Airworthiness Directives (ADs)
CAA-2024-10-008
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
- 2024/10/18
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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, 747SP, and 747SR series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 747-53A2912 RB, dated April 5, 2024.
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Model Number
- Boeing 747-100, 747-100B, 747-100B SUD,
747-200B, 747-200C, 747-200F, 747-300,
747-400, 747-400D, 747-400F, 747SP, and
747SR series airplanes.
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CAA AD Number
- CAA-2024-10-008
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2024-19-01
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Effective Date
- 2024/11/15
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Subject
- This AD requires repetitive inspections of the upper fastener row of the fuselage skin lap splice in a certain area for any crack, and applicable on-condition actions.
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Reference Publications (Revision/ATA/SB)
- ATA 34. Ref. Boeing Alert Requirements Bulletin 747-53A2912 RB, dated April 5, 2024.
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Remarks
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