N2151C

Substantial
None

Cessna 195 S/N: 16136

Accident Details

Date
Monday, May 31, 1999
NTSB Number
FTW99LA156
Location
CONROE, TX
Event ID
20001212X18786
Coordinates
30.379695, -95.380706
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The fatigue fracture of the left main landing gear spring at the clamping mechanism, as a result of fretting.

Aircraft Information

Registration
Make
CESSNA
Serial Number
16136
Engine Type
Reciprocating
Year Built
1954
Model / ICAO
195 C195
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
5
FAA Model
195B

Registered Owner (Current)

Name
ATKINSON PATRICK C
Address
7405 WINTERBLOOM WAY
City
FORT WORTH
State / Zip Code
TX 76123-2158
Country
United States

Analysis

On May 31, 1999, at 1458 central daylight time, a Cessna 195 single-engine tail wheel equipped airplane, N2151C, owned and operated by the pilot, was substantially damaged during landing at the Montgomery County Airport near Conroe, Texas. The private pilot and the three passengers were not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight originated from the David Wayne Hooks Memorial Airport, Houston, Texas, at 1430.

The pilot reported that during landing on runway 19, he made a wheel landing, and a tail high attitude was maintained until the tail started to lower with "speed drop off." During the landing roll, the pilot "heard a loud pop, then about 2 seconds later the [left] wing dropped to the runway and we started to slide." The aircraft slid about 50 to 75 feet before coming to a stop. The pilot found the left main landing gear in the middle of the runway, approximately 80 to 90 feet from where the airplane came to a stop.

An examination of the aircraft by the FAA inspector revealed that the left main landing gear was separated from the fuselage, the left wing was wrinkled, and the left aileron was damaged.

The inboard section of the separated left main landing gear spring was sent to the NTSB Materials Laboratory for examination. The examination revealed that "fatigue initiated from an area that contained fretting damage from contact with the clamping mechanism. Fretting on the upper surface extended almost to the aft edge of the spring. Similar areas of fretting were noted on the bottom surface near the fracture and around the bolt hole." See the enclosed Metallurgist's Factual Report for details of the examination.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW99LA156