P/N: 45as61014-1
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 45as61014-1 is a trim actuator for aircraft pitch-control systems. This component converts electrical or hydraulic signals from the cockpit or autopilot into linear motion that adjusts the horizontal stabilizer or trim tab position. By moving the trim surface, the actuator reduces control forces needed to maintain level flight and compensate for weight and balance changes.
Installation requires verification against the aircraft's Illustrated Parts Catalog (IPC) and adherence to applicable maintenance manual procedures. Ensure proper rigging and attachment hardware compatibility before flight operations.
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 45as61014-1 is a trim actuator for aircraft pitch-control systems. This component converts electrical or hydraulic signals from the cockpit or autopilot into linear motion that adjusts the horizontal stabilizer or trim tab position.
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 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 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.