4 fatalities

Fatal Aircraft Accident at Simplot Ranch Airstrip (N9006)

Challis, United States of AmericaFlight

On November 5, 1983, a De Havilland DHC-2 Beaver (registration N9006) operated by Air Unlimited was involved in an aviation accident near Challis, United States of America in flight. 4 people were killed. Investigators recorded the probable cause as: Occurrence #1: loss of control - in flight during maneuvering - turn to reverse direction. Contributing factors included mountainous/hilly, high, and rising terrain conditions; improper in-flight planning/decision by the pilot in command; inadequate clearance… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards
Aircraft registered N9006
Aircraft registered N9006. Photo: Lord of the Wings© from Toronto, Canada / CC BY-SA 2.0, via Wikimedia Commons

An aircraft crashed in a bench area near the Salmon River after a turn-around attempt. All four occupants were killed. No pre-impact mechanical failure was found.

Departure and Flight Path The pilot departed from the Simplot Ranch Airstrip, situated beside the middle fork of the Salmon River, approximately 27 miles northwest of Challis, Idaho. The aircraft initially headed downriver toward the northeast, although the intended destination was a U.S. Forest Service strip located about 7 miles upriver to the southwest. A course reversal was typically executed approximately 6 miles downriver from the departure point. However, the pilot attempted a turn-around over a relatively shallow bench area on the west side of the river, roughly 1.25 miles from the departure strip. According to the operator, this maneuver could have been performed under ideal conditions. The aircraft crashed in the bench area while maintaining a westerly heading. It came to rest in an upright attitude with minimal evidence of forward velocity but significant vertical collapse. No evidence of pre-impact mechanical malfunction or failure was discovered. All four occupants were killed in the accident.

Probable cause

Occurrence #1: loss of control - in flight during maneuvering - turn to reverse direction. Contributing factors included mountainous/hilly, high, and rising terrain conditions; improper in-flight planning/decision by the pilot in command; inadequate clearance by the pilot in command; airspeed not maintained by the pilot in command; and an inadvertent stall by the pilot in command. Occurrence #2: in flight collision with terrain/water during maneuvering - turn to reverse direction.