Casualties unknown

1984-07-28: Piper J3C-65 (N38279) — Denton, TX

Denton, TX, US

On July 28, 1984, a Piper J3C-65 (registration N38279) was involved in an aviation accident near Denton, TX. Investigators recorded the probable cause as: The pilot's failure to secure the front seat belt, which looped around the right rudder pedal and prevented full application of right rudder during spin recovery. 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 1781061362Data APIEditorial standards

A pilot lost control after entering a cross-control spin during stall practice. An unsecured front seat belt had looped around the right rudder pedal, preventing recovery.

What happened

The pilot reported that following takeoff, he performed three touch-and-go landings before initiating a series of stalls. During one of these maneuvers, the aircraft entered a cross-control spin to the left. The pilot attempted to apply full right rudder pedal pressure to recover from the spin but found that he could not generate sufficient force to effect a recovery.

The investigation

A physical examination of the aircraft was conducted after the incident. Investigators discovered that the front seat belt had not been secured properly prior to flight. As a result, the belt had looped around the right rudder pedal, physically obstructing its movement and preventing the pilot from applying the necessary control input.

Findings

The inability to recover from the spin was directly caused by the mechanical obstruction of the rudder pedal. The front seat belt was not fastened correctly, which allowed it to entangle with the right rudder pedal. This prevented the application of full right rudder authority during the critical recovery phase.

Safety message

Pilots must ensure that all seat belts are properly secured and free from obstructions before flight. Loose equipment in the cockpit can interfere with control inputs, particularly during high-workload phases such as stall recovery or spin entry.

Probable cause

The pilot's failure to secure the front seat belt, which looped around the right rudder pedal and prevented full application of right rudder during spin recovery.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X40335. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.