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WPR23LA271

2023-07-11 · Burlington, Washington, United States · None · 1 aircraft · Status: Completed

Airport BVS

Current FAA registration · N8889K

Make / Model
STINSON 108-1
Engine
FRANKLIN 6A4150 SERIES (150 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560716
ADS-B equipped
Yes — Mode-S AC3F2A

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s failure to maintain directional control during the landing roll with a quartering tailwind.

Factual narrative

The pilot in the tailwheel equipped airplane reported that, while landing with a crosswind, a gust of wind was encountered that “caught my tail” and pushed the airplane to the left. The pilot applied full right rudder, “not realizing my feet were partially on the brakes,” and full throttle to abort the landing. The airplane turned to the right and the pilot applied left rudder to keep the airplane on the runway. The airplane entered the runway safety area, impacted a berm, resulting in the airplane becoming airborne, sending it into the parking area at the airport. The airplane impacted the top of another airplane tied down in the parking area. The right wing and fuselage were substantially damaged. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. At the time of the accident, the pilot was landing on runway 29 with wind from 180° at 8 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained
  • — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on operation

Verbatim from NTSB's published report. Source file NTSB_2023_WPR23LA271.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.