P/N: 212-010775-7
Category: Fittings & Adapters
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 212-010775-7 is a tail rotor crosshead that converts control-tube motion into pitch changes at the blade grips. Installed within the tail rotor hub and pitch control assembly, this component transmits pedal inputs from the flight controls to the pitch links, enabling anti-torque rotor blade angle adjustment. Steel construction provides durability in the high-stress rotary environment.
Proper fitment requires verification with the aircraft's Illustrated Parts Catalog and installation per the applicable maintenance manual.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 212-010775-7 is a tail rotor crosshead that converts control-tube motion into pitch changes at the blade grips. Installed within the tail rotor hub and pitch control assembly, this component transmits pedal inputs from the flight controls to the pitch links, enabling anti-torque rotor blade angle adjustment.
Aircraft hardware is manufactured to military and aviation specifications. The TAIL ROTOR CROSS HEAD conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.
Aviation hardware is available in various materials including cadmium-plated steel, stainless steel, aluminum alloy, and titanium depending on the application. Contact us for material certification and specifications for the 212-010775-7.
Yes, we sell hardware in various quantities from single units to bulk lots. The TAIL ROTOR CROSS HEAD is available in: As Removed. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.