Document ID: chunk:federal_register_of_legislation:F2006B03704:body:0
Version: federal_register_of_legislation:F2006B03704
Segment Type: other
Provision Reference: 
Character Range: 0–817

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

 Beechcraft 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/5 Generator Leads 1/76

 Applicability: Model 200 S/Nos BB-2, BB-6 thru BB-76 and BB-78 thru BB-80.

             Requirement: 1. Visually inspect the generator output leads for chafing or discolouration in the area of the air conditioner compressor pulley housing and oil line coupling nut.

             2. Modify the generator lead routing in accordance with Beechcraft SI No 0768-358, Kit No 101-3011-1S.

            Note: FAA AD 75-25-01 refers.

            Compliance: Inspect within 25 hours time in service after 8 December 1975. Modify within 100 hours time in service after 8 December 1975.