SEA05LA077
2005-04-18 · Tupelo, Mississippi, United States · Serious · 1 aircraft · Status: Completed
Airport TUP
Aircraft involved
Probable cause & findings
A loss of engine power due to the inadequate in-flight planning and the pilot's failure to refuel the airplane resulting in fuel exhaustion.
Factual narrative
On April 18, 2005, at 1707 central daylight time, a Beech V35B Bonanza, N6645G, sustained substantial damage following a loss of engine power and subsequent forced landing in an open field approximately one-half mile northeast of the Tupelo Regional Airport, Tupelo, Mississippi. The airplane is owned by a private party and was being operated by the pilot as a 14 CFR Part 91 cross-country flight, when the accident occurred. The commercial pilot, the sole occupant of the airplane, sustained serious injuries. Visual meteorological conditions prevailed for the cross-country flight that originated in Fort Wayne, Indiana at 1430 CST. In a written statement dated April 26, the pilot reported that while on the return leg of the cross-county flight he noted (via the panel mounted fuel gauges) a lower than expected total fuel quantity. The pilot stated that after reviewing his fuel receipt, he discovered that the airplane had received 15 gallons total at the last fuel stop. He further stated that he had intended for 15 gallons to be added to each wing tank for a total of 30 gallons. The pilot reported that he recalculated the fuel load and determined that he had sufficient fuel to complete the trip. Approximately two hours later, while in a descent to his planned destination, the engine experienced a total loss of power. The pilot transmitted to the tower that he was unable to make the airport and subsequently landed in a field near Tupelo Airport. In his written statement, the pilot reported that he "...should have used manual calculations of fuel quantity to backup gauge indications." In a written statement the pilot reported that while on the return leg of the cross-county flight he noted (via the panel mounted fuel gauges) a lower than expected total fuel quantity. The pilot stated that after reviewing his fuel receipt, he discovered that the airplane had received 15 gallons total at the last fuel stop. He further stated that he had intended for 15 gallons to be added to each wing tank for a total of 30 gallons. The pilot reported that he recalculated the fuel load and determined that he had sufficient fuel to complete the trip. Approximately two hours later, while in a descent to his planned destination, the engine experienced a total loss of power. The pilot later reported that he should have used manual calculations of fuel quantity to backup gauge indications. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_SEA05LA077.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion). All research papers
- 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 · Abstract U.S. Civil Rotorcraft Accidents, 1963 through 1997
The U.S. National Transportation Safety Board (NTSB) has recorded 8,436 rotorcraft accidents during the period mid - 1963 through the end of 1997.
- NASA NTRS 2019 · Contractor Report (CR) A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2018 · Other Parachuting to Safety
NASA's Langley Research Center awarded Ballistic Recovery Systems, Inc., three Small Business Innovation Research (SBIR) contracts to research and develop a new, low cost, lightweight recovery system …