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Airworthiness Directives; Bell Helicopter Textron Canada (Bell) Helicopters

airworthiness · Rule · Final rule. · Published 2014-06-23 · Effective 2014-07-28 · 79 FR 35481

Document

Document number
2014-13263
Federal Register citation
79 FR 35481
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bell Helicopter Textron Canada (Bell)
Publication date
2014-06-23
Effective date
2014-07-28
FAA docket
Docket No. FAA-2013-0574

Abstract

We are superseding Airworthiness Directive (AD) 2003-05-03 for Bell Model 407 helicopters. AD 2003-05-03 required preflight checking and repetitively inspecting for a crack in certain tailbooms that have been redesigned, replacing the tailboom if there is a crack, modifying and re-identifying certain tailbooms, installing an improved horizontal stabilizer assembly, and assigning a 5,000 hour time-in-service (TIS) limit. This new AD retains the requirements of AD 2003-05-03 and requires additional inspection requirements. This AD was prompted by additional reports of cracked tailboom skins. The actions in this AD are intended to prevent separation of the tailboom and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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