# SDR DXTR2026090201

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 2, 2026
- Submitted: September 2, 2026
- Operation: General aviation
- Aircraft: [N572QS](https://openairdocs.org/aircraft/N572QS), registered now
- Make and model: Cessna 680A
- Registry model: [Cessna 680A](https://openairdocs.org/model/cessna-680a) (OpenAirDocs)
- 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](https://openairdocs.org/jasc/7230)
- 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
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DXTR2026090201

## Discrepancy

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.

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