Airworthiness Directives (ADs)
89-DC9-080
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
- 2000/02/09
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Applicability
- MD-90
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Model Number
- DC9
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CAA AD Number
- 89-DC9-080
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2000-01-17
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Effective Date
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Subject
- To prevent fatigue cracking of longerons 22 through 26 and the attaching frames, which could result in reduced structural integrity of the fuselage, and consequent loss of pressurization of the airplane.
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Reference Publications (Revision/ATA/SB)
- SB MD90-53-004
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Remarks
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Download
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