NTSB CAROL · Event
Event ATL97LA062
Aircraft involved
Probable cause & findings
The pilot's failure to select the fuller tank for takeoff that resulted in fuel starvation to the engine, and the subsequent total loss of engine power.
Factual narrative
On April 25, 1997, at 1100 eastern daylight time, a Cessna 140, N2351V, collided with the ground during an attempted emergency landing at the Clearwater Air Park, in Clearwater, Florida. The personal flight operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage. The pilot received minor injuries. The flight departed Clearwater, Florida, at 1058. The pilot reported that he had completed a touch and go landing and was climbing through 400 feet when he experienced a loss of engine power. The pilot initiated a left turn, and elected to return to the airport for an emergency landing. The airplane collided with the ground between the two parallel taxiways. Examination of the aircraft disclosed that there was no fuel in the left main fuel tank. A substantial amount of fuel was recovered from the right main fuel tank. During the initial examination of the cockpit area, the fuel selector was on the left tank. Examination of the airframe failed to disclose a mechanical problem. A review of current weather data disclosed that conditions were favorable for the formation of carburetor ice. The aircraft operation manual instructs the pilot to "set the fuel selector to the fullest tank. (Do not takeoff on less than 1/4 tank.)" The pilot reported that he had completed a touch and go landing and was climbing through 400 feet when he experienced a loss of engine power. The pilot initiated a left turn, and elected to return to the airport for an emergency landing. The airplane collided with the ground between the two parrellel taxiways. Examination of the aircraft disclosed that there was no fuel in the left main fuel tank. A substantial amount of fuel was recovered from the right main fuel tank. During the initial examination of the cockpit area, the fuel selector was on the left tank. Examination of the airframe failed to disclose a mechanical problem. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_ATL97LA062.txt.
Findings + structured fields enriched from FAA avall.mdb.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (fuel starvation). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2024 · arXiv preprint
On the shape of ice stalagmites
The growth of ice stalagmites obtained by the solidification of impacting droplets on a cooled substrate ($-50^{\circ}$C to $-140^{\circ}$C) is investigated experimentally.
- AOPA Air Safety Institute 2023 · Safety advisor
Safety Advisor: Fuel Awareness
AOPA Air Safety Institute safety advisor on preventing fuel-exhaustion and fuel-starvation accidents in general aviation. Covers pre-flight fuel planning, reserve requirements (14 CFR 91.151, 91.167),…
- NASA NTRS 2019 · Conference Paper
Particulate Emissions Hazards Associated with Fueling Heat Engines
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- NASA NTRS 2016 · Conference Paper
United Airlines LOFT training
Line oriented training is used in a broader, more generic sense that as a specific program under FAR 12.1409 and AC 120-35.
- Embry-Riddle Scholarly Commons 2016 · Conference paper
Late Morning Concurrent Sessions: Innovations in Aviation Technologies: Presentation: Wingsuit Materials Research – The Effect of Currently Used Materials on Wingsuit Aerodynamics.
While wingsuit flight is exhilarating and one of the fastest growing facets of sport skydiving, current wingsuit performance is poor at best.
- NASA NTRS 2013 · Conference Paper
Thermodynamic and fluid mechanic analysis of rapid pressurization in a dead-end tube
Three models have been applied to very rapid compression of oxygen in a dead-ended tube. Pressures as high as 41 MPa (6000 psi) leading to peak temperatures of 1400 K are predicted.
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