P/N: EM417-2
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 EM417-2 is an electromechanical actuator that converts electrical commands into rotary or linear motion for aircraft control valve positioning. This actuator drives environmental control system flow-control valves, regulating fluid flow through onboard systems. Installation and testing follow aircraft maintenance manual procedures and 14 CFR Part 43 guidelines.
The unit integrates with valve linkages and electrical control circuits to enable automated system regulation. Commonly referenced to SAE ARP5754 and ARP5724A standards for electromechanical actuator performance and compatibility.
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 EM417-2 is an electromechanical actuator that converts electrical commands into rotary or linear motion for aircraft control valve positioning. This actuator drives environmental control system flow-control valves, regulating fluid flow through onboard systems.
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.