AD/AA-1/16 - Structural and Control Surface Bondlines - Inspection

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Legislation au F2006B02027 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/ American Aviation) AA-1 Series Aeroplanes

 

AD/AA-1/16 Structural and Control Surface Bondlines - Inspection


9/76

 

Applicability: All models AA1 and AA1A with S/Nos. 0001 and subsequent and all model AA1B with S/Nos. 0001 to 0641.

 

Document: 1. Grumman American SB No. 155; or 2. FAA AD 76-17-03.

Compliance: Within 25 hours time in service after 21 September 1976 and there- after at intervals not exceeding 100 hours’ time in service until modified in accordance with SB No.

155.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.