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GAA16CA239

2016-04-23 · Defuniak Springs, Florida, United States · None · 1 aircraft · Status: Completed

Airport 54J

Aircraft involved

Probable cause & findings

The pilot's loss of directional control during the landing in gusting crosswind conditions resulting in a runway excursion, and the pilot's failure to attain a positive climb rate during the aborted landing and subsequent ground collision.

Factual narrative

According to the pilot of the tailwheel-equipped airplane, during the landing roll, the airplane encountered a crosswind gust and he applied right rudder. He reported that a subsequent wind gust lifted the right wing, triggering a ground loop to the right and the airplane exited the right side of the runway. He recalled that the airplane was headed for a water drainage catch basin and he decided to add full power, and attempt to fly out of the ground loop in an effort to avoid the catch basin. The right wheel of the airplane collided with the perimeter of the catch basin and the airplane spun to the right. The airplane sustained substantial damage to the left wing lift strut. According to the nearest meteorological aerodrome report, 19 miles south, the wind about the time of the accident was variable at 3 knots. The pilot landed on runway 27. The pilot reported that there were no mechanical anomalies or malfunctions with any portion of the airplane or engine prior to the accident that would have prevented normal flight operations. According to the pilot of the tailwheel-equipped airplane, during the landing roll, the airplane encountered a crosswind gust and he applied right rudder. He reported that a subsequent wind gust lifted the right wing, triggering a ground loop to the right and the airplane exited the right side of the runway. He recalled that the airplane was headed for a water drainage catch basin and he decided to add full power, and attempt to fly out of the ground loop in an effort to avoid the catch basin. The right wheel of the airplane collided with the perimeter of the catch basin and the airplane spun to the right. The airplane sustained substantial damage to the left wing lift strut. According to the nearest meteorological aerodrome report, 19 miles south, the wind about the time of the accident was variable at 3 knots. The pilot landed on runway 27. The pilot reported that there were not any mechanical anomalies or malfunctions with any portion the airplane prior to the accident that would have prevented normal flight operations. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Crosswind correction-Not attained/maintained - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Climb rate-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Effect on equipment
  • — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on equipment

Verbatim from NTSB's published report. Source file NTSB_2016_GAA16CA239.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (runway excursion). All research papers