AD/LEARJET/22 - Aft Engine Beam Pylon Bolts - Inspection

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

Legislation au F2006B11139 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/22 Aft Engine Beam Pylon Bolts - Inspection 5/80

Applicability: All model 23 S/Nos. 23-003 to 23-099;

 

All model 24 S/Nos. 24-100 to 24-357;

 

All model 25 S/Nos. 25-003 to 25-286 and 25-288.

 

Document: Gates Learjet SB 23/24/25-299. Compliance: As per requirement document.

Background: To ensure that the aft engine beam pylon bolts are secure and properly torqued.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.