N682RC

Substantial
Minor

CESSNA TU206GS/N: U20605537

Accident Details

Date
Friday, August 28, 2009
NTSB Number
WPR09LA423
Location
Ballard, WA
Event ID
20090828X74002
Coordinates
47.666667, -122.033332
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

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.

Aircraft Information

Registration
N682RC
Make
CESSNA
Serial Number
U20605537
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
TU206GC206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
COLLINS ROGER D
Address
15425 NE 144TH PL
Status
Deregistered
City
WOODINVILLE
State / Zip Code
WA 98072-6911
Country
United States

Analysis

On August 28, 2009, about 0648 Pacific daylight time, a Cessna TU206G, N682RC, nosed over during landing in the Shilshole Bay, Ballard, Washington. The pilot owned and operated the amphibious airplane. Visual meteorological conditions prevailed at the time of the personal flight, and no flight plan had been filed. The airplane was substantially damaged, and the commercial pilot received a minor injury. The flight was performed under the provisions of 14 Code of Federal Regulations Part 91, and it originated in Bremerton, Washington, about 0630.

The pilot reported to the National Transportation Safety Board investigator that about 15 minutes after taking off from the Bremerton National Airport, he experienced an electrical problem with his airplane. All electric current was lost. As a result, the airplane's fuel gauges indicated empty and he became concerned about flying over populated areas. Rather than continuing his intended flight to Payne Field, in Everett, Washington, the pilot opted to land in the Shilshole Bay marina to check his fuel state and investigate the electrical problem.

The pilot stated that he attempted to raise the landing gear by using the emergency gear retraction hand pump. He was able to confirm that both of the front gear were raised into the pontoons. However, the left main aft gear was still extended; it did not fully retract.

Upon touchdown in the water, the extended gear lifted the left pontoon up, and the right wing tip impacted the water. The airplane pitched forward, nosed over, and came to rest upside down in the salt water. The pilot further reported that without electrical power, the gear position indicator was inoperative.

Federal Aviation Administration (FAA) representatives examined the airplane following its recovery from the water. Due to the airplane's immersion in the water, no determination was made regarding the preimpact functionality of the airplane's electrical system.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09LA423