Airworthiness Directives (ADs)
CAA-2004-08-008A(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
- 2009/03/06
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Applicability
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes.
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Model Number
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes
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CAA AD Number
- CAA-2004-08-008A(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2009-04-06
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Effective Date
- 2009/04/02
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Subject
- To detect and correct the propagation
of fatigue cracks in the vicinity of oil cans on the web of the aft pressure bulkhead, which could result
in rapid decompression of the airplane and overpressurization of the tail section, and consequent loss
of control of the airplane.
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Reference Publications (Revision/ATA/SB)
- This AD supersedes AD 2004-16-09(CAA-2004-08-008),Ref:Boeing Alert Service Bulletin 747-53A2482 or Boeing Alert Service Bulletin 747-53A2482 R1.
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Remarks
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