Piper - 62743-006 - Spacer Bearing, Control System

Piper - 62743-006 - Spacer Bearing, Control System
P/N: 62743-006
Product Code: AFP840F
Certificate Type: FAA 8130-3
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The 62743-006 is a Piper OEM control system spacer bearing, used within aircraft flight control linkages to maintain correct alignment, spacing, and smooth movement between moving mechanical components. It functions as a precision spacer and bearing interface element in control system assemblies where controlled rotation or pivoting motion is required.
In typical Piper aircraft applications, this component is installed in flight control linkage systems, such as elevator, aileron, or rudder control assemblies (depending on aircraft model). Its primary role is to maintain proper geometry between connected parts while reducing friction and preventing metal-to-metal wear at pivot points.
The spacer bearing ensures that bolts or pins rotate freely without binding and that control loads are transmitted smoothly through the linkage system. It also helps maintain precise alignment, which is critical for consistent and predictable control response during flight.
Manufactured to Piper OEM specifications, the 62743-006 is typically made from bearing-grade metal or corrosion-resistant alloy material, selected for durability, low friction performance, and resistance to wear under cyclic loading and vibration.
Because it is part of the primary flight control system, wear or deformation can directly affect control feel, precision, and safety. Regular inspection for wear, elongation, or surface damage is required during scheduled maintenance.
Key features include:
Piper 62743-006 spacer bearing (control system component)
Used in flight control linkage assemblies (model dependent)
Maintains spacing and alignment between control components
Provides low-friction pivot interface in control systems
Prevents metal-to-metal wear in moving joints
Material: aircraft-grade bearing alloy or corrosion-resistant steel
Ensures smooth and precise control surface movement
Critical for elevator, aileron, or rudder linkage geometry
Subject to inspection for wear and dimensional integrity
Direct replacement part per Piper IPC specifications
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