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The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model H160-B helicopters. This AD was prompted by a report of the main rotor pitch rod rupturing during flight. This AD requires inspecting the upper and lower pitch rod end bearings on the pitch rods of the main rotor and depending on the results, corrective actions. This AD also requires reporting the results of the inspection. The FAA is issuing this AD to address the unsafe condition on these products.
Published
Mar 6, 2026
Effective
Mar 23, 2026
Citation
91 FR 10965
Agencies
2
Full text not available in our database.
View on Federal Register →Get a plain-English explanation of what this regulation does, which agencies are responsible, and how it affects existing rules.
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Docket No. FAA-2026-2288
Project Identifier MCAI-2026-00079-R
Amendment 39-23281
AD 2026-05-08
2120-AA64
14 CFR 39