Document ID: chunk:federal_register_of_legislation:F2006B06612:body:0
Version: federal_register_of_legislation:F2006B06612
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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/15 Lateral Console Panel 7/92

 Applicability: ATL, all types, to S/No 89 inclusive, except S/No 22, 28, 53, 71 and 82. Requirement:              Action in accordance with ROBIN SA SB No 7.
            Note: DGAC AD 91-018(A) refers.

            Compliance: Unless already accomplished; prior to further flight after 30 June 1992 if contact is evident, if no contact is evident accomplish modification prior to 31 July 1992.

            Background: The DGAC requires an inspection and modification in order to prevent contact between the rudder pedals and the lateral console panel which could lead to the rudder pedals jamming.