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Airworthiness Directives; Costruzioni Aeronautiche Giovanni Agusta S.p.A. Model A109A, A109AII, and A109C Helicopters

airworthiness · Rule · Final rule. · Published 1995-07-05 · Effective 1995-08-09 · 60 FR 34844

Document

Document number
95-15516
Federal Register citation
60 FR 34844
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1995-07-05
Effective date
1995-08-09
FAA docket
Docket No. 94-SW-12-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Costruzioni Aeronautiche Giovanni Agusta S.p.A. (Agusta) Model A109A, A109AII, and A109C helicopters, that requires a modification of the tail boom vertical fin to create inspection openings that permit initial and repetitive visual inspections for cracks in the vertical fin rear spar attachment area. This amendment is prompted by four reports of cracks in the tail boom vertical fin rear spar attachment area. The actions specified by this AD are intended to prevent failure of the vertical fin attachment caused by cracks in the tail boom vertical fin rear spar attachment area, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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