Summary
This amendment supersedes an existing airworthiness directive (AD) for the specified Agusta S.p.A. (Agusta) model helicopters. This AD results from a revised mandatory continuing airworthiness information (MCAI) issued by an aviation authority to identify and correct an unsafe condition on an aviation product. The aviation authority of Italy, with which we have a bilateral agreement, reports that the previous MCAI should not apply to newly redesigned and improved tail rotor blades. This AD requires the same inspections as the current AD but limits the applicability to only three part-numbered tail rotor blades. This AD requires actions that are intended to prevent fatigue failure of a tail rotor blade (blade), loss of a tail rotor, and subsequent loss of control of the helicopter.
Directive Details
AD Number
FAA-2008-0834
Document Number
E8-27611
Type
Rule
Publication Date
November 25, 2008
Effective Date
December 30, 2008
Affected Manufacturer
Agusta S.p.A. Model A109A and A109A II
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2008-0834
Topics
Official Documents
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