P/N: 137254b3
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
The 137254b3 is a self-lubricating rod end for aircraft control linkages. This articulating joint accommodates misalignment while transmitting loads in elevator push-pull assemblies and other control systems. Featuring a PTFE liner per AS81820 specifications, the rod end reduces friction and wear during repeated articulation.
Installation requires proper thread engagement and torque per aircraft maintenance manual guidance. Safetying and inspection follow FAA AC 43.13-1B standards for control system components.
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 137254b3 is a self-lubricating rod end for aircraft control linkages. This articulating joint accommodates misalignment while transmitting loads in elevator push-pull assemblies and other control systems.
The ROD END 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: New Surplus. 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 ROD END. 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 137254b3.