Casualties unknown

1996-01-28: Cessna 152 (N757UK) — Harry D Barrett — Conway, AR

Conway, AR, US

On January 28, 1996, a Cessna 152 (registration N757UK) operated by Harry D Barrett was involved in an aviation accident near Conway, AR. Investigators recorded the probable cause as: loss of engine power for undetermined reason(s), and failure of the pilot to maintain adequate airspeed, while maneuvering for a forced landing, which resulted in an inadvertent stall at low altitude. The gusty wind condition was a related factor. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

After 75 minutes of uneventful flight, the engine RPM began fluctuating and dropped into the teens, causing a loss of level flight. During a circling approach to a field, gusty winds were encountered, and the aircraft stalled, impacting the ground left wing down at a 45-degree nose-down angle.

Flight and Engine Malfunction

After approximately 75 minutes of uneventful flying, the engine RPM began to fluctuate. The pilot attempted to adjust the throttle and mixture, but noticed that the engine RPM had dropped into the teens. Level flight could not be maintained.

Approach and Descent

Gusty winds were encountered during a circling approach to a large, flat field. During the final descending turn, the pilot recalled that the airplane's nose was diving quickly toward the ground, and the stall warning activated briefly.

Witness Observations and Impact

Witnesses reported that the aircraft was maneuvering slowly and low to the ground, then it descended steeply and crashed. Ground scars indicated that the aircraft impacted with the left wing down and at approximately 45 degrees nose down relative to the terrain.

Investigation Findings

Atmospheric conditions were not conducive for carburetor icing. Fuel samples from the aircraft and the refueling source were found to be within standards. With the exception of worn or fouled spark plugs and out-of-tolerance valve tappet clearances, no conclusive mechanical anomalies were discovered. The engine was operated to 2360 RPM in a factory test cell, but the run was terminated due to vibrations induced from impact damage.

No probable cause was determined by the investigation.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X05128. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.