P/N: 6261305-3
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 |
|---|---|
| Serviceable | 1 Available |
The 6261305-3 is a rudder trim actuator assembly for Cessna 650 Citation III/IV/VI/VII aircraft. This metal construction component converts pilot inputs into controlled rudder trim tab positioning during flight operations. Located in the rudder trim mechanism, the actuator translates electrical or hydraulic signals to adjust trim settings for improved directional stability and control.
Installation requires verification against the aircraft's Illustrated Parts Catalog and adherence to the applicable maintenance manual procedures. Commonly found in MRO inventory for Citation series maintenance and repair.
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 6261305-3 is a rudder trim actuator assembly for Cessna 650 Citation III/IV/VI/VII aircraft. This metal construction component converts pilot inputs into controlled rudder trim tab positioning 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 A 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 A is available in: Serviceable. 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.