Installation of Full Set Fuel Nozzles [CFML]

B. Installation of Fuel Nozzles
   (1) Use new fuel nozzle EIPC 73-00-00-15-220A BOLTS (85) for the fuel nozzles (14).
   (2) Prepare all the 76 fuel nozzle bolts (bolts) (85) with lubricant CP2961tiodize grease T8E-H grease/anti-seize with BRUSH - ACID.

NOTE: The CP2961tiodize grease T8E-H grease/anti-seize will greatly reduce fallout of broken bolts and inserts in the future fuel nozzle maintenance.

   (3) Put all the 19 clean fuel nozzles (14) procured from Advanced Atomization Technologies L.L.C. on a bench and mark the fuel nozzles (14) No. 1 through No. 19.
   (4) Make a record of the fuel nozzle position with the related fuel nozzle serial number and part number.
   (5) Do a general visual inspection of the fuel nozzles (14) (Ref. AMM TASK 73-11-30-210-801).
   (6)    (7)      (a) Turn the fuel nozzle seal assembly (132) until the bolt holes line up.
     (b) Matchmark the fuel nozzle seal assembly (132) and orientation to the fuel nozzle (14).
   (8) Remove all CAP - BLANKING and COVER - BLANKING from the engine case and the fuel nozzles (14) that you install.
   (9) Put the 19 fuel nozzles (14) in position. Before you install one of the bolts (85), install the fuel nozzles (14) as follows:
     (a)        1 Half 1, RH side, aft looking forward includes fuel nozzles (14) No. 9, No. 8, No. 6, No. 7, No. 5, No. 4, No. 1, No. 2 and No. 3 installed from the 1:00 to 5:00 o’clock positions and do as follows:

• Fuel nozzle No. 9 - turn DOWN and into the case.
  
• Fuel nozzle No. 8 - turn DOWN and into the case.
  
• Fuel nozzle No. 6 - turn UP and into the case.
  
• Fuel nozzle No. 7 - turn DOWN and into the case.
  
• Fuel nozzle No. 5 - turn DOWN and into the case.
  
• Fuel nozzle No. 4 - turn DOWN and into the case.
  
• Fuel nozzle No. 1 - turn LEFT and into the case.
  
• Fuel nozzle No. 2 - turn LEFT and into the case.
  
• Fuel nozzle No. 3 - turn LEFT and into the case.
  

         a Move the fuel nozzle aft to engage swirl cup.
       2 Half 2, LH side, aft looking forward includes fuel nozzles (14) No. 14, No. 12, No. 11, No. 13, No. 10, No. 16, No. 15, No. 18, No. 19 and No. 17 installed from the 6:00 to 12:00 o’clock positions and do as follows:

• Fuel nozzle No. 14 - turn RIGHT and into the case.
  
• Fuel nozzle No. 12 - turn RIGHT and into the case.
  
• Fuel nozzle No. 11 - turn UP and into the case.
  
• Fuel nozzle No. 13 - turn UP and into the case.
  
• Fuel nozzle No. 10 - turn DOWN and into the case.
  
• Fuel nozzle No. 16 - turn UP and into the case.
  
• Fuel nozzle No. 15 - turn DOWN and into the case.
  
• Fuel nozzle No. 18 - turn RIGHT and into the case.
  
• Fuel nozzle No. 19 - turn RIGHT and into the case.
  
• Fuel nozzle No. 17 - turn RIGHT and into the case.
  

         a Move the fuel nozzle aft to engage swirl cup.
     (b)        1 Third 1, LH side, aft looking forward includes fuel nozzles (14) No. 16, No. 15, No. 18, No. 19 and No. 17 installed from the 9:00 to 12:00 o’clock positions and do as follows:

• Fuel nozzle No. 16 - turn UP and into the case.
  
• Fuel nozzle No. 15 - turn DOWN and into the case.
  
• Fuel nozzle No. 18 - turn RIGHT and into the case.
  
• Fuel nozzle No. 19 - turn RIGHT and into the case.
  
