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

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

Legislation au F2006B09173 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-8/18 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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.