AD/CERES/7 Amdt 1 - Turnover Truss - Modification

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

Legislation au F2006B04896 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

 


C.A.C. CA-28 (Ceres) Series Aeroplanes

 

AD/CERES/7

Amdt 1


Turnover Truss - Modification 9/99

 

Applicability: C.A.C. “Ceres” Aeroplanes S/Nos. 5(VH-CDO), 6(VH-CEG) and 13(VH-SSF). Document:               Ceres SB No. 45.

Compliance: Not later than 21 January 1980.

 

This Amendment becomes effective on 9 September 1999.

 

Note: Modifications performed in accordance with AD/CA-28/7 satisfy the requirements of this Directive.

 

Background:  In a recent accident involving overturn on landing the overturn truss collapsed with fatal consequences for the pilot.

 

The original issue of this Airworthiness Directive became effective on 31 January 1980.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.