Incident Overview
A helicopter experienced a loss of engine power, prompting the pilot to perform an autorotation. The subsequent run-on landing on a rough field resulted in substantial damage to the aircraft.
Postaccident Findings
After the accident, testing of the magneto showed that when rotated, none of the 12 leads produced a spark. Inspection of the distributor cap revealed that none of the points opened during rotation of the magneto, indicating a malfunction within the ignition system.
Prior Indications
An FAA inspector had heard the engine running roughly on the day before the accident. The inspector advised the pilot to have the engine inspected before further flight. In response, the pilot stated that such a condition was 'common on Enstrom helicopters when the engine is hot.'