Document ID: chunk:federal_register_of_legislation:F2006B11144:body:0
Version: federal_register_of_legislation:F2006B11144
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Gates Learjet 24 & 25 Series Aeroplanes

 AD/LEARJET/27 Horizontal Stabiliser Hinge Pin Bushing
                           Installation - Inspection

 12/81

            Applicability: All Gates Learjet models 24 and 25 with S/Nos. referenced in Gates Learjet Service Bulletin No. 23/24/ 25-311 or with S/Nos. referenced in subsequent issues of that Service Bulletin.

 Document: Gates Learjet SB 23/24/25-311.

 Compliance: Within 100 hours time in service after 31 December 1981.

            Background:  The horizontal stabiliser hinge pin bushings may move out of their mating fittings during normal service.