# SDR AUS20030590

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 1, 2003
- Submitted: July 14, 2003
- Operation: General aviation
- Make and model: Cessna 210A
- Registry model: [Cessna 210A](https://openairdocs.org/model/cessna-210a) (OpenAirDocs)
- Engine: Cont IO470E
- Propeller: Hartzl HCA2XF1
- System (JASC): [7820 · Engine Noise Suppressor](https://openairdocs.org/jasc/7820)
- Part: Muffler
- Part number: 125025113
- Condition: Cracked
- Location: Engine Exhaust
- Part time: 2,809 cycles
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AUS20030590

## Discrepancy

(AUS) RT MUFFLER PIPE CRACKED FOR APPROXIMATELY 75 PERCENT OF CIRCUMFERENCE AROUND JOINT AREA. CRACK WAS HIDDEN BY EXHAUST CLAMPS.

---
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.
