# SDR CA021129011

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 7, 2002
- Submitted: January 6, 2003
- Operation: Air carrier
- Make and model: Bell 206B
- Registry model: [Bell 206B](https://openairdocs.org/model/bell-206b) (OpenAirDocs)
- Aircraft time: 11,174 hours
- Engine: Allsn 250C20B
- System (JASC): [7261 · Turbine Engine Oil System](https://openairdocs.org/jasc/7261)
- Part: Connector
- Part number: 6848194
- Condition: Leaking
- Location: Engine Oil
- Stage of operation: IN
- How discovered: C
- Nature of condition: K
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA021129011

## Discrepancy

(CAN) AME INSTALLED TURBINE ASSEMBLY FOLLOWING OVERHAUL.   ON GROUND RUN SEVERE OIL LEAK WAS OBSERVED FROM 6 & 7 PRESSURE OIL CONNECTOR ('TEE FITTING) AREA.  INSPECTION REVEALED THAT TWO RETAINING BOLTS HAD LESS THAN 10 IN/LBS. BREAK TORQUE.  AME REPLACED CRUSH SEALS, REASSEMBLED TUBING AND AFTER SATISFACTORY GROUND RUN, RETURNED A/C TO SERVICE.

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