NTSB CAROL · Event
Event WPR14CA138
Registry · N624RM
FAA Aircraft Registry record.
Make / Model
DG FLUGZEUGBAU GMBH DG 1000S
Engine
NONE NONE
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20090408
ADS-B equipped
Yes — Mode-S A8269C
Registrant of record
DAVIS GARY L
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate in-flight planning/decision to maneuver the glider where the lift was not sufficient to maintain flight, resulting in an off airport landing.
Factual narrative
The pilot stated that the purpose of the flight was for him to take his cousin, the sole passenger, around the local ski area. After departure, the glider was towed to about 9,000 feet mean sea level (msl) and adjacent to the ski area. The pilot maneuvered the glider in a 300-degree turn to the right and realized that he was at a lower altitude than the ridge. He continued toward the ridge in an effort to gain lift off of the canyons. As the glider continued to lose altitude, it descended below 6,000 feet msl and the pilot began to look for terrain that would be favorable for an off-airport landing. After deciding on a location, the pilot deployed the airbrakes and with the glider about 10 to 15 feet above ground level (agl), he intentionally stalled. The glider mushed into the ground with little horizontal speed. During the accident sequence the glider incurred substantial damage to the tail boom and wings. The pilot reported no pre impact mechanical malfunctions or failures with the glider that would have precluded normal operation. The pilot stated that the purpose of the flight was for him to take his cousin, the sole passenger, around the local ski area. After departure, the glider was towed to about 9,000 feet mean sea level (msl) and adjacent to the ski area. The pilot maneuvered the glider in a 300-degree turn to the right and realized that he was at a lower altitude than the ridge. He continued toward the ridge in an effort to gain lift off of the canyons. As the glider continued to lose altitude, it descended below 6,000 feet msl and the pilot began to look for terrain that would be favorable for an off-airport landing. After deciding on a location, the pilot deployed the airbrakes and with the glider about 10 to 15 feet above ground level (agl), he intentionally stalled. The glider mushed into the ground with little horizontal speed. During the accident sequence the glider incurred substantial damage to the tail boom and wings. The pilot reported no pre impact mechanical malfunctions or failures with the glider that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-Thermal lifting-Decision related to condition - C
- C Personnel issues-Task performance-Planning/preparation-Flight planning/navigation-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2014_WPR14CA138.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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