Airworthiness Directives (ADs)
87-DC9-068
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
- 1998/11/26
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Applicability
- DC-9-31
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Model Number
- DC9
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CAA AD Number
- 87-DC9-068
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 98-23-11
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Effective Date
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Subject
- To detect and correct fatigue cracking in the fuselage skin or doubler at the corners of the forward service door doorjamb, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane.
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Reference Publications (Revision/ATA/SB)
- SB DC9-53-288
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Remarks
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Download
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