1 fatality

14 Aug 2025: CESSNA 172L (N2860Q) — Pilot — Walters, OK

Walters, OK, United States

On 14 Aug 2025, a CESSNA 172L (registration N2860Q) operated by Pilot was involved in an aviation accident near Walters, OK. One person was killed. This summary draws on records from NTSB; 17 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Cessna 172L (N2860Q) was destroyed in an accident near Walters, Oklahoma, on August 14, 2025. The pilot sustained fatal injuries. The airplane was operated under Part 91 as a personal flight.

Accident Details

On August 14, 2025, at approximately 0934 central daylight time, a Cessna 172L, registration N2860Q, was destroyed when it impacted terrain near Walters, Oklahoma. The pilot, who was the sole occupant, sustained fatal injuries. The airplane was operated under Title 14 Code of Federal Regulations as a Part 91 personal flight.

Pilot Information

The pilot was an independent flight instructor based at Lawton-Fort Sill Regional Airport (LAW) in Lawton, Oklahoma. The airport authority permitted the pilot to use the airplane for pilot proficiency purposes. Airport personnel were unaware of the pilot's schedule for any flight training activity on the day of the accident, as the pilot maintained that schedule independently. An airframe and powerplant mechanic at LAW stated that the pilot did not report any mechanical discrepancies with the airplane before the flight.

Flight History

Radar data indicated that the airplane departed from runway 17 at LAW at about 0833. After departure, the airplane proceeded eastbound for approximately 10 miles before beginning a series of turns while maintaining a relatively constant altitude with no large deviations. During the final minute of radar data, the airplane executed a right turn and proceeded northbound, decreasing in altitude and gaining airspeed until the radar track ended.

Wreckage and Impact

The accident site exhibited features consistent with a nose-down, high-speed impact with terrain. The airspeed indicator, which had separated from the main wreckage, indicated approximately 155 knots. Ground scarring included a hole several inches deep where the airplane nose struck, surrounded by scars from the main landing gear wheels and both wings. The wings, fuselage, empennage, and control surfaces were contained within the main wreckage. Both wings were crushed inward to their respective main wing spars, and the wing flaps were in the retracted position. The airplane's pitch trim was approximately in the neutral position. The propeller separated from the engine and displayed rotational features including chordwise scratching and twisting.