Airworthiness Directive

AD 2008-14-03 Amendment 39-15598

Federal Aviation Administration · 14 CFR part 39

FR document
E8-14736
Amendment
39-15598
Published
2008-07-10
Models covered
2
Last live check
Not yet re-verified
AD

2008-14-03

FR doc E8-14736

AD 2008-14-03Published 2008-07-10Effective 2008-08-14

Requires 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.

Full official 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.

Applies to 2 models in our index