WPR12CA159
2012-04-07 · Westport, Washington, United States · Minor · 1 aircraft · Status: Completed
Airport 14S
Current FAA registration · N1183K
- Make / Model
- LUSCOMBE 8E
- Year of manufacture
- 1946 · 66 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560418
- ADS-B equipped
- Yes — Mode-S A04CB6
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s inadequate crosswind compensation, which resulted in a loss of directional control during the landing roll.
Factual narrative
The pilot reported that because of the left 10- to 15-knot quartering headwind, on short final approach he descended using airspeed about 5 knots faster than normal. The airplane bounced upon touching down on the runway, and then it began drifting toward the runway’s edge. Despite the pilot’s efforts at stopping the drift, the airplane veered off the side of the runway and rolled onto an adjacent grassy area. As the airplane decelerated in the grass, the airplane rolled into a 1-foot-deep trough and nosed over. This event resulted in breaking the windshield, bending the engine mounts, vertical stabilizer and rudder, and other airframe damage. The pilot further reported that no mechanical malfunction or failure occurred with the airplane during the accident flight. The pilot reported that, because of the left 10- to 15-knot quartering headwind, on short final approach, he descended at an airspeed about 5 knots faster than normal. The airplane bounced upon touching down on the runway and began drifting toward the runway’s edge. Despite the pilot’s efforts to stop the drift, the airplane exited the side of the runway, rolled onto an adjacent grassy area and into a 1-foot-deep trough, and nosed over. The windshield broke, and the engine mounts, vertical stabilizer, and rudder were bent. The pilot reported that no mechanical malfunction or failure occurred with the airplane during the accident flight. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Environmental issues-Physical environment-Terrain-Rough terrain-Contributed to outcome
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Crosswind correction-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Response/compensation - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2012_WPR12CA159.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.