Tail Rotor Servo
The 41011300-105 Tail Rotor Servo is a hydraulically actuated flight control component that plays a vital role in the yaw control system of rotorcraft. Installed in the tail rotor control loop, it transmits pilot pedal inputs to the tail rotor blades, regulating anti-torque response and directional stability. Engineered for precision and reliability, this servo is essential for safe helicopter maneuvering, especially during hover and low-speed operations.
Part Number: 41011300-105
Functions & Key Features:
- Hydraulic Control Actuation: Translates pilot yaw commands into mechanical tail rotor input
- Yaw Stability & Directional Control: Crucial for anti-torque balance and ground maneuvering
- Robust Aerospace Construction: Withstands harsh environmental and vibration conditions
- OEM-Certified Design: Meets strict airworthiness and performance standards
- High Cycle Life: Designed for continuous operation in dynamic rotorcraft environments
Applications:
The 41011300-105 T/R Servo is used in:
- Light and medium helicopters equipped with hydraulic-assisted tail rotor control systems
- OEM installations and fleet maintenance programs
- Tail rotor system overhauls or replacements for enhanced safety and handling
Typical helicopter models may include:
- Bell 407 and derivatives
- MD Helicopters (applicability depending on configuration)
- Other rotorcraft platforms using compatible servo control systems
PAG Support:
We provide full-service support for the 41011300-105 Tail Rotor Servo, including:
- OEM part sourcing, new and exchange units
- Certified repair and overhaul (FAA/EASA/TCCA)
- Functional and dynamic bench testing
- Helicopter tail rotor system troubleshooting and diagnostics
- Fast turnaround times and global AOG shipping
- Extensive experience supporting rotary-wing flight control systems
Contact Us for Related Parts & Compatible Components:
- 41011400-103 – Main Rotor (M/R) Servo
- 41011300-101 – Alternate T/R Servo model
- 407-010-413-105 – Pitch Link Assembly for tail rotor control
- 406-010-413-137 – Main Rotor Pitch Link
- 204-076-014-005 – Hydraulic Reservoir Assembly
- 407-340-100-103 – Collective Control Assembly
- Servo Test Equipment (GPM-100) – For MRO diagnostics and validation
