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Airworthiness Directives; Bell Helicopter Textron, a Division of Textron Canada, Model 206B and 206L Helicopters

airworthiness · Rule · Final rule. · Published 1995-11-22 · Effective 1995-12-27 · 60 FR 57823

Document

Document number
95-28517
Federal Register citation
60 FR 57823
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1995-11-22
Effective date
1995-12-27
FAA docket
Docket No. 93-SW-04-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to Bell Helicopter Textron, a Division of Textron Canada (BHT), Model 206B and 206L helicopters, that currently requires a revision to the Limitations section of the FAA-approved Supplemental Type Certificate (STC) Rotorcraft Flight Manual Supplement (RFMS) until replacement of the engine power-out warning sensor on BHT Model 206B and 206L helicopters equipped with Allison 250-C20R engines in accordance with certain supplemental type certificates. This amendment requires a revision to the Limitations section of the STC RFMS, but removes the requirement for replacement of the engine power-out warning sensor. This amendment is prompted by a reevaluation of the need for an engine power-out warning sensor based on the lack of reported operational occurrences of the false engine-out warnings. The actions specified by this AD are intended to maintain a heightened pilot awareness that false engine-out warnings may occur when practicing autorotations and could result in an unnecessary emergency autorotative landing.

Source

Authoritative
Federal Register document
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