Airworthiness Directives (ADs)
87-747-285A
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
- 2001/06/19
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Applicability
- 747
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Model Number
- 747
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CAA AD Number
- 87-747-285A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2001-11-06
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Effective Date
- 2001/07/16
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Subject
- To detect and correct fatigue cracking of the skin, splice fittings, bulkhead web, and outer chord of the body station (BS) 1480 bulkhead at the overwing longeron splice, which could result in reduced structural integrity of the fuselage and the inability to carry limit load.
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Reference Publications (Revision/ATA/SB)
- ASB747-53A2390, R1.
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Remarks
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Download
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