Airworthiness Directive

AD 2000-06-10 Amendment 39-11651

Federal Aviation Administration · 14 CFR part 39

FR document
00-7552
Amendment
39-11651
Published
2000-03-30
Models covered
1
Last live check
Not yet re-verified
AD

2000-06-10

FR doc 00-7552

AD 2000-06-10Published 2000-03-30Effective 2000-04-14

Requires preflight checking and repetitively inspecting the tail boom for a crack and replacing the tail boom if a crack is found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) applicable to Bell Helicopter Textron Canada (BHTC) Model 407 helicopters. This action requires preflight checking and repetitively inspecting the tail boom for a crack and replacing the tail boom if a crack is found. This amendment is prompted by four reports of cracks on the tail boom in the area of the horizontal stabilizer. The actions specified in this AD are intended to prevent separation of the tail boom and subsequent loss of control of the helicopter.

Applies to 1 model in our index