Incident Overview
While cruising at 4,000 feet MSL, the engine quit without warning. The pilot was forced to execute an emergency landing on rolling farm terrain.
Forced Landing and Impact
During the landing, both main landing gear separated from the aircraft. The aircraft then slid through a barbed wire fence before coming to a stop.
Fire
Following the slide through the fence, the aircraft caught fire.
Metallurgical Examination
A metallurgical examination was conducted on the failed engine component. The examination revealed a fatigue failure of the idle set screw (part number 2424273-10) that controls the diaphragm setting in the Bendix fuel injection system. The stem of the screw failed as a result of reversed bending stresses caused by side-to-side forces. The source noted that this type of failure could not be explained, as the principal force applied to the adjustment screw would primarily be a twisting motion rather than a side-to-side applied force.