AD/JETSTREAM/79 - Main Landing Gear Brake Unit

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

Legislation au F2006B10949 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

 


British Aerospace BAe 3100 (Jetstream) Series Aeroplanes

 

AD/JETSTREAM/79 Main Landing Gear Brake Unit 10/98 DM

Applicability: Jetstream Series 3100 and 3200 aircraft as detailed in the requirement document. Requirement:               Action in accordance with British Aerospace Regional Aircraft Alert Service Bulletin

32-A-JA980540.

 

Note: UK CAA AD 003-07-98 refers.

 

Compliance: Unless already accomplished, action in accordance with Part 1 and Part 2 of the Requirement document before 31 July 1998.

 

This airworthiness directive becomes effective on 22 July 1998.

 

Background: An incident has occurred where a brake unit heat pack was found to be totally worn when the indicator pins showed 0.1 inches of wear remaining. This directive requires a check of the wear remaining length indicated by the wear indicator pins and inspection to determine that the indicator pins are set correctly. There is a possibility that a fully worn heat pack in a brake unit may not be indicated as such by the indicator pins if not set correctly, which is a potentially unsafe condition.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.