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WPR14CA221

2014-06-03 · McCall, Idaho, United States · None · 1 aircraft · Status: Completed

Airport MYL

Current FAA registration · N505V

Make / Model
BOEING A75N1(PT17)
Year of manufacture
1943 · 71 years old at event
Engine
CONT MOTOR W670 SERIES (250 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20020327
ADS-B equipped
Yes — Mode-S A64E5E

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

Loss of directional control during landing rollout due to a wind disturbance, which resulted in a runway veeroff and impact with a ditch.

Factual narrative

The owner-pilot departed his home airport in the tailwheel-equipped airplane for a personal local flight. He spent about 45 minutes conducting airwork, and then returned for some practice landings and takeoffs, the first three of which were uneventful. According to the pilot, the ASOS (automated surface observing system) broadcast stated that the wind was from 220 degrees at 10 knots, so he selected runway 16 for the fourth landing. The pilot reported that he lost directional control during the landing rollout due to a wind disturbance. The airplane exited the east side of the runway, struck a ditch, and upended onto its nose. The right outboard wing was substantially damaged. Initial review of the recorded hourly wind data suggested that the winds were variable. The high resolution wind data revealed that the wind speed and direction both varied significantly in the minutes surrounding the accident time. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The owner-pilot departed his home airport in the tailwheel-equipped airplane for a personal local flight. He spent about 45 minutes conducting airwork, and then returned for some practice landings and takeoffs, the first three of which were uneventful. According to the pilot, the ASOS (automated surface observing system) broadcast stated that the wind was from 220 degrees at 10 knots, so he selected runway 16 for the fourth landing. The pilot reported that he lost directional control during the landing rollout due to a wind disturbance. The airplane exited the east side of the runway, struck a ditch, and upended onto its nose. The right outboard wing was substantially damaged. Initial review of the recorded hourly wind data suggested that the winds were variable. The high resolution wind data revealed that the wind speed and direction both varied significantly in the minutes surrounding the accident time. The pilot reported no preimpact 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • — Environmental issues-Conditions/weather/phenomena-Wind-Variable wind-Effect on operation
  • — Environmental issues-Physical environment-Terrain-Sloped/uneven-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2014_WPR14CA221.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.