AD/G1159/30 - Fuselage, Rudder Actuator Structural Attachment Points - Inspection

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

Legislation au F2006B10033 Not 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

 


Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes

 

AD/G1159/30 Fuselage, Rudder Actuator Structural

Attachment Points - Inspection


12/81

 

Applicability: All model G1159 (Gulfstream II) aeroplanes which have achieved 3000 hours (or more) time in service since manufacture.

 

Document: Gulfstream American C.B. No. 303.

 

Compliance: Unless already accomplished, inspect within 50 hours time in service after 10 November, 1981.

 

Background:  Operator reports involving the following discrepancies, elongated bolt holes, cracks and loose fasteners in the rudder actuator attachment area, have been received by the manufacturer.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.