Casualties unknown

Float-Equipped Cessna 150F Experiences Uncommanded Spin During Stall Demonstration (N6296R)

Anchorage, AK, US

On July 20, 2000, a Cessna 150F (registration N6296R) operated by Craig L. Ketchum was involved in an aviation accident near Anchorage, AK. Investigators recorded the probable cause as: The failure of the pilot-in-command (CFI) to adequately supervise the instructional flight. Factors in the accident were an inadvertent spin entry by the student, and the pilot-in-command's failure to utilize adequate altitude for a stall demonstration. 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 flight instructor and his daughter, the student pilot, were conducting a stall demonstration in a float-equipped Cessna 150F when the aircraft entered an uncommanded inverted left spin. The instructor recovered at 300 feet AGL, but the aircraft struck the ground during the nose-down descent.

Accident Details

A flight instructor, who also owns the aircraft, was providing flight instruction to his daughter in a Cessna 150F equipped with floats. The instructor was demonstrating an approach-to-landing stall at approximately 2,000 feet mean sea level with 20 degrees of flaps deployed. During the stall, the student pilot applied cross-control inputs, causing the left wing to drop and the airplane to enter an uncommanded inverted left spin. The instructor regained upright flight at about 300 feet above ground level by increasing engine power. During the recovery, the airplane descended in a nose-down attitude and struck the ground.

Aircraft Information

The Cessna 150F had been modified with a 160-horsepower engine and fixed floats. The aircraft qualified for float installation when the previous owner/mechanic designated it as a Cessna 150G. Configuration changes included different propellers, propeller spacers, larger wheels and tires, and a heavier nose wheel strut assembly. As a floatplane, the airplane was required to be operated in the normal category, and intentional spins were prohibited.

Pilot and Operational Factors

The instructor reported that no data was available to him about the consequences or recovery techniques for an inadvertent spin. A center of gravity calculation for the accident flight placed the airplane within approved weight and balance limits. Toxicological analysis of the pilot's samples revealed the presence of an over-the-counter antihistamine and a prescription anti-depression medication.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X21359. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.