AD/RB211/13 - Thrust Reverser Functional Test
1AD/RB211/13 - Thrust Reverser Functional Test
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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).