NTSB CAROL · Event
Event LAX06TA234
Aircraft involved
Probable cause & findings
failure of the winch operator to maintain an adequate winch tow speed, resulting in a stall and hard landing.
Factual narrative
On July 11, 2006, about 1500 Pacific daylight time, a LET Super Blanik L-23 glider, N381BA, collided with terrain during takeoff from the US Army Airfield at Los Alamitos, California. The Civil Air Patrol (CAP) was operating the airplane as a local instructional flight under the provisions of 14 CFR Part 91. The commercial pilot and the student pilot were not injured; the glider sustained substantial damage. Visual meteorological conditions prevailed, and no flight plan had been filed. The CAP reported that they were using a winch to launch the glider. They were experimenting with a new plasma launch rope. With the new rope, the winch operator could not see the glider until it became airborne. As the winch operator watched the glider become airborne, he diverted his eyes from the winch gauges. When he looked back at them, he realized that he was accelerating it faster than he desired. He reduced the winch's power momentarily. The glider stalled at 80 feet above ground level. It landed hard, which resulted in substantial damage to the left wing. The Glider Flying Handbook (FAA-H-8083-13) discusses a normal into the wind ground launch. It notes that a pilot should be ready for a takeoff any time that the towline is attached to the glider. It advises the pilot to smoothly raise the nose to the proper pitch attitude after liftoff, and watch for an increase in airspeed. The handbook says to avoid raising the nose too rapidly or steeply, as it may be difficult or impossible for the pilot to recover from the steep pitch attitude if the towline breaks or the launch mechanism loses power. It also says to avoid raising the nose too slowly, as the glider may gain excessive airspeed or not attain the planned release speed. If this situation occurs, it advises the pilot to pull the release, and land straight ahead. The glider stalled and collided with terrain during takeoff. The operator was using a winch to launch the glider and as the winch operator watched it become airborne, he diverted his eyes from the winch gauges. When he looked back at them, he realized that he was accelerating the glider faster than desired and he reduced the winch's power momentarily. The glider stalled at 80 feet above ground level and it landed hard, which resulted in substantial damage to the left wing. The Glider Flying Handbook (FAA-H-8083-13) notes that a pilot should be ready for a takeoff any time that the towline is attached to the glider. It advises the pilot to smoothly raise the nose to the proper pitch attitude after liftoff, and watch for an increase in airspeed. The handbook says to avoid raising the nose too rapidly or steeply, as it may be difficult or impossible for the pilot to recover from the steep pitch attitude if the towline breaks or the launch mechanism loses power. It also says to avoid raising the nose too slowly, as the glider may gain excessive airspeed or not attain the planned release speed. If this situation occurs, it advises the pilot to pull the release, and land straight ahead. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_LAX06TA234.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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