NTSB CAROL · Event
Event LAX01LA238
Registry · N122MS
FAA Aircraft Registry record.
Make / Model
STAUDACHER MARK W VJ-22MS SPORTSMAN
Year of manufacture
2023
Engine
CONT MOTOR O-200-B (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20230417
ADS-B equipped
Yes — Mode-S A05C44
Registrant of record
STAUDACHER MARK W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Failure of the pilot to maintain directional control during landing.
Factual narrative
On Saturday, July 7, 2001, at 1310 hours Pacific daylight time, a Sparks KR-2, N122MS, was substantially damaged when it struck a runway light at Gillespie Field, San Diego, California. The private pilot, who was the only occupant, was not injured. Visual meteorological conditions prevailed for the flight, which was conducted by the owner under 14 CFR Part 91. The airplane departed Brown Field, San Diego, at 1250 for the flight to Gillespie Field, where the accident occurred. No flight plan was filed. The pilot, who was the original owner and builder of this aircraft, was interviewed by an investigator from the National Transportation Safety Board shortly after the accident. He stated that while he was decelerating during his landing rollout, he encountered a gust of wind from the left, which caused the airplane to become airborne again with the left wing high. He added power and avoided a stall, but had drifted off the runway. The left main landing gear hit a runway light, causing the airplane to ground loop, which damaged the outboard 2 feet of the left wing when it contacted the ground. The pilot stated that he would repair the wing and fly the airplane again. He stated that the damage was easy to repair and would take only a few days to complete. According to the pilot, he had approximately 2,000 hours of flight time, 700 of which was in the accident airplane. He had logged 50 hours in this airplane within the last 90 days. The pilot, who was the original owner and builder of this aircraft, stated that while he was decelerating during his landing rollout, he encountered a gust of wind from the left, which caused the airplane to become airborne again with the left wing high. He added power and avoided a stall, but had drifted off the runway. The left main landing gear hit a runway light, causing the airplane to ground loop, which damaged the outboard 2 feet of the left wing. The pilot stated that he would repair the wing and fly the airplane again. He stated that the damage was easy to repair and woud take only a few days to complete. According to the pilot, he had approximately 2,000 hours of flight time, 700 of which was in the accident airplane. He had logged 50 hours in this airplane within the last 90 days. When asked how he could prevent this accident from happening in the future, he stated "Don't go flying." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_LAX01LA238.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…
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