airworthiness · Rule · Final rule. · Published 2025-07-10 · Effective 2025-08-14 · 90 FR 30581
Document
Document number
2025-12873
Federal Register citation
90 FR 30581
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2025-07-10
Effective date
2025-08-14
FAA docket
Docket No. FAA-2025-0617
Abstract
The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS-365N2, AS 365 N3, EC 155B, EC155B1, SA- 365N, and SA-365N1 helicopters. This AD was prompted by reports of loss of tightening torque between the upper ball bearing end and the main rotor (MR) servo-control. This AD requires inspecting the tightening torque and, depending on the results, taking corrective action. This AD also requires reporting information. The FAA is issuing this AD to address the unsafe condition on these products.