What was found
(AUS) LEFT ENGINE FIRST STAGE COMPRESSOR BLADES (8 OFF) SUFFERED REPAIRABLE FOD DAMAGE. THE FOD WAS THEN DEFLECTED BACK THROUGH THE INLET SCREEN.
- Difficulty date
- August 12, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Beech 1900C
- Engine
- Pwa PT6A65B
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Blade
- Condition
- Damaged
- Location
- Compressor
- Stage of operation
- CR
- Nature of condition
- C
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.