P/N: 365a27-3511-06
Category: Controls & Cables
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 PITCH CRANK LEVER may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: New Surplus. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the PITCH CRANK LEVER. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 365a27-3511-06.