Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Aerospatiale Rallye Series Aeroplanes
AD/MSR/26 Wing Structural Fatigue Life Limitation 3/80
Applicability: All series 235E aircraft.
Requirement: Retire the wing main spar and the centre section splice plates from service.
Note: This fatigue life limitation will be reviewed upon receipt of future substantiation data from the manufacturer.
Compliance: Upon or prior to achieving 2800 hours component time in service.
Background: Based on information provided by the manufacturer, a safe fatigue life has been determined for the wing structure.
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