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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.

Source

Authoritative
Federal Register document
Machine
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