Airworthiness Directives (ADs)
CAA-2006-11-014
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
- 2006/11/29
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Applicability
- This AD applies to Boeing 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, certificated in any category; as identified in Boeing Alert Service Bulletin 747-53A2675, dated October 12, 2006.
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Model Number
- 747
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CAA AD Number
- CAA-2006-11-014
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-24-05
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Effective Date
- 2006/12/12
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Subject
- To detect and correct fatigue cracks at the fastener rows of the fuselage skin in section 41, which could join together and cause a loss of structural integrity and rapid decompression of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Alert Service Bulletin 747-53A2675
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Remarks
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