WPR12CA175
2012-04-16 · Winslow, Arizona, United States · None · 1 aircraft · Status: Completed
Airport INW
Current FAA registration · N25E
- Make / Model
- LUSCOMBE 8E
- Year of manufacture
- 1947 · 65 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560130
- ADS-B equipped
- Yes — Mode-S A25589
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot did not maintain directional control during the landing roll.
Factual narrative
The pilot said he purchased the airplane 3 days before the accident and was flying it from California to Connecticut. He was landing the airplane to purchase fuel. He said that the wind was variable at 3 to 6 knots, and generally a right crosswind. During touchdown, he overcorrected with rudder control and the airplane ground looped to the right. The left main landing gear failed, and the left wing was bent and wrinkled. The pilot said that he purchased the airplane 3 days before the accident and was flying it across the country. He was landing the airplane to purchase fuel. He said that the wind was variable at 3 to 6 knots and generally a right crosswind. During touchdown, he overcorrected with rudder control, and the airplane ground looped to the right. The left main landing gear failed, and the left wing was bent and wrinkled. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- 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
Verbatim from NTSB's published report. Source file
NTSB_2012_WPR12CA175.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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.