Airworthiness Directives (ADs)
CAA-2008-07-004
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
- 2008/07/11
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Applicability
- McDonnell Douglas Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes, certificated in any category.
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Model Number
- McDonnell Douglas Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes
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CAA AD Number
- CAA-2008-07-004
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2008-13-29
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Effective Date
- 2008/08/12
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Subject
- To detect and correct such cracking, which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Alert Service Bulletin MD80-53A301, Revision 1
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Remarks
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Download
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