NTSB Identification: WPR09LA166
14 CFR Part 91: General Aviation
Wednesday, March 25, 2009
Paso Robles, CA
Probable Cause Approval Date:
REIMUS Sonex FR1, registration:
Injuries: 1 Serious.
NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.
During cruise flight the engine of the experimental amateur-built airplane began to run rough and then lose all power. The pilot/builder then performed a forced landing in a vineyard. During the landing sequence, the airplane struck a trellis and sustained substantial damage to the firewall and right wing. Postaccident examination of the engine revealed that the valve clearance for three of the cylinder head rocker arms was beyond adjustment tolerances; additionally, one of the pushrods was loose within the cylinder head and did not make contact with its associated rocker arm. The pilot performed maintenance about 24 flight hours prior to the accident flight which included adjusting the rocker arm valve clearance. The pilot noted in the engine logbook that the valves were gapped at the manufacturer’s recommended setting. The pilot was not aware of the engine manufacturer's requirement to apply a specific torque to the valve rocker adjustment nuts during adjustment, and as such, did not tighten the nuts to the recommended torque level.
The National Transportation Safety Board determines the probable cause(s) of this
A total loss of engine power during cruise flight due to the pilot/builder’s failure to follow the engine manufacturer’s maintenance instructions and apply the correct torque to the rocker arm nuts during maintenance.