Airworthiness Directives (ADs)
CAA-2008-08-007
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
- 2008/08/19
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Applicability
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747SR, and 747SP series airplanes.
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Model Number
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747SR, and 747SP Series Airplanes
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CAA AD Number
- CAA-2008-08-007
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2008-16-14
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Effective Date
- 2008/09/17
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Subject
- To prevent reduced structural integrity of the fuselage.
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Reference Publications (Revision/ATA/SB)
- 1.This AD supersedes FAA AD 94-15-06(CAA-83-747-224).
2.Boeing Alert Service Bulletin 747-53A2312, dated June 12, 1989; Boeing Service Bulletin 747-53A2312, Revision 1, including ''Addendum,'' dated March 29, 1990; Boeing
Service Bulletin 747-53A2312, including the ''Addendum,'' Revision 2, dated October 8, 1992; or
Boeing Service Bulletin 747-53A2312, Revision 3, dated February 8, 2007.
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Remarks
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