Airworthiness Directives; Agusta S.p.A. Model A109E Helicopters
airworthiness · Rule · Final rule. · Published 2005-05-09 · Effective 2005-06-13 · 70 FR 24305
Document
Document number
05-8952
Federal Register citation
70 FR 24305
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Agusta S.p.A. Model A109E
Publication date
2005-05-09
Effective date
2005-06-13
FAA docket
Docket No. FAA-2005-20292
Abstract
This amendment adopts a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109E helicopters that requires visually inspecting each main transmission support fitting (fitting) attachment bolt (bolt) for a fracture, a crack, or looseness, and verifying the torque on each fitting bolt. This amendment is prompted by two incidents of fatigue failure of the bolts that secure the transmission rear support fittings to the helicopter. The actions specified by this AD are intended to detect a fracture, a crack, or looseness of a fitting bolt, and prevent fatigue failure of a fitting bolt and subsequent loss of control of the helicopter.