P/N: 600-92301-65
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 600-92301-65 is a horizontal stabilizer trim actuator for Bombardier Learjet aircraft. This component drives the stabilizer jackscrew to adjust pitch trim during flight operations. Installed within the tailplane trim mechanism, it modulates stabilizer incidence to maintain desired aircraft pitch attitude.
The actuator interfaces with the flight control system and responds to trim commands from the flight deck. Maintenance and rigging must follow the aircraft maintenance manual specifications. Verify part compatibility in the Illustrated Parts Catalog before installation on your airframe.
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 600-92301-65 is a horizontal stabilizer trim actuator for Bombardier Learjet aircraft. This component drives the stabilizer jackscrew to adjust pitch trim 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 ACTUATOR, HORIZONTAL STAB TRIM 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, HORIZONTAL STAB TRIM 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.