Document ID: chunk:federal_register_of_legislation:F2006B04153:body:0:p2
Version: federal_register_of_legislation:F2006B04153
Segment Type: other
Provision Reference: 
Character Range: 2807–3612

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

            This Amendment results from a review of airframe ADs for the Beech heavy twin engine models. The SIRM references have been updated, and an additional reference added to cover the model 88 series. The requirement to inspect the fittings has been deleted because it is separately detailed by the current issue of AD/BEECH 65/22.
            The Note relating to bolt torque has been deleted because the relevant manuals have been corrected and the referenced AD cancelled.

 David Alan Villiers
 Delegate of the Civil Aviation Safety Authority 20 September 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 4 October 2000.