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Rolls-Royce Non-Modification Service Bulletin RB.211-72-G448

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Service bulletin · Rolls-Royce

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Copies of this document that the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist.

Revision 4RB 211-72-G448 R4 · 63 pages · 1.2 MB

© Rolls-Royce plc. Filed by the FAA in regulations.gov docket FAA-2007-28059; AD 2015-02-20 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

Docket FAA-2007-28059 (document 0031) · AD 2008-18-08, AD 2012-10-12, AD 2013-15-10, AD 2015-02-20

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U.S. DOT/FAA - Service Information - 2U.S. DOT/FAA - Service Information - 2 · 61 pages · 1.2 MB

© Rolls-Royce plc. Filed by the FAA in regulations.gov docket FAA-2007-28059; AD 2015-02-20 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

Docket FAA-2007-28059 (document 0020) · AD 2008-18-08, AD 2012-10-12, AD 2013-15-10, AD 2015-02-20

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Manufacturer
Rolls-Royce
Type
Non-Modification Service Bulletin
Number
RB.211-72-G448
Latest revision known
RB.211-72-G448, Revision 4, dated August 21, 2014
Copies
2 files of 2 revisions

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

ADs that cite it · 1

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

AD 2015-02-20Intermediate-pressure compressor (IPC) rotor shaft · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 22 moreEffective Mar 11, 2015 · Revisions 2, 3 and 4

Also cited in 1 proposed AD.