P/N: 0501154-2
Category: Structural Components
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 0501154-2 is an idler plate that serves as an intermediate pivot point in aircraft control linkages. This durable metal component redirects and supports cable runs while maintaining proper alignment in mechanical systems. Installed in control-cable routing applications where direction changes are required, the idler plate prevents cable misalignment and reduces binding during control surface movement.
Installation follows the applicable aircraft maintenance manual with proper torque specifications. Verify part applicability in your aircraft's Illustrated Parts Catalog before replacement.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 0501154-2 is an idler plate that serves as an intermediate pivot point in aircraft control linkages. This durable metal component redirects and supports cable runs while maintaining proper alignment in mechanical systems.
The IDLER PLATE may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the IDLER PLATE. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 0501154-2.