N182KT

Substantial
None

Cessna 182S/N: 52854

Accident Details

Date
Monday, September 21, 2020
NTSB Number
ANC20LA098
Location
King Salmon, AK
Event ID
20200923X61025
Coordinates
58.672779, -156.642500
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The fatigue fracture failure of the left main landing gear U-bolt during landing, which resulted in the collapse and separation of the left main landing gear spring.

Aircraft Information

Registration
Make
CESSNA
Serial Number
52854
Engine Type
Reciprocating
Model / ICAO
182C182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
182A

Registered Owner (Current)

Name
MATHEW KATIE E
Address
13237 ROSSER DR
City
EAGLE RIVER
State / Zip Code
AK 99577-6731
Country
United States

Analysis

On September 21, 2020, about 1405 Alaska daylight time, a Cessna 182C airplane, N182KT, sustained substantial damage when it was involved in an accident near King Salmon, Alaska. The private pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, after a normal touchdown in crosswind conditions, the left main landing gear (MLG) began to shake and rattle. The shaking continued and became more severe as the airplane continued the landing roll, and the airplane subsequently began to veer to the left and exited the runway. As the airplane came to rest, the left MLG spring separated from the fuselage, resulting in substantial damage to the left horizontal stabilizer and elevator.

An initial examination of the airplane by the pilot revealed that the left MLG spring U-bolt and MLG support bolt fractured, allowing the left MLG spring to separate from the fuselage.

A visual and microscopic examination of the left MLG spring attach hardware revealed a fatigue crack in the U-bolt that emanated in the first thread root of the U-bolt and propagated substantially through the thickness of the thread until it reached a critical size and ultimately failed due to overstress. Examination of the MLG bolt revealed that the bolt fractured within the shank due to shear loads.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC20LA098