# SDR 05FDEA02226

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 3, 2005
- Submitted: August 5, 2005
- Operation: Air carrier
- Aircraft: [N671FE](https://openairdocs.org/aircraft/N671FE), registered now
- Make and model: Airbus A300 F4-605R
- Registry model: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (OpenAirDocs)
- Aircraft serial: 778
- Aircraft time: 12,695 hours, 6,847 cycles
- Engine: Ge CF680
- Engine time: 12,658 hours, 6,582 cycles
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Powerplant
- Part number: CF680C2A5F
- Part serial: 70524
- Condition: Cracked
- Location: Flange
- Part time: 12,658 hours, 6,582 cycles
- Stage of operation: NR
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/05FDEA02226

## Discrepancy

W/O 29493, NR N00177, ENGINE NR 1 AT FORWARD INBOARD LOWER HOIST POINT, THE FLANGE   IS CRACKED AT IT'S BASE.    FPI IAWM NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL.  SWAB ETCHED DAMAGED AREA   IAW TASK 70-24-01-110-34 PER GESPM STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND   PER AMM 72-23-00-8-F REMOVED AND REPLACED HOIST BRKTS IAW GE MM 72-23-01

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