Document ID: chunk:federal_register_of_legislation:F2006B03702:body:0
Version: federal_register_of_legislation:F2006B03702
Segment Type: other
Provision Reference: 
Character Range: 0–1061

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 200/48 Ailerons 1/90

 Applicability:  Model B200 with S/N BB-1246 through BB-1271, and BB-1273 through BB-1285.
            Model A200 CT with S/N BP-59 through BP-63. Model B200 C with S/N BP-64 through BP-66 and BV-1 through BV-8. Any aircraft which may have installed a replacement aileron for any reason subsequent to 1 January 1985.

 Requirement:   Action in accordance with Beechcraft Mandatory SB No 2256.

            Note: FAA AD 89-22-14 refers.

            Compliance: Prior to exceeding 100 hours time in service after 25 January 1990 or at the next scheduled inspection for issue of a Maintenance Release after 25 January 1990, whichever occurs later.

            Background: Country of origin AD. Foam may retain water and create an aileron out of balance condition. The out of balance limit could result in control surface flutter.