P/N: 418-00500-001
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 418-00500-001 is an electromechanical trim actuator for pitch and roll control surfaces. This unit drives stabilizer or trim-tab mechanisms to reduce pilot control forces during flight operations. The actuator converts electrical input into linear motion, positioning trim devices as commanded by the flight control system.
Commonly installed in general aviation and business aircraft trim systems, it interfaces directly with stabilizer linkages and control rigging. Installation requires verification against the aircraft's Illustrated Parts Catalog and adherence to maintenance manual procedures for proper alignment and travel limits.
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 418-00500-001 is an electromechanical trim actuator for pitch and roll control surfaces. This unit drives stabilizer or trim-tab mechanisms to reduce pilot control forces 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 TRIM ACTUATOR,PITCH ROLL 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 TRIM ACTUATOR,PITCH ROLL 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.