Airworthiness Directives (ADs)
86-MD82-055A
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
- 1997/09/08
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Applicability
- MD80 series
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Model Number
- DC9
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CAA AD Number
- 86-MD82-055A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 96-23-07 R1
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Effective Date
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Subject
- To prevent fatigue cracking in the vertical leg of the rear spar lower cap of the wing, which could lead to reduced structural integrity of the wing.
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Reference Publications (Revision/ATA/SB)
- SB 57-184
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Remarks
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Download
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