Airworthiness Directives (ADs)
CAA-2010-03-002
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
- 2010/03/09
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Applicability
- The Boeing Company 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.
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Model Number
- Boeing Company 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
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CAA AD Number
- CAA-2010-03-002
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2010-05-03
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Effective Date
- 2010/04/08
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Subject
- To detect and correct fatigue cracking at multiple
adjacent locations in the subject areas, which could connect to form large cracks and result in reduced
structural integrity leading to rapid decompression and consequent loss of control of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Alert Service Bulletin 747-51A2060.
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Remarks
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