Document ID: chunk:federal_register_of_legislation:F2006B09934:body:0
Version: federal_register_of_legislation:F2006B09934
Segment Type: other
Provision Reference: 
Character Range: 0–980

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-200/21 Teijin Seiki Fuel Strainer
                  P/N Fif-40000 - Inspection and Modification

 4/84

            Applicability: All FA-200-160, 180 and 180 AO aircraft equipped with Teijin Seiki fuel strainer P/N FIF-40000.

 Document: Fuji SB No. 200-005 including Teijin Seiki SB No TS-SB-72.

                  Compliance: Phase I: Within 10 hours time in service after 9 March 1984 and thereafter at intervals not exceeding 100 hours time in service until Phase II as per SB is accomplished.

            Phase II: After obtaining the necessary spare part, but not later than 1 February 1985.

            Background:  There have been instances reported where the stack pipe inside the fuel strainer become lodged upwards into the fuel inlet gallery, thus restricting the fuel flow.