AD/AC-112/11 - Elevator and Rudder Hinge Fittings - Inspection and/or Replacement
1AD/AC-112/11 - Elevator and Rudder Hinge Fittings - Inspection and/or Replacement
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meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-description: CASA Airworthiness Directive meta-generator: Aspose.Words for .NET 22.10.0 meta-keywords: Issue 3/1980,Aircraft below 5700 kg,Gulfstream (Rockwell) 112 Series Aeroplanes,Elevator and Rudder Hinge Fittings - Inspection and/or Replacement,11 title: Airworthiness Directive - AD/AC-112/11 - Elevator and Rudder Hinge Fittings - Inspection and/or Replacement
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Gulfstream (Rockwell) 112 Series Aeroplanes
AD/AC-112/11 Elevator and Rudder Hinge Fittings - Inspection
and/or Replacement
Applicability: All models 112 with S/Nos. 13003 and 3 to 544.
All models 112TC and 112TCA with S/Nos. 13001 to 13309.
Document: Rockwell International SL No. SL-112-46.
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.