P/N: 35-524386-3
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 35-524386-3 is an actuator for the elevator trim tab system on Beechcraft piston aircraft. This component adjusts the trim tab position within the tailplane trim mechanism, allowing pilots to control elevator trim during flight. The actuator integrates with the 35-524386 assembly family and operates through mechanical linkages to the flight control system.
Installation and rigging must follow the aircraft's approved maintenance manual and Illustrated Parts Catalog specifications. Verify compatibility with your specific Beechcraft model before installation.
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 35-524386-3 is an actuator for the elevator trim tab system on Beechcraft piston aircraft. This component adjusts the trim tab position within the tailplane trim mechanism, allowing pilots to control elevator trim 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.