AD/ROCK-114/10 - Elevator and Rudder Hinge Fittings - Inspection and/or Replacement

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

Legislation au F2006B06643 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) 114 Series Aeroplanes

 

AD/ROCK-114/10  Elevator and Rudder Hinge Fittings - Inspection and/or Replacement

Applicability: All model 114 with S/Nos. 14000 to 14499. Document:  Rockwell International SL No. SL-114-17.


3/80

Compliance: Unless already accomplished, within 100 hours time in service after 31 March 1980.

 

Background: There is a possibility of elongation of holes in the hinge fittings and cracks in the rudder spar developing in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.