NTSB CAROL · Event
Event LAX01LA038
Registry · N3621R
FAA Aircraft Registry record.
Make / Model
BEECH A36
Year of manufacture
1977 · 23 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19880902
ADS-B equipped
Yes — Mode-S A41645
Registrant of record
BATEMAN RANDY
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's misjudged altitude approaching the airstrip and his failure to maintain airspeed resulted in the glider's collision with trees.
Factual narrative
On November 11, 2000, about 1515 hours Pacific standard time, a Schweizer SGS 1-36, N3621R, operated by the Lake Elsinore Soaring Club, Lake Elsinore, California, collided with trees approaching the Skylark Field in Lake Elsinore. The glider was substantially damaged, and the student pilot was seriously injured. The flight was performed under 14 CFR Part 91. Visual meteorological conditions prevailed. No flight plan was filed for the student pilot's solo instructional flight, which originated from the airstrip about 1358. According to the student's flight instructor, on September 23, 2000, he had authorized his student to solo the glider in the local area. Regarding the accident flight, after about 1 hour the student planned to return for landing at the airstrip. Approaching the field, the student misread his altimeter and initiated a circle to lose altitude. Midway through the turn the student realized his error, noted that he was low, and headed directly back toward the airstrip. The glider continued to lose lift, and the student did not initiate emergency procedures to make an off-site landing in nearby available fields. The flight instructor further stated that while attempting to stretch the glide, the glider stalled and collided with tree branches. Thereafter, it impacted the ground hard about 1/2 mile from the airstrip. The glider came to rest in the front yard of a trailer park. The student pilot elaborated by reporting that he believed the accident was caused by his error in checking the altimeter and misreading it by 800 to 1,000 feet. After soaring for about 1 hour, the student pilot headed back to the departure airstrip for landing. Approaching the airstrip, the student misread his altimeter by 800 to 1,000 feet and initiated a circle to lose altitude. Midway through the turn the student realized his error and noted that he was, in fact, low whereupon he headed directly back toward the airstrip. The glider continued to lose lift, and the student did not initiate emergency procedures to make an off-site landing in nearby available fields. While attempting to stretch the glide, the glider stalled and collided with tree branches. Thereafter, it impacted the ground hard about 1/2 mile from the airstrip. The glider came to rest in the front yard of a trailer park. Nearly 2 months prior to the accident flight, the student's flight instructor authorized the student to fly the glider in solo flight. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_LAX01LA038.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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