AD/AA-1/1A - Control Cables and Pulleys - Inspection
1AD/AA-1/1A - Control Cables and Pulleys - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/AA-1/1A - Control Cables and Pulleys - Inspection.
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 NK,Aircraft below 5700 kg,Gulfstream (Grumman American/ American Aviation) AA-1 Series Aeroplanes,Control Cables and Pulleys - Inspection,1A title: Airworthiness Directive - AD/AA-1/1A - Control Cables and Pulleys - Inspection
?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 (Grumman American/ American Aviation) AA-1 Series Aeroplanes
AD/AA-1/1A Control Cables and Pulleys - Inspection NK
Applicability: All models.
Requirement: Thoroughly clean and inspect all rudder, aileron and elevator control pulleys and cables where the cables pass under the pulley grouping forward of the wing centre spar.
Note: To adequately inspect the cable it will be necessary to actuate the controls to the full deflection to expose the complete cable pulley contact area for examination.
Compliance: Within 100 hours’ time in service after 25 February 1972 and thereafter at intervals not exceeding 100 hours’ time in service.