Airworthiness Directive

AD 2011-26-10 Amendment 39-16900

Federal Aviation Administration · 14 CFR part 39

FR document
2011-32895
Amendment
39-16900
Published
2012-01-06
Models covered
1
Last live check
Not yet re-verified
AD

2011-26-10

FR doc 2011-32895

AD 2011-26-10Published 2012-01-06Effective 2012-01-23

Requires modifying and testing the lateral and longitudinal cyclic trim actuator assemblies.

Full official abstract

We are adopting a new airworthiness directive (AD) for Enstrom Helicopter Corporation (Enstrom) Model F-28C, F-28C-2, F-28F, 280C, 280F, 280FX TH-28, 480, and 480B helicopters with certain trim relays to require modifying and testing the lateral and longitudinal cyclic trim actuator assemblies. This AD was prompted by four failures in the cyclic trim system on certain Enstrom model helicopters that resulted in reduced controllability of the helicopter. These actions are intended to prevent failure of the cyclic trim system and subsequent loss of control of the helicopter.

Applies to 1 model in our index