AD/CERES/7 Amdt 1 - Turnover Truss - Modification
1AD/CERES/7 Amdt 1 - Turnover Truss - Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.