70351?38801?102 Main Rotor Pitch Control Link Assembly – Sikorsky H?60/S?70 Cyclic?Collective Flight?Control Rod

Description

The 70351?38801?102 Main Rotor Pitch Control Link Assembly is a precision?engineered flight?control rod used on Sikorsky H?60 and S?70 series helicopters. This linkage transmits swashplate?driven cyclic and collective inputs to the main rotor pitch horns, enabling accurate blade pitch adjustments essential for lift generation, maneuvering, and overall rotor stability. Manufactured from high?strength alloys with corrosion?resistant rod ends and spherical bearings, it is designed to withstand continuous cyclic loading, vibration, and tensile forces encountered during demanding helicopter operations. Adjustable end fittings ensure proper alignment, preload, and smooth control response throughout the aircraft’s flight envelope.

Key Specs:

Manufacturer: Sikorsky Aircraft (CAGE 78286)
Function: Transfers swashplate motion to main rotor pitch horns
Category: Main rotor flight?control linkage
Applications: Sikorsky H?60 / S?70 helicopter platforms
Dimensions: Approx. 35" x 3" x 3" (typical main rotor pitch link size)
Weight: ~5.0 lbs
Compliance: Manufactured to military and aerospace?grade rotor?control standards
This pitch control link supports precise pitch authority, stable rotor performance, and long?term reliability across military and commercial Sikorsky helicopter fleets.

Features

• Designed for accurate transfer of cyclic and collective control inputs.
• Reinforced alloy construction optimized for high rotor?system loads.
• Precision spherical bearings provide smooth, low?friction articulation.
• Engineered to resist vibration, tensile stress, and high?cycle fatigue.
• Corrosion?resistant hardware enhances long?term durability.
• Adjustable end fittings support precise pitch?control geometry.
• Improves rotor responsiveness, lift stability, and maneuvering performance.

Frequently Asked Questions