Airworthiness Directives; Eurocopter France Model SA-365N1, AS-365N2, and SA-366G1 Helicopters
airworthiness · Rule · Final rule. · Published 2000-05-17 · 65 FR 31256
Document
Document number
00-12354
Federal Register citation
65 FR 31256
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2000-05-17
FAA docket
Docket No. 99-SW-34-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to Eurocopter France Model SA-365N1, AS-365N2, and SA-366G1 helicopters and requires conducting inspections of each tail rotor blade for bonding separation, measuring the clearance between the tip of each tail rotor blade and the circumference of the air duct, and replacing the blade if necessary. This amendment is prompted by an inflight incident in which the tail rotor blades were significantly damaged due to bonding separation. The actions specified by this AD are intended to prevent damage to a tail rotor blade, loss of tail rotor control, and subsequent loss of control of the helicopter.