No fatalities

1 Sep 2020: Stinson 108-3 (N909C) — Pilot — Coleman, MI

Coleman, MI, United States

On 1 Sep 2020, a Stinson 108-3 (registration N909C) operated by Pilot was involved in an aviation accident near Coleman, MI. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s improper installation of the generator drive gear, which resulted in a total loss of engine power. This summary draws on records from NTSB; 17 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On September 1, 2020, a Stinson 108-3 experienced total engine power loss and made a forced landing in a soybean field, nosing over. The pilot was uninjured. Postaccident examination found a missing cotter pin on the generator drive gear.

Accident Details

On September 1, 2020, at 1100 eastern daylight time, a Stinson 108-3, registration N909C, was substantially damaged when it was involved in an accident near Coleman, Michigan. The pilot was uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Forced Landing

The pilot stated that the airplane had been flying for about 45 minutes before it experienced a total loss of engine power. The pilot then performed a forced landing to a soybean field, where it rolled for about 180 feet and nosed over. This resulted in substantial damage to the fuselage and empennage.

Postaccident Examination

Postaccident examination of the engine, conducted by a Federal Aviation Administration representative, revealed that the single generator drive gear for the ignition system had separated into several pieces. The drive gear shaft installation called for a castellated nut with a cotter pin to retain the drive gear, but the cotter pin had not been installed. This allowed the nut to back off. The generator was installed by the pilot, who did not hold a mechanic certificate, during his overhaul of the engine. The pilot stated that he performed the overhaul and installation under the supervision of a mechanic with an airframe and powerplant ratings. No other mechanical anomalies with the engine were noted.

Contributing factors

Magneto/distributor — FailureMaintenance personnelPilot