N89694

Substantial
None

CESSNA 152 S/N: 15282828

Accident Details

Date
Thursday, August 24, 1995
NTSB Number
MIA95LA213
Location
LUMBERTON, MS
Event ID
20001207X04333
Coordinates
30.999479, -89.450157
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, STEERING SYSTEM (ROD END BOLT) DUE TO A BENDING OVERSTRESS SEPARATION WHICH RESULTED IN LOSS OF DIRECTIONAL CONTROL.

Aircraft Information

Registration
N89694
Make
CESSNA
Serial Number
15282828
Engine Type
Reciprocating
Model / ICAO
152 C152
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BEETS LARRY JOE
Address
307 LOFTIN RD
Status
Deregistered
City
COLUMBIA
State / Zip Code
MS 39429-9238
Country
United States

Analysis

On August 24, 1995, about 1350 central daylight time, a Cessna 152, N89694, registered to a private owner, operating as a 14 CFR Part 91 instructional flight crashed on takeoff at the I.H. Bass Jr. Memorial Airport, Lumberton, Mississippi. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage. The student pilot reported no injuries. The flight was originating at the time of the accident.

The student pilot stated as he began his takeoff roll the airplane veered to the left. He applied right rudder and the airplane continued to the left. Full right rudder was applied and the airplane jerked to the left. He pulled the power off, applied right brake, and the airplane went off the left side of the runway and nosed over.

Examination of the runway surface by an FAA inspector revealed an arc like skid mark about 30 feet long which ended at the edge of the runway. Further examination of the nose gear by the FAA inspector revealed a broken rod bolt through the threaded shank between the locking nut and the bearing head.

The rod end from the right nose steering linkage, at the nose wheel steering collar was forwarded to the NTSB Materials Laboratory for analysis. Examination of the rod end revealed it was fractured through the threaded shank between the locking nut and the bearing head. The fracture face on the bearing head was obscured by corrosion deposits, but the mating face was clean. Magnified examination of the clean face revealed features typical of bending overstress separation. (For additional information see NTSB Metallurgist's Factual Report No. 95-143).

The component was released to the registered owner on September 15, 1995.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA95LA213