P/N: 128-520004-1
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 |
|---|---|
| As Removed | 2 Available |
The 128-520004-1 is a rudder pedal rod assembly that transfers pilot input from the cockpit pedals to the directional control system. This linkage component connects the pedal cluster to the bellcrank mechanism, enabling rudder deflection during flight. Used in Textron Hawker 400/400XP aircraft, the assembly features steel construction with AN/MS hardware interfaces.
Installation requires torque verification per the aircraft maintenance manual and compatibility confirmation in the Illustrated Parts Catalog.
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 128-520004-1 is a rudder pedal rod assembly that transfers pilot input from the cockpit pedals to the directional control system. This linkage component connects the pedal cluster to the bellcrank mechanism, enabling rudder deflection during flight.
The ROD ASSEMBLY -RUDDER PEDAL. 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 ROD ASSEMBLY -RUDDER PEDAL.. 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 128-520004-1.