Summary
We are superseding airworthiness directive (AD) 2012-02-13 for certain Airbus Helicopters, Inc. (Airbus Helicopters) Model EC130B4 helicopters. AD 2012-02-13 required inspecting certain areas of the tailboom/Fenestron junction frame (junction frame) for a crack. This AD retains the requirements of AD 2012-02-13, expands the inspection area of the junction frame, and reduces the repetitive inspection interval. These actions are intended to detect a crack in the junction frame, which could result in detachment of the Fenestron and subsequent loss of control of the helicopter.
Directive Details
AD Number
FAA-2014-0757
Document Number
2014-23594
Type
Rule
Publication Date
October 7, 2014
Effective Date
October 22, 2014
Affected Manufacturer
Airbus Helicopters, Inc. (Previously Eurocopter France)
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2014-0757
Topics
Official Documents
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