NTSB CAROL · Event
Event DFW05CA061
Aircraft involved
Probable cause & findings
The loss of engine power due to fuel exhaustion as result of the pilot's improper fuel calculations, and his inadequate in-flight planning decision. A contributing factor was the pilot's failure to complete an emergency pre-landing checklist, which resulted in a fuel surge during his first attempted landing into the field.
Factual narrative
On January 24, 2005, approximately 1245 central standard time, a Maule M-4-210C single-engine airplane, N9866M, was substantially damaged during a forced landing following a reported loss of engine power, approximately five miles east of McAlister Regional Airport (MLC), near McAlister, Oklahoma. The private pilot, who was the sole occupant and owner of the airplane, sustained minor injuries. Visual meteorological conditions prevailed, and a flight plan was not filed for the personal flight, which was conducted under 14 Code of Federal Regulation Part 91. The cross-country flight originated from the Jackson International Airport (JAN), near Jackson, Mississippi, at 0800. In a telephone interview with an NTSB representative, the private pilot reported that during the trip, he had been monitoring his fuel quantity based on calculations derived from the fuel flow indications by a fuel flow meter that was installed in his airplane. He stated that he was convinced he had enough fuel to make it to MLC; however, when the airplane was approximately five miles east of MLC, "the engine quit." The pilot noticed that the fuel quantity indicators indicated that the fuel tanks were empty. The pilot then elected to execute a forced landing into a cow pasture to the south; however, he did not complete the emergency pre-landing checklist, which included instructions to pull the mixture to an "idle cut-off" position and turn off the ignition switch. The pilot added that he circled the field once to lose altitude and attempted to land in a southerly direction when the engine got a "surge of fuel" and "restarted at full cruise power." The pilot then made a 180-degree turn to stay in the field. During the turn, the engine lost power again, and "the airplane stalled and landed hard." An examination of the airplane by a Federal Aviation Administration (FAA) Inspector, who travelled to the accident site, revealed that the fuel tanks were empty, the right wing had partially separated from the fuselage, and the wing struts on both sides of the airplane were damaged. Additionally, all three landing gear had collapsed and the propeller was damaged. At 1253, the automated weather observing system at MLC reported wind from 210 degrees at 13 knots, visibility 10 statute miles, clear skies, temperature 55 degrees Fahrenheit, dew point 23 degrees Fahrenheit, and a barometric pressure setting of 30.17 inches of Mercury. The private pilot reported that during the trip, he had been monitoring his fuel quantity based on calculations derived from the fuel flow indications by a fuel flow meter that was installed in his airplane. He was convinced that he had enough fuel to make it to his destination; however, when the airplane was approximately five miles east of the airport, the engine quit. The pilot looked down and noticed that the fuel quantity indicators indicated that the fuel tanks were empty. The pilot then elected to execute a forced landing into a cow pasture to the south; however, he did not complete an emergency pre-landing checklist, which included instructions to pull the mixture to an "idle cut-off" position and turn off the ignition switch . He circled the field once to lose altitude and attempted to land in a southerly direction when the engine got a "surge of fuel" and "restarted at full cruise power." The pilot then made a 180-degree turn to stay in the field. During the turn, the engine lost power once again, and "the airplane stalled and landed hard." An examination of the airplane by an FAA Inspector revealed that the fuel tanks were empty. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_DFW05CA061.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.
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- 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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