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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 ↗.

Related research

Matched on aircraft type or causal vocabulary (engine failure). All research papers