N3124N

Substantial
None

CESSNA 120S/N: 13382

Accident Details

Date
Saturday, October 24, 2015
NTSB Number
WPR16LA018
Location
Lone Pine, CA
Event ID
20151027X01906
Coordinates
36.588890, -118.047500
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The fracture of the left main landing gear (MLG) wheel axle due to fatigue, which resulted in the separation of the left MLG wheel during takeoff from a dirt airstrip.

Aircraft Information

Registration
N3124N
Make
CESSNA
Serial Number
13382
Engine Type
Reciprocating
Year Built
1947
Model / ICAO
120C120
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MARKLE-ALLEN INIGO G
Address
110 SUTTER ST APT 24
Status
Deregistered
City
TEHACHAPI
State / Zip Code
CA 93561-2429
Country
United States

Analysis

On October 24, 2015, about 1500 Pacific daylight time, a tailwheel-equipped Cessna 120 airplane, N3124N, sustained substantial damage following a nose over during takeoff at the Lone Pine Airport, Lone Pine, California. The private pilot was not injured. The flight was being operated as a personal cross country flight under the provisions of 14 Code of Federal Regulations Part 91 when the accident occurred. Visual meteorological conditions prevailed and no flight plan had been filed for the flight destined to Tehachapi, California.

In a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge, the pilot stated that he was on his way back home from a weekend trip. During the takeoff roll on the dirt runway, just after raising the tail off the ground, he felt the sensation of hitting soft soil with the left main landing gear. He attempted to correct for the condition, but the left main landing gear wheel continued to drag, and then the airplane suddenly nosed over. During the nose over, the airplane sustained substantial damage to the wings and empennage.

Postaccident examination of the airplane revealed that the left main landing gear wheel axle was fractured. A detailed examination of the fracture surface by the NTSB Materials Laboratory showed a fatigue fracture that emanated from the outer surface of a circumferential weld between the lateral tube portion and the vertical plate portion of the axle. The fatigue crack portions at the origin areas was covered with yellow deposits. The yellow deposits was identified by EDS spectra as zinc chromate, a compound found in primer paint.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR16LA018