NTSB CAROL · Event
Event CEN23LA118
Registry · N2722K
FAA Aircraft Registry record.
Make / Model
LUSCOMBE 8E
Year of manufacture
1947 · 76 years old at event
Engine
CONT MOTOR C85 SERIES (85 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19560623
ADS-B equipped
Yes — Mode-S A2B092
Registrant of record
N2722K LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to attain/maintain lateral airplane control during landing, which resulted in an impact with the runway surface.
Factual narrative
On February 19, 2023, at 1330 central standard time, a Luscombe 8E, N2722K, was substantially damaged when it was involved in an accident near Houston, Texas. The commercial pilot was uninjured. The airplane was operated as a Code of Federal Regulations Part 91 personal flight. The pilot stated that the landing touchdown was uneventful. During landing rollout and about 1,630 ft down the runway, the airplane “lurched to the left,” rolled inverted, and came to rest on the runway. The pilot stated that the left wing strut failed at its midpoint. Airport surveillance video showed that during landing the airplane’s right wing moved upward and the left wing descended and contacted the runway. The airplane then nosed over onto the runway. Postaccident examination of the airplane revealed that it was equipped with heel brakes. Examination of the brake system and flight control system revealed no mechanical anomalies that would have precluded normal operation. The examination of the left wing strut revealed that it had failed in overload. The airplane sustained substantial damage that included damage to the fuselage, vertical stabilizer, and left wing strut. The pilot stated that the landing touchdown was uneventful but that during landing rollout the airplane lurched to the left, rolled inverted, and came to rest on the runway. The pilot stated that the airplane’s left wing strut failed at its midpoint. Airport surveillance video showed that during landing the airplane’s right wing moved upward and the left wing descended and contacted the runway. The airplane then nosed over onto the runway and sustained substantial damage. Postaccident examination of the left wing strut revealed that it had failed in overload from having contacted the runway. Examination of the airplane revealed no mechanical anomalies that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Not attained/maintained
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2023_CEN23LA118.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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.
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