# SDR 95ZZZX1117

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 18, 1995
- Submitted: March 26, 2000
- Operation: General aviation
- Aircraft: N535A
- Make and model: Cessna 402B
- Registry model: [Cessna 402B](https://openairdocs.org/model/cessna-402b) (OpenAirDocs)
- Aircraft serial: 402B0591
- Engine: Cont TSIO520E
- System (JASC): [7324 · Fuel Divider](https://openairdocs.org/jasc/7324)
- Part: Flow Divider
- Part number: 63432610A9
- Condition: Defective
- Location: Engine Fuel
- Stage of operation: IN
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/95ZZZX1117

## Discrepancy

PILOT REPORTED LT ENGINE WOULD NOT MAKE A CLEAN SHUT DOWN.  INVESTIGATION REVEALED FLOW DIVIDER CHECK VALVE WAS PASSING FUEL BELOW PRESET PRESSURE.  FOUND RUBER DIAPHRAGM DRIED OUT DUE TO LACK OF USE.

---
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.
