P/N: 45-521212-604
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 45-521212-604 is a Beechcraft flap actuator assembly that converts control inputs into mechanical motion for trailing-edge flap positioning. This actuator drives flap extension and retraction in the wing system, responding to pilot commands through the flight control network. Installation requires verification of part-number applicability in the aircraft's Illustrated Parts Catalog and adherence to wing flap system rigging procedures outlined in the maintenance manual.
Proper installation ensures synchronized flap operation and maintains aerodynamic integrity during all flight phases.
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 45-521212-604 is a Beechcraft flap actuator assembly that converts control inputs into mechanical motion for trailing-edge flap positioning. This actuator drives flap extension and retraction in the wing system, responding to pilot commands through the flight control network.
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: 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.