P/N: 6361215-13
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 6361215-13 is a rudder trim actuator assembly for Cessna Citation 525 and 560 aircraft. This jack assembly drives the rudder trim mechanism to adjust yaw balance and control pressure during flight operations. The actuator interfaces with the flight control system to maintain directional stability without requiring continuous pilot input on the rudder pedals.
Installation requires verification against the aircraft's Illustrated Parts Catalog and compliance with applicable Aircraft Maintenance Manual procedures. Proper functioning ensures efficient trim control and reduced pilot workload during extended flight.
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 6361215-13 is a rudder trim actuator assembly for Cessna Citation 525 and 560 aircraft. This jack assembly drives the rudder trim mechanism to adjust yaw balance and control pressure during flight operations.
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.