N9637X

Substantial
None

CESSNA 210BS/N: 21057937

Accident Details

Date
Tuesday, August 9, 2022
NTSB Number
CEN22LA378
Location
Clinton, AR
Event ID
20220810105706
Coordinates
35.597039, -92.448352
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A fatigue crack in the hydraulic actuator, which resulted in the loss of hydraulic fluid and the pilot’s inability to fully extend the landing gear.

Aircraft Information

Registration
Make
CESSNA
Serial Number
21057937
Engine Type
Reciprocating
Year Built
1962
Model / ICAO
210BC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
210B

Registered Owner (Current)

Name
CYPRESS PEAK LLC
Address
1773 WAY RD
City
PICKENS
State / Zip Code
MS 39146-9447
Country
United States

Analysis

On August 9, 2022, about 1057 central daylight time, a Cessna 210B airplane, N9637X, sustained substantial damage when it was involved in an accident near Clinton, Arkansas. The pilot was uninjured. The airplane was being operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that the landing gear retracted normally during takeoff; however, when he attempted to extend the landing gear in preparation for the landing, the nosewheel extended and locked into place but the main landing gear did not fully extend. The pilot completed the checklist items for “landing gear emergency operation,” but the landing gear still did not fully extend and lock into place. Unable to extend the main landing gear, the pilot elected to accomplish the landing with the nosewheel extended and the main landing gear in the trail position. The pilot shut down the engine when the landing was assured to protect the engine. After the touchdown and during deceleration, the airplane rolled slightly to the left and the left elevator and horizontal stabilizer contacted the runway, which resulted in substantial damage to both structures.

Postaccident examination revealed a fracture of the hydraulic actuator which allowed the hydraulic fluid to escape the system. After removal, the hydraulic actuator was sent to the National Transportation Safety Board Materials Laboratory for a detailed fracture analysis. The barrel of the housing was sectioned to separate the cracked area from the rest of the assembly. The examination of the fracture surfaces revealed features consistent with fatigue cracking having initiated along the retaining ring groove of the actuator, propagating outward in a circumferential direction. Once the fatigue crack grew to its terminal size, the remainder of the cross-section fractured from mixed overstress and fatigue. This cracking led to part of the housing barrel fracturing in overstress, allowing the release of the internal pressurized hydraulic fluid.

Maintenance records for the airplane show that overhauled main landing gear actuators were installed on June 10, 2021, about 14 months and 179 hours of airframe total time before the accident occurred.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA378