We are superseding airworthiness directive (AD) 2014-12-51 for Airbus Helicopters (previously Eurocopter France) Model EC130B4 and EC130T2 helicopters. AD 2014-12-51 required repetitively inspecting the tailboom to Fenestron junction frame (junction frame) for a crack. This new AD retains the requirements of AD 2014-12-51, changes the applicability from helicopters with certain hours time-in-service (TIS) to junction frames with certain hours TIS, and adds a compliance time for sling cycles to the junction frame inspection interval. The actions of this AD are intended to detect a crack and to prevent failure of the junction frame, which could result in loss of the Fenestron and subsequent loss of control of the helicopter.
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Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France)
We are superseding airworthiness directive (AD) 2014-12-51 for Airbus Helicopters (previously Eurocopter France) Model EC130B4 and EC130T2 helicopters. AD 2014-12-51 required re...
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81 FR 26103
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“Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France),” thefederalregister.org (May 2, 2016), https://thefederalregister.org/documents/2016-09235/airworthiness-directives-airbus-helicopters-previously-eurocopter-france.