AD/DHC-6/40 - Wing Struts - Inspection and Modification

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

Legislation au F2006B09129 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

 


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.

 

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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.