NTSB CAROL · Event
Event LAX01LA264
Registry · N131LH
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-6A
Year of manufacture
1993 · 8 years old at event
Engine
LYCOMING 0-360-A1D (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19930614
ADS-B equipped
Yes — Mode-S A07FEA
Registrant of record
OBREITER ROBERT JR
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain control of his airplane during the landing flare.
Factual narrative
On July 27, 2001 about 1851 Pacific daylight time, a Williams RV-6A, N131LH, owned and operated by the pilot, made a hard landing on runway 25 at the Jack Northrop Field, Hawthorne, California. The experimental airplane was substantially damaged. Neither the certificated airline transport pilot nor the passenger was injured. Visual meteorological conditions prevailed during the personal flight. No flight plan was filed. The flight was performed under 14 CFR Part 91, and it originated from Alamosa, Colorado, about 1230 mountain daylight time. The pilot verbally reported to the National Transportation Safety Board investigator that he had to add engine power during the landing flare. However, the airplane likely stalled and "dropped hard" onto the runway. The left wing broke. In the pilot's completed accident report, he indicated that he had landed long because the airplane's hangar was at the far end of runway 25. During the landing flare a windshear or gust lifted the right wing upward, and the left wing tip contacted the runway. He attempted to increase engine power to compensate for the upset, but he was not successful. At 1853, Hawthorne reported its surface wind was from 250 degrees at 7 knots. No gusts were reported. The (great circle) distance between Alamosa and Hawthorne is about 643 nautical miles. The pilot was unclear regarding his exact departure time. However, he stated that the flight was performed nonstop. Upon arriving at the destination airport, the pilot elected to land long on runway 25 in order to be closer to the airplane's hangar. According to the pilot, during landing flare a windshear or gust was encountered. Although he attempted to take corrective action, he lost control of his airplane, it impacted the runway hard, and a wing broke. No gusts were reported by the airport facility that indicated the local wind was from 250 degrees at 7 knots. The pilot had arrived at the destination airport after flying over 643 nautical miles on a nonstop flight. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_LAX01LA264.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 or causal vocabulary (stall). 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 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