LAX92LA392
1992-09-17 · COLUMBIA, California, United States · None · 1 aircraft · Status: Completed
Airport O22
Current FAA registration · N39087
- Make / Model
- LUSCOMBE 8A
- Year of manufacture
- 1941 · 51 years old at event
- Engine
- CONT MOTOR A&C65 SERIES (65 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19571030
- ADS-B equipped
- Yes — Mode-S A48659
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE FAILURE OF THE STUDENT TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRCRAFT DURING THE LOW SPEED PORTION OF THE LANDING ROLL. A FACTOR IN THE ACCIDENT WAS THE LACK OF BRAKE PEDALS AT THE INSTRUCTOR'S SEAT POSITION ON THE RIGHT SIDE OF THE COCKPIT.
Factual narrative
THE INSTRUCTOR SAID THE STUDENT MADE THREE PRIOR LANDINGS IN THE AIRCRAFT. ON THE FOURTH LANDING, THE AIRCRAFT DECELERATED TO ABOUT 15 MILES PER HOUR WHEN IT BEGAN VEERING OFF THE RUNWAY. THE INSTRUCTOR SAID THE RIGHT SEAT POSITION DOES NOT HAVE BRAKES AND HE COULD NOT CONTROL THE AIRCRAFT WITH RUDDER ALONE DUE TO THE REDUCED SPEED. THE AIRCRAFT GROUND LOOPED, COLLAPSING THE RIGHT LANDING GEAR AND DAMAGING THE WING. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_LAX92LA392.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
- Embry-Riddle Scholarly Commons 2020 · Conference paper Concurrent Sessions: Session 8A - Technology in Aviation
- arXiv 2020 · arXiv preprint Continuation Method with the Trusty Time-stepping Scheme for Linearly Constrained Optimization with Noisy Data
The nonlinear optimization problem with linear constraints has many applications in engineering fields such as the visual-inertial navigation and localization of an unmanned aerial vehicle maintaining…