AD/DHC-8/32 - Landing Gear Hydraulic Selector Valve

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

Legislation au F2006B09188 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-8/32 Landing Gear Hydraulic Selector Valve 7/94

Applicability: All DHC-8-100 series aircraft S/N 003 through 038 not incorporating modification 8/0530.

 

Requirement: Unless previously carried out action in accordance with de HAVILLAND Dash 8 Alert Service Bulletin A8-32-117.

 

Note: Transport Canada AD CF-94-05 refers.

 

Compliance: Within 300 hours time in service from 30 June 1994 or by 30 October 1994, whichever occurs first.

 

Background: The manufacturer has advised that pilot valve leakage which has not been corrected may, when combined with a low voltage condition, lead to an inadvertent landing gear retraction.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.