Helicopter Tail Rotor Control System Components
The 350A33-1058-02 Control Lever is a precision mechanical component used in the tail rotor control assembly of Airbus AS350 and H125 helicopters. It functions as a critical pivot arm that translates pilot pedal input into tail rotor pitch changes, directly affecting yaw control. Manufactured to meet stringent aerospace standards, this lever is essential for smooth, responsive control during flight operations.
Functions:
- Transmits pedal input into tail rotor pitch movement
- Acts as a linkage point in the tail rotor control chain
- Enables accurate and stable yaw control
- Designed to operate reliably under high vibration and load
- Maintains control alignment and mechanical feedback consistency
Applications:
The 350A33-1058-02 is installed on Airbus AS350 series helicopters, including the H125. It is part of the tail rotor pitch control linkage and plays a vital role in directional control and anti-torque response. Used across diverse rotorcraft missions including air medical transport, law enforcement, utility work, and aerial tourism, the part ensures safe handling and maneuverability.
PAG support:
Precision Aviation Group (PAG) provides complete support for the 350A33-1058-02 Control Lever, including:
- FAA/EASA-certified repairs and overhauls
- OEM-approved and PMA part availability
- Rapid global distribution and AOG support
- Tail rotor system diagnostics and installation consultation
- Lifecycle tracking and exchange units for operational continuity
Contact Us for Related parts:
- 350A33-0200-07 – Tail Rotor Gearbox
- 350A33-0200-05 – Tail Rotor Gearbox
- 350A33-1091-00 – Tail Rotor Pitch Change Arm
- 350A33-0X01-XX – Tail Rotor Gear Box (Series)
- 350A32-0500-02 – Rotor Brake Assembly
- 350A32-001X-00 – Main Gear Box Assembly
