NTSB CAROL · Event
Event FTW96LA042
Registry · N30RV
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-4
Year of manufacture
1999
Engine
LYCOMING 0-360-A1D (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20150630
ADS-B equipped
Yes — Mode-S A31E84
Registrant of record
HARRIS JOHN W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to refuel the airplane which led to a loss of engine power due to fuel exhaustion, and the pilot's failure to maintain adequate airspeed.
Factual narrative
On November 11, 1995, approximately 1735 central standard time, a Lodge RV-4, N30RV, registered to, and operated by the pilot as a Title 14 CFR Part 91 personal flight, was destroyed during a forced landing following a loss of power. Visual meteorological conditions prevailed and no flight plan was filed. The private pilot-in-command and his passenger sustained serious injuries. The flight originated from Aero Country Airpark, McKinney, Texas, about 5 minutes prior to the accident. The pilot reported that, after takeoff he "climbed to 1,800 feet MSL and leveled off." During a turn to the left, "the engine stopped." He further reported that, "seconds-later the aircraft stalled and began rolling inverted." He stated that, he "over reacted to the right and the aircraft stalled again." After the second stall, he "pushed the stick forward to regain airspeed and control." He then, "managed to get the aircraft almost level" [and] out of a dive, when contact with the ground was made." A witness observed the airplane "losing altitude fast" and "leveling off just prior to" ground impact. Examination of the airplane by a FAA inspector revealed the following: The right wing main fuel tank did not have usable fuel, and the fuel found in the left tank measured 1/2 inch on a measuring stick. Also, the fuel selector handle was found in the "right main open" position and both fuel quantity gauges indicated "near" empty. Additionally, the crankshaft was rotated and continuity was established through the accessory gears. All four cylinders had compression and valve action, and the magnetos produced spark through all wire leads when rotated by hand. No engine defects were observed. The pilot reported that after leveling off at 1,800 feet MSL, and during a left turn, the engine lost total power. During the emergency descent the airplane stalled twice prior to impacting the ground. A witness observed the airplane 'losing altitude fast' and 'leveling off just prior to' ground impact. Postaccident examination revealed that the right wing main fuel tank did not have usable fuel, and the fuel in the left tank measured 1/2 inch on a measuring stick. The fuel selector handle was found in the 'right main open' position, and both fuel quantity gauges indicated near empty. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_FTW96LA042.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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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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