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.