No fatalities

Cessna 182K Runway Departure at Branson West Municipal Airport (N2893R)

Branson West, MO, United States

On October 30, 2011, a CESSNA 182K (registration N2893R) operated by BRIGMAN PRODUCTIONS INC was involved in an aviation accident near Branson West, MO. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to ensure that his seat was in a locked position before takeoff, which resulted in the seat sliding rearward and the subsequent loss of directional control. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

A Cessna 182K, N2893R, sustained substantial damage after departing the runway during takeoff at Branson West Municipal Airport on October 30, 2011. The pilot and three passengers were uninjured.

Incident Overview and Flight Details On October 30, 2011, at approximately 1111 central daylight time, a Cessna 182K with the registration N2893R sustained substantial damage when it departed the runway during takeoff and struck a ditch. The incident occurred at Branson West Municipal Airport (FWB) in Branson West, Missouri. The aircraft was registered to Brigman Productions, Inc., and the pilot was operating it under 14 Code of Federal Regulation Part 91 as a personal flight. The flight was originating at the time of the accident, with an intended destination of Hutchinson Municipal Airport (HUT) in Hutchinson, Kansas. Visual meteorological conditions prevailed, and the flight was not operated on a flight plan. No injuries were reported to the pilot or his three passengers. ## Pilot Account and Mechanical Factors The pilot reported that the pilot seat released and slid rearward during the takeoff roll. He stated that he reduced engine power and could still reach the rudder pedals, but was unable to actuate the brakes. Subsequently, the airplane went off the runway and struck a drainage ditch. ## Regulatory Compliance and Post-Accident Examination On June 17, 2011, the Federal Aviation Administration issued Airworthiness Directive (AD) 2011-10-09, which replaced a previous directive. The AD required repetitive inspections and replacement of parts, if necessary, for the seat rail and seat rail holes, seat pin engagement, seat rollers, washers, and axle bolts or bushings, the wall thickness of the roller housing and the tang, and lock pin springs. The airplane's most recent annual inspection, dated October 12, 2011, indicated that AD 2011-10-09 had been complied with and no defects were noted. Additionally, a post-accident examination of the seat mechanism by Federal Aviation Administration inspectors revealed no anomalies.

Contributing factors

Incorrect use/operationDirectional control — Not attained/maintainedPilot