Document ID: chunk:federal_register_of_legislation:F2006B09931:body:0
Version: federal_register_of_legislation:F2006B09931
Segment Type: other
Provision Reference: 
Character Range: 0–988

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-200/19
 Amdt 2

 Rudder Pedal System 11/89

 Applicability: All models FA-200 with S/Nos. 12 to 297. Requirement:  Action in accordance with FHI SB No. 200-002 Rev C.
            Note: JCAB AD TCD-1455A-1-89 refers.

            Compliance: Within 50 hours time in service after 3 December 1984 or prior to the first flight during which aerobatics are to be performed, whichever is earlier. Thereafter at:

              1. each inspection for Maintenance Release issue, or

b.    periods not to exceed 1000 hours time in service if Technical Bulletin 200-22 is embodied.

            Background:  Overtravel of the rudder pedals and incorrect rudder control system operation has been experienced. Amendment 2 introduces a relieving modification to extend the inspection periodicity to 1000 hours.