Summary
On August 06, 2021, a Piper J3C-65 (N6269H) was involved in an incident near Gosport, IN. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: 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.
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.
This incident is documented in NTSB report CEN21LA359. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N6269H.
Accident Details
Probable Cause and Findings
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.
Aircraft Information
Registered Owner (Current)
Analysis
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.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA359