Airworthiness Directives (ADs)
CAA-2011-08-011
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
- 2011/08/26
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Applicability
- This AD applies to The Boeing Company 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; as identified in Boeing Alert Service Bulletin MD80-57A242, Revision 1, dated January 7, 2011.
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Model Number
- The Boeing Company 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-2011-08-011
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2011-17-11
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Effective Date
- 2011/09/26
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Subject
- To detect and correct such fatigue cracking, which could result in fuel leaks, damage to the wing skin or other structure, and consequent reduced structural integrity of the wing.
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Reference Publications (Revision/ATA/SB)
- ATA 57. Ref. Service Bulletin MD80-57A242
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Remarks
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