Airworthiness Directive

AD 2000-04-15 Amendment 39-11598

Federal Aviation Administration · 14 CFR part 39

FR document
00-4371
Amendment
39-11598
Published
2000-02-28
Models covered
2
Last live check
Not yet re-verified
AD

2000-04-15

FR doc 00-4371

AD 2000-04-15Published 2000-02-28Effective 2000-03-14

Requires inspecting the swashplate assembly drive pin (drive pin) for damage or looseness, torque testing to determine if the interference fit between the drive pin and rotating ring (ring) is adequate, and replacing any…

Full official abstract

This amendment adopts a new airworthiness directive (AD) applicable to Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, and 230 helicopters. This action requires inspecting the swashplate assembly drive pin (drive pin) for damage or looseness, torque testing to determine if the interference fit between the drive pin and rotating ring (ring) is adequate, and replacing any unairworthy drive pin. This amendment is prompted by an accident investigation that revealed fatigue failure of a drive pin. The actions specified in this AD are intended to prevent fatigue failure of a drive pin and subsequent loss of control of the helicopter.

Applies to 2 models in our index