NTSB CAROL · Event
Event CEN11CA016
Registry · N44KW
FAA Aircraft Registry record.
Make / Model
WILKINSON KEVIN L EASY EAGLE I
Year of manufacture
2010 · 0 years old at event
Engine
VOLKSWAGEN CONVERSION (36 hp)
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20100604
ADS-B equipped
Yes — Mode-S A5493A
Registrant of record
WILKINSON KEVIN L
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons.
Factual narrative
The sport pilot had just departed in his single-engine experimental airplane on a local flight when he experienced a total engine failure at an altitude of 500-700 feet. The pilot was unable to land on the remaining length of runway so he made a forced landing to a plowed field directly off the end of the runway. The airplane sustained damage to all three landing gear, the fuselage, and both wings. An examination of the engine revealed that a source of the power loss could not be determined. No other anomalies were found with the airplane. The sport pilot had just departed in his experimental airplane on a local flight when he experienced a total engine failure at an altitude of 500-700 feet above the ground. The pilot was unable to land on the remaining length of runway and therefore he elected to make a forced landing to a plowed field directly off the end of the runway. The airplane sustained damage to all three landing gear, the fuselage, and both wings. During a postaccident examination of the engine, the source of the power loss could not be determined; no other anomalies were found with the airplane. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2010_CEN11CA016.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 (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 ↗