ERA11CA057
2010-11-12 · Livingston, New York, United States · Serious · 1 aircraft · Status: Completed
Airport 1A1
Current FAA registration · N46014
- Make / Model
- AERONCA 0-58B
- Year of manufacture
- 1943 · 67 years old at event
- Engine
- CONT MOTOR A&C65 SERIES (65 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19570504
- ADS-B equipped
- Yes — Mode-S A59C33
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper fuel management, which resulted in a loss of engine power due to fuel exhaustion.
Factual narrative
The pilot stated that the airplane's 15-gallon fuel tank was about half-full when he departed on a local flight. At the conclusion of the one-hour flight, while on approach to the airport, the airplane’s engine stopped producing power. The pilot set up for a forced landing to a southerly-oriented runway, and about 200 feet above the ground, the engine started and the aircraft climbed. The engine ran for several seconds and stopped again. The pilot then attempted to circle and land on the northerly-oriented runway. As he approached the runway, the pilot pulled back on the stick but there was no elevator control effectiveness. The airplane impacted the ground, the landing gear collapsed, and the engine firewall sustained substantial damage. Post accident examination by a Federal Aviation Administration inspector revealed that the fuel tank was void of fuel, and no fuel drained from the wing fuel sump when tested. The pilot reported there were no mechanical malfunctions or anomalies with the airplane. The pilot stated that the airplane's 15-gallon fuel tank was about half-full when he departed on a local flight. At the conclusion of the one-hour flight, while on approach to the airport, the airplane’s engine stopped producing power. He set up for a forced landing to a southerly-oriented runway, and about 200 feet above the ground, the engine re-started and the aircraft climbed. The engine ran for several seconds and stopped again. He then attempted to circle and land on the northerly-oriented runway. As he approached the runway, he pulled back on the control yoke to bleed off some airspeed, but there was no elevator control effectiveness as the airplane was close to a stall. The airplane impacted the ground, the landing gear collapsed, and the engine firewall sustained substantial damage. Postaccident examination by a Federal Aviation Administration inspector revealed that the fuel tank was void of fuel, and no fuel drained from the wing fuel sump when tested. The pilot reported there were no mechanical malfunctions or anomalies with the airplane. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA11CA057.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (stall, fuel exhaustion). All research papers
- 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…