NTSB CAROL · Event
Event NYC93LA050
Registry · N4266B
FAA Aircraft Registry record.
Make / Model
MAULE M-7-260
Year of manufacture
2000
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
20001106
ADS-B equipped
Yes — Mode-S A51515
Registrant of record
CARPENTER STEVEN WARREN
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO FOLLOW THE BEFORE LANDING CHECK LIST IN THE PILOT OPERATORS HANDBOOK IN NOT SELECTING THE FULLEST FUEL TANK FOR LANDING, WHICH RESULTED IN FUEL STARVATION AND SUBSEQUENT ENGINE FAILURE.
Factual narrative
THE FLIGHT DEPARTED WITH 45 GALLONS OF FUEL ON BOARD. AFTER 1.3 HOURS OF FLYING, AS THE AIRPLANE ENTERED THE AIRPORT DOWNWIND LEG, THE ENGINE QUIT. UNABLE TO GLIDE TO THE AIRPORT, THE PILOT LANDED THE AIRPLANE GEAR UP IN A FIELD. POST ACCIDENT INVESTIGATION REVEALED A FULL LEFT FUEL TANK AND NO FUEL REMAINING IN THE RIGHT TANK. A POST ACCIDENT TEST RUN OF THE ENGINE WAS ACCOMPLISHED WITH NO PROBLEMS NOTED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_NYC93LA050.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 starvation, engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
Browse the full corpus — academia portal ↗