← FAA Federal Register actions

Airworthiness Directives; Bell Helicopter Textron Canada Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4 Helicopters

airworthiness · Rule · Final rule. · Published 2008-07-10 · Effective 2008-08-14 · 73 FR 39577

Document

Document number
E8-14736
Federal Register citation
73 FR 39577
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2008-07-10
Effective date
2008-08-14
FAA docket
Docket No. FAA-2008-0040

Abstract

We are adopting a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4 helicopters. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority to identify and correct an unsafe condition on an aviation product. The aviation authority of Canada, with which we have a bilateral agreement, states in the MCAI: "It has been determined that some helicopters have been fitted with a CRES steel fitting, part number (P/N) 407-030-750-103, and the installation of the tailboom attachment bolt does not meet the design criteria." We are issuing this AD to require actions that are intended to address the unsafe condition that results from an improper installation of the tailboom attachment bolt in the upper left-hand tailboom attachment CRES steel fitting.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown