Airworthiness Directives (ADs)
CAA-2013-11-016
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
- 2013/11/26
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Applicability
- This AD applies to The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes, as identified in Boeing Alert Service Bulletin 747-53A2682, Revision 1, dated May 24, 2012.
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Model Number
- The Boeing Company Model 747 series airplanes.
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CAA AD Number
- CAA-2013-11-016
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2013-23-15
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Effective Date
- 2013/12/30
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Subject
- FUSELAGE - Section 42 Fuselage Frame Shear Tie End Fasteners - External Skin Crack Inspection
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Reference Publications (Revision/ATA/SB)
- (i) This AD supersedes FAA AD 2009-06-02 (CAA-2009-03-005). (ii) Boeing Alert Service Bulletin 747-53A2682, Revision 1, dated May 24, 2012.
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Remarks
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