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Atlas / NTSB / WPR11CA237

NTSB CAROL · Event

Event WPR11CA237

2011-05-26 Sedona, Arizona, United States Airport · KSEZ None 1 aircraft Status: Completed

Registry · N7792P

FAA Aircraft Registry record.

Make / Model

PIPER PA-24-250

Year of manufacture

1962 · 49 years old at event

Engine

LYCOMING 0-540 SERIES (250 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19620116

ADS-B equipped

Yes — Mode-S AA8D22

Registrant of record

ADKINS BRIAN KEITH

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain directional control on the landing roll out. Contributing to the accident was the pilot's decision to attempt a landing in crosswind conditions that exceeded the maximum demonstrated capability of the airplane.

Factual narrative

Prior to entering the traffic pattern with the intention to land, the pilot contacted the pilot of an airplane that had just landed to inquire about the wind conditions. The pilot that had landed reported the wind was “a little squirrelly but not bad.” The pilot elected to continue his entry into the traffic pattern and made an uneventful landing. During the landing roll, the airplane veered to the left and exited the runway colliding with a tree and substantially damaging the left wing. At the time of the accident, the airport was reporting the wind as variable from 140 degrees to 200 degrees at 13 knots, gusting 32 knots. According to the pilot operating handbook, the maximum demonstrated crosswind component of the airplane is 17 knots. The pilot reported that there were no preimpact mechanical malfunctions or failures with the airframe or engine that would have precluded normal flight. Prior to entering the traffic pattern with the intention to land on runway 21, the pilot contacted the pilot of another airplane that had just landed to inquire about the wind conditions. The pilot that previously landed reported the wind was “a little squirrelly but not bad.” The pilot elected to continue his entry into the traffic pattern and made an uneventful landing. During the landing roll, the airplane veered to the left and exited the runway colliding with a tree and substantially damaging the left wing. At the time of the accident, the airport was reporting the wind as variable from 140 degrees to 200 degrees at 13 knots, gusting 32 knots. According to the pilot operating handbook, the maximum demonstrated crosswind component of the airplane was 17 knots. The pilot reported that there were no preimpact mechanical malfunctions or failures with the airframe or engine that would have precluded normal flight. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Variable wind-Contributed to outcome
  • Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Contributed to outcome
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • F Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - F
  • F Aircraft-Aircraft oper/perf/capability-Aircraft capability-Maximum crosswind component-Capability exceeded - F

Verbatim from NTSB's published report. Source file NTSB_2011_WPR11CA237.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.