No fatalities

Cessna TU206G Nosed Over During Water Landing in Shilshole Bay (N682RC)

Ballard, WA, United States

On August 28, 2009, a CESSNA TU206G (registration N682RC) was involved in an aviation accident near Ballard, WA. No fatalities were reported. Investigators recorded the probable cause as: The pilot's precautionary water landing with partially extended landing gear. Contributing to the accident was the unidentified anomaly with the airplane's electrical system, which rendered the gear position indicator system inoperative. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1785761257Data APIEditorial standards

On August 28, 2009, a Cessna TU206G amphibious airplane, N682RC, nosed over during a water landing in Shilshole Bay, Ballard, Washington. The pilot reported an electrical problem and extended landing gear. The aircraft sustained substantial damage; the pilot suffered minor injury.

Accident Narrative

On August 28, 2009, at approximately 0648 Pacific daylight time, a Cessna TU206G amphibious airplane, registration N682RC, nosed over during a landing in Shilshole Bay, Ballard, Washington. The flight was conducted under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed, and no flight plan was filed. The airplane originated from Bremerton, Washington, about 0630.

Pilot's Report

The pilot, who also owned the aircraft, reported to the National Transportation Safety Board investigator that approximately 15 minutes after departing Bremerton National Airport, an electrical problem occurred, resulting in a total loss of electric current. The fuel gauges subsequently indicated empty, prompting concern about flying over populated areas. Instead of continuing to the intended destination of Payne Field in Everett, Washington, the pilot chose to land in Shilshole Bay marina to verify fuel quantity and investigate the electrical issue.

The pilot stated that he attempted to raise the landing gear using the emergency gear retraction hand pump. He confirmed that both front gear retracted into the pontoons, but the left main aft gear remained extended and did not fully retract.

During the water touchdown, the extended gear caused the left pontoon to lift, resulting in the right wing tip contacting the water. The airplane then pitched forward, nosed over, and came to rest inverted in the salt water. The pilot further noted that the gear position indicator was inoperative due to the loss of electrical power.

Post-Accident Examination

Following recovery of the airplane from the water, Federal Aviation Administration representatives examined it. Due to the airplane's immersion, no determination could be made regarding the preimpact functionality of the electrical system.

Contributing factors

Causes

Pilot

Other contributing factors

Inoperative