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
All series 235E aircraft.
Retire the wing main spar and the centre section splice plates from service.
This fatigue life limitation will be reviewed upon receipt of future substantiation data from the manufacturer.
Upon or prior to achieving 2800 hours component time in service.
Based on information provided by the manufacturer, a safe fatigue life has been determined for the wing structure.