NTSB CAROL · Event
Event CHI99LA340
Aircraft involved
Probable cause & findings
the failure of the fuel pump and the misjudged touchdown point by the pilot. A factor was the high vegetation.
Factual narrative
On September 9, 1999, at 1736 central daylight time, a Navion model A, N4527K, piloted by a private pilot, sustained substantial damage during a forced landing, to runway 35 (3,000 feet by 50 feet, dry/concrete), at the Flying V Airport, Utica, Nebraska, following an engine failure during cruise flight. The aircraft impacted terrain short of the approach end of the runway. The personal 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 reported no injuries to himself or his one passenger. The flight originated from the Lincoln Municipal Airport, Lincoln, Nebraska, at 1710 and was en route to the Kearney Airport, Kearney, Nebraska. In a written statement, the pilot said, "... at 4,500 feet, the engine died suddenly and completely. I immediately turned on [the] boost pump, which did no good. I then, turned back 180 degrees and headed for NE23 (Utica, NE) which we had just passed. I notified Lincoln App [approach] of our problem and that re-start procedures didn't work." The pilot then said, "I thought I was set up to touch down halfway down the runway, let [the] gear down, got three lights, and then pumped down the rest of the flaps." The pilot said that he touched down approximately 150 feet from the end of the runway and on rollout the landing gear collapsed due to the presence of "...five feet tall fireweeds." During a post accident examination of the airplane, the engine driven fuel pump drive pin was found to be sheared. No other preexisting anomalies were found with respect to the aircraft or its systems. The pilot said, '... at 4,500 feet, the engine died suddenly and completely. I immediately turned on [the] boost pump, which did no good. I then, turned back 180 degrees and headed for NE23 (Utica, NE) which we had just passed. I notified Lincoln App [approach] of our problem and that re-start procedures didn't work.' The pilot then said, 'I thought I was set up to touch down halfway down the runway, let [the] gear down, got three lights, and then pumped down the rest of the flaps.' The pilot said that he touched down approximately 150 feet from the end of the runway and on rollout the landing gear collapsed due to the presence of '...five feet tall fireweeds.' During a post accident examination of the airplane, the engine driven fuel pump drive pin was found to be sheared. No other preexisting anomalies were found with respect to the aircraft or it's systems Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_CHI99LA340.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…
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