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Airworthiness Directives (ADs)

87-DC9-061A

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
1999/04/02
Applicability
DC-9-10,-20,-30,-40,-50,MD-81,-82,-83,-87,-88,C-9
Model Number
DC9
CAA AD Number
87-DC9-061A
Aeronautics Authority of Original AD
FAA
Original AD Number
98-13-35R1
Effective Date
Subject
To prevent fatigue cracks in the skin and longerons of the fuselage, which could result in loss of the structural integrity of the fuselage, and consequently, lead to rapid depressurization of the airplane.
Reference Publications (Revision/ATA/SB)
SB 53-235
Remarks
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