N2118S

Substantial
None

CESSNA T210LS/N: 21061081

Accident Details

Date
Wednesday, July 1, 2009
NTSB Number
CEN09LA417
Location
Santa Teresa, NM
Event ID
20090707X52718
Coordinates
31.881111, -106.704719
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the landing gear accumulator seal for undetermined reasons. Contributing to the accident was the pilot’s failure to confirm the status of the landing gear.

Aircraft Information

Registration
Make
CESSNA
Serial Number
21061081
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
T210LC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
T210L

Registered Owner (Current)

Name
ABES ERIKA
Address
9816 SAIGON DR
City
EL PASO
State / Zip Code
TX 79925-5339
Country
United States

Analysis

On July 1, 2009, at 0830 mountain daylight time, a Cessna T210L airplane, N2118S, was substantially damaged during landing at Dona Ana County Airport (5T6), Santa Teresa, New Mexico. The private pilot was not injured. The flight was being conducted under the provisions of Title 14 Code of Federal Regulations Part 91 without a flight plan. The flight originated at Cielo Dorado Estates Airport (TA50), El Paso, Texas, and was terminating at the time of the accident. Visual meteorological conditions prevailed at the time of the accident.

The pilot reported he lowered the landing gear handle on downwind to land and heard the gear cycle down. He told the investigator he could not recall if he saw green, gear down indicator lights. While in the landing flare he heard someone call "gear, gear" on the radio, but it was too late for him to go around. The left main gear collapsed on touchdown and the airplane exited the side of the runway. The pilot did not recall hearing the gear warning horn prior to landing.

Examination of the airplane revealed substantial damage to the horizontal stabilizer and the elevator. The right main and nose landing gear were found in a down and locked position and the left main was in the gear well. During initial inspection by FAA investigators the left landing gear did not extend fully and lock into position during manual extension, but the gear operated correctly and did lock down when hydraulic power was applied to the system. The hydraulic system was found to be properly serviced and the three gear indicator lights operated properly when the gear was extended and locked. The airplane was taken to a repair station and the landing gear was examined further. No abnormalities were found with the airplane at that time. The witness who made the radio call of “gear, gear” could not be located.

In the months after the accident, and following the repairs to the airplane, the pilot had four additional landing gear malfunctions and failures to extend. He said he had to manually extend the gear during each instance. After the fourth occurrence, the nose gear up-lock actuator and the landing gear accumulator were removed and resealed. The seal in the landing gear accumulator was found to leak. The accumulator requires gaseous nitrogen or dry air. The seals from the accumulator were not retained by maintenance personnel and were not available for examination by investigators. The reason for the failure of the seals was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA417