NTSB CAROL · Event
Event LAX96LA060
Registry · N6LS
FAA Aircraft Registry record.
Make / Model
BEECH E-55
Year of manufacture
1981 · 14 years old at event
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19801219
ADS-B equipped
Yes — Mode-S A7C398
Registrant of record
9 SECONDS CONSULTING LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's selection of the wrong runway for the prevailing wind conditions, and his failure to maintain an adequate airspeed during the base-to-final turn.
Factual narrative
On December 1, 1995, at 1418 hours Pacific standard time, a Laister Sailplane LP-15, N6LS, collided with the ground during the base-to-final turn while landing at Krey Field, Adelanto, California. The glider was operated as a personal flight when the accident occurred. The glider was destroyed and the certificated private pilot was seriously injured. Visual meteorological conditions prevailed. Witnesses reported the pilot was towed toward the east to an altitude of 3,000 feet above ground level (agl), and the weather conditions at the time of landing favored a landing to the west. The glider was observed on a downwind leg of the traffic pattern heading west into the wind. An FAA designated pilot examiner for gliders witnessed the accident. The speed and altitude of the glider was reported as slow and low. During the base-to-final turn for runway 09 about 50-75 feet agl, the left wing of the glider was observed to drop. The witness said the glider appeared to stall and then descend to ground impact. Examination of the glider by the airport manager after the accident did not reveal any evidence of mechanical failure or malfunction. The field is equipped with three windsocks. According to witnesses, the windsocks were indicating a wind from the west at 10-12 knots at the time of the accident. THE PILOT ENTERED THE AIRSTRIP TRAFFIC PATTERN AND SET UP FOR A DOWNWIND FINAL APPROACH TO RUNWAY 9. THE WINDSOCKS WERE INDICATING A WIND FROM THE WEST AT 10-12 KNOTS AND FAVORED A LANDING TO THE WEST. AN FAA DESIGNATED PILOT EXAMINER FOR GLIDERS WITNESSED THE ACCIDENT AND REPORTED THAT THE SPEED AND ALTITUDE OF THE GLIDER WAS SLOW AND LOW. THE GLIDER BEGAN A BASE-TO-FINAL TURN ABOUT 50-75 FEET AGL AND THE LEFT WING OF THE GLIDER DROPPED. THE EXAMINER SAID THE GLIDER APPEARED TO STALL AND THEN DESCEND TO GROUND IMPACT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_LAX96LA060.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…
Browse the full corpus — academia portal ↗