Airworthiness Directives (ADs)
CAA-2006-06-010(已有後續修訂版)
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
- 2006/06/20
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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-2006-06-010(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-12-12
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Effective Date
- 2006/07/17
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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 2001-14-22(CCAA AD 90-747-364)
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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Download
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