# SDR 2011F00121

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 6, 2010
- Submitted: May 27, 2011
- Operation: General aviation
- Aircraft: APBEU
- Make and model: Airbus A310-300
- Registry model: [Airbus A310-300](https://openairdocs.org/model/airbus-industrie-a310-300) (OpenAirDocs)
- Engine: Ge CF680C2A8
- Engine time: 43,619 hours, 13,874 cycles
- System (JASC): [7250 · Turbine Section](https://openairdocs.org/jasc/7250)
- Part: Blade
- Part number: 1538M90P12
- Part serial: PCMFFEP4
- Condition: Broken
- Location: Hpt Stage 1
- Part time: 9,195 hours, 3,380 cycles
- Stage of operation: IN
- How discovered: B
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/2011F00121

## Discrepancy

HPT STAGE 1 BLADE FOUND BROKEN AND MISSING DURING ROUTINE BSI, ON FOLLOWING CF6-80C2A8 ENGINES  SN  659611, 659399, 659526, 659392, 659408, 659612, 659414.  SECONDARY DAMAGE WAS ALSO OBSERVED ON NUMBER OF BLADES.  ALL THE BLADES WAS NEW WHEN INSTALLED.

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