Document ID: chunk:federal_register_of_legislation:F2006B11325:body:0
Version: federal_register_of_legislation:F2006B11325
Segment Type: other
Provision Reference: 
Character Range: 0–729

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.