Airworthiness Directives, Eurocopter France Model AS332C, L, and L1 Helicopters
airworthiness · Rule · Final rule. · Published 1999-01-28 · Effective 1999-03-04 · 64 FR 4288
Document
Document number
99-1236
Federal Register citation
64 FR 4288
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-01-28
Effective date
1999-03-04
FAA docket
Docket No. 97-SW-41-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to Eurocopter France (Eurocopter) Model AS332C, L, and L1 helicopters, that requires the replacement of certain main rotor hub spindles (spindles) and flapping hinge pins (pins). This amendment is prompted by testing of aged frequency adapters, which shows that premature failure of the spindles and pins can occur due to increased loading from increased stiffness of the aged frequency adapters. The actions specified by this AD are intended to prevent the loss of a main rotor blade and subsequent loss of control of the helicopter.