Airworthiness Directives (ADs)
CAA-2006-02-006
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
- 2006/02/10
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Applicability
- Model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F Airplanes
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Model Number
- MD11
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CAA AD Number
- CAA-2006-02-006
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-03-13
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Effective Date
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Subject
- To prevent corrosion and subsequent cracking of studbolts, which could result in failure of the flap hinge fittings and their possible separation from the wing rear spar, and consequent reduced controllability of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Service Bulletin DC10–57–154 & Boeing Service Bulletin MD11–57–076.
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Remarks
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