Document ID: chunk:federal_register_of_legislation:F2006B03623:body:0
Version: federal_register_of_legislation:F2006B03623
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Character Range: 0–1079

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

 Beechcraft 18 Series Aeroplanes

 AD/BEECH 18/4
 Amdt 1

 Horizontal Stabiliser Spar - Inspection NK

 Applicability: Model C-18S, D-18S and AT-11, not modified to Beech SB D-18-48.

             Requirement: 1. Inspect the horizontal stabiliser front spar and sub-spar for cracks at the points of attachment to the fuselage.

2.    Remove the stabiliser and stabiliser lower skin panel and inspect for cracks in the front spar and sub-spar.

3.    If cracking has occurred modify the stabiliser attachment in accordance with Beechcraft Service Bulletin No. D-18-48 or to the satisfaction of the Secretary before further flight.

 Compliance: For Para. 1 - At intervals not exceeding 10 hours time in service.

                    For Para. 2 - At intervals not exceeding 500 hours time in service from the last inspection.

                   Federal Register of Legislative Instruments F2006B03623