Event Description
The pilot reported that shortly after applying takeoff power, the airplane deviated left of the runway centerline. While attempting to correct, the right main wheel assembly and right landing gear strut collapsed.
Post-Accident Examination
Examination of the wheel assembly and tire showed the outboard wheel subassembly fractured along the bead seat ring in multiple locations. The inboard wheel subassembly also exhibited multiple fractures, and the brake disc had partially separated from the wheel.
Aircraft Information
The Type Certificate Data Sheet for the airplane lists several approved wheel-brake assemblies. The wheel assembly installed on the accident airplane was not among the approved configurations. Furthermore, the installed wheel assembly was not approved for use with tires larger than size 7.00-6, but the airplane was equipped with 8.00-6 tires. The airplane's most recent annual inspection occurred on March 7, 2002.