Yes. PA-32R-301T (the turbocharged Saratoga SP) is listed on the FAA-PMA supplement as an eligible aircraft for MC67184-000.
Yes, the installation and match drilling requires special tooling, capabilities, and treatments. The complete installation procedure is detailed in the Instructions for Continued Airworthiness (ICA) under the MC67184-000 documents tab.
Yes. Both the PA-34-200 and PA-34-200T are listed as eligible aircraft for MC67184-000.
The axle is secured with an AN4-31A bolt, NAS1149F0432P washer, and MS21042-4 nut.
MC67184-000 directly replaces Piper P/N 67184-000. This axle is a sub-component of the Piper axle assembly P/N 67183-000, which is itself a sub-component of strut assemblies P/N 67307-004 and P/N 67037-006.
Signs that the axle may need replacement include visible cracks or separation from the strut, a wheel that is tilted or not perpendicular to the gear leg, and surface discoloration, rust streaks, or hairline cracks. If any of these conditions are present, remove the axle for magnetic particle inspection.
Piper does not sell P/N 67184-000 as a standalone part. The only path through the OEM is to purchase the complete main landing gear strut assembly, which includes numerous components beyond the axle and represents a significant unnecessary expense when the axle alone is the problem. MC67184-000 is designed specifically to solve this.