AD/RB211/13 - Thrust Reverser Functional Test

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

Legislation au F2006B06544 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Rolls Royce Turbine Engines - RB211 Series

 

AD/RB211/13 Thrust Reverser Functional Test 6/91

Applicability: All RB211-524G and 524H engines not incorporating the requirements of Rolls Royce Service Bulletin RB211-78-9347.

 

Requirement: Action in accordance with the requirements of Rolls Royce Mandatory Service Bulletin RB211-78-9274.

 

Compliance: As detailed in Requirement Document.

 

Background: This Directive requires a functional test to be carried out following any abandoned take-off where the thrust reversers have been deployed. This requirement reflects advice that following an abandoned take-off, thrust reverser operation times may become extended (10 seconds or more).

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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.