COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Fokker F27 Series Aeroplanes AD/F27/114 Amdt 1 Applicability: All models. Main Landing Gear Torque Links 11/87 Requirement: Action in accordance with Dowty Rotol SB 32-161B R2. Compliance: Prior to 1 January 1989. Background: The manufacturer reports a number of torque links have been incorrectly machined during manufacture. Amendment 1 of this Directive references Revision 2 of the Requirement Document which extends the batch numbers identified as being incorrectly machined.