Document ID: chunk:federal_register_of_legislation:F2006B03933:body:0
Version: federal_register_of_legislation:F2006B03933
Segment Type: other
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Character Range: 0–809

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

 Beechcraft 400 Series Aeroplanes

AD/BEECH 400/6 Escape Hatch Substructure Rivets 4/94

            Applicability: Model 400A aircraft with serial numbers RK-1 through RK-57, RK-59, RK-60, and RK-62 through RK-66.

            Model 400T aircraft with serial numbers TT-02 through TT-30, and TT-32.

 Requirement: Action in accordance with Beechcraft Mandatory Service Bulletin 2509.

            Note: FAA AD 93-25-15 Amdt 39-8779 refers.

 Compliance: Within 200 hours' time in service after 31 March 1994.

            Background: The FAA received reports that, during production, incorrect rivets may have been installed in the escape hatch substructure.