P/N: 6361215-21
Category: Valves & Actuators
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 | 1 Available |
The 6361215-21 is a rudder trim actuator assembly for Cessna Citation 525/560 aircraft. This component provides controlled adjustment of the rudder trim tab position through electrical or hydraulic input, maintaining directional control authority during flight. The actuator converts control signals into linear motion to position the trim servo as commanded by the flight crew.
Installation requires verification against the aircraft's Illustrated Parts Catalog and adherence to the Aircraft Maintenance Manual procedures. Follows aerospace actuator standards including SAE ARP4255 design guidance.
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 6361215-21 is a rudder trim actuator assembly for Cessna Citation 525/560 aircraft. This component provides controlled adjustment of the rudder trim tab position through electrical or hydraulic input, maintaining directional control authority during flight.
Hydraulic component compatibility depends on the aircraft system design. Common aviation hydraulic fluids include MIL-PRF-5606 (mineral-based), MIL-PRF-83282 (synthetic), and Skydrol (phosphate ester). Verify the ACTUATOR against your aircraft maintenance manual for fluid compatibility.
Overhauled and repaired hydraulic components are pressure-tested per manufacturer specifications and include 8130-3 documentation. The ACTUATOR is available in: As Removed. Contact us for test documentation on your selected condition.
In-stock hydraulic components ship same business day before 3 PM EST. We provide 24/7 AOG support at (904) 998-9101 for urgent hydraulic system needs. RFQ submissions are typically quoted within 24 hours.