Document ID: chunk:federal_register_of_legislation:F2006B04080:body:0
Version: federal_register_of_legislation:F2006B04080
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 60 (Duke) Series Aeroplanes

AD/BEECH 60/19 Moisture Barrier Fuselage Station 306.421 11/72

 Applicability: All models.

 Requirement: To prevent possible interference with elevator movement, accomplish the following:

            Starting at the cutout for the elevator bell crank, slit the moisture barrier vertically upward using a knife, razor blade or similar tool. Extend this cut through the "velcro" strip which attaches the moisture barrier to the front spar of the horizontal stabiliser.

            Note: In making the slit do not damage the spar.

 Compliance: Within 25 hours' time in service after 3 November 1972 unless already accomplished.