Accident Sequence
The pilot was en route to the next field to be sprayed when, at an altitude of 500 feet, the engine lost power. Attempts to restore full power were unsuccessful, prompting the pilot to select a nearby field for an emergency landing. During the autorotative touchdown, the helicopter rolled over onto its right side.
Examination Findings
Subsequent examination of the engine revealed metal particles in the oil pump screen and oil filter element. Further inspection showed that the #1 cylinder connecting rod cap was wedged between the second crankshaft lobe and the engine case. The engine had accumulated 935.1 hours since its last major overhaul.
Examination of the helicopter structure disclosed that the landing skid and cross-tubes were fractured into several pieces. Fracture analysis indicated that all fractures were due to overload.
No other anomalies were reported.