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

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

Legislation au F2006B11144 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.