Airworthiness Directives (ADs)
CAA-2005-05-008
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
- 2005/05/24
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Applicability
- 777-200 and 777-300
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Model Number
- 777
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CAA AD Number
- CAA-2005-05-008
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2005-10-17
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Effective Date
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Subject
- To prevent fatigue cracks in the lower t-chord at the bolt holes common to the paddle fittings that could result in fractures of one or more of the t-chord segments, which could lead to detachment of the lower wing panel and consequent loss of the wing.
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Reference Publications (Revision/ATA/SB)
- SB 777-57A0040, Revision 2
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Remarks
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Download
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