Resumen
We are revising Airworthiness Directive (AD) 2011-22-05 for Eurocopter France (Eurocopter) Model AS350B, B1, B2, B3, BA, C, D, D1, AS355E, F, F1, F2, N, and NP helicopters with certain tail rotor (T/R) pitch control rods (control rods) installed. AD 2011-22-05 required checking the control rod for play before the first flight of each day. This new AD requires checking the control rod for play within 30 hours time-in-service (TIS) and, if no bearing play is detected, thereafter at intervals not to exceed 30 hours TIS. The actions in this AD are intended to prevent failure of a T/R control rod, loss of T/R control, and subsequent loss of control of the helicopter.
Detalles de la directiva
Número de AD
FAA-2011-1158
Número de documento
2014-04282
Tipo
Rule
Fecha de publicación
March 13, 2014
Fecha de entrada en vigor
April 17, 2014
Fabricante afectado
Airbus Helicopters (Type Certificate Previously Held By Eurocopter France) (Airbus Helicopters)
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2011-1158
Temas
Documentos oficiales
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