No fatalities

Engine Crankshaft Fatigue Leads to Forced Landing and Power Line Strike in Idaho (N7306U)

Boise, United States of AmericaTakeoff (climb)

On August 27, 1982, a Cessna 207 Skywagon/Stationair (registration N7306U) operated by Salmon Air was involved in an aviation accident near Boise, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: loss of engine power(total) - mech failure/malf - Phase of operation: takeoff - initial climb - Findings: (c) engine assembly, crankshaft - fatigue; Occurrence #2: forced landing - Phase of operation: approach; Occurrence #3: in flight… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

During initial climb from Boise to Salmon, the engine surged and lost power. An emergency landing resulted in a collision with a utility pole and subsequent crash. Investigation found crankshaft fatigue.

Accident Overview

The pilot filed a company flight plan for a VFR flight from Boise to Salmon, Idaho. During initial climb, the engine surged, then seemed to return to normal operation. The pilot reduced power to 33 inches of manifold pressure and set the propeller to 2,550 rpm. Shortly thereafter, the engine began losing power again, experienced a second surge, and then the propeller stopped.

Emergency Landing

During the emergency landing, the pilot elected to cross over a road and land in an open field. He saw a power line along the road at the edge of the field and chose to cross under it. However, he did not see a single telephone pole on the opposite side of the road. The left wing struck the pole, causing the aircraft to cartwheel and crash. Three occupants escaped with minor injuries; four others were uninjured.

Investigation Findings

An investigation revealed that the crankshaft had failed from fatigue. The official findings identified four occurrences: loss of engine power due to mechanical failure (crankshaft fatigue), a forced landing, an in-flight collision with an object (utility pole), and an in-flight collision with terrain. The pilot performed the maneuver during the approach phase, and terrain conditions included high obstructions (utility pole).

Probable cause

Occurrence #1: loss of engine power(total) - mech failure/malf - Phase of operation: takeoff - initial climb - Findings: (c) engine assembly, crankshaft - fatigue; Occurrence #2: forced landing - Phase of operation: approach; Occurrence #3: in flight collision with object - Phase of operation: approach - vfr pattern - final approach - Findings: (f) terrain condition - high obstruction(s); (3) Maneuver - performed - pilot in command; (f) object - utility pole; Occurrence #4: in flight collision with terrain/water - Phase of operation: descent - uncontrolled