P/N: 418-00862-701
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 |
|---|---|
| Serviceable | 2 Available |
The 418-00862-701 is a pitch/roll trim actuator for aircraft flight-control systems. This electromechanical component provides motor-driven linear adjustment of trim tabs or stabilizers to relieve control forces and maintain aircraft attitude during flight. The actuator responds to pilot trim inputs and autopilot commands, converting electrical signals into precise mechanical movement.
Installed in elevator trim systems per airframe maintenance manual specifications, it enables fine-tuning of pitch and roll stability without continuous control pressure.
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 418-00862-701 is a pitch/roll trim actuator for aircraft flight-control systems. This electromechanical component provides motor-driven linear adjustment of trim tabs or stabilizers to relieve control forces and maintain aircraft attitude 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 PITCH/ROLL TRIM 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 PITCH/ROLL TRIM ACTUATOR is available in: Serviceable. 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.