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Airworthiness Directives (ADs)

2002-10-016

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date
2002/10/22
Applicability
Model S-76A, S-76B and S-76C helicopters, except those having a serial number of 760501, or 760506 through 760515
Model Number
S76
CAA AD Number
2002-10-016
Aeronautics Authority of Original AD
FAA
Original AD Number
2002-21-07
Effective Date
Subject
To detect installation of an incorrect main rotor spindle attachment bolt (bolt), which could result in reduced hub or bolt fatigue life, separation of the main rotor blade at the spindle attachment, and subsequent loss of control of the helicopter.
Reference Publications (Revision/ATA/SB)
ASB No. 76-65-52 (321)
Remarks
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