Airworthiness Directives (ADs)
CAA-2006-03-004
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
- 2006/03/13
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Applicability
- 747-200C, -200F, -400, - 400D, and -400F Series
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Model Number
- 747
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CAA AD Number
- CAA-2006-03-004
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-05-09
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Effective Date
- 2006/04/13
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Subject
- To detect and correct fatigue cracks in the overlapping (upper) skin, upper fastener row of the lap joints of the fuselage skin in sections 41, 42, and 46, which could adversely affect the structural integrity of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Alert Service Bulletin 747-53A2499
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Remarks
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Download
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