N9597X

Substantial
None

CESSNA 210BS/N: 21057897

Accident Details

Date
Wednesday, October 18, 2023
NTSB Number
CEN24LA018
Location
Pueblo, CO
Event ID
20231023193285
Coordinates
38.289947, -104.498020
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 failure of the right main landing gear hydraulic actuator, which resulted in a loss of hydraulic fluid that prevented the pilot from lowering the landing gear to the fully extended position.

Aircraft Information

Registration
Make
CESSNA
Serial Number
21057897
Engine Type
Reciprocating
Model / ICAO
210BC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
210B

Registered Owner (Current)

Name
DAVIDSON RONALD A
Address
1469 N CHALLENGER LN
City
PUEBLO WEST
State / Zip Code
CO 81007
Country
United States

Analysis

On October 18, 2023, about 1736 mountain daylight time, a Cessna 210B airplane, N9597X, was substantially damaged when it was involved in an accident near Pueblo, Colorado. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that during landing gear retraction after takeoff, he heard a “pop” from the rear cockpit area, and the landing gear retraction handle did not return to the center position as expected. He attempted to extend the landing gear, but they would not extend. He performed the emergency extension procedures; the landing gear doors opened, and the landing gear came out of their respective landing gear wells. However, only the nose landing gear locked into the down position, and the main landing gear remained partially extended.

The pilot contacted the Pueblo Municipal Airport (PUB), Pueblo, Colorado, airport traffic control tower and chose to remain airborne for several hours to burn off fuel. The pilot made multiple additional attempts to lower the landing gear. These were unsuccessful, and the pilot eventually landed on runway 8R at PUB. During the landing, the nose landing gear remained in the down position and the main landing gear were in a partially extended position. The airplane skidded to a stop and incurred substantial damage to the left horizontal stabilizer and elevator.

Postaccident examination of the airplane revealed that the right hydraulic actuator was fractured. The actuator was further examined by the NTSB Materials Laboratory. This examination revealed features consistent with fatigue cracking initiating along the retaining ring groove of the actuator, the remainder of the cross-section fracturing from mixed overstress and fatigue once the fatigue crack grew to its terminal size, and the housing barrel then fracturing in overstress.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN24LA018