P/N: s1820-4
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 | 2 Available |
The s1820-4 is a Cessna rod end featuring a spherical bearing joint for aircraft control linkages. This component provides articulating connection on push-pull tubes and threaded control rods, allowing controlled misalignment in flight-control assemblies. Manufactured to MS21151/MS21153 specifications, the rod end enables smooth pivoting action essential for aileron, elevator, and rudder control systems.
Installation requires proper thread engagement and hardware clamp-up on the bearing race per aircraft maintenance manual procedures. Steel construction with corrosion-resistant finish.
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 s1820-4 is a Cessna rod end featuring a spherical bearing joint for aircraft control linkages. This component provides articulating connection on push-pull tubes and threaded control rods, allowing controlled misalignment in flight-control assemblies.
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 s1820-4.