Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France)
airworthiness · Rule · Final rule. · Published 2016-05-02 · Effective 2016-06-06 · 81 FR 26103
Document
Document number
2016-09235
Federal Register citation
81 FR 26103
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2016-05-02
Effective date
2016-06-06
FAA docket
Docket No. FAA-2015-3970
Abstract
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.