Airworthiness Directives; Brantly International, Inc. Helicopters
airworthiness · Rule · Final rule. · Published 2014-10-07 · Effective 2014-11-12 · 79 FR 60339
Document
Document number
2014-23592
Federal Register citation
79 FR 60339
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2014-10-07
Effective date
2014-11-12
FAA docket
Docket No. FAA-2012-1093
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.