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Airworthiness Directives; Bell Helicopter Textron, Inc., Model 214ST Helicopters

airworthiness · Rule · Final rule. · Published 1996-04-05 · Effective 1996-05-10 · 61 FR 15184

Document

Document number
96-8384
Federal Register citation
61 FR 15184
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1996-04-05
Effective date
1996-05-10
FAA docket
Docket No. 95-SW-26-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to Bell Helicopter Textron, Inc. (BHTI) Model 214ST helicopters with certain tailboom assemblies and a certain emergency float kit installed, that requires initial and repetitive inspections of the tailboom for cracks until modifications of the tailboom are accomplished. This amendment is prompted by several reports of cracks in the lower aft skin of the tailboom assembly. The actions specified by this AD are intended to prevent cracks in the tailboom assembly, which could result in structural failure of the tailboom and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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