Airworthiness Directive

AD 2012-10-01 Amendment 39-17050

Federal Aviation Administration · 14 CFR part 39

FR document
2012-12399
Amendment
39-17050
Published
2012-05-25
Models covered
1
Last live check
Not yet re-verified
AD

2012-10-01

FR doc 2012-12399

AD 2012-10-01Published 2012-05-25Effective 2012-06-29

Requires replacing certain tailboom attachment hardware and at certain intervals thereafter, determining the torque of that tailboom attachment hardware.

Full official abstract

We are adopting a new airworthiness directive (AD) for Bell Helicopter Textron Canada Limited (BHTC) Model 427 helicopters which requires replacing certain tailboom attachment hardware and at certain intervals thereafter, determining the torque of that tailboom attachment hardware. This AD was prompted by a review of the tailboom attachment installation, which revealed that the torque value of the bolts specified in the BHTC Model 427 Maintenance Manual and applied during manufacturing was incorrect and exceeded the torque range recommended for the bolts. The actions are intended to prevent an over- torque of the tailboom attachment bolt (bolt), bolt failure, loss of the tailboom, and subsequent loss of control of the helicopter.

Applies to 1 model in our index