What was found
(AUS) RH ENGINE COMPRESSOR FIRST STAGE BLADES DAMAGED BY FOD - AIRCRAFTHAD PREVIOUSLY OPERATED FROM GRAVEL STRIPS
- Difficulty date
- August 13, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Beech B200C
- Engine
- Pwa PT6A42
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Compressor Blade
- Part number
- 310652101
- Condition
- Fod
- Location
- Turb Eng Comp
- Component
- Pwa · PT6A42
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.