Airworthiness Directives; Eurocopter France (Eurocopter) Model AS332C, AS332L, AS332L1, and AS332L2 Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2011-10-27 · Effective 2011-11-14 · 76 FR 66606
Document
Document number
2011-27673
Federal Register citation
76 FR 66606
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2011-10-27
Effective date
2011-11-14
FAA docket
Docket No. FAA-2011-0939
Abstract
This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter model helicopters. This action requires inspecting the upper end fitting ball joints of the main rotor servocontrols for lateral play, and depending on the findings either repetitively inspecting the ball joint or replacing the servocontrol. This amendment is prompted by reports of noncompliant swaging of the end fitting ball joints on main rotor servocontrols. Investigation has shown that the swaging load applied to the ball joints was 1.3 metric tons instead of the specified 13 metric tons. The actions specified in this AD are intended to prevent failure of the upper end fitting ball joints of the main rotor servocontrols, failure of the upper end fittings, and loss of control of the helicopter.