Airworthiness Directives (ADs)
88-DC9-073A
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.
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Issue Date
- 1999/06/17
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Applicability
- DC-9 and C-9
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Model Number
- DC9
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CAA AD Number
- 88-DC9-073A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 99-08-05R1
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Effective Date
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Subject
- To prevent fatigue cracking of the fuselage frames and longerons 16R and 17R, which could result in reduced structural integrity of the airplane.
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Reference Publications (Revision/ATA/SB)
- SB DC9-53-267
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Remarks
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Download
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