Airworthiness Directives (ADs)
CAA-2005-07-020
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
- 2005/07/27
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Applicability
- 747-100B SUD, -200B, -300, -400, and -400D Series
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Model Number
- 747
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CAA AD Number
- CAA-2005-07-020
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2005-15-08
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Effective Date
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Subject
- To detect and correct fatigue cracking in certain fuselage stringers, which, if left undetected, could result in fuselage skin cracking that reduces the structural integrity of the skin panel, and consequent rapid depressurization of the airplane.
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Reference Publications (Revision/ATA/SB)
- 747-53A2484
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Remarks
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Download
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