P/N: s1819-4
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 | 13 Available |
The s1819-4 is a rod end bearing designed for aircraft control linkages and cable terminations. This spherical joint accommodates misalignment between push-pull rods, torque tubes, and control cables while maintaining smooth articulation. Manufactured to MS2115 or AS81935 specifications, it features a steel body with a precision ball socket for reliable performance in flight control systems.
Installation requires verification of thread size and bearing type per the aircraft maintenance manual. Commonly used in aileron, elevator, and rudder control connections on general aviation and corporate aircraft.
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 s1819-4 is a rod end bearing designed for aircraft control linkages and cable terminations. This spherical joint accommodates misalignment between push-pull rods, torque tubes, and control cables while maintaining smooth articulation.
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 s1819-4.