NTSB CAROL · Event
Event MIA97LA054
Aircraft involved
Probable cause & findings
the pilot's improper planning/decision, by failing to ensure there was sufficient fuel for continued flight, which resulted in fuel exhaustion and subsequent collision with objects (concrete blocks) during a forced landing. Factors relating to the accident were: a partially inoperative fuel gauge, which provided a false fuel indication, and the pilot's operation of the airplane with the known deficiency.
Factual narrative
On January 1, 1997, about 1341 eastern standard time, a Cessna 150K, N5813G, registered to a private individual, was substantially damaged during a forced landing near the Daytona Beach Regional Airport, Daytona Beach, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 personal flight. The private-rated pilot and one passenger sustained serious injuries. The flight originated about 1 minute earlier from the Daytona Beach Airport. The pilot stated that before departure he was aware that one of the fuel gauges was inoperative and during the preflight of the airplane he used a wooden stick that was labeled half and full. Before departure on the first leg the fuel tanks were slightly less than full. The flight departed, performed airwork, then flew south to the Kennedy Space Center (KSC) where a fly-by was performed. The flight continued south of the KSC and performed a full stop landing at an airport. Before departure the pilot checked the fuel tanks using the stick and it indicated 1/2. The flight departed and he performed a full stop landing with taxi back at another airport then continued to the Daytona Beach Airport. He performed two touch-and-go landings then during the landing roll of the third, after applying power to go around, he recognized that the engine was not developing full power. With insufficient runway remaining, he elected to continue and about 200 feet above ground level, the engine began coughing and the propeller stopped. With obstructions ahead the pilot intentionally stalled the airplane which collided with concrete blocks. He further stated to a police officer that the engine may have quit because he ran out of fuel. The airplane was examined the following day by an FAA airworthiness inspector who stated that when he arrived, the airplane was in the process of being dismantled. The non-ruptured fuel tanks were drained and found to contain 3.0 gallons of fuel. According to the airplane type certificate data sheet, the total unusable fuel quantity is 3.5 gallons. Following recovery of the airplane the engine was started and operated to about 750 rpm. Impact damage prevented engine operation to full rated rpm. No discrepancies were noted during the engine run. Before the first of several legs of flight, the pilot used a wooden stick to confirm the fuel quantity, since one of the fuel gauges was inoperative. He then departed, performed airwork, and continued to a landmark, where a flyby was performed. The pilot landed at an airport, remained a short time, then during the preflight, he noted that the fuel quantity indicated about 1/2. The flight departed, and the pilot flew to another airport, and performed a full stop landing with taxiback. He then departed on a return flight to the original departure airport, where he performed two touch-and-go landings. During the takeoff roll of the third touch-and-go, the pilot noted that the engine was not producing full power; however, with insufficient runway remaining to stop, he elected to continue. About 200 feet above ground level, the engine coughed, then the propeller stopped. Subsequently, the airplane collided with concrete blocks during a forced landing. The pilot stated to a police officer that he believed the engine quit because he ran out of fuel. Postcrash examination of the airplane by an FAA inspector revealed 3.0 gallons of fuel remaining in the fuel tanks. According to the airplane type certificate data sheet, the unusable fuel quantity was 3.5 gallons. Following recovery of the airplane, the engine was started, and it operated to 750 rpm. Impact damage precluded operating the engine to a higher rpm. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_MIA97LA054.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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