N4796K

Substantial
None

Cessna P210NS/N: P21000323

Accident Details

Date
Sunday, February 10, 2008
NTSB Number
SEA08LA079
Location
Carefree, AZ
Event ID
20080228X00246
Coordinates
33.818054, -111.897781
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The collapse of the landing gear during landing rollout for undetermined reasons.

Aircraft Information

Registration
Make
CESSNA
Serial Number
P21000323
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
P210NC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
P210N

Registered Owner (Current)

Name
96K LLC
Address
39382 N SPUR CROSS RD
City
CAVE CREEK
State / Zip Code
AZ 85331-8528
Country
United States

Analysis

On February 9, 2008, about 1845 mountain standard time, a Cessna P210N, N4796K, was substantially damaged when the left main landing gear collapsed during landing roll on runway 24 at the Sky Ranch Airport at Carefree (18AZ), Carefree, Arizona. The commercial pilot, the sole occupant of the airplane, was not injured. The airplane was registered to 96K LLC of Scottsdale, Arizona, and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91. Night visual meteorological conditions prevailed and no flight plan was filed for the cross-country flight that departed from the Telluride Regional Airport, Telluride, Colorado, at 1700.

In a written statement, the pilot reported that after an uneventful flight, he entered the traffic pattern for runway 24 and proceeded to make a "normal left pattern approach." Shortly after landing, during the landing roll, the pilot stated he thought he "had blown the left tire" followed by the airplane settling onto its left side a second or two later. The airplane veered to the left and exited the runway, subsequently coming to rest upright adjacent to the runway.

A Federal Aviation Administration inspector conducted a post accident inspection and reported that the left horizontal stabilizer and elevator sustained substantial damage during the accident sequence. Further examination revealed the landing gear warning horn was found inoperative due to a disconnected cable between the throttle switch and the warning horn. The inspector reported that during the landing gear examination the gear was cycled (with the airplane elevated on jack stands) to the down and locked position and no anomalies were noted.

The reason for the gear collapse is undetermined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08LA079