AD/DHC-6/13 - Flap Control Push Rod Assembly - Modification

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

Legislation au F2006B09100 Not 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-6/13 Flap Control Push Rod Assembly - Modification 8/68

Applicability: All models with S/Nos. 1 to 105 not modified in Mod. Bulletin No. 6/1085. Document:               De Havilland Canada Mod. Bulletin No. 6/1085.

Compliance: Before 1 January 1969.

 

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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.