NTSB CAROL · Event
Event LAX99LA033
Aircraft involved
Probable cause & findings
The failure of the pilot to maintain sufficient airspeed, which resulted in the aircraft entering a stall/mush flight condition that continued to impact. A factor in the accident was the pilot's lack of familiarity with the type of aircraft.
Factual narrative
On November 16, 1998, at 0845 hours Pacific standard time, an experimental The Old Hen Crow G1, N6349T, was destroyed when the aircraft struck power transmission lines and crashed while approaching to land at the Tehachapi, California, Municipal Airport. The private pilot received serious injuries. Visual meteorological conditions prevailed for the personal flight operating under the provisions of 14 CFR Part 91 and no flight plan was filed. The pilot reported that the accident occurred on the first flight of the aircraft following a 2.5-year restoration. He reported that the climb performance was poor after takeoff and, after making several shallow banked turns, he returned to the airport. He recalled that while on downwind leg for runway 11 he looked inside the cockpit and when he looked back outside "the aircraft was going down." The aircraft was not in a spin. The pilot reported having no prior flight experience in this type aircraft and that there were no mechanical malfunctions of the aircraft. A Kern County Sheriff's Deputy, who responded to the scene, told the Safety Board investigator that, at the accident scene, the pilot told her he had "stalled the plane out." The pilot reported that the accident occurred on the first flight of the experimental aircraft following a 2.5-year restoration. The climb performance was poor after takeoff and, after several shallow banked turns, he returned to the airport. He recalled that while approaching the airport he looked inside the cockpit and when he looked back outside 'the aircraft was going down.' The pilot reported having no prior flight experience in this type aircraft and there were no mechanical malfunctions of the aircraft. A sheriff's deputy told the Safety Board investigator that, at the accident scene, the pilot told her he had 'stalled the plane out.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_LAX99LA033.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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