P/N: 20-2722-07-00
Category: Flight Computers
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 20-2722-07-00 is a torsion spring for rudder control systems that applies rotational preload to center and return the rudder to neutral position. Manufactured from aircraft spring steel for high-cycle endurance in primary flight-control linkages, this spring installs between pedal or control horn brackets. Qualified maintenance personnel must fit and adjust the spring per aircraft maintenance manual specifications to ensure correct breakout force and full rudder travel.
Critical for responsive rudder control and pilot safety.
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 20-2722-07-00 is a torsion spring for rudder control systems that applies rotational preload to center and return the rudder to neutral position. Manufactured from aircraft spring steel for high-cycle endurance in primary flight-control linkages, this spring installs between pedal or control horn brackets.
Avionics compatibility depends on your aircraft model and existing installation. The TIRSION SPRING, RUDDER is available in: New Surplus. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.