AD/DHC-6/21 Amdt 1 - Elevator Connecting Rod - Inspection

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

Legislation au F2006B09108 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-6/21

Amdt 1

Applicability: All models.


Elevator Connecting Rod - Inspection 2/72

 

Requirement:  Inspect all elevator connecting rods (irrespective of Batch No.) by means of the method detailed in De Havilland Aircraft of Canada SB No. 6/238 except those previously subjected to a detailed inspection.

 

Compliance: Within 25 hours time in service after 14 February 1972.

 

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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.