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Copies · 2
Copies of this document that the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist.
Revision 2
© Rolls-Royce plc. Filed by the FAA in regulations.gov docket FAA-2012-1327; AD 2013-12-01 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
U.S. DOT/FAA - Service Information - 2
© Rolls-Royce plc. Filed by the FAA in regulations.gov docket FAA-2012-1327; AD 2013-12-01 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Manufacturer
- Rolls-Royce
- Type
- Non-Modification Service Bulletin
- Number
- RB.211-72-G872
- Latest revision known
- RB.211-72-G872, Revision 2, dated March 8, 2013
- Copies
- 2 files of 2 revisions
A newer revision may exist than any OpenAirDocs knows of: check with the manufacturer.
ADs that cite it · 4
Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.
AD 2020-06-16Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60AD 2017-03-02LP compressor blade · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60AD 2014-16-10LP compressor blades · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60AD 2013-12-01LP compressor blades · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60
Also cited in 2 proposed ADs.