NTSB CAROL · Event
Event ERA16LA184
Registry · N78193
FAA Aircraft Registry record.
Make / Model
GLOBE GC-1B
Year of manufacture
1947 · 69 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19690307
ADS-B equipped
Yes — Mode-S AA97EC
Registrant of record
TROXELL JAY C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airplane control when it encountered a wind gust during climbout.
Factual narrative
On May 14, 2016, at 1310 eastern daylight time, a Globe GC-1B, N78193, was substantially damaged during climb out from Green Landings Airport (WV22), Hedgesville, West Virginia. The pilot was seriously injured and passenger received minor injuries. The airplane was registered to and operated by private individual in accordance with Title 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan was filed for the local flight. The flight was originating at the time of the accident.According to the pilot, he had just purchased the airplane the day of the accident. Prior to departure he conducted a run up and taxied to the grass strip runway for takeoff from runway 3. He said that the takeoff was uneventful and during climb out all engine indications were normal. When the airplane reached about 100 ft above ground level (agl), he said that it banked sharply to the left. He attempted to level wings but was unsuccessful. The nose of the airplane pitched down and the airplane collided with the ground. The pilot reported that he only accumulated 3 flight hours in make and model. According to a witness, he watched the airplane perform a run up prior to takeoff. He said that runway windsock indicated gusty winds and a slight quartering tailwind. He also noticed that the airplane did not use the entire length of the runway for the take off. As the airplane began its takeoff roll it drifted to the left and rotated. The engine was at full power and the airplane was at a high pitch as it began climbing rapidly. The witness observed a rapid aileron input and the airplane stalled. Initial examination of the airplane by a West Virginia State Trooper revealed that the airplane came to rest in the front of a residential home. Both wings were buckled and the horizontal stabilizers were broken away from the empennage. Examination of the engine and flight controls by a Federal Aviation Administration inspector revealed no anomalies that would have precluded normal operation. The weather conditions at the Hagerstown, Washington County Regional Airport (HGR), approximately 13 nautical miles from the accident site, were winds at 290° at 13 knots with 22 knot gusts, light rain and 8 statute miles visibility, with scattered clouds at 4,900 ft agl. The commercial pilot indicated that he purchased the airplane the day of the accident. Before departure, he conducted an airplane run-up and taxied to the runway for takeoff; the takeoff was uneventful, and engine indications were normal. However, the airplane encountered an uncommanded roll at an altitude of about 100 ft above ground level. He attempted to level the wings but was unsuccessful. The nose of the airplane pitched down, and the airplane collided with the ground. A witness who watched the run-up before takeoff stated that a runway windsock indicated a gusting crosswind (with a slight tailwind component); he then observed what seemed like a rapid aileron input during the takeoff, and the airplane stalled. Postaccident examination of the engine and flight controls revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. Thus, it is likely that the pilot was unable to regain control of the airplane when the airplane encountered a wind gust. 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 Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation - C
Verbatim from NTSB's published report. Source file
NTSB_2016_ERA16LA184.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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