BELL 407 near Mountain City, TN — 2016-06-03
- Date
- 2016-06-03
- Location
- Mountain City, TN, USA
- Aircraft
- BELL 407
- Registration
- N4999
- Category
- Helicopter
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Initial climb
Probable cause
An incorrect and unapproved repair of the engine compressor diffuser performed by a machinist at a repair facility, which resulted in failure of the compressor diffuser aft plate and a partial loss of engine power.
NTSB narrative
During the initial climb, about 125 ft above ground level, the commercial pilot of the helicopter heard a loud noise that was accompanied by a left yaw, rapidly increasing measured gas temperature, and decreasing power turbine rpm. During the subsequent forced landing, the helicopter landed hard, which spread the skids and resulted in substantial damage. Examination of the engine revealed a partial separation of the compressor diffuser, which allowed intake air to leak before combustion. Metallurgical examination of the compressor diffuser revealed that a portion of the aft plate had separated near a braze joint; however, manufacturer specifications indicated that the aft plate should have been a single component, not two components joined together by a brazing process. The compressor diffuser had been overhauled by a repair facility and installed on the accident helicopter about 98 hours of operation before the accident. Information from the repair facility revealed that a machinist had joined a second ring to the compressor diffuser aft plate using a brazing process. There was no approval for that process and it is likely that the machinist performed the procedure to correct a mistake made during a dimensional shim repair, which was an approved procedure.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Approval for compressor diffuser repair process was not obtained from manufacturer or FAA.
NTSB coding
Evidence available
- Photos
- 7 docket documents
Docket documents7
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