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Airworthiness Directives; Bell Helicopter Textron Canada (Bell) Helicopters

airworthiness · Rule · Final rule. · Published 2015-08-20 · Effective 2015-09-24 · 80 FR 50550

Document

Document number
2015-20509
Federal Register citation
80 FR 50550
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bell Helicopter Textron Canada (Bell)
Publication date
2015-08-20
Effective date
2015-09-24
FAA docket
Docket No. FAA-2014-0643

Abstract

We are superseding Airworthiness Directive (AD) 2001-13-51 for Bell Model 206L-4, 407, and 427 helicopters. AD 2001-13-51 required inspecting certain driveshafts for a crack, a loose bolt or nut, or red powder residue and replacing a driveshaft if there is a crack, a loose bolt or nut, or red powder residue. AD 2001-13-51 also required notifying the FAA within 10 days if a crack is found in the driveshaft. This new AD retains the inspection requirement of AD 2001-13-51, expands the applicability to include the Model 429 helicopter, and removes the reporting requirement. This AD is intended to prevent failure of a driveshaft, loss of drive to the main rotor system, and a subsequent emergency landing.

Source

Authoritative
Federal Register document
Machine
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