Airworthiness Directives (ADs)
CAA-2006-05-001(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
- 2006/05/08
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Applicability
- 747-100, 747-100B, 747-100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR series
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Model Number
- B-747-400
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CAA AD Number
- CAA-2006-05-001(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-09-06
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Effective Date
- 2006/06/07
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Subject
- To detect and correct fatigue cracking of certain lower lobe fuselage frames, which could lead to fatigue cracks in the fuselage skin, and consequent rapid decompression of the airplane.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 99-07-12(CCAA AD 88-747-299);Ref. ASB 747-53A2408 or 747-53A2408R1
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Remarks
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Download
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