CHI01LA018
2000-10-18 · NEW ULM, Minnesota, United States · None · 1 aircraft · Status: Completed
Airport ULM
N2016F has since been reassigned. It is now registered to a different aircraft (CESSNA 172S, built 2025), which was not involved in this event.
Aircraft involved
Probable cause & findings
The engine failure for undetermined reasons, the pilot not attaining proper runway alignment, and the misjudged flare by the pilot. A factor was the runway light.
Factual narrative
On October 18, 2000, at 1930 central daylight time, a Beech model 95-C55, N2016F, piloted by a private pilot, sustained substantial damage during a precautionary landing following a reported loss of engine power on initial climb following takeoff from runway 15 (4,401 feet by 75 feet, dry asphalt) at the New Ulm Municipal Airport, New Ulm, Minnesota. The flight was conducted under the provisions of 14 CFR Part 91 and was not on a flight plan. Visual meteorological conditions prevailed at the time of the accident. The pilot, who was the sole occupant, was not injured. The flight was originating at the time of the accident and was en route to the Flying Cloud Airport, Minneapolis, Minnesota. In a written statement, the pilot said that he experienced a loss of engine power shortly takeoff at about 25 to 50 feet above ground level, prior to landing gear retraction. He said that it appeared to be the left engine that lost power. He said that he closed the throttles and attempted to land on the remaining runway but the airplane had drifted to the right and he landed hard and struck a runway light. The pilot attempted to land the multi-engine airplane on the remaining runway following a loss of engine power on takeoff. The aircraft landed hard and struck a runway light. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_CHI01LA018.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 (engine failure). All research papers
- 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…