Document ID: chunk:federal_register_of_legislation:F2006B09933:body:0
Version: federal_register_of_legislation:F2006B09933
Segment Type: other
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Character Range: 0–700

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-200/20 Fuselage Rear Bulkhead - Inspection 2/83

 Applicability: All models with S/Nos. up to and including S/N 296. Document:  Fuji Service Bulletin No. FAS 200-003.
            Compliance: Within the next 100 hours time in service and thereafter at intervals not exceeding 100 hours time in service, until modified in accordance with SB FAS 200-003.

            Background: Cracks have been found in the upper corners of the fuselage bulkhead at F.S. 7105, near the horizontal stabiliser main spar attachment.