What was found
FAULT: DURING 100 HR 2ND STAGE HPT BORESCOPE RE-INSPECT OF ENGINE, FOUND PREVIOUS CRACK ON SUCTION SIDE OF BLADE HAS MIGRATED BEYOND LIMITS. RESOLUTION: REMOVED ENGINE UNSERVICEABLE & RETURNED TO PWC FOR REPAIR.
- Difficulty date
- September 2, 2026
- Submitted
- September 2, 2026
- Operation
- General aviation
- Aircraft
- N572QS
- Make and model
- Cessna 680A
- Aircraft serial
- 680A0133
- Aircraft time
- 8,869 hours, 5,871 cycles
- Engine
- Pwc PW306D1
- Engine time
- 9,281 hours, 6,170 cycles
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Compressor Blade
- Part number
- 30B770301
- Condition
- Cracked
- Location
- 2nd Stage Hpt
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.