and pulled fasteners and a crease was noted not allowing us to perform permanent repair per [engineering order]. [Engineering order] part 1 step 2 clearly states ensure dent is smooth and no creases or loose or pulled fasteners. The picture on page 4 of the [engineering order] you can see the 'well defined line' where there is underlying structure. [Engineering order] was not signed at time of release either. Slat is being repaired at ZZZ1 with another repair scheme outside the srm.[I suggest to] train our maintenance personnel better for damage evaluation and provide them with the tools necessary.
Original NASA ASRS Text
Title: Technician reported that Maintenance at the prior station did not evaluate and document a damaged slat correctly.
Narrative: Aircraft X was in ZZZ when they discovered a dent on #1 slat. Their evaluation of the dent was accomplished with what appears to be tape? [Engineering Department] was notified and an [engineering order] was issued and item was placed on dip to be repaired in 1 FC. Once in ZZZ1 the dent was re-evaluated prior to permanent repair being performed and pulled fasteners and a crease was noted not allowing us to perform permanent repair per [engineering order]. [Engineering order] part 1 step 2 clearly states ensure dent is smooth and no creases or loose or pulled fasteners. The picture on page 4 of the [engineering order] you can see the 'well defined line' where there is underlying structure. [Engineering order] was not signed at time of release either. Slat is being repaired at ZZZ1 with another repair scheme outside the SRM.[I suggest to] train our maintenance personnel better for damage evaluation and provide them with the tools necessary.
Data retrieved from NASA's ASRS site 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.