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Attributes | |
ACN | 1515127 |
Time | |
Date | 201801 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Aircraft 1 | |
Make Model Name | B757-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Flight Plan | IFR |
Component | |
Aircraft Component | Powerplant Mounting |
Person 1 | |
Function | Technician |
Person 2 | |
Function | Technician |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Deviation - Procedural Published Material / Policy |
Narrative:
During performance of engineering order (east.O) of a B757 on left engine; there was a discovery of torque variance between forward engine mount bolts ending in -1; -2 [as] opposed to the -3. Members of the facility's engine change crew recognized torque difference between the aircraft maintenance manual (amm); called out in [the] east.O; and our normal engine change paperwork job card by nearly 100 feet lbs. Of torque. Then searched local inventory found all bolts in stock were -3. Proceeded to verify all stock in company were -3 to include; a scenario of ordering a -1/ -2 changes to a -3 in the system. The inspector went to verify bolts installed in engine by taking a picture of 1 out of the 4 bolts. He saw a line of numerals that appeared to be part numbers ending in the numeral 3 then a substantial space. He verified with another mechanic if he concurred it being a -3 bolt. We proceeded with full confidence; that -3 bolts were installed. Due to [the] generation of [a different] east.O; next base maintenance removed and replaced left forward engine mount bolts and barrel nuts; discovering that the bolts installed were indeed-2 bolts and incorrectly identified by inspector as a -3; subsequently realizing the bolts were over torqued.
Original NASA ASRS Text
Title: Maintenance personnel reported that the engine mounts on a Boeing 757 were over-torqued because the part number of the mount bolts were incorrect.
Narrative: During performance of Engineering Order (E.O) of a B757 on left Engine; there was a discovery of torque variance between Forward Engine Mount Bolts ending in -1; -2 [as] opposed to the -3. Members of the facility's engine change crew recognized torque difference between the Aircraft Maintenance Manual (AMM); called out in [the] E.O; and our normal engine change paperwork job card by nearly 100 feet lbs. of torque. Then searched local inventory found all bolts in stock were -3. Proceeded to verify all stock in company were -3 to include; a scenario of ordering a -1/ -2 changes to a -3 in the system. The inspector went to verify bolts installed in engine by taking a picture of 1 out of the 4 bolts. He saw a line of numerals that appeared to be Part Numbers ending in the numeral 3 then a substantial space. He verified with another mechanic if he concurred it being a -3 bolt. We proceeded with full confidence; that -3 bolts were installed. Due to [the] generation of [a different] E.O; next base maintenance removed and replaced Left Forward Engine Mount bolts and barrel nuts; discovering that the bolts installed were indeed-2 bolts and incorrectly identified by inspector as a -3; subsequently realizing the bolts were over torqued.
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.