P/N: 212-010-403-005
Category: Linkages, Rods & Bellcranks
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| Condition | Price | Stock |
|---|---|---|
| As Removed | $850.00 | 1 Available |
The 212-010-403-005 is a lever assembly for Bell 212 (UH-1N) main rotor control linkage. This component transmits pilot inputs from the cyclic and collective controls to the rotor head, enabling pitch control of main rotor blades. Classified under NSN 1615-00-471-5918 and FSC 1615, the assembly integrates into the rotor drive mechanism where precise actuation is critical for flight control.
Installation and rigging must follow the helicopter's maintenance manual or FAA AC 43.13-1B standards. Proper alignment and secure attachment ensure reliable control response during all flight regimes.
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 212-010-403-005 is a lever assembly for Bell 212 (UH-1N) main rotor control linkage. This component transmits pilot inputs from the cyclic and collective controls to the rotor head, enabling pitch control of main rotor blades.
The 212-010-403-005 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 212-010-403-005 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.