Document ID: chunk:federal_register_of_legislation:F2006B09249:body:0
Version: federal_register_of_legislation:F2006B09249
Segment Type: other
Provision Reference: 
Character Range: 0–735

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-8/9 Flap Track No.5 Fail Safe Straps 10/89

 Applicability: Serial number 1 through 119.

            Requirement: Action in accordance with Boeing Canada DHC-8 Service Bulletin No. 8-57-10 dated 31 March 1989.

            Note: Transport Canada AD CF-89-02 refers.

            Compliance: Within 500 hours time in service after 5 October 1989, or prior to 5 January 1990, whichever occurs first.

            Background: Some fatigue failures have occurred on subject straps because of incorrect installation.