TM 55-2840-231-23
3-7. COMBUSTION SECTION – INSTALI.ATION - Cont.
ENGINE/
1. First Stage
Nozzle Shield
2. Plugs (22)
3. Combustion
Liner (3)
4. Retaining
Rings (17)
NOTE
This paragraph provides instruction
for installing the combustion section
on the engine while the engine is
installed in turnover stand (tool no
6795579). If the turnover stand is
used, rotate the engine in the stand
to a vertical position with the
compressor on the bottom.
Install first stage nozzle
shield (21), if removed.
Antiseize Compound (item 6, Appendix D).
Apply antiseize compound
LockWire (item 7, Appendix D).
and install two positioning
plugs (22). Tighten to 100 to
150 in.-lb. (1.15 to 1.7 kg/m) and
secure with lockwire.
Place combustion liner (3)
over first stage turbine
nozzle shield with igniter
plug opening at the nine
o’clock position (as viewed
from rear of engine).
Slip retaining rings (17’)
over the large ends of
compressor discharge air
tubes (18).
Change 8
3-17
