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Airworthiness Directives; Robinson Helicopter Company Model R22 Helicopters

airworthiness · Rule · Final rule. · Published 2003-02-19 · Effective 2003-03-26 · 68 FR 7911

Document

Document number
03-3772
Federal Register citation
68 FR 7911
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Robinson Helicopter Company Model R22
Publication date
2003-02-19
Effective date
2003-03-26
FAA docket
Docket No. 2001-SW-44-AD

Abstract

This amendment adopts a new airworthiness directive (AD) for Robinson Helicopter Company (RHC) Model R22 helicopters that requires inspecting the tail rotor pitch control assembly for roughness or binding of the pitch control bearings (bearings) by hand-rotating the pitch control bearing housing (housing). If the housing does not rotate freely, the AD requires replacing the unairworthy pitch control assembly with an airworthy unit. This amendment is prompted by reports of failure of the tail rotor pitch control assembly due to improperly lubricated bearings on the RHC Model R22 helicopters. The actions specified by this AD are intended to detect corrosion of the bearings and to prevent bearing failure and subsequent loss of directional control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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