9882010-1 - Textron Aviation OEM Cylinder Actuator

9882010-1 – Textron Aviation OEM Cylinder Actuator

Available now on the Airparts.aero Marketplace.

Overview

The Textron Aviation 9882010-1 is a genuine OEM, flight-critical hydraulic cylinder actuator, engineered for the thrust reverser system on various Cessna Citation business jets. This is not a simple cylinder; it is a high-performance, precision-machined hydraulic actuator responsible for translating hydraulic pressure into the powerful mechanical force required to deploy and stow the engine's thrust reverser buckets or doors. Manufactured to Textron's exacting standards, this actuator is built to withstand the extreme pressures, temperatures, and vibrations of the engine nacelle environment, ensuring reliable and symmetrical thrust reverser operation.

Key Features

• High-Pressure Hydraulic Actuation: Designed to operate flawlessly within the aircraft's 3000 PSI hydraulic system. It features a honed cylinder bore and a precision-lapped piston with high-performance seals to provide smooth, leak-free actuation.
• Thrust Reverser System Component: A primary actuator in the cascade-type or target-type thrust reverser system. Its precise and synchronized movement is essential for effective reverse thrust generation during the landing rollout.
• High-Strength Steel Construction: Fabricated from high-tensile strength, heat-treated steel alloys to provide the immense force needed to move the reverser doors against the aerodynamic loads of the engine's exhaust stream.
• Corrosion-Resistant Finish: Plated with a durable, corrosion-resistant finish to protect the actuator from the harsh environmental conditions and high temperatures within the engine nacelle.
• Genuine Textron OEM Part: As a genuine factory component, it guarantees perfect fitment, certified hydraulic performance, and seamless integration with the aircraft's thrust reverser control logic and structural mounting points.

Technical Specifications

• Part Number: 9882010-1
• Component Type: Hydraulic Cylinder Actuator
• Primary Application: Thrust Reverser Actuation
• Actuation Fluid: Aircraft Hydraulic Fluid (e.g., Skydrol)
• Operating Pressure: Designed for 3000 PSI systems.
• Material: High-Strength Steel Alloy
• Certification: FAA Production Approval

Aircraft Compatibility

The 9882010-1 is a key component in the thrust reverser systems of some of the most popular and successful business jets in the world. It is imperative to consult the specific aircraft's Illustrated Parts Catalog (IPC) for final verification.

• Primary Aircraft Models:
  • Cessna Citation 560: Ultra, Encore, Excel, XLS, XLS+
  • Cessna Citation 650: Citation III, VI, VII
  • Cessna Citation 750: Citation X

Applications

The 9882010-1 is a flight-critical component for safe and efficient ground operations:

• Aircraft Deceleration: Its sole purpose is to deploy the thrust reverser doors, which redirect engine exhaust forward to create reverse thrust and dramatically reduce the aircraft's landing distance.
• System Overhaul & Repair: A primary component to be overhauled or replaced when troubleshooting thrust reverser system faults, hydraulic leaks, or during scheduled major inspections.

Why Choose 9882010-1?

The thrust reverser system is a critical safety system, especially for operations on shorter or contaminated runways. The symmetrical and reliable deployment of the reverser doors is paramount. Using a genuine Textron Aviation 9882010-1 OEM actuator is the only way to ensure the component has the certified material strength, precise internal tolerances, and high-performance seals required to function flawlessly under extreme loads. For a system this critical to stopping performance, there is no substitute for a fully traceable, certified OEM part.

Order Your 9882010-1 Actuator Now

Ensure the reliability and safety of your aircraft's thrust reverser system with a genuine Textron Aviation OEM component. Visit Airparts.aero to inquire about new or overhauled 9882010-1 actuators today.

The 9882010-1 is a linear hydraulic actuator that converts fluid power into mechanical work. When commanded to deploy, high-pressure hydraulic fluid is directed by a control valve to one side of the actuator's internal piston. The pressure (P) acting over the area (A) of the piston face creates an immense force (F=P×A) that extends the actuator's rod. This linear motion is transferred via linkages to the thrust reverser doors, pushing them into the engine's exhaust stream. To stow the reverser, hydraulic pressure is applied to the opposite side of the piston. The precision honing of the cylinder and the design of the piston seals are critical for preventing internal bypass, ensuring that the full hydraulic force is converted into mechanical motion for powerful and reliable deployment.

Note: This is a flight-critical system component. Installation, rigging, and testing must be performed by a certified A&P or AME mechanic with experience in Citation hydraulic and thrust reverser systems, in strict accordance with the current Textron Aviation maintenance manual. A full operational check, including checks for symmetrical deployment and proper indication, is required after installation.