AD/DHC-8/9 - Flap Track No.5 Fail Safe Straps

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B09249 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.