P/N: 9912111-1
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 9912111-1 is a main landing gear actuator for the Cessna Citation IIS (Model 550S). This hydraulic actuator converts pressurized fluid commands into controlled linear motion to extend and retract the landing gear strut. Installed within the landing gear hydraulic system, it positions the gear assembly during takeoff and landing cycles.
Installation and rigging must follow the aircraft maintenance manual specifications. Verify compatibility with your aircraft's Illustrated Parts Catalog before installation to ensure proper fit and function.
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 9912111-1 is a main landing gear actuator for the Cessna Citation IIS (Model 550S). This hydraulic actuator converts pressurized fluid commands into controlled linear motion to extend and retract the landing gear strut.
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 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 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.