Summary
We are adopting a new airworthiness directive (AD) for the specified ECF model helicopters. This AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the aviation authority of the European Aviation Safety Agency (EASA). The MCAI AD reports the separation and loss of a stainless steel ring (75 millimeter (mm) in diameter) from a tail rotor blade (blade) sleeve resulting in severe, high-frequency vibrations, which can lead to damage to the fenestron blades, loss of yaw control, and subsequent loss of control of the helicopter.
Directive Details
AD Number
FAA-2010-0426
Document Number
2010-23098
Type
Rule
Publication Date
September 22, 2010
Effective Date
October 27, 2010
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2010-0426
Topics
Official Documents
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