Airworthiness Directives (ADs)
89-747-337A(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
- 2001/11/01
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Applicability
- All Model 747 series
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Model Number
- 747
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CAA AD Number
- 89-747-337A(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2001-22-04
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Effective Date
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Subject
- To detect and correct fatigue cracking of certain areas of the fuselage skin, which could result in reduced structural integrity of the fuselage, and consequent rapid depressurization of the airplane.
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Reference Publications (Revision/ATA/SB)
- SB 747-53A2444R1, R2, AD 2000-14-04
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Remarks
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Download
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