Airworthiness Directive

AD 2002-22-10 Amendment 39-12935

Federal Aviation Administration · 14 CFR part 39

FR document
02-27791
Amendment
39-12935
Published
2002-11-06
Models covered
1
Last live check
Not yet re-verified
AD

2002-22-10

FR doc 02-27791

AD 2002-22-10Published 2002-11-06Effective 2002-11-21

Requires visually inspecting the brackets that attach the horizontal stabilizer slat (slat) to the stabilizer for a crack.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD) for Bell Helicopter Textron Canada Limited (BHTCL) Model 407 helicopters that requires visually inspecting the brackets that attach the horizontal stabilizer slat (slat) to the stabilizer for a crack. If a crack is found, that AD also requires replacing the slat assembly before further flight. Also, that AD requires installing airworthy, segmented slat assemblies by a specified date. Installing segmented slat assemblies was considered terminating action for the requirements of that AD. This amendment requires, initially and at certain time intervals, checking each slat assembly for a cracked bracket and, if a crack is found, replacing any unairworthy slat assembly with an improved, airworthy slat assembly. This amendment also requires replacing, modifying, and installing identification plates on slats on certain helicopters at specified time intervals. This amendment is prompted by two additional reports of cracked brackets. The actions specified by this AD are intended to prevent a slat from separating, contacting a rotor blade, and resulting in subsequent loss of control of the helicopter.

Applies to 1 model in our index