AD/L.40/9 Amdt 1 - Wing Structural Life Limitation
1AD/L.40/9 Amdt 1 - Wing Structural Life Limitation
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.