N6269H accident

NTSB CEN21LA359 · 2021-08-06 · Gosport, IN

Docket — crew, injuries and powerplant

Summary

The pilot stated that, during cruise flight, the airplane experienced “significant” vibration, which was followed by a total loss of engine power. The pilot performed a forced landing to a field, during which the airplane nosed over and impacted terrain. Postaccident examination of the airplane engine revealed that the No. 4 cylinder exhaust valve stem was broken at its base and the seat was turned sideways. Pieces of the stem were found in the cylinder. The failure of the exhaust valve resulted in reduced engine compression leading to the total loss of engine power.

Full narrative

On August 5, 2021, about 2030 eastern daylight time, a Piper J3C-65, N6269H, was substantially damaged when it was involved in an accident near Gosport, Indiana. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that, during cruise flight, the airplane experienced “significant” vibration, which was followed by a total loss of engine power. The pilot performed a forced landing to a field that caused the airplane to nose over and impact terrain, resulting in substantial damage to the rudder and cowling.

Postaccident examination of the airplane engine revealed that the No. 4 cylinder exhaust valve stem was broken at its base. The valve seat was turned sideways, and pieces of broken metal were found in the cylinder. The cylinder’s rockers and springs did not exhibit any failure.

Probable cause

A total loss of engine power during cruise flight due to the failure of a cylinder exhaust valve stem, which led to a forced landing during which the airplane impacted terrain. The National Transportation Safety Board determined the probable cause of this accident.

Circumstances

Event type
Accident
Highest injury
None
Weather conditions
Visual Meteorological Cond
Light condition
Day
Sky condition
NONE
Ceiling (ft)
0
Visibility (sm)
10
Wind direction
0
Temperature (F)
77
Distance from field
0.0

Aircraft

RegistrationMakeModelDamageFAR part
N6269H — — SUBS 091

Sequence of events

#OccurrencePhase
1 Enroute Loss of engine power (total) Climb
2 Landing Off-field or emergency landing Cruise
3 Landing Collision during takeoff/land Cruise
4 Enroute Powerplant sys/comp malf/fail defining Climb

Findings

Finding
Aircraft-Aircraft power plant-Engine (reciprocating)-(general)-Failure cause