Airworthiness Directives; Eurocopter France Model EC120 Helicopters
airworthiness · Rule · Final rule. · Published 2005-05-09 · Effective 2005-06-13 · 70 FR 24304
Document
Document number
05-8951
Federal Register citation
70 FR 24304
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Eurocopter France Model EC120
Publication date
2005-05-09
Effective date
2005-06-13
FAA docket
Docket No. FAA-2005-20289
Abstract
This amendment adopts a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC120 helicopters that requires inspecting the tail rotor drive shaft (drive shaft) damper half-clamps (half-clamps) to determine if they are centered on the friction ring, and if not correctly positioned, centering the half-clamps on the friction ring. This amendment is prompted by the discovery of half- clamps that were incorrectly positioned. The actions specified by this AD are intended to detect incorrect positioning of the drive shaft half-clamps, and to prevent interference of the half-clamps with the drive shaft, which could result in scoring on the drive shaft, failure of the drive shaft, and subsequent loss of control of the helicopter.