• Fuel nozzle No. 17 - turn RIGHT and into the case.
  

         a Move the fuel nozzle aft to engage swirl cup.
       2 Third 2, RH side, aft looking forward includes fuel nozzles (14) No. 5, No. 4, No. 1, No. 2 and No. 3 installed from the 1:00 to 3:00 o’clock positions and do as follows:

• Fuel nozzle No. 5 - turn DOWN and into the case.
  
• Fuel nozzle No. 4 - turn DOWN and into the case.
  
• Fuel nozzle No. 1 - turn LEFT and into the case.
  
• Fuel nozzle No. 2 - turn LEFT and into the case.
  
• Fuel nozzle No. 3 - turn LEFT and into the case.
  

         a Move fuel nozzle aft to engage swirl cup.
       3 Third 3, LH side and RH side, aft looking forward includes fuel nozzles (14) No. 14, No. 12, No. 11, No. 13, No. 10, No. 9, No. 8, No. 6 and No. 7 installed from the 3:00 to 9:00 o’clock positions and do as follows:

• Fuel nozzle No. 14 - turn RIGHT and into the case.
  
• Fuel nozzle No. 12 - turn RIGHT and into the case.
  
• Fuel nozzle No. 11 - turn UP and into the case.
  
• Fuel nozzle No. 13 - turn UP and into the case.
  
• Fuel nozzle No. 10 - turn DOWN and into the case.
  
• Fuel nozzle No. 9 - turn DOWN and into the case.
  
• Fuel nozzle No. 8 - turn DOWN and into the case.
  
• Fuel nozzle No. 6 - turn UP and into the case.
  
• Fuel nozzle No. 7 - turn DOWN and into the case.
  

         a Move the fuel nozzle aft to engage swirl cup.
   (10)    (11)

C. Torque Pattern of the Fuel Nozzle Bolts
   (1) TORQUE the bolts (85) to between 103 and 87 lbf.in (1.16 and 0.98 m.daN ) . Start at the close-fitting bolt hole (No. 1) followed by the elongated bolt hole (No. 2) and then the remaining two bolt holes (No. 3 and No. 4).

CAUTION: IF YOU MUST LOOSEN THREE OR MORE BOLTS OF AN ADJACENT FUEL NOZZLE FOR ACCESS, REPLACE THE FUEL NOZZLE SEAL ASSEMBLY. IT CAN BE NECESSARY TO LOOSEN AND REMOVE AN ADJACENT FUEL NOZZLE TO LET YOU TURN THE FUEL NOZZLE INTO THE COMBUSTION CASE. IF YOU DO NOT OBEY THIS INSTRUCTION, FUEL LEAKAGE CAN OCCUR.

   (2) TORQUE the bolts (85) again to between 151 and 129 lbf.in (1.71 and 1.46 m.daN ) . Start at the close-fitting bolt hole (No. 1) followed by the elongated bolt hole (No. 2) and then the remaining two bolt holes (No. 3 and No. 4).

NOTE: One of the four fuel nozzle (14) bolt holes is elongated.

NOTE: It can be helpful to tag hardware with the correct torque between shifts, but a correct shift turnover plan with your quality assurance program must be started.

   (3)      (a) If the bolts (85) are found unseated or suspected to be unseated, remove the bolts (85) and install the new EIPC 73-00-00-15-220A BOLTS (85) with excess CP2961tiodize grease T8E-H grease/anti-seize.
   (4) Put a verification mark line across the bolts (85) and fuel nozzle base with a temporary marking (Material No.CP5061) .

D. Torque the Fuel Nozzle B-nuts
   (1) Torque the fuel manifold B-nuts (131) as follows:
     (a) Triple-torque all 38 fuel manifold B-nuts (131). Start with the lowest numbered fuel nozzle (14) No. 1 and do as follows:
       1 TORQUE the fuel manifold B-nuts (131) to between 308 and 262 lbf.in (3.48 and 2.96 m.daN ) .
       2 Loosen the fuel manifold B-nuts (131) until you can turn them with your fingers.
       3 TORQUE the fuel manifold B-nuts (131) again to between 308 and 262 lbf.in (3.48 and 2.96 m.daN ) .
       4 TORQUE the fuel manifold B-nuts (131) a third time to between 308 and 262 lbf.in (3.48 and 2.96 m.daN ) .
       5 Put a mark across the fuel manifold B-nut (131) and the fuel nozzle (14) fitting with a temporary marking (Material No.CP5061) to show that the fuel manifold B-nut (131) has been torqued.
       6      (b) Do an inspection as follows:
       1 Have an inspector different from the one who torqued the fuel manifold B-nuts (131) in Para. 4.D.(1) (a) to do the inspection.
       2 The inspector must start the check from the fuel nozzle (14) No. 1 and TORQUE the fuel manifold B-nuts (131) again to between 308 and 262 lbf.in (3.48 and 2.96 m.daN ) , sequentially around in a CW direction, aft looking forward. On each fuel nozzle (14), torque the pilot secondary B-nut first, followed by the pilot primary main B-nut.
       3      (c)

