Airworthiness Directives (ADs)
CAA-2006-06-010A
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
- 2007/08/16
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Applicability
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-300, 747-400, 747-400D, and 747SR series airplanes.
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Model Number
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-300, 747-400, 747-400D, and 747SR Series Airplanes.
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CAA AD Number
- CAA-2006-06-010A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2007-16-08
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Effective Date
- 2007/09/13
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Subject
- To detect and correct fatigue cracks
that could extend and fully sever the frame, which could result in development of skin cracks that
could lead to rapid depressurization of the airplane.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 2006-12-12(CAA-2006-06-010).Ref. Boeing Alert Service Bulletin 747-53A2451 or Boeing Alert Service Bulletin 747-53A2451, Revision 1.
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Remarks
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