Document ID: chunk:federal_register_of_legislation:F2009L04657:body:0:p2
Version: federal_register_of_legislation:F2009L04657
Segment Type: other
Provision Reference: 
Character Range: 2895–4030

and thereafter at intervals not to exceed 150 hours TIS.
             For Requirement 2 - After the Requirement 1 operational check.
             For Requirement 3 - Within 25 hours TIS after the effective date of this Directive.
             This Amendment becomes effective on 22 December 2009.
Background:  Operator reports involving the following discrepancies, elongated bolt holes, cracks and loose fasteners in the rudder actuator attachment area, have been received by the manufacturer.
             The original issue of this Directive only applied to GII and GIIB series aeroplanes and required initial and repetitive operational checks of the takeoff warning system.
             This amendment continues the repetitive operational checks and extends the applicability of the Directive to include G-III aeroplanes and certain G-IV aeroplanes; it also requires a modification of the takeoff warning range indication system for
             G-IV aeroplanes.

             The original issue of this Directive became effective on 17 May 1990.

William David
Delegate of the Civil Aviation Safety Authority

11 December 2009