P/N: 365a27-3511-06
Category: Linkages, Rods & Bellcranks
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
The 365a27-3511-06 is a pitch crank lever for helicopter flight-control linkages. This component pivots within control mixing or quadrant assemblies to translate pilot inputs through the bellcrank mechanism. The lever transfers motion between control rods and cables, enabling pitch authority to the rotor system.
Airbus Helicopters catalogs this part as a critical airframe component for rotorcraft pitch control. Installation and rigging must follow the approved Aircraft Maintenance Manual for your specific helicopter model. Verify compatibility in the Illustrated Parts Catalog before ordering.
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 365a27-3511-06 is a pitch crank lever for helicopter flight-control linkages. This component pivots within control mixing or quadrant assemblies to translate pilot inputs through the bellcrank mechanism.
The 365a27-3511-06 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 365a27-3511-06 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.