AD/GA-7/6 - Rudder Bellcrank Torque Tube - Inspection and Modification

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

Legislation au F2006B10150 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 American) GA-7 Series Aeroplanes

 

AD/GA-7/6 Rudder Bellcrank Torque Tube - Inspection NK

and Modification

 

Applicability: All model GA-7 with S/Nos. GA7-0002 to GA-70038, GA7- 0040, GA7-0042 to GA7-0087.

 

Document: Gulfstream American SB No. ME-16.

 

Compliance: 1. Inspect within 10 hours time in service after 28 February 1979.

 

2. Modify as per requirement document.

 

Background:  Partial loss of rudder control may occur if free play in the rudder circuit exceeds 1 degree.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.