70106-08006-044 Tail Rotor Control Rod – OEM Anti?Torque Flight Control Linkage for Sikorsky H?60/S?70

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70106-08006-044 Tail Rotor Control Rod is a Sikorsky OEM linkage that transfers pilot inputs to the tail rotor pitch system. Designed for H?60/S?70 helicopters, it supports precise yaw authority, anti?torque stability, and reliable directional control.

70106-08006-044

Spare Parts

Description

The 70106-08006-044 Tail Rotor Control Rod is a precision?built flight?control linkage used on Sikorsky H?60 and S?70 series helicopters. This component transmits mechanical inputs from the tail rotor servo to the pitch change mechanism, enabling accurate adjustment of tail rotor blade pitch for yaw control and anti?torque stabilization. Constructed from high?strength alloys with corrosion?resistant rod ends and spherical bearings, it is engineered to withstand continuous cyclic loading, vibration, and tensile forces encountered during demanding helicopter operations. The assembly incorporates adjustable end fittings to ensure proper alignment, preload, and smooth control response throughout the aircraft’s flight envelope.

Key Specs:

Manufacturer: Sikorsky Aircraft (CAGE 78286)
Function: Transfers servo motion to tail rotor pitch change mechanism
Category: Tail rotor flight?control linkage
Applications: Sikorsky H?60 / S?70 helicopter platforms
Dimensions: Approx. 20" x 3" x 3" (typical tail rotor control rod size)
Weight: ~3.0 lbs
Compliance: Manufactured to military and aerospace?grade rotor?control standards
This tail rotor control rod ensures precise yaw authority, stable anti?torque performance, and long?term reliability across military and commercial Sikorsky helicopter fleets.

Features

  • Transfers servo motion to the tail rotor pitch system.
  • High?strength alloy tube for reliable load capacity.
  • Spherical bearings provide smooth, low?friction movement.
  • Designed to withstand high?frequency vibration.
  • Corrosion?resistant components for long?term durability.
  • Adjustable ends allow precise alignment and preload.
  • Supports consistent yaw authority and anti?torque stability.

Frequently Asked Questions

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