Perform a one-time inspection of the affected main rotor upper and lower pitch rod end bearings (specific P/Ns listed in the AD) within 5 flight hours after the original effective date, in accordance with the EASB. If any discrepancy is found, contact Airbus Helicopters for approved corrective actions before further flight.

Stay updated on rotorcraft airworthiness directives—check our Rotorcraft Network and AD Summaries archive for future posts on Airbus, Bell, Sikorsky, and other models.

Applicability: All Airbus Helicopters H160-B helicopters, except those manufactured on or after 18 March 2026.

Effective Date: Revision 1 effective 02 April 2026 (original issue 10 February 2026).

Categories: Airworthiness Directives, Airbus Helicopters, Main Rotor System, Inspections