AD/ROCK-114/10 - Elevator and Rudder Hinge Fittings - Inspection and/or Replacement
1AD/ROCK-114/10 - Elevator and Rudder Hinge Fittings - Inspection and/or Replacement
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/ROCK-114/10 - Elevator and Rudder Hinge Fittings - Inspection and/or Replacement.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
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) 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.