NTSB CAROL · Event
Event IAD02LA059
Registry · N341KS
FAA Aircraft Registry record.
Make / Model
SCHLEICHER ASK-21
Year of manufacture
2002 · 0 years old at event
Engine
NONE NONE
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20030220
ADS-B equipped
Yes — Mode-S A3C1F7
Registrant of record
SKYLINE SOARING CLUB INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to recognize the loss of orographic lift conditions. A factor was the loss of orographic lift.
Factual narrative
On June 16, 2002, about 1545 eastern daylight time, a Schleicher ASK21 glider, N341KS, was substantially damaged when it impacted trees, then terrain, while maneuvering near Woodstock, Virginia. The certificated commercial pilot and the passenger received minor injuries. Visual meteorological conditions prevailed and no flight plan was filed for the flight that departed the Front Royal-Warren County Airport (FRR), Front Royal, Virginia. The local personal flight was conducted under 14 CFR Part 91. After he departed behind a tow airplane about 1530, the pilot flew toward the Massanutten Ridge. The glider was released from the tow airplane in the vicinity of Signal Knob, and flew about 10 miles along the ridge. In a written statement, the pilot reported that while he was ridge soaring along Massanutten mountain, he "failed to recognize that the wind speed necessary to generate sufficient orographic lift had diminished." He also stated that he "failed to execute an alternate plan of turning toward the Shenandoah Valley, while he had enough altitude above the trees to safely make the turn." The pilot reported that when he attempted to make the turn toward the valley, "into very weak ridge lift," the glider stalled and "mushed" into the trees. The glider slid through the trees, then impacted the ground in a nose low attitude. The pilot also stated that he evaluated the weather conditions prior to his departure by visual observation, and talking to other pilots. He noted there was an overcast cloud layer about 4,000 feet, and the shadows from the clouds demonstrated there was "good orographic lift" in the area. The winds at the surface were from 270 degrees at 10 knots, and at the ridge top they were from 270 degrees about 15-20 knots. The pilot reported approximately 445 hours of total flight experience, 186 of which, were in make and model. He also reported no mechanical deficiencies with the glider. According to the pilot, the glider sustained substantial damage to both wings, the fuselage, and the horizontal stabilizer. Weather reported at Winchester Regional Airport (OKV), Winchester, Virginia, 24 miles to the northeast, at 1540, included wind from 280 degrees at 12 knots, gusting to 17 knots, 10 miles visibility, and clear skies. After being released from the tow plane, the pilot flew the glider for about 10 miles along a ridge. According to the pilot, he failed to recognize that the wind speed necessary to generate sufficient orographic lift had diminished, and also failed to execute a turn toward the valley while he had sufficient altitude to clear the terrain. As he executed a turn "into very weak ridge lift," the glider stalled, and mushed into trees. The pilot reported that his evaluation of the weather conditions prior to his departure predicted "good orographic lift" in the area. He also reported no mechanical deficiencies 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_IAD02LA059.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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