Document ID: chunk:federal_register_of_legislation:F2006B10115:body:0
Version: federal_register_of_legislation:F2006B10115
Segment Type: other
Provision Reference: 
Character Range: 0–975

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

 Grumman G21 (Goose) Series Aeroplanes

                        AD/G21/1 Below Floor Control System Components - Inspection

10/77

 Applicability: All models.

 Requirement: 1. Remove and disassemble:

                (i)       Elevator Torque Tube Assembly P/N 12755,

(ii)    Rudder Torque Tube Assembly P/N 12756,

(iii)  Rudder Pedal Torque Tube Assembly LH and RH P/N 12757 and 12758,

                (iv)   Hinge Support Assembly P/N 12725.

             2. Inspect all parts for corrosion and/or cracks using visual and dye penetrant or magnetic particle techniques.

            Note: FAA AD 73-12-6 Amendment 39-1657 refers.

            Compliance: Initially before issue of Certificate of Airworthiness and there- after at intervals not exceeding 2000 hours time in service or two years whichever occurs first.