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Airworthiness Directives; Robinson Helicopter Company (Robinson) Model R22, R22 Alpha, R22 Beta, and R22 Mariner Helicopters, and Model R44, and R44 II Helicopters

airworthiness · Rule · Final rule. · Published 2010-11-24 · Effective 2010-12-29 · 75 FR 71532

Document

Document number
2010-29203
Federal Register citation
75 FR 71532
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2010-11-24
Effective date
2010-12-29
FAA docket
Docket No. FAA-2010-0711

Abstract

This amendment adopts a new airworthiness directive (AD) for Robinson Model R22, R22 Alpha, R22 Beta, and R22 Mariner helicopters, and Model R44 and R44 II helicopters. This AD requires visually inspecting each tail rotor (T/R) control pedal bearing block support (support) for a crack, measuring the thickness of each support, installing support safety tabs on certain supports, and replacing supports of a certain thickness during the next 2,200 hour overhaul. This amendment is prompted by two reports of Model R22 helicopters experiencing broken supports during flight, which resulted in the T/R control pedals becoming jammed. The actions specified by this AD are intended to prevent the supports from breaking, which can bind the T/R control pedals, resulting in a reduction of yaw control and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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