Accident Details
During an aerial application flight, the pilot was maneuvering at approximately 15 feet above an alfalfa field when a noise emanated from the engine, followed by engine seizure. The pilot executed a forced landing in the underlying soft field. Upon touchdown, the helicopter rolled over due to the uneven terrain.
Maintenance History
A review of maintenance records indicated that the engine had operated about 482 hours since its last overhaul.
Engine Examination
Post-accident examination of the engine revealed that the number two connecting rod was broken at its crankshaft end. Inspection of the associated cylinder and piston showed evidence of detonation. Similar excessive heat exposure signatures were observed on the other five piston heads. Additionally, a small hole was found chaffed into the fuel primer line. Carbon deposits and burned rotor fingers were present in both magnetos.
Findings
The investigation documented the mechanical failures and conditions found, but no probable cause was stated in the source.