Airworthiness Directives (ADs)
87-MD11-061
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
- 1998/12/31
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Applicability
- MD11
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Model Number
- MD11
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CAA AD Number
- 87-MD11-061
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 98-25-15
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Effective Date
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Subject
- To prevent failure of the attachment bolts on the forward and aft flanges of the No. 4 banjo fitting and the pylon carry-through cap due to fatigue cracking, and consequent reduced controllability of the airplane during flight and ground operation.
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Reference Publications (Revision/ATA/SB)
- SB MD11-55-013
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Remarks
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Download
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