P/N: 212-010775-7
Category: General Aircraft Parts
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.
The 212-010775-7 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-010775-7 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.