P/N: 50-521153-2
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 50-521153-2 is a flap actuator assembly for Beechcraft aircraft, converting pilot inputs into controlled wing flap positioning. This electromechanical actuator integrates into the high-lift system's flap drive mechanism, translating control commands into precise deflection angles. Installation requires verification against the aircraft's Illustrated Parts Catalog and rigging per the maintenance manual to ensure proper flap synchronization and travel limits.
NSN 1680-00-692-7517.
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 50-521153-2 is a flap actuator assembly for Beechcraft aircraft, converting pilot inputs into controlled wing flap positioning. This electromechanical actuator integrates into the high-lift system's flap drive mechanism, translating control commands into precise deflection angles.
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.