Document ID: chunk:federal_register_of_legislation:F2006B03616:body:0
Version: federal_register_of_legislation:F2006B03616
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 18 Series Aeroplanes

 AD/BEECH 18/18
 Amdt 1

 Applicability: All models.

      Control Columns and Elevator Control Arm Assembly - Inspection

 12/87

            Requirement: Inspect the Control Columns and Elevator Control Arm Assembly as detailed in Beechcraft SI 0889-155. In addition inspect for cracks on the Control Column Assembly P/N 187510, tubing, outer surface for a distance of 11 cm up the tube above the lower welded tube splice. The same area on the co-pilot's Control Column is also to be inspected. The inspection is to be performed using visual and either magnetic particle, or penetrant procedures; or

            FAA AD 77-19-07.

 Compliance: Within 100 hours after 31 December 1977 and thereafter at 300 hour intervals.

                   Federal Register of Legislative Instruments F2006B03616