P/N: 96-380021-17
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 | 2 Available |
| As Removed | 1 Available |
The 96-380021-17 is a flap actuator for Beechcraft piston aircraft wing-control systems. This component converts hydraulic or electrical input into linear motion to extend and retract wing flaps during flight operations. The actuator interfaces with flight-control linkages and drive mechanisms to position flaps at commanded angles.
Installation requires verification against the aircraft's Illustrated Parts Catalog and rigging per Beechcraft maintenance manual specifications. Commonly found on select Beechcraft models for coordinated flap operation and flight-envelope management.
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 96-380021-17 is a flap actuator for Beechcraft piston aircraft wing-control systems. This component converts hydraulic or electrical input into linear motion to extend and retract wing flaps during flight operations.
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, 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.