No fatalities

Helicopter Water Impact After Engine Power Loss (N5695D)

West Branch, MI, US

On June 15, 2003, an Enstrom 280C (registration N5695D) was involved in an aviation accident near West Branch, MI. No fatalities were reported. Investigators recorded the probable cause as: Fatigue-type failure of the number one connecting rod cap, with galling at the fatigue initiation point and other bearing interface areas, leading to loss of engine power during initial climb. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-09-03Data APIEditorial standards

A helicopter impacted water during an autorotation after losing engine power on initial climb. The pilot landed upright about 75 feet offshore in 2.5 feet of water. A broken connecting rod cap showed fatigue-type failure.

Incident Overview and Pilot Report A helicopter struck water while in an autorotation after the pilot reported a loss of engine power during the initial climb. The pilot brought the aircraft down upright approximately 75 feet from the shore, where it came to rest in about 2-1/2 feet of water. ## Post-Accident Inspection An examination of the helicopter confirmed continuity of the flight controls. Both fuel tanks were found to contain 25 gallons of fuel, and the engine contained 8 quarts of oil. The main and tail rotors also showed drivetrain continuity. ## Mechanical Findings Inspectors found a large hole in the crankcase near the number one engine cylinder, with the number one connecting rod protruding from the opening. Examination of the broken connecting rod cap revealed fracture features consistent with a fatigue-type failure. In addition, the material around the fatigue initiation point was galled, as were several other areas of the bearing interface.

Probable cause

Fatigue-type failure of the number one connecting rod cap, with galling at the fatigue initiation point and other bearing interface areas, leading to loss of engine power during initial climb.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030626X00964. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.