AD/DHC-6/48 - Introduction of Beta Range Test Switch

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

Legislation au F2006B09136 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-6/48 Introduction of Beta Range Test Switch 2/80

Applicability: DHC-6 Aircraft S/No. 1 thru 450.

 

Document: 1. De Havilland Aircraft of Canada Ltd., SB No. 6/309, Rev. C; or

 

2. Transport Canada Airworthiness Directive CF-79-24 De Havilland Canada. Compliance:              Within next 500 hours time in service after 31 March 1980.

Background: Investigations of two accidents overseas where inadvertent reverse thrust was suspected, drew attention to the need to ensure that serviceability of the beta back-up system could always be checked before flight. Incorporation of the beta range test switch ensures that such a check can be accomplished.

 

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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.