Airworthiness Directive

AD 2000-16-06 Amendment 39-11860

Federal Aviation Administration · 14 CFR part 39

FR document
00-20404
Amendment
39-11860
Published
2000-08-16
Models covered
1
Last live check
Not yet re-verified
AD

2000-16-06

FR doc 00-20404

AD 2000-16-06Published 2000-08-16Effective 2000-09-20

Requires replacing arm clamp screws (screws) in the yaw, roll, pitch, and collective syncro resolvers, and installing a guard bracket on the yaw, roll, pitch, and collective syncro resolvers.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 430 helicopters. This AD requires replacing arm clamp screws (screws) in the yaw, roll, pitch, and collective syncro resolvers, and installing a guard bracket on the yaw, roll, pitch, and collective syncro resolvers. This AD is prompted by an operator's report that a yaw control channel jammed during freedom-of-control checks following maintenance. The actions specified by this AD are intended to prevent a jammed flight control and subsequent loss of control of the helicopter.

Applies to 1 model in our index