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Airworthiness Directives (ADs)

90-S76-040

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
2001/02/05
Applicability
S-76A, S-76B, and S-76C helicopters
Model Number
S76
CAA AD Number
90-S76-040
Aeronautics Authority of Original AD
FAA
Original AD Number
2001-01-04
Effective Date
Subject
To detect corrosion of the threaded joint in the rod assembly and prevent a collapse of the landing gear and subsequent loss of control of the helicopter during landing.
Reference Publications (Revision/ATA/SB)
SB 76A-32-03R1
Remarks
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