selecting said first burner dome from said sequence of burner domes to be adjusted.
20. The method of claim 19, wherein said selecting said first burner dome includes:
setting a flag to identify an adjusted burner dome in said plurality of burner domes to be adjusted for said first burner mode.
21. The method of claim 1, wherein said adjusting a ring flame temperature at said first burner dome in said gas turbine engine to determine a maximum ring flame temperature operational boundary includes:
incrementing said ring flame temperature at said first burner dome in said gas turbine engine by a predetermined amount; and
detecting the activation of a acoustics and blow out avoidance logic.
22. The method of claim 1, wherein said adjusting a ring flame temperature at said first burner dome in said gas turbine engine to determine a maximum ring flame temperature operational boundary includes: