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Airworthiness Directives (ADs)

89-DC9-081

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.

Issue Date
2000/02/14
Applicability
DC-9, MD-90-30, 717-200, and MD-88
Model Number
DC9
CAA AD Number
89-DC9-081
Aeronautics Authority of Original AD
FAA
Original AD Number
2000-03-51Emergency
Effective Date
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
Reference Publications (Revision/ATA/SB)
ASB DC9-27A362, MD90-27A034, 717-27A0002
Remarks
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