AD/RB211/10 Amdt 1 - High Pressure Compressor Disc
1AD/RB211/10 Amdt 1 - High Pressure Compressor Disc
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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/RB211/10
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.