AD/AC-112/8 Amdt 1 - Aileron Hinge Supports - Inspection and Modification

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

Legislation au F2006B02192 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-112/8

Amdt 1


Aileron Hinge Supports - Inspection and Modification


7/78

 

Applicability: Models 112 and 112B with S/Nos. 13000 and 3 to 544; Model 112TC with S/Nos. 13001 to 13108;

Model 112TCA with S/Nos. 13150 to 13260. Document: Rockwell International SB No. SB-112-60A.

Compliance: 1. Unless already accomplished as per SB No. 112-60, initially inspect before further flight as per Part 1 of SB No. 112-60A and perform external visual inspection before each subsequent flight until modified.

 

Note: Pilot in command may perform and certify for visual inspection.

 

2. Unless already accomplished as per SB No. 112-60, modify as per Part 2 of SB No. 112-60A within 100 hours’ time in service after 15 August 1978.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.