Airworthiness Directives (ADs)
89-DC9-081B
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
- 2000/08/30
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Applicability
- DC-9, MD-90-30, 717-200, and MD-88
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Model Number
- DC9
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CAA AD Number
- 89-DC9-081B
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2000-15-15
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Effective Date
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Subject
- To prevent loss of pitch trim capability due to excessive wear of the jackscrew assembly of the horizontal stabilizer, which could result in loss of vertical control of the airplane.
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Reference Publications (Revision/ATA/SB)
- ASB DC9-27A362, DC9-27A362R02, MD90-27A034, MD90-27A034R02, 717-27A0002, or 717-27A002R02
Ref. 本案於2004/11/25同意遠東所提AMOC(函號:標準四字第09400336820號)如紙本附件.
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Remarks
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