Airworthiness Directive

AD 96-18-05 Amendment 39-9729

Federal Aviation Administration · 14 CFR part 39

FR document
96-22141
Amendment
39-9729
Published
1996-08-30
Models covered
1
Last live check
Not yet re-verified
AD

96-18-05

FR doc 96-22141

AD 96-18-05Published 1996-08-30Effective 1996-09-16

Requires a visual inspection of the tailboom skin in the areas around the nutplates and in the areas of the tailboom drive shaft cover retention clips for cracks and corrosion using a 10-power or higher magnifying glass.

Full official abstract

This amendment supersedes an existing priority letter airworthiness directive (AD), applicable to Bell Helicopter Textron, A Division of Textron Canada Ltd. (BHTC) Model 206L, 206L-1, and 206L-3 helicopters, that currently requires a visual inspection of the tailboom skin in the areas around the nutplates and in the areas of the tailboom drive shaft cover retention clips for cracks and corrosion using a 10-power or higher magnifying glass. This amendment requires the same actions as the existing AD, but corrects a part number that was incorrectly stated in that AD. This amendment is prompted by a recent accident and several reports of fatigue cracks in the tailboom skin in the areas around the nutplates for the tail rotor fairing and in the areas of the tail rotor drive shaft cover retention clips. The actions specified by this AD are intended to prevent failure of the tailboom and subsequent loss of control of the helicopter.

Applies to 1 model in our index