AD/AC-112/12 - Rudder Rib - Inspection

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

Legislation au F2006B02182 Not 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 (Rockwell) 112 Series Aeroplanes

 

AD/AC-112/12 Rudder Rib - Inspection 3/82

Applicability: Models 112 and 112B S/Nos. 3 to 544 and 13000.

 

Models 112TC and 112TCA S/Nos. 13001 to 13309. Document: Gulfstream American Service Bulletin No. SB-112-68.

Compliance: Unless already accomplished within the last 100 hours’ time in service, inspect IAW Part I before further flight and thereafter at intervals not exceeding 100 hours time in service until Part II is accomplished.

 

Background:  In service reports of cracks in rudder tip rib at balance weight attachment hole 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.