AD/LEARJET 35/18 - Horizontal Stabiliser Hinge Pin Bushing Installation - Inspection

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

Legislation au F2006B11096 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

 


Gates Learjet 35 and 36 Series Aeroplanes

 

AD/LEARJET 35/18 Horizontal Stabiliser Hinge Pin Bushing

Installation - Inspection


12/81

 

Applicability: All models 35 & 36 with S/Nos. referenced in Gates Learjet Service Bulletin No.

35/36-27-13 or with S/Nos. referenced in subsequent issues of that Service Bulletin.

 

Document: Gates Learjet SB 35/36-27-13.

 

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.