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Airworthiness Directives; Agusta S.p.A. Model A109C, A109E, and A109K2 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2008-05-09 · Effective 2008-05-27 · 73 FR 26316

Document

Document number
E8-10054
Federal Register citation
73 FR 26316
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2008-05-09
Effective date
2008-05-27
FAA docket
Docket No. FAA-2008-0524

Abstract

This document supersedes Airworthiness Directive (AD) 2001-24- 07 R1 and adopts AD 2007-26-52, which was sent previously to all known U.S. owners and operators of Agusta S.p.A. (Agusta) Model A109C, A109E, and A109K2 helicopters by individual letters. This AD requires inspections for swelling, deformation, bonding separation, or a crack on each main rotor blade (MRB) with a certain tip cap installed, and if any of these conditions are found that exceed the prescribed limits, replacing the MRB before further flight. This amendment is prompted by a report of the in-flight loss of part of a tip cap. The actions specified in this AD are intended to prevent an increase in vibration of the MRB and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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