Document ID: chunk:federal_register_of_legislation:F2006B06621:body:0
Version: federal_register_of_legislation:F2006B06621
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Robin Aviation Series Aeroplanes

AD/ROBIN/23 Anti-Tab Control 7/95

 Applicability: All Model R 2000 and HR 200 aircraft, serial numbers 250 through 271. Requirement:               Action in accordance with Avions Pierre Robin Mandatory Service Bulletin 137.
            Note: DGAC AD 94-183(A)R1 refers.

 Compliance: Unless already accomplished, within 100 hours time in service after 22 June 1995.

            Background: The DGAC requires installation of a friction lock device on the sliding stop tube in order to improve the operating condition of the anti-tab control.