Airworthiness Directives; Eurocopter France Model SA330J Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2010-09-02 · Effective 2010-09-17 · 75 FR 53857
Document
Document number
2010-21578
Federal Register citation
75 FR 53857
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Eurocopter France Model SA330J
Publication date
2010-09-02
Effective date
2010-09-17
FAA docket
Docket No. FAA-2010-0825
Abstract
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2010-16-51, which was sent previously to all known U.S. owners and operators of Eurocopter France (Eurocopter) Model SA330J helicopters by individual letters. This AD requires, within 10 hours time-in-service (TIS), inspecting for a gap between the main gearbox (MGB) oil cooling fan assembly (fan) rotor blade and the upper section of the guide vane bearing housing. This inspection must be accomplished by using a feeler gauge attached to a rigid rod. If the feeler gauge cannot be inserted between the blade and the housing, this AD requires replacing the two fan rotor shaft bearings with two airworthy bearings. This AD is prompted by the separation of a fan rotor blade that caused puncture holes in the transmission deck. This condition, if not corrected, could lead to damage to the hydraulic lines and flight controls, and subsequent loss of control of the helicopter.