CEN25LA089
2025-01-27 · Brush, Colorado, United States · Minor · 1 aircraft · Status: Completed
Airport 7V5
Current FAA registration · N1739K
- Make / Model
- LUSCOMBE 8E
- Year of manufacture
- 1946 · 79 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560323
- ADS-B equipped
- Yes — Mode-S A127EF
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The failure of the left main landing gear forward strut.
Factual narrative
The pilot reported that the airplane touched down on all 3 landing gear wheels. During the landing roll at about 30 to 35 miles per hour, the left main landing gear collapsed. The airplane came to rest upright on its nose and left wing and the fuselage and left wing sustained substantial damage. The pilot reported the winds were calm during the landing. Postaccident examination by the airplane owner revealed the left main landing gear strut was fractured, and the rear strut was bent aft. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Aircraft-Aircraft systems-Landing gear system-Main gear strut/axle/truck-Failure
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2025_CEN25LA089.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
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- Pilots of America Community ↗
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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.