Document ID: chunk:federal_register_of_legislation:F2006B06541:body:0
Version: federal_register_of_legislation:F2006B06541
Segment Type: other
Provision Reference: 
Character Range: 0–846

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/RB211/10
 Amdt 1

 High Pressure Compressor Disc 9/87

 Applicability: RB211-524 Series Engines.

            Requirement:  Remove from service, stage 1 and stage 2 high pressure compressor disc assemblies identified by serial number in Rolls Royce Service Bulletin RB211-72-A7774 Rev 2 Appendix 3 and Appendix 4.

            Note: FAA AD 86-15-01 Amdt 39-5346 refers.

 Compliance: In accordance with Requirement Document.

            Background: This Directive has been amended to reflect the manufacturers latest revision to Service Bulletin RB211-72-A7774. The revision, in part, increases the number of discs in Appendix 3 and Appendix 4.