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AD FAA-2026-2288

Airworthiness Directives; Airbus Helicopters

Resumen

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.

Detalles de la directiva

Número de AD

FAA-2026-2288

Número de documento

2026-04451

Tipo

Rule

Fecha de publicación

March 6, 2026

Fecha de entrada en vigor

March 23, 2026

Cierre de comentarios

April 20, 2026

Fabricante afectado

Airbus

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2026-2288

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de Airbus →

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AD FAA-2026-2288 — Airworthiness Directives; Airbus Helicopters