AD/GA-7/8 - Rudder Bellcrank - Inspection and Modification

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

Legislation au F2006B10152 In force Legislative Instrument

Legislation content

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-7/8 Rudder Bellcrank - Inspection and Modification NK

Applicability: All models GA-7 with S/Nos. GA7-0002 to GA7-0093, GA7- 0096 to GA7-0099, and any model GA-7 which may have been fitted with rudder bellcrank assembly P/N 7CS10534-3 shipped from Grumman American Savannah, Georgia facility prior to 12 April 1979.

 

Document: Grumman American SB No. ME-19.

 

Compliance: 1. Inspect within 25 hours time in service after 4 July 1979.

 

2. Modify within 100 hours time in service after 4 July 1979.

 

Background: The rudder bellcrank may crack due to loads induced by wind gusts while aeroplane is parked.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.