Airworthiness Directives (ADs)
CAA-2006-05-013
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
- 2006/05/25
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Applicability
- McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40,DC-9-50, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83),and DC-9-87 (MD-87), MD-88, MD-90-30 and Model 717-200 Airplanes
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Model Number
- McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40,DC-9-50, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83),and DC-9-87 (MD-87), MD-88, MD-90-30 and Model 717-200 Airplanes
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CAA AD Number
- CAA-2006-05-013
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-10-14
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Effective Date
- 2006/06/21
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Subject
- To prevent cracks in the cargo door pan, which could result in the inability to fully pressurize an airplane, possible pressure loss, or possible rapid decompression of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Service Bulletin Revision 717–52–0007R1, Boeing Service Bulletin DC9–52–189R2 and Boeing Service Bulletin MD90–52–014R1.
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Remarks
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