P/N: 101-524079-3
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 |
|---|---|
| As Removed | 1 Available |
The 101-524079-3 is a rudder trim tab actuator assembly for Beechcraft King Air aircraft. This component converts pilot input into linear motion to position the rudder trim tab, enabling directional trim control during flight. The actuator interfaces with the flight control system to adjust yaw balance and reduce control pressure.
Installation requires verification against the aircraft's Illustrated Parts Catalog and rigging per the applicable maintenance manual to ensure proper trim tab positioning and system function.
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 101-524079-3 is a rudder trim tab actuator assembly for Beechcraft King Air aircraft. This component converts pilot input into linear motion to position the rudder trim tab, enabling directional trim control 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 TAB 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 TAB 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.