Document ID: chunk:federal_register_of_legislation:F2006B06789:body:0
Version: federal_register_of_legislation:F2006B06789
Segment Type: other
Provision Reference: 
Character Range: 0–671

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.