Document ID: chunk:federal_register_of_legislation:F2006B03619:body:0
Version: federal_register_of_legislation:F2006B03619
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Character Range: 0–1114

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

 Beechcraft 18 Series Aeroplanes

AD/BEECH 18/20 Lower Rudder Torque Tube - Inspection 6/78

 Applicability: All models D18C, D18S, E18S, E18S-9700, G18S, H-18, C-45G TC-45G, C-45H,
            TC-45J (SNB-5), JRB-6, 3N, 3M and 3NM modified in accordance with STC SA 1243WE, S1016WE or SA360WE.

            Requirement: Visually inspect the lower rudder torque tube P/N 452606-7 for cracks in the area of the access hole.

            Note 1: Cracked tubes in which the length of cracks does not exceed 0.50 inch (12.5 mm) may be repaired to a scheme approved by the Secretary. If cracks exceed 0.50 inch the tube shall be replaced before further flight.

            Note 2: FAA AD 78-10-1 AMDT. 39-3210 refers.

            Compliance: Within 100 hours time in service after 30 June 1978 and thereafter at intervals not exceeding 100 hours time in service.

                   Federal Register of Legislative Instruments F2006B03619