Airworthiness Directives (ADs)
CAA-2006-04-012(已有後續修訂版)
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
- 2006/04/17
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Applicability
- Model DC-8-11, DC-8- 12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43; DC -8F-54, DC-8F-55; DC-8-50, -60, - 60F, -70, -70F; DC-9-10, -20, -30, -40, -50; DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87) and MD-88.
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Model Number
- MD-82
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CAA AD Number
- CAA-2006-04-012(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2006-07-25
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Effective Date
- 2006/05/16
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Subject
- To prevent failure of the rudder pedal bracket assembly, which could result in the loss of rudder and braking control at either the captain's or first officer's position.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 89-14-02; Ref. McDonnell Douglas DC–8 Alert Service Bulletin A27–273R1, DC–9 Alert Service Bulletin A27–307R1, DC–9 Alert Service Bulletin A27–307R4, DC–9 Alert Service Bulletin A27–307R5 and DC–9 Alert Service Bulletin A27–307R6.
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Remarks
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Download
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