Airworthiness Directives; Eurocopter France Model AS-365N2, AS 365 N3, EC 155B, EC155B1, SA-365N, N1, and SA-366G1 Helicopters
airworthiness · Rule · Final rule. · Published 2006-07-26 · Effective 2006-08-30 · 71 FR 42254
Document
Document number
06-6472
Federal Register citation
71 FR 42254
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2006-07-26
Effective date
2006-08-30
FAA docket
Docket No. FAA-2004-18850
Abstract
This amendment revises an existing airworthiness directive (AD) for Eurocopter France (Eurocopter) Model AS-365N2, AS 365 N3, EC 155B, EC155B1, SA-365N, N1, and SA-366G1 helicopters that currently requires inspecting the main gearbox (MGB) base plate for a crack and replacing the MGB if a crack is found. This amendment increases the time intervals for inspecting the MGB base plate and includes minor editorial changes throughout the AD. This amendment is prompted by crack growth tests that indicate that the inspection intervals can be increased without affecting safety. The actions specified by this AD are intended to detect a crack in an MGB base plate and prevent failure of one of the MGB attachment points to the frame, which could result in severe vibration and subsequent loss of control of the helicopter.