What was found
(CAN) DURING A HOT SECTION INSPECTION OF THE NR 1 ENGINE, DAMAGE WAS FOUND AT THE 1ST STAGE COMPRESSOR IN THE FORM OF AN AIRFOIL TIP BENT BEYOND LIMITS.
- Difficulty date
- June 1, 2014
- Submitted
- March 12, 2015
- Operation
- General aviation
- Make and model
- Beech 200BEECH
- Aircraft time
- 24,349 hours
- Engine
- Pwa PT6A41
- Propeller
- Hartzl HCB3TN3
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Compressor
- Condition
- Damaged
- Location
- Nr 1 Engine
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.