Airworthiness Directives; Agusta S.p.A. (Agusta) Model A119 and AW119 MKII Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2010-09-02 · Effective 2010-09-17 · 75 FR 53859
Document
Document number
2010-21593
Federal Register citation
75 FR 53859
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Agusta S.p.A. (Agusta) Model A119 and AW119 MKII
Publication date
2010-09-02
Effective date
2010-09-17
FAA docket
Docket No. FAA-2010-0824
Abstract
This document publishes in the Federal Register an amendment adopting Emergency Airworthiness Directive (AD) 2010-12-51, which was sent previously to all known U.S. owners and operators of the specified Agusta model helicopters by individual letters. This AD requires, before further flight, removing the forward boot from the hub-locking nut (nut) and inserting a gauge between the tail rotor control rod (rod) and nut until the gauge stops. This AD then requires, depending on the depth measurement from the face of the nut, either reidentifying the tail rotor gearbox (TGB) with a new part number (P/N) or replacing the TGB and the associated parts with airworthy parts. This AD is prompted by a report of a missing rod bushing (bushing) from a 90- degree TGB installed on a Model AW119 MKII helicopter. The Agusta Model A119 helicopters also have the affected TGB installed; therefore, they are also included in the applicability of this AD. The actions specified by this AD are intended to detect a missing bushing in the TGB and to prevent abnormal vibration, damage to the tail rotor system, loss of the yaw control function, and subsequent loss of control of the helicopter.