Casualties unknown

Stall and Spin in Valley Results in Fatal Crash (N13900)

Glenallen, AK, US

On August 28, 1994, a Piper PA-18 (registration N13900) was involved in an aviation accident near Glenallen, AK. Investigators recorded the probable cause as: The pilot's failure to maintain adequate airspeed during a steep turn, which resulted in an aerodynamic stall and subsequent spin into terrain, exacerbated by gusty wind conditions. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A light aircraft stalled and spun into the ground while executing a steep turn in mountainous terrain. Strong wind gusts were present during the incident.

What happened

The accident occurred when an airplane crashed while attempting to reverse its direction of flight within a valley environment. According to the sole survivor, who was seated in the rear and survived only briefly before succumbing to injuries, the crew was executing a steep left-hand turn at the time of the incident. During this maneuver, the aircraft entered a stall and subsequently spun directly into the ground.

The passenger noted that he did not have access to the flight controls from his position in the rear seat. He expressed the opinion that if he had been able to manipulate the controls, he might have successfully recovered the aircraft prior to impact. The weather conditions in the area were reported as having winds estimated at 10 knots with gusts reaching up to 50 knots.

The investigation

Investigative efforts focused on the physical evidence of the crash site and the testimonial account provided by the surviving passenger. The mechanical condition of the aircraft prior to impact was not detailed in the available records, but the flight dynamics described suggest a loss of control due to aerodynamic stall during a high-load maneuver.

Findings

Several critical factors contributed to this fatal accident. The primary cause was the stall and spin initiated during a steep turn. Environmental conditions played a significant role, with wind gusts to 50 knots creating turbulent air that likely exacerbated the stall characteristics or made recovery more difficult. The terrain in the valley provided no margin for error once the aircraft entered the unrecoverable spin attitude.

The flight phase was identified as a maneuvering segment where the pilot attempted to reverse direction. The combination of steep bank angles, potential wind shear, and the inherent risks of low-altitude turning flight led to the catastrophic loss of control. 1 fatal injury was reported among those on board, with no survivors remaining after the initial impact.

Safety message

This accident highlights the extreme danger of performing steep turns in confined valleys, particularly when weather conditions include strong wind gusts. Pilots must be acutely aware that stall speeds increase significantly with bank angle and that recovery from a spin at low altitude often leaves insufficient altitude to regain controlled flight. Understanding aircraft performance limits in turbulent air is essential for survival in mountainous terrain.

Probable cause

The pilot's failure to maintain adequate airspeed during a steep turn, which resulted in an aerodynamic stall and subsequent spin into terrain, exacerbated by gusty wind conditions.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X01924. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.