AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection

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

Legislation au F2006B02128 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

 


Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

 

AD/AC/69 Main Landing Gear Torque Link Pin Retaining Bolt - Inspection


9/78

 

Applicability: All models 500A, 500B, 500U, 500S, 560F, 680F(P), 680FL, 680FL(P), 680T, 680V

and 680W with S/Nos. 871 to 1876, and Model 500S with S/Nos. 3050 and subsequent; All model 681 with S/Nos. 6001 to 6072;

All model 685 with S/Nos. 1200 to 12066;

 

All models 690, 690A and 690B with S/Nos. 11001 and subsequent.

 

Document: Rockwell International SL No. 319.

 

Compliance: Within 25 hours’ time in service after 22 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.