AD/SC7/14 - Flap Mechanism Support Structure - Inspection and Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06789 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Short SC7 (Skyvan) Series Aeroplanes

 

AD/SC7/14 Flap Mechanism Support Structure - Inspection

and Modification Applicability: All models as referenced in Alert SB No. 27-A64, Rev. 4. Document:               Short Alert SB No. 27-A64, Rev. 4.


9/79

Compliance: Unless already accomplished, within 50 hours time in service after 2 October 1979.

 

Background: In service cracking has developed in some overseas operated Short SC7s in the support structure for the flap mechanism located in the centre section.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.