CHI04LA147
2004-06-04 · Manitowoc, Wisconsin, United States · None · 1 aircraft · Status: Completed
Airport MTW
Current FAA registration · N404DK
- Make / Model
- NORTH AMERICAN T-28C
- Year of manufacture
- 1956 · 48 years old at event
- Engine
- WRIGHT R-1820 SER (1475 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19800108
- ADS-B equipped
- Yes — Mode-S A4BBD2
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Failure of the number 4 piston articulating rod resulting in a complete loss of engine power during initial climb. The ditch was a contributing factor.
Factual narrative
On June 4, 2004, about 1820 central daylight time, a North American T-28C, N404DK, owned and piloted by an airline transport pilot, was substantially damaged during a forced landing following a loss of engine power shortly after takeoff from runway 35 (5,000 feet by 100 feet, asphalt) at the Manitowoc County Airport (MTW), Manitowoc, Wisconsin. The flight was operating under 14 CFR Part 91 and was not on a flight plan. Visual meteorological conditions prevailed. The pilot reported no injuries. The local flight was originating at the time of the accident. The pilot stated that as he was reducing to climb power after takeoff, about 200 feet above ground level, he felt a severe vibration and heard several "bangs." He reported that the engine "wound down". He made a slight left turn toward an open field adjacent to a barn to set up for a gear-up forced landing. He noted that the touchdown was smooth and the aircraft slid for approximately 335 feet. The aircraft yawed as it slid and came to a stop when the tail struck a ditch adjacent to a roadway. A post-accident examination determined that the #4 articulating rod had failed resulting in the engine failure. The pilot reported that the engine had accumulated 10,005 hours total time, with 11.4 hours since overhaul. The airplane was substantially damaged during a forced landing after takeoff following a loss of engine power. The pilot stated that as he was reducing to climb power after takeoff, about 200 feet above ground level, when he felt a severe vibration and heard several "bangs." He reported that the engine "wound down". He made a slight left turn toward an open field adjacent to a barn to set up for a gear-up forced landing. He noted that the touchdown was smooth and the aircraft slid for approximately 335 feet. The aircraft yawed as it slid and came to a stop when the tail struck a ditch adjacent to a roadway. A post-accident examination determined that the #4 articulating rod had failed resulting in the engine failure. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_CHI04LA147.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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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…