N56LG

Substantial
None

AVIAT A-1 S/N: 1313

Accident Details

Date
Tuesday, August 13, 1996
NTSB Number
SEA96LA190
Location
WORLAND, WY
Event ID
20001208X06627
Coordinates
44.000141, -107.949958
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

overload failure of the landing gear axle, after its design stress limits had been exceeded at some undetermined time.

Aircraft Information

Registration
N56LG
Make
AVIAT
Serial Number
1313
Engine Type
Reciprocating
Model / ICAO
A-1 HUSK
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HALFRICH WILLIAM C
Address
8749 BLACKOAKS LN N
Status
Deregistered
City
MAPLE GROVE
State / Zip Code
MN 55311-1468
Country
United States

Analysis

On August 13, 1996, at 1150 mountain daylight time, an Aviat Inc. A-1, N56LG, registered to Scott Erickson Aviation and operated by the pilot as a 14 CFR Part 91 personal flight, nosed over during the landing roll on a dirt airstrip near Worland, Wyoming. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane was substantially damaged and the commercial pilot and his passenger were not injured. The flight had departed from Fairburn, South Dakota, approximately two hours prior to the accident.

The pilot reported in a written statement, that he landed the airplane into the wind. As the airplane touched down, the right main landing gear collapsed. The airplane veered to the right and nosed over. After the accident, the right main landing gear tire was found approximately 100 feet from the airplane, to the left of the runway.

A metallurgical inspection of the right side wheel axle was performed by AADFW, Inc. Euless, Texas. The results of the tests revealed that the chemical and physical properties of the tube were acceptable and no defects in the material quality were noted. The specialist performing the test reported that "the fracture was an overload fracture that started on the bottom of the tube and progressed upwards. This fracture progression is consistent with a large upward load on the end of the axle such as would be experienced in a hard landing." The fracture passed through a toe weld, however, the specialist determined that the weld had nothing to do with the initiation of the fracture. The timing of the overload failure 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# SEA96LA190