NTSB CAROL · Event
Event ERA14LA391
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain adequate airspeed while maneuvering, which resulted in an aerodynamic stall and spin. Contributing to the accident was the student pilot's failure to properly assess her physical condition prior to conducting the flight.
Factual narrative
On August 17, 2014, about 1520 central daylight time, a Let L-23 Super Blanik glider, N266SE, was substantially damaged when it impacted trees and terrain while maneuvering for landing at Merkel Field Sylacauga Municipal Airport (SCD), Sylacauga, Alabama. The student pilot was seriously injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local instructional flight, which was operated under the provisions of Title 14 Code of Federal Regulations Part 91. The pilot stated that she conducted a preflight inspection of the glider and added ballast for the solo flight. She described the tow as "normal," and after about 30 minutes of flight, elected to return to the airport. Her last recollection was turning the glider at an altitude of about 1,800 feet and airspeed of 45 knots to allow room for another glider in the pattern to land. She then "vaguely" remembered the glider entering an aerodynamic stall. She recalled impacting a tree, and subsequently egressing the glider. She stated that the glider performed normally throughout the flight, with no mechanical malfunctions or anomalies. In a statement to a Federal Aviation Administration (FAA) inspector, the pilot stated that she felt nauseated on the morning of the accident, and had also taken an over-the-counter decongestant around 0800. She further stated that she was not properly hydrated before or during the flight, which may have contributed to her general condition. The pilot's flight instructor was flying with another student at the time of the accident. He did not witness the accident, but recalled seeing the accident glider in the traffic pattern for runway 27 at an altitude about 1,800 feet, and felt that it was "in a good position" to land behind his glider. A witness reported to the FAA inspector who responded to the scene that he observed the accident glider approach SCD from the north. He watched the glider enter a steep right bank followed by a stall. The glider recovered before subsequently entering a right spin. The witness observed the glider complete two full rotations in a near-vertical attitude before it disappeared from view behind a tree line. A second witness recounted that the accident glider was on the right downwind leg of the traffic pattern for runway 27 when it stalled and entered a spin. After about one half rotation, it appeared to recover before entering a second spin to the right. He stated that the glider completed two rotations before disappearing from view. The glider came to rest in a near-vertical position in trees approximately 1 mile north of runway 27 at SCD, and sustained substantial damage to the forward cabin area and wings. The pilot held a student pilot certificate, and reported 33 total hours of flight experience, of which 3 hours were in the accident glider make and model. According to FAA airworthiness records, the glider was manufactured in 1993. Its most recent annual inspection was completed in April 2014. The 1535 weather observation at Thomas C Russell Field Airport (ALX), Alexander City, Alabama, located about 23 miles southeast of the accident site, included wind from 200 degrees at 10 knots with gusts to 15 knots, 10 miles visibility, clear skies, and an altimeter setting of 30.01. Remarks noted distant lightning in all quadrants. The student pilot was maneuvering the glider to land at the conclusion of a local solo flight. While turning to allow for spacing with another glider in the airport traffic pattern, the pilot "vaguely" recalled the glider entering an aerodynamic stall. The glider subsequently impacted a tree, resulting in serious injury to the student pilot and substantial damage to the glider. Two witnesses observed the accident glider in the traffic pattern, and both recounted that it entered a right spin before descending to ground impact. The pilot stated that her preflight inspection of the glider revealed no anomalies and that the glider performed normally throughout the flight. She further stated that she felt nauseated the morning of the accident, had taken an over-the-counter decongestant medication, and was not properly hydrated before or during the flight. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded - C
- F Personnel issues-Physical-Impairment/incapacitation-(general)-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2014_ERA14LA391.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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