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Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230 and 430 Helicopters

airworthiness · Rule · Final rule. · Published 2008-07-10 · Effective 2008-08-14 · 73 FR 39569

Document

Document number
E8-14718
Federal Register citation
73 FR 39569
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2008-07-10
Effective date
2008-08-14
FAA docket
Docket No. FAA-2008-0039

Abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, 230 and 430 helicopters that requires rewiring and testing the fuel valve switch on each engine and testing the ignitor system. This amendment is prompted by an in-flight incident in which a fuel valve switch failed, causing the fuel valve to inadvertently close. The actions specified by this AD are intended to prevent interruption of the fuel supply caused by failure of the fuel switch, which could result in loss of engine power and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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