CESSNA 172 near Oloh, MS — 2017-11-25
- Date
- 2017-11-25
- Location
- Oloh, MS, USA
- Aircraft
- CESSNA 172
- Registration
- N739KW
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Climb
Probable cause
A partial loss of engine power due to the failure of the No. 3 valve key (exhaust).
NTSB narrative
The pilot reported that, while the airplane was about 3,500 ft above mean sea level, the engine produced a "very rapid metallic banging/clanging noise," along with an instant loss of engine rpm. The engine was creating a "violent shaking" of the entire airframe. After about 20 seconds of applying carburetor heat, the pilot applied full mixture and started adjusting the throttle to obtain more power. He reported that, with more power applied, the shaking became more violent, along with a loss of engine rpm. The pilot realized that the engine power at this point was not sufficient to hold altitude. During a forced landing to a field, both wings and the fuselage sustained substantial damage. Examination of the airframe and propeller found no preimpact mechanical malfunctions or failures that would have precluded normal operation. Examination of the engine revealed the No. 3 piston area displayed internal impact marks from the piston impacting the exhaust valve. The No. 3 exhaust valve was open and displayed impact marks from contact with the piston. The No. 3 valve spring seat (upper exhaust) was impact damaged with fractured pieces of the valve key (exhaust) and the valve stem cap (exhaust) laying on the bottom of the rocker area of the cylinder head. The No. 3 exhaust valve assembly moved freely inside the valve seats and was contacting the top of the piston. Based on the available evidence, the partial loss of engine power was likely due to the No. 3 valve key (exhaust) failing, which resulted in a substantial reduction in engine power output. The reason for the failure was undetermined, as the service history of the valve key was unknown.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have opted for an emergency landing sooner after engine power loss.
NTSB coding
Evidence available
- Photos
- 5 docket documents
Docket documents5
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