Document ID: chunk:federal_register_of_legislation:F2006B05349:body:0
Version: federal_register_of_legislation:F2006B05349
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Partenavia P68 Series Aeroplanes

 AD/P68/21 Horizontal Stabilator to Fuselage Frame
                       Attachment - Check Torque

 4/83

            Applicability: All Partenavia P68, P68B, P68C, P68C-TC and P68 Observer aircraft with S/Nos. 1 to 289 except S/Nos. 234, 256, 259, 269 and 288.

            Requirement: Check torque AN4-6A bolts securing the horizontal stabilator torque tube brackets to fuselage frame. If necessary retorque to correct torque value 78-83 LB inches.

            Note: RAI AD 83-3 and Partenavia SB No. 57 refer.

 Compliance: Before further flight.