Document ID: chunk:federal_register_of_legislation:F2006B09173:body:0
Version: federal_register_of_legislation:F2006B09173
Segment Type: other
Provision Reference: 
Character Range: 0–890

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Bombardier (Boeing Canada/De Havilland) DHC-8 Series Aeroplanes

AD/DHC-8/18 Elevator Control Quadrant Lever 4/92

 Applicability: Model DHC-8 series 100 with serial number 1 through 126 inclusive. Requirement:  In accordance with Boeing Canada de Havilland Division SB A8-27-45 Rev A.
            Note: Transport Canada AD CF-88-25 refers.
 Compliance: Unless already accomplished; within 50 hours time in service after 2 April 1992. Background:              An elevator control quadrant lever was found to be incorrectly installed on a Dash 8.
            The incorrect installation caused permanent deformation of the associated push rod.
            If not corrected, this condition could result in loss of associated elevator control.