Airworthiness Directive

AD 2015-12-02 Amendment 39-18175

Federal Aviation Administration · 14 CFR part 39

FR document
2015-13852
Amendment
39-18175
Published
2015-06-09
Models covered
1
Last live check
Not yet re-verified
AD

2015-12-02

FR doc 2015-13852

AD 2015-12-02Published 2015-06-09Effective 2015-07-14

Requires installing a placard and revising the limitations section of the rotorcraft flight manual (RFM).

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bell Helicopter Textron Canada Limited (Bell) Model 206L-1, 206L-3, and 206L-4 helicopters. This AD requires installing a placard and revising the limitations section of the rotorcraft flight manual (RFM). This AD was prompted by several incidents of third stage engine turbine wheel failures caused by excessive vibrations at certain engine speeds during steady-state operations. The actions of this AD are intended to prevent turbine failure, engine power loss, and subsequent loss of control of the helicopter.

Applies to 1 model in our index