Summary
We are superseding airworthiness directive (AD) 2013-08-17 for Airbus Helicopters Model SA-365N, SA-365N1, AS-365N2, AS 365 N3, and SA-366G1 helicopters. AD 2013-08-17 required initial and recurring inspections of the 9-degree fuselage frame for a crack and repairing the frame if a crack exists. This new AD modifies the compliance times and expands the inspection area of the 9-inch frame. The actions of this AD are intended to detect a crack in the 9-degree frame to prevent loss of structural integrity and subsequent loss of control of the helicopter.
Directive Details
AD Number
FAA-2015-3741
Document Number
2016-10286
Type
Rule
Publication Date
May 6, 2016
Effective Date
June 10, 2016
Affected Manufacturer
Airbus Helicopters (Type Certificate Previously Held by Eurocopter France)
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2015-3741
Topics
Official Documents
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