What was found
(CAN) DURING APPROACH, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION ACCOMPANIED BY NOISE AND VIBRATION. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT ISPECTION REVEALED A FRACTURED INLET CASE STRUT. (TC NR 20060129016)
- Difficulty date
- December 13, 2005
- Submitted
- June 6, 2006
- Operation
- General aviation
- Make and model
- Bell 212
- Engine
- Pwa PT6T3B
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Case
- Condition
- Fractured
- Location
- Compressor
- Stage of operation
- AP
- How discovered
- O
- Nature of condition
- R, E, J
- Precautionary procedure
- E
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.