CHI01LA142
2001-05-16 · Muscatine, Iowa, United States · Minor · 1 aircraft · Status: Completed
Airport MUT
Current FAA registration · N4348Q
- Make / Model
- VAN'S AIRCRAFT RV-6
- Year of manufacture
- 1992 · 9 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19921113
- ADS-B equipped
- Yes — Mode-S A53579
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The engine failure for undetermined reasons. Factors were the low altitude, the trees, the presence of the irrigation system, the ditch and the soft ground.
Factual narrative
On May 16, 2001, at 1800 central daylight time, an amateur-built Baldwin RV-6, N4348Q, piloted by a private pilot, sustained substantial damage during a nose over while executing a forced landing. The airplane lost engine power on initial climb after takeoff from runway 24 (5,500 feet by 100 feet, concrete) at the Muscatine Municipal Airport, Muscatine, Iowa. The 14 CFR Part 91 personal flight was not on a flight plan and was operating in visual meteorological conditions. The pilot and his one passenger received minor injuries. The local flight was originating at the time of the accident. The pilot reported that he, "Was departing Muscatine, Iowa airport [at] 6:00 pm for a local flight. After the normal systems checks and engine runup, I began my departure. At approx. 400' AGL the RPM started to fall off. I checked carb heat, mixture. Both set properly. Pumped throttle since it seemed like the problem could be fuel flow. (Tanks were full, fuel valve turned to right tank, fuel pump on.) After 10-15 seconds from begining of problem the engine stopped." The pilot landed the aircraft in a field containing a tree line, an irrigation system and a drainage ditch. The pilot said, "The soil was soft and sandy. On touchdown the gear dug in and the plane flipped over to its back." The Federal Aviation Administration conducted a postaccident examination of the aircraft. The examination of the aircraft failed to reveal any anomalies. The airplane nosed over during a forced landing following a loss of engine power on initial climb after takeoff. The pilot reported that, "At approx. 400' AGL the RPM started to fall off. I checked carb heat, mixture. Both set properly. Pumped throttle since it seemed like the problem could be fuel flow. (Tanks were full, fuel valve turned to right tank, fuel pump on.) After 10-15 seconds from begining of problem the engine stopped." The pilot landed the aircraft in a field containing a tree line, an irrigation system and a drainage ditch. The pilot said, "The soil was soft and sandy. On touchdown the gear dug in and the plane flipped over to its back." An examination of the aircraft failed to reveal any anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_CHI01LA142.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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…