P/N: 390-386004-0005
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 | 1 Available |
The 390-386004-0005 is a pitch trim actuator that repositions the stabilizer or trim tab to reduce control forces during flight. This linear actuator assembly converts electrical or hydraulic input into controlled movement of the pitch trim system. It maintains the aircraft's pitch attitude by holding the trim surface at commanded positions, reducing pilot workload on long flights.
Installation requires verification against the aircraft's Illustrated Parts Catalog and adherence to the applicable maintenance manual rigging procedures.
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 390-386004-0005 is a pitch trim actuator that repositions the stabilizer or trim tab to reduce control forces during flight. This linear actuator assembly converts electrical or hydraulic input into controlled movement of the pitch trim system.
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 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 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.