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AD/FA-200/21 - Teijin Seiki Fuel Strainer P/N Fif-40000 - Inspection and Modification
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AD/FA-200/21 - Teijin Seiki Fuel Strainer P/N Fif-40000 - Inspection and Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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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.