NTSB CAROL · Event
Event ATL95LA141
Aircraft involved
Probable cause & findings
improper planning/decision by the pilot, which resulted in fuel exhaustion and loss of engine power; and the pilot's failure to maintain adequate airspeed, while turning to make a forced landing, which resulted in a stall and impact with the terrain.
Factual narrative
On July 22, 1995, about 1638 eastern daylight time, a Wheeler Fisher Classic, homebuilt airplane, N942RW, collided with the ground, during an uncontrolled descent, at Marietta, Georgia. The airplane was operated by the owner/pilot under the provisions of 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed. A flight plan was not filed for the personal flight. There were minor injuries to the private pilot, and his passenger, and the airplane was substantially damaged. The flight originated about one hour prior to the accident. According to the FAA operations inspector who interviewed the pilot and passenger, the engine quit as the airplane was being turned from the downwind to the base leg, for runway 27, at McCollum Field. An air traffic controller, in the tower at McCollum Field, stated that the pilot reported a loss of engine power, the airplane turned toward the runway, then appeared to stall. The passenger stated that as the airplane crossed over the field, to enter the downwind, the fuel gauge was indicating about one gallon. There was no odor of fuel at the accident site, and the fuel tank was separated from the airframe. THE PILOT REPORTED THAT THE ENGINE LOST POWER AS THE AIRPLANE WAS BEING TURNED FROM DOWNWIND TO BASE LEG, WHILE IN THE TRAFFIC PATTERN TO LAND ON RUNWAY 27. ACCORDING TO INFORMATION FROM A TOWER CONTROLLER, THE AIRPLANE TURNED TOWARD THE RUNWAY AND APPEARED TO STALL. IT THEN ENTERED A STEEP DESCENT, DISAPPEARED BEHIND TREES, AND CRASHED. THE PILOT REPORTED THERE WERE FIVE GALLONS OF GASOLINE IN THE FUEL TANK BEFORE DEPARTURE. THE PASSENGER SAID THE FUEL QUANTITY INDICATOR SHOWED ONE GALLON OF FUEL AS THE AIRPLANE ENTERED THE LANDING PATTERN. THERE WAS NO ODOR OF FUEL AT THE ACCIDENT SITE, AND THE FUEL TANK WAS TORN LOOSE FROM THE AIRPLANE DURING IMPACT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_ATL95LA141.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, fuel exhaustion). 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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