LAX02LA079
2002-02-04 · Warner Springs, California, United States · None · 1 aircraft · Status: Completed
Airport CL35
Current FAA registration · N34292
- Make / Model
- SCHWEIZER SGS 2-33A
- Year of manufacture
- 1975 · 27 years old at event
- Engine
- NONE NONE
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19751118
- ADS-B equipped
- Yes — Mode-S A3C86A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain directional control during the landing sequence.
Factual narrative
On February 4, 2002, about 1215 hours Pacific standard time, a Schweizer SGS 2-33A, N34292, collided with trees on final landing approach and landed hard on runway 26 at the Warner Springs Gliderport (CL35), Warner Springs, California. The glider, owned by Associated Gliders of Southern California and rented by the pilot, was operated under the provisions of 14 CFR Part 91. The glider sustained substantial damage. The student pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed for the local area instructional flight and no flight plan had been filed. The flight originated from CL35. The Safety Board investigator interviewed the student pilot. The pilot stated that he was doing pattern work. The takeoffs were to be circuit tows, and he was to practice frontal slips and normal landings. He stated that this was the first tow of the morning. He was about 800 feet above ground level (agl) and the approach seemed normal; however, there was a little turbulence. He turned on final and attempted a frontal slip to a landing. The glider started to drift to the left. The student pilot stated that he must have cross-controlled the glider and could not return the glider to runway centerline. He maneuvered to avoid a tree and stalled the glider as the left wing contacted the tree. The student pilot stated that the glider "pancaked into the runway." He further stated that there were no mechanical discrepancies with the glider. On approach, the glider drifted off the runway centerline and the left wing contacted a tree and landed hard on the runway. The student pilot was unable to return the glider to the runway centerline after his control input cross-controlled the glider, and it drifted further off the centerline. He maneuvered to avoid a tree and stalled the glider. The pilot noted no mechanical anomalies with the glider. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_LAX02LA079.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 or causal vocabulary (stall, turbulence). All research papers
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA) Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Conference Paper Prediction of stall and post-stall behavior of airfoils at low and high Reynolds numbers
An interactive boundary-layer method, together with the e(super n)-approach to the calculation of transition, has been used to predict the stall and post-stall behavior of airfoils at low and high Rey…
- arXiv 2026 · arXiv preprint Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- 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 2025 · arXiv preprint Explainable LiDAR 3D Point Cloud Segmentation and Clustering for Detecting Airplane-Generated Wind Turbulence
Wake vortices - strong, coherent air turbulences created by aircraft - pose a significant risk to aviation safety and therefore require accurate and reliable detection methods.