Airworthiness Directives (ADs)
CAA-2011-07-008
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
- 2011/07/20
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Applicability
- 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 MD80-55A067, dated June 24, 2010.
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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-2011-07-008
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2011-15-01
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Effective Date
- 2011/08/19
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Subject
- To detect and correct such cracking damage, which could result in the structure being unable to support limit load, and could lead to the loss of the vertical stabilizer.
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Reference Publications (Revision/ATA/SB)
- ATA 55. Ref. Service Bulletin MD80-55A067
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Remarks
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Download
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