Airworthiness Directives (ADs)
CAA-2013-06-008A(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
- 2013/07/01
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Applicability
- Bombardier Inc. model DHC-8-102, -103, -106, -201, -202, -301, -311, -314 and -315aeroplanes, serial numbers 003 through 672.
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Model Number
- Bombardier Inc. models DHC-8 aeroplanes.
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CAA AD Number
- CAA-2013-06-008A(已有後續修訂版)
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Aeronautics Authority of Original AD
- Transport Canada Civil Aviation
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Original AD Number
- CF-2013-17R1
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Effective Date
- 2013/07/05
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Subject
- Fractured Wing-to-Fuselage Strut Attachment Joint Bolt
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Reference Publications (Revision/ATA/SB)
- (i) This AD Superseded TCCA AD CF-2013-17 (CAA-2013-06-008). (ii)Bombardier Service Bulletin (SB) 8-57-47, Revision A, dated 29 May 2013, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada.
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Remarks
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