Helicopter Tail Rotor Control System Components
The 350A33-1058-03X Tail Rotor Control Lever is a critical mechanical linkage component used in the tail rotor pitch control system of Airbus AS350 and H125 helicopters. It functions as an actuator arm that translates pilot pedal inputs into mechanical movement, enabling precise pitch adjustments of the tail rotor blades. The lever is engineered to meet demanding aerospace performance and fatigue-resistance requirements, ensuring safe and stable yaw control in all flight phases.
Functions:
- Transfers pedal movement to tail rotor pitch links
- Enables controlled yaw correction and anti-torque balance
- Supports smooth transition and precise directional response
- Designed to perform under high vibration and stress conditions
- Maintains mechanical integrity within the tail rotor control chain
Applications:
Used in Airbus AS350 series helicopters including the H125, the 350A33-1058-03X Tail Rotor Control Lever is a key part of the directional control system. It is essential for mission types such as emergency medical services, aerial utility work, police aviation, VIP transport, and firefighting—where flight precision and stability are critical.
PAG Support:
Precision Aviation Group (PAG) supports the 350A33-1058-03X Tail Rotor Control Lever with OEM and PMA-approved parts, FAA and EASA-certified MRO services, global inventory stocking and AOG response, technical consultation for tail rotor system installation and troubleshooting, and exchange programs to reduce downtime and support fleet readiness.
Contact Us for Related Parts:
- 350A33-1058-02 – Control Lever
- 350A33-1058-03 – Tail Rotor Control Lever
- 350A33-0200-07 – Tail Rotor Gearbox
- 350A33-0200-05 – Tail Rotor Gearbox
- 350A33-1091-00 – Tail Rotor Pitch Change Arm
- 350A32-0500-02 – Rotor Brake Assembly
- 350A32-001X-00 – Main Gear Box Assembly
