N6094B

Substantial
None

CESSNA T210M S/N: 21062681

Accident Details

Date
Friday, February 17, 1995
NTSB Number
FTW95LA120
Location
MONTROSE, CO
Event ID
20001207X02969
Coordinates
38.490009, -107.869491
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

THE BENT LANDING GEAR EMERGENCY EXTENSION ASSEMBLY AND THE ACCUMULATION OF AIRFRAME ICE WHICH INTERFERED WITH LANDING GEAR ACTIVATION. A FACTOR WAS THE ALTERNATOR FAILURE FOR UNKNOWN REASONS.

Aircraft Information

Registration
Make
CESSNA
Serial Number
21062681
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
T210M C210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
T210M

Registered Owner (Current)

Name
T 210 TELLURIDE CORP
Address
610 E HYMAN AVE
City
ASPEN
State / Zip Code
CO 81611-1923
Country
United States

Analysis

On February 17, 1995, at 1115 mountain standard time, a Cessna T210M, N6094B, was substantially damaged during a precautionary landing at the Montrose, Colorado, Airport. The pilot and his two passengers were not injured. Visual meteorological conditions prevailed for this personal flight which departed Aspen, Colorado, for Telluride, Colorado, at 0900. No flight plan was filed.

While in cruise flight, the electrical system failed and the pilot elected to proceed to Montrose, an intermediate airport along his route of flight. He contacted the airport on a cellular phone and had equipment standing by while he orbited the area and tried to lower the landing gear by the alternate method.

The nose landing gear locked in place but the mains remained in trail. After burning off fuel, a landing was made and the aircraft went off the side of the runway sustaining damage to the right horizontal stabilizer and right wing tip.

According to a mechanic, who examined the aircraft, he could find no abnormalities in the electrical system. He stated, the electrical failure was probably the result of the pilot failing to turn on the alternator. The pilot said he used proper procedures in operating the electrical system.

According to the same mechanic, the inability of the pilot to lower the landing gear by the alternate method was due to a gear linkage rod being bent. The mechanic said that there was a considerable amount of ice on the aircraft, when he first examined it, following the landing, and that the ice may have interfered with landing gear actuation causing the rod to bend.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA120