AD/L.40/9 Amdt 1 - Wing Structural Life Limitation

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B11050 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.