Airworthiness Directives (ADs)
CAA-2004-04-006
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
- 2004/04/01
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Applicability
- Model 747-400F
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Model Number
- 747
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CAA AD Number
- CAA-2004-04-006
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2004-06-12
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Effective Date
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Subject
- To detect and correct fatigue cracks in the fuselage skin and frame shear tie assemblies, which could propagate and result in possible in-flight decompression of the airplane.
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Reference Publications (Revision/ATA/SB)
- Special Attention Service Bulletin 747-53-2480
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Remarks
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Download
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