Airworthiness Directive

AD 2012-14-07 Amendment 39-17121

Federal Aviation Administration · 14 CFR part 39

FR document
2012-17561
Amendment
39-17121
Published
2012-07-19
Models covered
2
Last live check
Not yet re-verified
AD

2012-14-07

FR doc 2012-17561

AD 2012-14-07Published 2012-07-19Effective 2012-08-03

Requires inspecting certain hydraulic servo actuators (servo) to determine whether the shaft turns independently of the nut or the clevis assembly, and additional actions based upon the inspection's outcome.

Full official abstract

We are adopting an airworthiness directive (AD) superseding an existing airworthiness directive for Bell Helicopter Textron Canada (Bell) Model 407 and 427 helicopters. The existing AD requires inspecting certain hydraulic servo actuators (servo) to determine whether the shaft turns independently of the nut or the clevis assembly, and additional actions based upon the inspection's outcome. The AD also requires reidentifying the servo. Since we issued that AD, Bell has learned that additional servos may need repair or removal. This AD expands the scope of the current AD to include inspections for all servos, and requires that servos meeting inspection requirements be marked with the letter "V" after the part number on the data plate. The actions are intended to detect any loose or misaligned parts in the servo that could lead to failure of the servo and subsequent loss of helicopter control.

Applies to 2 models in our index