# SDR CA980330019

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 8, 1998
- Submitted: January 19, 2001
- Operation: General aviation
- Make and model: Beech 200BEECH
- Aircraft time: 10,067 hours
- Engine: Pwa PT6A41
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Part number: 310092205
- Condition: Faulty
- Location: Nr 1 Engine
- Part time: 2,175 cycles
- Component: Pwa
- Stage of operation: CL
- How discovered: O
- Nature of condition: R
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA980330019

## Discrepancy

(CAN) DURING CLIMB THE NR 1  ENGINE WAS TEMPERATURE LIMITED. THE NR 1 ENGINE POWER LEVER WAS STAGGERED 1 INCH BEHIND ITS NORMAL POSITION. FLIGHT CONTINUED AT REDUCED POWER TO NEXT AVAILABLE AIRPORT. NO FAULT FOUND ON GROUND RUN, BOTH BLEED VALVES (P/NS 310092205 & 310092302) WERE REPLACED AND THE T5 SYSTEM WAS CHECKED AS A PRECAUTION. NO FURTHER PROBLEMS WERE ENCOUNTERED.

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