Casualties unknown

Ground Loop Incident During Touchdown (N6383H)

Hurricane, UT, US

On July 19, 2002, a Cessna 150L (registration N6383H) was involved in an aviation accident near Hurricane, UT. Investigators recorded the probable cause as: The pilot's failure to maintain directional control during the landing roll, which resulted in a ground loop and off-airport departure. 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 drifted sideways during landing on a calm day. The pilot applied full power to recover but lost control, resulting in a ground loop and significant structural damage off the runway.

What happened

The pilot executed a landing with full flaps deployed. As the aircraft approached the ground, it began to drift laterally toward one side of the runway before the tail wheel made contact with the surface. In an effort to regain directional control and prevent the aircraft from leaving the paved area, the pilot applied maximum engine power. However, this input proved ineffective at counteracting the drift. The airplane subsequently entered a ground loop, pivoting violently across the runway surface. It ultimately departed the right side of the runway, coming to rest in the adjacent terrain.

The investigation

Post-accident examination revealed extensive structural damage resulting from the loss of control during the landing roll. The impact forces tore off the left main landing gear assembly. Additional damage was sustained by the engine mount, the left wing structure, the left aileron, the fuselage, and the horizontal stabilizer. These failures are consistent with the high lateral loads generated by the ground loop maneuver.

Findings

The pilot reported that wind conditions were calm at the time of the accident. The lack of crosswind component suggests that environmental factors were not the primary driver of the drift. The sequence of events indicates a failure to maintain directional control during the critical phase of touchdown and rollout. The application of full power, while intended as a recovery technique, likely exacerbated the yawing moment due to propeller slipstream effects on the vertical stabilizer or asymmetric thrust if one engine was involved, though the specific aircraft configuration is not detailed here. The ultimate loss of control resulted in the aircraft leaving the runway environment.

Safety message

Pilots must maintain strict directional control during the landing roll, particularly when drifting occurs. Relying solely on power application to correct lateral drift can be ineffective or counterproductive depending on the aircraft type and wind conditions. Proper use of rudder and brake inputs is essential to keep the aircraft aligned with the runway centerline.

Probable cause

The pilot's failure to maintain directional control during the landing roll, which resulted in a ground loop and off-airport departure.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020730X01249. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.