Airworthiness Directives; Agusta S.p.A. Model AB412 Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 1999-12-20 · Effective 2000-01-04 · 64 FR 71012
Document
Document number
99-32735
Federal Register citation
64 FR 71012
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Agusta S.p.A. Model AB412
Publication date
1999-12-20
Effective date
2000-01-04
FAA docket
Docket No. 99-SW-63-AD
Abstract
This amendment adopts a new airworthiness directive (AD) applicable to Agusta S.p.A. Model AB412 helicopters. This action requires removing and replacing certain main rotor yokes with airworthy main rotor yokes before further flight. This amendment is prompted by the fatigue failure of a main rotor yoke (yoke). Fatigue analysis indicates that certain yokes are on the low end of the manufacturer's tolerance for thickness and do not have the desired margin of safety. This condition, if not corrected, could result in fatigue failure of the yoke, loss of a main rotor blade, and subsequent loss of control of the helicopter.