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Thu, Apr 16, 2015

AD: Agusta S.p.A. Helicopters

AD NUMBER: 2015-05-52

PRODUCT: Agusta S.p.A. (Agusta) Model A109, A109A, A109A II, A109C, A109K2, A109E, A119, A109S, AW119 MKII, and AW109SP helicopters, which was sent previously to all known U.S. owners and operators of these helicopters.

ACTION: Final Rule; request for comments

SUMMARY: This AD requires inspecting certain tail rotor (T/R) pitch control links (pitch links) for freedom of movement, corrosion, excessive friction of the spherical bearings, and cracks.

This AD is prompted by a report of an in-flight failure of a pitch link on an Agusta Model AW119 MKII helicopter. These actions are intended to prevent loss of T/R pitch control and subsequent loss of control of the helicopter.

DATES: This AD becomes effective April 29, 2015 to all persons except those persons to whom it was made immediately effective by Emergency AD (EAD) 2015-05-52, issued on March 4, 2015, which contains the requirements of this AD. Comments on this AD must be received by June 15, 2015.

FMI: AD

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