No fatalities

Stinson 108 Forced Landing After Engine Failure in Missouri (N8775K)

Halfway, MO, United States

On December 5, 2012, a STINSON 108-2 (registration N8775K) operated by HUFF MIKE W was involved in an aviation accident near Halfway, MO. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to properly maintain the airplane and engine, which resulted in a total loss of engine power due to improperly installed magnetos and a broken camshaft. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

On December 5, 2012, a Stinson 108 (N8775K) made a forced landing near Halfway, Missouri, after engine power loss. The pilot sustained minor injuries; the aircraft was substantially damaged.

Accident

On December 5, 2012, at 1300 central standard time, a Stinson 108, registration N8775K, experienced a loss of engine power and executed a forced landing to a field near Halfway, Missouri. The private pilot, who was the sole occupant, sustained minor injuries. The airplane was substantially damaged. The flight had departed Eads Ridge Airport (MO68), Fair Grove, Missouri, at 1240. Visual meteorological conditions prevailed for the personal flight conducted under 14 Code of Federal Regulations Part 91, and no flight plan was filed.

Aircraft Damage and Engine Examination

According to an FAA aviation safety inspector who interviewed the pilot and examined the airplane, the pilot reported that after about 20 minutes of flight, the engine began making an unusual grinding noise, followed by a loss of power. During the forced landing attempt, the left main landing gear struck a powerline. The airplane landed hard, resulting in substantial damage to both wings, the fuselage, and an engine mount. The left main landing gear and propeller were also damaged. Examination of the engine revealed that the magnetos were not properly secured to the engine and were loose. When the magnetos were removed, the inspector visually observed that the camshaft was broken.

Maintenance and Pilot Information

A review of the engine maintenance logbooks showed that the airplane's last annual inspection was conducted on January 8, 2008. The pilot held a private pilot certificate for airplane single-engine land. His last FAA third-class medical certificate was issued on March 4, 2009, and his last biennial flight review was completed on August 31, 2008. The pilot reported a total flight time of 761 hours, of which 437 hours were in the accident airplane. He stated that he had flown approximately 3 hours in the 90 days prior to the accident and was preparing for a biennial flight review when the event occurred.

Contributing factors

Engine (reciprocating) — FailurePilot