AD/DHC-2/20 - Control Column Torque Tubes - Inspection

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Legislation au F2006B09038 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-2 (Beaver) Series Aeroplanes

 

AD/DHC-2/20 Control Column Torque Tubes - Inspection 9/80

Applicability: All models DHC-2 and DHC-2 Mk. III. Document:  De Havilland Aircraft of Canada SB No. 2/28.

Compliance: Initially inspect within 25 hours time in service after 18 September 1980 and thereafter as noted in De Havilland Aircraft of Canada SB No. 2/28.

 

Background:  Three overseas operators have reported cracks in the horizontal torque tube at the base of the control column.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.