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Airworthiness Directives (ADs)

87-DC9-069

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
1998/12/22
Applicability
MD80s
Model Number
DC9
CAA AD Number
87-DC9-069
Aeronautics Authority of Original AD
FAA
Original AD Number
98-24-33
Effective Date
Subject
To prevent fatigue cracking of longerons 22 through 26 and the attaching frames, which could result in reduced structural integrity of fuselage, and consequent loss of pressurization of the airplane.
Reference Publications (Revision/ATA/SB)
SB 53-265
Remarks
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