Document ID: chunk:federal_register_of_legislation:F2006B11050:body:0
Version: federal_register_of_legislation:F2006B11050
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Meta Sokol L.40 Series Aeroplanes

 AD/L.40/9
 Amdt 1

 Wing Structural Life Limitation 2/73

 Applicability: All models with wing main spar lower caps exceeding 4000 hours time in service.

            Requirement: Retire from service the centre section and outer wing main spar lower caps, including the centre section to outer wing attachment fittings.

 Compliance: 31 March 1975.