N2215T

Substantial
None

CESSNA A185F S/N: 185-1367

Accident Details

Date
Thursday, May 27, 1993
NTSB Number
SEA93LA124
Location
BELLEVUE, WA
Event ID
20001211X12491
Coordinates
47.550010, -122.139129
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

FAILURE OF THE RIGHT MAIN LANDING GEAR SHOCK STRUT.

Aircraft Information

Registration
Make
CESSNA
Serial Number
185-1367
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
A185F C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
A185E

Registered Owner (Current)

Name
BACKCOUNTRY WAGONS LLC
Address
38 E WASHINGTON ST STE C
City
KALISPELL
State / Zip Code
MT 59901-3974
Country
United States

Analysis

On May 26, 1993, at 1830 hours Pacific daylight time, an amphibian Cessna A185F, N2215T, nosed over during landing on Lake Washington, Bellevue, Washington. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane was substantially damaged and the certificated airline transport pilot and his three passengers were not injured. The flight had originated from Stuart Island, Washington, on May 26, 1993, at 1800 hours, and was en route to Bellevue.

The pilot reported that he had cockpit indications, and visual indications on the floats that the landing gear was in the up and locked position for the landing on the water. After touch down, the airplane veered to the right. The pilot applied full left rudder, however, the right wing tip contacted the water and the airplane nosed over.

Witnesses located on the shore reported that they observed that the right main landing gear was extended, while the left main and nose gear were retracted.

After the airplane was retrieved, it was found that the two screws that attach the casing to the piston at the top of the right main gear shock strut were broken. A metallurgical examination of the two screws revealed that, "Examination with the aid of a low power binocular microscope (up to 50X) revealed that both breaks had features typical of over stress separation under direct shear loads." The top edges of the screw holes in the shock strut casing revealed fresh rub marks.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA93LA124