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Airworthiness Directives (ADs)

88-DC9-073

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
1999/04/21
Applicability
DC-9 and C-9
Model Number
DC9
CAA AD Number
88-DC9-073
Aeronautics Authority of Original AD
FAA
Original AD Number
99-08-05
Effective Date
Subject
To prevent fatigue cracking of the fuselage frames and longerons 16R and 17R, which could result in reduced structural integrity of the airplane.
Reference Publications (Revision/ATA/SB)
SB DC9-53-267
Remarks
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