Airworthiness Directives; Eurocopter France Model SA341G, SA342J, and SA-360C Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2001-11-23 · Effective 2001-12-10 · 66 FR 58663
Document
Document number
01-29189
Federal Register citation
66 FR 58663
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2001-11-23
Effective date
2001-12-10
FAA docket
Docket No. 2001-SW-48-AD
Abstract
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2001-19-51, which was sent previously to all known U.S. owners and operators of Eurocopter France (ECF) Model SA341G, SA342J, and SA-360C helicopters by individual letters. This AD requires, before further flight, replacing a certain unairworthy main rotor head torsion tie bar (tie bar) with an airworthy tie bar. This AD also requires revising the limitations section of the maintenance manual by adding a life limit for certain tie bars. This AD is prompted by an accident involving an ECF Model SA341G helicopter due to the failure of a tie bar. The actions specified by this AD are intended to prevent failure of a tie bar, loss of a main rotor blade, and subsequent loss of control of the helicopter.