# SDR CA021117002

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 10, 2002
- Submitted: December 2, 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: 35,988 hours
- Engine: Ge CF680C2A5
- System (JASC): [7500 · Engine Bleed Air System](https://openairdocs.org/jasc/7500)
- Part: Duct
- Part number: 13842515
- Condition: Cracked
- Location: Engine
- 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/CA021117002

## Discrepancy

(CAN) BLEED DUCT ON AIRFRAME SIDE OF ENGINE BLEED VALVE ON TAKE TO REVERSER AIR MOTOR OF NR 1 ENGINE WAS FOUND CRACKED AND SEVERELY LEAKING. DUCT WAS REPLACED AND A LEAK CHECK WAS CARRIED OUT AND NONE WERE FOUND.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.