2 fatalities

Test Flight Ends in Stall and Collision with Terrain, Two Killed (N81502)

Checotah, United States of AmericaFlight

On October 9, 1984, a Rockwell Gulfstream 695A Jetprop 1000 (registration N81502) operated by Gulfstream Aerospace Corporation (GAC Corporation) was involved in an aviation accident near Checotah, United States of America in flight. 2 people were killed. Investigators recorded the probable cause as: Loss of control due to airspeed not maintained (pilot in command) and inadvertent stall/spin (pilot in command), followed by in-flight collision with terrain during uncontrolled descent. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 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 a test flight involving VMC demonstrations and maximum performance single-engine climbs, the pilot allowed the aircraft to stall at low altitude. The aircraft struck the ground, killing both occupants.

Accident Sequence

During a test flight, the pilot was performing a VMC (minimum control speed) test and maximum performance single-engine climbs. Witness descriptions of the aircraft's movements at the beginning of the accident sequence indicate that the VMC test was in progress immediately before the accident occurred. The pilot allowed the aircraft to stall at an altitude that was too low to permit recovery before ground impact occurred. The subsequent collision with terrain resulted in the deaths of both occupants.

Official Findings

The investigation identified two occurrences: first, a loss of control during maneuvering in flight, and second, an in-flight collision with terrain during an uncontrolled descent. The probable cause for the loss of control was determined to be:

  • The pilot's failure to maintain airspeed, leading to an inadvertent stall/spin.

The collision with terrain was the outcome of the uncontrolled descent following the loss of control.