The 96217-000 is a Piper OEM airframe bracket used as a structural mounting component in various light aircraft assemblies. Based on parts catalog listings, it is classified simply as a “bracket” and is used to support, locate, or secure adjacent mechanical or structural components within the aircraft airframe system.

In Piper aircraft, brackets like the 96217-000 are commonly found in roles such as supporting control system routing, securing fairings or interior panels, mounting equipment to the airframe structure, or acting as attachment points for secondary structural elements. While not typically a primary load-bearing structural member, it is still a certified aircraft part and contributes to overall system rigidity and correct alignment of assemblies.

These components are usually manufactured from aircraft-grade aluminum alloy or corrosion-protected steel, depending on the installation location and load requirements. The geometry is application-specific and designed to match exact airframe attachment points defined in the Piper Illustrated Parts Catalog (IPC).

Because brackets are critical alignment and support elements, correct installation and condition are important. Any deformation, corrosion, or elongation of mounting holes can lead to misalignment of connected systems or increased wear on adjacent components.

Key features include:

Piper 96217-000 airframe bracket (OEM structural support component) 
Used for mounting and supporting aircraft systems or structure
Installed in airframe assemblies (location varies by aircraft model)
Material: typically aluminum alloy or corrosion-protected steel
Ensures correct alignment of attached mechanical or structural parts
Not usually primary load-bearing but still structurally significant
Must be inspected for cracks, deformation, and hole wear
Designed to match precise IPC-defined mounting geometry
Common across Piper light aircraft airframe configurations