Document ID: chunk:federal_register_of_legislation:F2006B10150:body:0
Version: federal_register_of_legislation:F2006B10150
Segment Type: other
Provision Reference: 
Character Range: 0–694

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Gulfstream (Grumman American) GA-7 Series Aeroplanes

AD/GA-7/6 Rudder Bellcrank Torque Tube - Inspection NK

       and Modification

            Applicability: All model GA-7 with S/Nos. GA7-0002 to GA-70038, GA7- 0040, GA7-0042 to GA7-0087.

 Document: Gulfstream American SB No. ME-16.

 Compliance: 1. Inspect within 10 hours time in service after 28 February 1979.

            2. Modify as per requirement document.

            Background:  Partial loss of rudder control may occur if free play in the rudder circuit exceeds 1 degree.