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Airworthiness Directives; Airbus Helicopters

airworthiness · Rule · Final rule. · Published 2026-03-03 · Effective 2026-04-07 · 91 FR 10311

Document

Document number
2026-04164
Federal Register citation
91 FR 10311
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2026-03-03
Effective date
2026-04-07
FAA docket
Docket No. FAA-2025-5034

Abstract

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, and AS332L2 helicopters. This AD was prompted by a report of rupture of the scissors link of the rotating swashplate assembly due to a seized ball joint-cups assembly. This AD requires replacing the rotor shaft assembly, modifying the rotating swashplate assembly to replace each of the three ball joint-cups assemblies with one-piece self-lubricated spherical bearings, and modifying the scissors hinges and swashplate trunnions on the main rotor, as applicable, and applying an anti- corrosion agent, if applicable. This AD also prohibits installing a main rotor hub (MRH) assembly or rotor shaft assembly on a helicopter unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
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