What was found
ENGINE REMOVED FOR EGT LIMITATION. DISASSEMBLY INSPECTION DETECTED CRACKED BLADE SLOTS ON DISK (6TH STAGE). DISK REMOVED FROM ROTOR AND FORWARDED TO PRATT & WHITNEY ENGINEERING IN THE BLADED CONDITION. CYCLES: 2,127.
- Difficulty date
- August 1, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa F117PW100
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Disk
- Part number
- 1B3506
- Condition
- Cracked
- Location
- Hpc Module
- Part time
- 857 hours
- 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.