CEN12CA117
2011-12-17 · Atchison, Kansas, United States · None · 1 aircraft · Status: Completed
Airport K59
Aircraft involved
Probable cause & findings
The pilot's inadequate directional control during the landing roll.
Factual narrative
During the landing roll, the airplane swerved to the left side of the runway. The pilot attempted to regain directional control of the tailwheel equipped airplane by applying left aileron, right rudder, and wheel brake to no avail. The airplane departed the edge of the runway into an area of soft ground and nosed over. During the accident the airplane’s fuselage sustained substantial damage. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. During the landing roll, the airplane swerved to the left side of the runway. The pilot attempted to regain directional control of the tailwheel-equipped airplane by applying left aileron, right rudder, and wheel brake to no avail. The airplane departed the edge of the runway into an area of soft ground and nosed over, sustaining substantial damage to the fuselage. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2011_CEN12CA117.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.