Airworthiness Directives (ADs)
CAA-2005-06-014
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
- 2005/06/27
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Applicability
- 747-400F
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Model Number
- 747
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CAA AD Number
- CAA-2005-06-014
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2005-13-05
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Effective Date
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Subject
- To prevent fatigue cracks in the upper chord, upper chord strap, and web of the upper deck floor beams and the resultant failure of the floor beams. Failure of a floor beam could result in damage to critical flight control cables and wire bundles that pass through the floor beam, and consequent loss of controllability of the airplane.
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Reference Publications (Revision/ATA/SB)
- ASB 747-53A2443
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Remarks
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Download
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