Summary
This amendment supersedes an existing emergency airworthiness directive (EAD) for the specified Agusta S.p.A. (Agusta) model helicopters. That EAD currently requires inspecting the main rotor scissor fitting assembly to determine if there are 2 washers installed under the head of each main rotor scissor fitting assembly fixing bolt (fixing bolt). If there are not 2 washers installed under the head of each fixing bolt, that EAD requires replacing each fixing bolt and installing 2 washers under the head of each fixing bolt. This superseding airworthiness directive (AD) is prompted by the determination that a wrong part number (P/N) for the main rotor scissor fitting assembly was listed in the EAD. This AD retains the requirements of the EAD and corrects a P/N for the main rotor scissor fitting assembly. The actions specified by this AD are intended to prevent a crack in a fixing bolt, failure of a fixing bolt, and subsequent loss of control of the helicopter.
Directive Details
AD Number
FAA-2011-0823
Document Number
2011-21476
Type
Rule
Publication Date
August 26, 2011
Effective Date
September 12, 2011
Affected Manufacturer
Agusta S.p.A. Model A109A, A109A II, A109C, and A109K2
Criticality
critical
Emergency
Yes
Docket ID
Docket No. FAA-2011-0823
Topics
Official Documents
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