ARMY TM 5-6115-612-34 NAVY AG -320B0-MME-000 8-2. COMBUSTION  CHAMBER  CASE  ASSEMBLY. (cont) c. Overhaul   (cont) (f) Inspect   combustion   chamber   for carbon deposits.  Clean in accordance with paragraph 8- 2b. (g) Inspect combustion  chamber  for cracks.  Replace if cracks are found. (h) Bend deflector tabs of combustion chamber    back    to    position    (I)    Replace    combustion chamber if tabs or washers are missing or broken. (k) Install    combustion    chamber    on turbine nozzle.  The fit should be snug all around.  If not, replace liner (k) Install combustion chamber in combustion  chamber  case.    Chamber  should  fit  snugly on   exhaust   port.      If   chamber   rotates   easily,   replace chamber. (10)  Inspect and overhaul related combustion chamber case components. (a)Inspect and replace or overhaul the fuel injection nozzles in accordance with Chapter 5. (b) Replace    igniter    if    threads    are damaged    beyond    repair    or    if    insulator    is    burned, chipped, or cracked. (c) Replace     EGT     thermocouple     if threads  of  terminals  are  damaged  beyond  repair  or  if thermocouple   has   been   broken   insulators   or   a   bent sheath. (11)  Reassemble  the  combustion  chamber case assembly. NOTE Pay  particular  attention  to  detail  during assembly. Maintain all fits and tolerances.    If  the  unit  is  to  be  left  for even     a     short     period     in     a     partially disassembled  state  cover,    cap,  or  plug all   openings.      Before   assembling   any part, make certain the parts is thoroughly   clean.      Wipe   all   parts   and surfaces with a clean, lint-free cloth. (a) Aline ignitor openings on combustion chamber and combustion chamber case. (b) Slide     combustion     chamber     (6, Figure 8-3) into combustion chamber case (7). (c) Coat   threads   of   alinement   bolts (4)     with     anti-seize     compound,     MIL-A-907.          Insert washers  (5)  and  bolts  (4)  in  combustion  chamber  case. Torque to 25 35 inch pounds (2.83 3.96 Nm). (d) Apply  anti-seize  compound,  MIL- A907, to ignitor (1).  Install washer (2.1), gasket (2), and ignitor (1) in combustion chamber case. (e) Coat threads of EGT thermocouple  (3)  with  anti-seize  compound,  MIL-A-907, and install thermocouple (3). (f) Coat threads of bolts (6, Figure 8- 4)  with  anti-seize  compound,  MIL-A-907.    Install  nozzle covers (1 0) and fuel nozzles (8).    Secure  with  washers (7)  and  bolts  (6).    Torque  to  20  25  inch  pounds  (2.26 2.83  Nm)  and  lockwire  bolts  using  MS20995-C20  and lockwire nuts using MS20995-C32. 8-16  Change 4