P/N: f20g8011209-14
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 f20g8011209-14 is a rod end for aircraft flight-control linkages. This articulating joint connects a threaded rod to a bellcrank or actuator, accommodating misalignment and low-torque rotation under load. Manufactured from steel or corrosion-resistant steel (CRES) per SAE AS6039 standards (MS21150–MS21153 family).
Installation requires locking devices and keys per applicable NAS/AS standards, with torque and assembly procedures following the aircraft maintenance manual. Used throughout control systems on general and commercial aviation 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 f20g8011209-14 is a rod end for aircraft flight-control linkages. This articulating joint connects a threaded rod to a bellcrank or actuator, accommodating misalignment and low-torque rotation under load.
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 f20g8011209-14.