Document ID: chunk:federal_register_of_legislation:F2006B09129:body:0
Version: federal_register_of_legislation:F2006B09129
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 DHC-6 (Twin Otter) Series Aeroplanes

 AD/DHC-6/40 Wing Struts - Inspection and Modification 4/76 Applicability:              All models with S/Nos. 1 to 462, 464, 465, 468, 469, 472, 473, 474, 478 and 481. Document:               De Havilland of Canada SB No. 6/342.
 Compliance: 1. Inspect within 120 hours time in service after 31 May 1976.

            2. Modify within 360 hours time in service after 31 May 1976.