N7592Y

Substantial
None

CESSNA R182S/N: R18200141

Accident Details

Date
Monday, November 22, 2021
NTSB Number
WPR22LA047
Location
Puyallup, WA
Event ID
20211123104302
Coordinates
47.103920, -122.287200
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

An overstress fracture of the left main landing gear pivot assembly, which resulted in the failure of the left main landing gear to fully extend and lock into place.

Aircraft Information

Registration
Make
CESSNA
Serial Number
R18200141
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
R182C82R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
R182

Registered Owner (Current)

Name
CLOVER PARK TECHNICAL COLLEGE
Address
4500 STEILACOOM BLVD SW
City
LAKEWOOD
State / Zip Code
WA 98499-4004
Country
United States

Analysis

On November 22, 2021, about 1349 Pacific standard time, a Cessna R182, N7592Y, was substantially damaged when it was involved in an accident near Puyallup, Washington. The flight instructor and private pilot receiving instruction were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The instructor reported that the intent of the flight was to conduct a stage check for the pilot receiving instruction, who was preparing for an upcoming practical test. They completed several maneuvers in the practice area and were returning to the airport when the instructor requested that the pilot perform a simulated emergency landing gear extension. The pilot noticed that the left main landing gear did not extend. Despite multiple attempts to cycle the landing gear, which included utilizing the emergency landing gear extension procedures, they were unable to extend the left main landing gear. The instructor took control of the airplane and chose to land the airplane with the landing gear retracted.

Postaccident examination of the airplane revealed that the fuselage was substantially damaged. A subsequent examination of the airplane revealed the left main landing gear pivot assembly shaft had fracture-separated near the pivot housing, which prevented the left main landing gear from extending or retracting.

The left landing gear pivot assembly was sent to National Transportation Safety Board Materials Laboratory, Washington, DC, for examination, which revealed characteristics consistent with a shear overstress fracture in clockwise torsion. A review of the airplane’s maintenance records could not determine the age of the component, or if any maintenance had been performed on the assembly.

The operator reported that the accident airplane had always been flown with a flight instructor or examiner on board and no hard landings were reported or documented before the accident flight.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR22LA047