Airworthiness Directive

AD 99-16-09 Amendment 39-11244

Federal Aviation Administration · 14 CFR part 39

FR document
99-20057
Amendment
39-11244
Published
1999-08-09
Models covered
1
Last live check
Not yet re-verified
AD

99-16-09

FR doc 99-20057

AD 99-16-09Published 1999-08-09Effective 1999-08-24

Requires verifying the torque on the vertical fin attachment bolts (bolts); inspecting the vertical fin and tailboom fittings for cracks, elongation of bolt holes, distortion and corrosion; and re-verifying the torque on the…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Bell Helicopter Textron Canada (BHTC) Model 230 helicopters. This action requires verifying the torque on the vertical fin attachment bolts (bolts); inspecting the vertical fin and tailboom fittings for cracks, elongation of bolt holes, distortion and corrosion; and re-verifying the torque on the bolts after inspecting the fittings. This amendment is prompted by a report of a loose vertical fin, which was discovered during a post-flight inspection. The actions specified in this AD are intended to prevent loss of torque of the bolts, which could lead to fracture of the bolts, separation of the vertical fin from the helicopter, and loss of control of the helicopter.

Applies to 1 model in our index