NTSB CAROL · Event
Event ATL95LA165
Registry · N11AA
FAA Aircraft Registry record.
Make / Model
JONKER SAILPLANES (PTY) LTD JS3
Year of manufacture
2019
Engine
M&D FLUGZE MD-TJ42
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20190427
ADS-B equipped
Yes — Mode-S A029DB
Registrant of record
ADAMS ALAND B
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain flying speed which resulted in an aerodynamic stall.
Factual narrative
0n September 9, 1995, at 1417 central daylight time, an Allen Mustang II, N11AA, collided with the ground during a climbout from runway 22 at Marion County-Brown Field in Jasper, Tennessee. The personal flight operated under the provisions of 14 CFR Part 91, with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The aircraft sustained substantial damage; the pilot and passenger were fatally injured. The flight's exact departure time from Collegedale, Tennessee, was not determined. The fixed based operator at Collegedale Airport reported that the aircraft was refueled with eight gallons of aviation fuel before the flight departed for Jasper. There were no reports of the exact time the flight landed at Jasper. During the flight's attempted departure from Jasper, there were several witnesses at the airport. According to witnesses, the pilot executed a steep, left climbing turn after the lift off from runway 22. The witnesses also stated that the climb attitude appeared excessive, and remained excessive until the airplane stalled; the airplane subsequently rolled left and entered a spin. Examination of the airframe failed to disclose a mechanical problem or system malfunction. The examination of the accident site revealed that the aircraft sustained frontal ground impact damage. The engine assembly was displaced rearward into the cockpit area, and the wing assemblies sustained leading edge damage. Further examination revealed that the empennage was torn from the fuselage. An examination of the cockpit area disclosed that the pilot and passenger seat belt and shoulder harness assemblies had failed; both restraint systems were torn apart at the web stitching. An examination of the engine assembly failed to disclose a malfunction. The engine assembly sustained impact damage that also damaged the carburetor assembly. The examination revealed that the engine had been modified with an electronic ignition system that replaced one of the two normally installed magnetos. The one installed magneto was field checked, and produced an ignition spark on all cylinders. Despite the impact damage, the engine assembly was rotated, and no binding was noted. The autopsy on the pilot was conducted by Dr. Robert Harlen, at the Office of Forensic Science in Nashville, Tennessee, on September 9, 1995. Toxicological examinations were negative for drugs and alcohol. Witnesses reported that the pilot executed a steep left climbing turn after lift off from runway 22. They also stated that the climb attitude remained steep until the airplane stalled. Examination of the aircraft failed to disclose a mechanical failure or system malfunction. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_ATL95LA165.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 ↗