AD/DHC-8/53 - Roll Disconnect System

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

Legislation au F2006B09209 In force Legislative Instrument

Legislation content

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-8/53 Roll Disconnect System 6/98

Applicability: DHC-8 aircraft, Models 102, 103, 106, 201, 202, 301, 311, 314, and 315, with serial

numbers 3 through 433.

 

Requirement: Install Modification 8/2376 in accordance with de Havilland Service Bulletin 8-27- 79, Revision A.

 

Note: Transport Canada AD CF-98-04 refers.

 

Compliance: Before 21 November 1998.

 

This airworthiness directive becomes effective on 21 May 1998.

 

Background: Several incidents have been reported of uncommanded roll system disconnects during landing.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.