P/N: 365a31-1998-02
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 | 4 Available |
The 365a31-1998-02 is a blade pitch lever for helicopter rotor control systems. This component transmits pilot control inputs through the pitch-change linkage to adjust rotor blade angles during flight. Used in Airbus Helicopters collective and cyclic pitch mechanisms, the lever converts control movements into precise blade angle changes for altitude, speed, and directional control.
Installation requires proper rigging per the aircraft maintenance manual and verification against the helicopter's Illustrated Parts Catalog to ensure correct linkage geometry and control response.
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 365a31-1998-02 is a blade pitch lever for helicopter rotor control systems. This component transmits pilot control inputs through the pitch-change linkage to adjust rotor blade angles during flight.
The 365a31-1998-02 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 365a31-1998-02 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.