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Rolls-Royce Service Bulletin RB.211-72-F227

Service bulletin · Rolls-Royce

Revision 1Service Information · 21 pages · 138 KB

© Rolls-Royce plc. Filed by the FAA in regulations.gov docket FAA-2012-1198; AD 2012-25-08 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

Docket FAA-2012-1198 (document 0002) · AD 2012-25-08

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Manufacturer: Rolls-Royce
Type: Service Bulletin
Number: RB.211-72-F227
Latest revision known: RB.211-72-F227, Revision 1, dated October 8, 2007

A newer revision may exist than any OpenAirDocs knows of: check with the manufacturer.

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ADs that cite it · 3

Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.

AD 2012-25-08High pressure/ intermediate pressure (HP/IP) turbine bearing support oil feed tube outer heat shield · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60Effective Jan 10, 2013 · Revision 1 AD 2008-24-03High-pressure/intermediate-pressure (HP/IP) turbine bearing internal oil vent tube, scavenge tube, and tube heat shields; vent flow restrictor · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60Effective Dec 15, 2008 · Revision 1 AD 2007-24-09High pressure/intermediate pressure (HP/IP) turbine bearing oil feed tube · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60Effective Dec 14, 2007 · Revision 1