Airworthiness Directives (ADs)
88-747-298
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
- 1999/04/01
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Applicability
- 747
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Model Number
- 747
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CAA AD Number
- 88-747-298
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 99-07-03
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Effective Date
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Subject
- To detect and correct fatigue cracks in the edge frame web and doubler of the number 1 main entry door cutout, which could result in rapid decompression of the airplane.
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Reference Publications (Revision/ATA/SB)
- ASB 747-53A2414
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Remarks
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Download
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