What was found
(CAN) THE #1 ENGINE WAS SHUTDOWN FOLLOWING THE LOSS OF MAIN OIL PRESSURE, WHICH WAS SUBSEQUENTLY FOUND TO BE CAUSED BY DAMAGED THREADS ON A PLUG ON THE REDUCTION GEARBOX.
- Difficulty date
- September 16, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa PW119B
- System (JASC)
- 7210 · Turbine Engine Reduction Gear
- Part
- Plug
- Condition
- Damaged
- Location
- Reduction Gearbx
- Part time
- 4,613 hours
- Stage of operation
- NR
- Nature of condition
- J, K
- Precautionary procedure
- E
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.