Airworthiness Directives (ADs)
86-747-261
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
- 1997/01/31
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Applicability
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Model Number
- 747
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CAA AD Number
- 86-747-261
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 96-26-04
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Effective Date
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Subject
- To detect and correct fatigue cracking of body station (BS) 300 and BS 320fuselage frames adjacent to the nose wheel well (NWW), which could result in collapse of the NWW pressure bulkhead, and subsequent rapid decompression of airplane.
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Reference Publications (Revision/ATA/SB)
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Remarks
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Download
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