Document ID: chunk:federal_register_of_legislation:F2006B11091:body:0
Version: federal_register_of_legislation:F2006B11091
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Gates Learjet 35 and 36 Series Aeroplanes

                         AD/LEARJET 35/13  Upper Cabin Door Lock Mechanism Bolts - Modification

 Applicability: All model 35 with S/Nos. 35-001 to 35-274 and 278;

            All model 36 with S/Nos. 36-001 to 36-044.

4/80

            Requirement: Modify the upper cabin door lock mechanism bolts by installing Gates Learjet Kit No. AMK 79-9.

 Compliance: Within 150 hours time in service after 30 April 1980.

            Background: Modification kit AMK 79-9 provides an additional safety feature to the upper cabin door lock mechanism by installing drilled bolts and lockwiring these bolts in-situ.