Airworthiness Directives (ADs)
CAA-2006-04-001
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
- 2006/04/06
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Applicability
- DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD- 90-30
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Model Number
- MD-82
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CAA AD Number
- CAA-2006-04-001
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-07-11
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Effective Date
- 2006/05/05
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Subject
- To prevent fatigue cracking of the aft attach fitting of the spoiler link and consequent failure of the fitting. Failure of the fitting could result in an asymmetrical lift condition and consequent reduced controllability of the airplane.
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Reference Publications (Revision/ATA/SB)
- Aerotech Manufacturing Service Bulletin DC9-27- 01-AMI5139, Revision "A,'' dated June 19, 2003
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Remarks
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Download
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