# SDR CA020628004

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 5, 2001
- Submitted: July 8, 2002
- Operation: Air carrier
- Make and model: Airbus A310-300
- Registry model: [Airbus A310-300](https://openairdocs.org/model/airbus-industrie-a310-300) (OpenAirDocs)
- Aircraft time: 36,575 hours
- Engine: Ge CF680C2A5
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Blade
- Condition: Damaged
- Location: Compressor
- Stage of operation: TO
- How discovered: O
- Nature of condition: C, J
- Precautionary procedure: C
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA020628004

## Discrepancy

(CAN) COMPRESSOR STALL ON TAKE OFF IN LRM, ON ENGINE NR 2 , MTCE FOUND AFTER VISUAL INSPECTION, 2 BLADES DAMAGED. FURTHER INSPECTION C/OUT IN ACCORDANCE WITH AMM 72-00-00 P.600, REVEALED DAMAGE ON HIGH PRESSURE COMPRESSOR. NUMEROUS BLADES NICKED, CURLED, TORN OR PARTIALLY MISSING. DAMAGE NOT WITHIN LIMITS I.A.W. AMM 72-31-00 P.602. MAINTENANCE REPLACED THE ENGINE I.A.W. AMM 71-00-00.

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