P/N: 96-526000-619
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 |
|---|---|
| New Surplus | 1 Available |
The 96-526000-619 is a rudder trim actuator assembly for Beechcraft piston aircraft. This component drives the rudder trim tab, enabling in-flight yaw trim adjustments from the cockpit. The actuator connects the pilot's trim control input to the trim tab mechanism, allowing fine directional control during cruise and approach phases.
Classified under ATA Chapter 27 and subject to export control ECCN 9A991.d. Installation requires verification of IPC compatibility and rigging per the applicable aircraft maintenance manual to ensure proper trim tab travel and control response.
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 96-526000-619 is a rudder trim actuator assembly for Beechcraft piston aircraft. This component drives the rudder trim tab, enabling in-flight yaw trim adjustments from the cockpit.
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 ASSEMBLY - TRIM RUD 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 ASSEMBLY - TRIM RUD is available in: New Surplus. 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.