NTSB CAROL · Event
Event FTW97LA355
Aircraft involved
Probable cause & findings
the pilot's improper planning/decision, by failing to ensure timely refueling of the airplane, which resulted in fuel exhaustion, loss of engine power, and a forced landing.
Factual narrative
On September 22, 1997, at 0730 central daylight time, a Grumman AG5B airplane, N1194L, registered to a private owner and operated by Britt Air, Inc., was substantially damaged during a forced landing following a loss of engine power due to fuel exhaustion, near Texarkana, Arkansas. The private pilot and the passenger received serious injuries. Visual meteorological conditions prevailed for the Title 14 CFR Part 91 personal flight. An IFR flight plan was filed for the night cross-country flight that originated in Lawrenceville, Georgia, approximately 0300. The pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that the route of flight was from Lawrenceville to Dallas with a stop at Texarkana to refuel. The pilot stated that he switched the fuel tank selector after the first thirty minutes of flight, again at one hour thirty minutes after take off, two hours thirty minutes and three hours thirty minutes after take off. The airplane was approximately 10 miles from the Texarkana Regional Airport, on final approach for landing, when the engine lost power. The pilot stated that he "immediately" switched tanks and the engine restarted. Approximately one minute later the engine quit a second time. The pilot notified air traffic control that the aircraft had run out of fuel and he would not be able to make it to the airport. The pilot initiated a right turn toward a flat, unplowed field and during the turn "the airplane stalled." The pilot reported that he "dropped the nose of the aircraft" to regain control and continued to the field. The airplane impacted a highway short of the intended field, and came to rest inverted, on top of a fence. The pilot reported that the aircraft had 5 hours of fuel on board when the flight departed Lawrenceville. The pilot reported that the engine quit the first time 4 hours and 9 minutes after takeoff. The pilot stated that he had recorded the fuel consumption on a previous flight to determine the fuel consumption rate, but never actually performed the calculation due to an illness in the family. Rescue personnel stated that no fuel was observed around the wreckage and there was no fire. The following weather conditions were observed at the Texarkana Regional Airport at the time of the accident: wind from 070 degrees at 6 knots, visibility 10 miles and scattered clouds at 11,000 feet. The pilot had a accumulated a total of 1,244 hours of which 52 hours were in this make and model. Examination of the aircraft by the FAA inspector revealed that the engine separated from the airframe. The right wing tip separated from the wing. The nose gear and left main gear separated from the aircraft. The cross-country flight originated in Lawrenceville, Georgia, and was to proceed to Texarkana, Arkansas, to refuel and then proceed to the final destination of Dallas, Texas. The airplane was approximately 10 miles from Texarkana, when the engine lost power. The pilot reported that the engine lost power 4 hours 9 minutes after take off. He 'immediately' switched fuel tanks, and the engine restarted. Approximately one minute later, the engine lost power again. The pilot notified air traffic control that he had run out of fuel and would not be able to reach the airport. He initiated a forced landing to a flat, unplowed field. During a turn to the field, the airplane stalled. The pilot was able to regain control of the airplane, and continued toward the field. The airplane touched down short of the intended field, and came to rest inverted on top of a fence. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW97LA355.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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