Airworthiness Directives (ADs)
CAA-2016-08-007
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
- 2016/08/17
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Applicability
- This AD applies to 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, certificated in any category, as identified in Boeing Alert Service Bulletin 747-53A2862, Revision 1, dated July 24, 2015.
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Model Number
- Boeing 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-2016-08-007
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2016-16-10
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Effective Date
- 2016/09/14
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Subject
- To detect and correct fatigue cracking and missing fasteners of the station 320 crown frame, cracking of the window post number 3, and cracking of the window upper sill, which could result in an in-flight decompression and a loss of structural integrity of the fuselage.
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Reference Publications (Revision/ATA/SB)
- ATA 53. Reference: Boeing Alert Service Bulletin 747-53A2862, Revision 1, dated July 24, 2015.
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Remarks
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