Airworthiness Directives; Eurocopter France Model SA330F, G, and J Helicopters
airworthiness · Rule · Final rule. · Published 2000-11-14 · Effective 2000-12-19 · 65 FR 68071
Document
Document number
00-28722
Federal Register citation
65 FR 68071
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2000-11-14
Effective date
2000-12-19
FAA docket
Docket No. 2000-SW-14-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD) that applies to Eurocopter France Model SA330F, G, and J helicopters and requires inspecting the tail rotor blade (blade) skin for cracks and replacing, as necessary, the blade. This amendment requires skin bonding and eddy current inspections of the blade skin for cracks and would reference a more recent service bulletin (SB). This amendment is prompted by improved inspection methods and by the manufacturer revising the SB referenced in the current AD. The actions specified by this AD are intended to prevent fatigue cracking of a blade, failure of a blade, and subsequent loss of control of the helicopter.