GAA16CA022

Factual narrative

The pilot reported that he received information Papa prior to landing, information Papa was wind 240 degrees at 20 knots, and he was landing on runway 33. He reported that it "occurred" to him that it was a 20 knot direct crosswind. The pilot reported that while landing in crosswind conditions, he was "holding extreme" left aileron to compensate for the crosswind. He reported that as the airplane touched down, a gust lifted the left wing, and he was "unable to keep it down" with aileron control inputs. Subsequently the right wing impacted the runway, and the airplane ground looped. The pilot reported that there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The airplane sustained substantial damage to the right aileron. According to the manufacturer, the accident airplane's Owner's Manual does not specify a demonstrated maximum crosswind component, however a similar make and model airplane's Pilot Operating Handbook specifies a maximum demonstrated crosswind component of 12 knots. The pilot reported that he received information Papa prior to landing, information Papa was wind 240 degrees at 20 knots, and he was landing on runway 33. He reported that it "occurred" to him that it was a 20 knot direct crosswind. The pilot reported that while landing in crosswind conditions, he was "holding extreme" left aileron to compensate for the crosswind. He reported that as the airplane touched down, a gust lifted the left wing, and he was "unable to keep it down" with aileron control inputs. Subsequently the right wing impacted the runway, and the airplane ground looped. The pilot reported that there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The airplane sustained substantial damage to the right aileron.  According to the manufacturer, the accident airplane's Owner's Manual does not specify a demonstrated maximum crosswind component, however a similar make and model airplane's Pilot Operating Handbook specifies a maximum demonstrated crosswind component of 12 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

• C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
• 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
• C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Crosswind correction-Capability exceeded - C
• — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Effect on operation