NTSB CAROL · Event
Event FTW96LA076
Registry · N19LV
FAA Aircraft Registry record.
Make / Model
CESSNA T337G
Year of manufacture
1972 · 23 years old at event
Engine
CONT MOTOR TSIO-360 SER (225 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19720901
ADS-B equipped
Yes — Mode-S A166E0
Registrant of record
LEON RUBEN D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper planning/decision, which resulted in fuel exhaustion, due to an inadequate supply of fuel. A factor relating to the accident was: the lack of suitable terrain for the forced landing.
Factual narrative
On December 24, 1995, at 1430 central standard time, a Cessna 150M, N19LV, sustained substantial damage during the forced landing following a loss of engine power near Round Rock, Texas. The student pilot was not injured. The airplane was being operated as an instructional flight under Title 14 CFR part 91. The last leg of the solo cross country flight originated in Temple, Texas, at 1400. Visual meteorological conditions prevailed and a flight plan was not filed. During an interview, conducted by the FAA inspector, and on the Pilot/Operator Report, the solo student pilot reported the following. Fuel was checked and a flight log (enclosed) prepared prior to departing Austin. The round robin cross country flight departed Austin, Texas, at 1125, with en route stops at Brownwood, Texas, and Temple, Texas. The flight was conducted with a "high power setting" and fuel was not purchased during any portion of the flight. During the return to Austin, the "engine quit," an emergency was declared to Austin Approach Control, and the emergency landing was initiated to an open field. During the landing roll, the nose gear collapsed in the "soft soil" and the airplane nosed over before coming to rest inverted. The FAA inspector examined the airplane and reported structural damage to the wings, propeller, firewall, rudder, and stabilizers. There were no mechanical discrepancies noted with the airplane. There was "evidence of a residual amount of fuel in the wings, fuel filter, and at the carburetor." During a telephone interview, conducted by the investigator-in-charge, the owner/operator reported that he found no mechanical discrepancies that would have contributed to a power loss. His written statement was never submitted to the Board. The flight originated at Austin, Texas, at 1125 with two en route stops. Fuel was not purchased during any portion of the flight. During the return route to Austin, Texas, there was a total loss of engine power. A forced landing was made in an open field with soft soil, but the airplane nosed over. An FAA inspector reported 'evidence of a residual amount of fuel in the wings, fuel filter, and at the carburetor.' The FAA inspector and the owner/operator found no mechanical discrepancies that would have contributed to a power loss. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_FTW96LA076.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),…
- 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 …
Browse the full corpus — academia portal ↗