Document ID: chunk:federal_register_of_legislation:F2006B09936:body:0
Version: federal_register_of_legislation:F2006B09936
Segment Type: other
Provision Reference: 
Character Range: 0–909

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

 Fuji FA-200 Series Aeroplanes

 AD/FA-200/23
 Amdt 1

 Control Column 1/90

            Applicability: All models which have not been modified in accordance with Fuji Technical Bulletin 200-020, dated 30 May 1989.

            Requirement: Using an approved dye penetrant method, inspect the control column tube for cracking in the lock pin hole area.

            Compliance: Prior to further flight after 5 January 1987 and thereafter at each scheduled inspection for Maintenance Release issue.

            Background: The Authority has received a report of control column failure in flight. The tube fractured at the lock pin hole.

            Amendment 1 introduces a modification which constitutes terminating action for the inspection requirements.