Airworthiness Directive

AD 2014-20-16 Amendment 39-17989

Federal Aviation Administration · 14 CFR part 39

FR document
2014-23592
Amendment
39-17989
Published
2014-10-07
Models covered
1
Last live check
Not yet re-verified
AD

2014-20-16

FR doc 2014-23592

AD 2014-20-16Published 2014-10-07Effective 2014-11-12

Requires inspecting each main rotor (M/R) blade for a crack or delamination and removing the blade if a crack exists or if the delamination exceeds certain thresholds.

Full official abstract

We are adopting a new airworthiness directive (AD) for Brantly International, Inc. (Brantly) Model B-2, Model B-2A, and Model B-2B helicopters with certain main rotor blades. This AD requires inspecting each main rotor (M/R) blade for a crack or delamination and removing the blade if a crack exists or if the delamination exceeds certain thresholds. This AD was prompted by multiple reports of M/R blade cracks and an incident in which a crack that originated near the M/R blade trailing edge resulted in the loss of a large section of the M/R blade. The actions of this AD are intended to prevent loss of the M/R blade and subsequent loss of control of the helicopter.

Applies to 1 model in our index