NTSB CAROL · Event
Event FTW95LA400
Registry · N5DT
FAA Aircraft Registry record.
Make / Model
CESSNA 150K
Year of manufacture
1970 · 25 years old at event
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19700622
ADS-B equipped
Yes — Mode-S A6359B
Registrant of record
FIVE DELTA TANGO LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO REFUEL THE AIRPLANE RESULTING IN FUEL EXHAUSTION. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING.
Factual narrative
On September 16, 1995, at 1345 central daylight time, a Cessna 150K, N5DT, nosed over during a forced landing near Victoria, Texas. The airplane sustained substantial damage and the private pilot was not injured. The personal flight operating under Title 14 CFR Part 91 departed Halletsville, Texas, at 1320. No flight plan was filed and visual meteorological conditions prevailed. The pilot reported he intended to fly from Frankston, Texas, to Corpus Christi, Texas, with a "fuel stop" in Victoria. "Fuel consumption was higher than normal" and he landed short of Victoria at Hallettsville, Texas, for a "rest stop and fuel check." He performed a "visual check" of the fuel tanks which showed "one quarter in each tank." The airport at Halletsville "was deserted" and the pilot elected to continue on to Victoria without refueling. While on base leg for landing on runway 17 at Victoria, the pilot saw another aircraft on a "four mile final." Following completion of a "360 [degree] turn for spacing," the engine lost power. The pilot landed the airplane short of the runway in a water-filled rice field and it nosed over. According to a Federal Aviation Administration inspector, the airplane came to rest inverted in approximately 18 inches of water. The firewall, engine mount, cowling, propeller and left wing tip were damaged. Water immersion prevented determination of the quantity of fuel in the wing tanks. According to the manufacturer's specifications for the airplane, "one quarter in each tank" equates to a total of 3 gallons usable fuel. Calculations based on the manufacturer's performance data indicated the 25 minute flight from Halletsville to Victoria required approximately 3 gallons of fuel. THE PILOT REPORTED HIS 'FUEL CONSUMPTION WAS HIGHER THAN NORMAL' ON THE CROSS COUNTRY TRIP FROM FRANKSTON, TEXAS, TO VICTORIA, TEXAS. HE LANDED SHORT OF VICTORIA AT HALLETSVILLE AND PERFORMED A 'VISUAL' CHECK OF THE TANKS WHICH SHOWED 'ONE QUARTER IN EACH TANK.' THE HALLETSVILLE AIRPORT 'WAS DESERTED' AND HE ELECTED TO CONTINUE ON TO VICTORIA WITHOUT REFUELING. WHILE ON BASE LEG FOR LANDING AT VICTORIA, THE PILOT MADE A 360 DEGREE TURN FOR SPACING. UPON COMPLETION OF THE TURN, THE ENGINE LOST POWER. A FORCED LANDING WAS MADE TO A WATER-FILLED RICE FIELD AND THE AIRPLANE NOSED OVER. ACCORDING TO THE MANUFACTURER'S SPECIFICATIONS FOR THE AIRPLANE, 'ONE QUARTER IN EACH TANK' EQUATES TO A TOTAL OF 3 GALLONS USABLE FUEL. CALCULATIONS BASED ON THE MANUFACTURER'S PERFORMANCE DATA INDICATED THE 25 MINUTE FLIGHT FROM HALLETSVILLE TO VICTORIA REQUIRED APPROXIMATELY 3 GALLONS OF FUEL. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_FTW95LA400.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 (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.
- 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),…
- Semantic Scholar 2023 · Article (AIAA SCITECH 2023 Forum)
The Impact of Multi-Stack Fuel Cell Configurations on Electrical Architecture for a Zero Emission Regional Aircraft
All-electric aircraft can eliminate greenhouse gas emissions during aircraft mission, but the low predicted energy storage density of batteries (=0.5 kWh/kg), and their life cycle, limits aircraft pay…
- Semantic Scholar 2022 · Article (IEEE Transportation Electrification Conference and Expo)
Minimising the effect of degradation of fuel cell stacks on an integrated propulsion architecture for an electrified aircraft
Proton Exchange Membrane Fuel Cells (PEMFC) are receiving interest as an electrical source of energy for aircraft propulsion electrification.
- 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 …
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