E. Torquing of the Fuel Nozzle Brackets with Associated Hardware Attached
   (1) If any bolt that attaches any clamp, retaining strap, tube, duct or other bracket was loose or removed to make the fuel nozzle bracket flexible, torque the bolt to the components as follows:
   (2)      (a) Apply a layer of engine oil (Material No.CP2442) to the threads of three bolts (20).
     (b) Attach the turbine center frame accelerometer (18) to the electrical harnesses support bracket (133) on the fuel nozzle pad with a bolt (20) and the loop clamp (23).
     (c) Attach the right T48 harness (22) to the electrical harnesses support bracket (133) with the loop clamp (21) and the bolt (20).
     (d) Attach the left T48 harness (19) to the electrical harnesses support bracket (133) with the loop clamp (21) and the bolt (20).
     (e) TORQUE the bolts (20) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
   (3) PRE SB 72-0190
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135) and (136).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (140) and (138) and bolts (135) and (136).
     (c) TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF PRE SB 72-0190
     (d) POST SB 72-0190
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135) and (136).
     (e) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (140) and (138) and bolts (135) and (136).
     (f) Attach the core compartment cooling right side tube (141) to the core compartment cooling support bracket (144) with the cushioned loop clamp (142) and bolt (143).
     (g) Attach the turbine center frame accelerometer (18) to the core compartment cooling support bracket (144) on the fuel nozzle pad with a bolt (20) and loop clamp (23).
     (h) TORQUE the bolts (20), (143), (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0190
   (4)      (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135) and (136).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (145) and (138) and bolts (135) and (136).
     (c) TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
   (5) POST SB 72-0190
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (88) and (53).
     (b) Attach the start bleed fuel tubes (147) and (149) to the fuel hydraulic support bracket (148) with the two clamps (146) and two bolts (88).
     (c) Attach the core compartment cooling right side tube (55) to the fuel hydraulic support bracket (148) with one bolt (53) and one clamp (54).
     (d) TORQUE the bolts (88) and (53) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0190
     (e) POST SB 72-0270
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (88).
     (f) Attach the start bleed fuel tubes (147) and (149) to the fuel hydraulic support bracket (148) with the two clamps (146) and two bolts (88) and do as follows:
       1 TORQUE the bolts (88) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0270
   (6)      (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135) and (136).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
   (7) POST SB 72-0190
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolt (68).
     (b) Attach the PS3 air tube (67) to the PS3 support bracket (150) with the loop clamp (69) and bolt (68) and do as follows:
       1 TORQUE the bolt (68) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
END OF POST SB 72-0190
   (8)      (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135), (136) and (68).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (140) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (c) Attach the PS3 air tube (67) to the PS3 support bracket (151) with the loop clamp (69) and bolt (68) and do as follows:
       1 TORQUE the bolt (68) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
   (9) PRE SB 72-0113
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135), (153), (136), (152) and (100).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold inlet supply bracket (155) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (c) Attach the inlet supply fuel manifold bracket (154) and the fuel manifold inlet supply bracket (155) with the bolt (153) and do as follows:
       1 TORQUE the bolt (153) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
     (d) Attach the bracket (108) to the bracket (110) with the bolt (152) and do as follows:
       1 TORQUE the bolt (152) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (e) Attach the tube (102) to the bracket (110) with the two bolts (100) and loop clamps (105) and (98) and do as follows:
       1 TORQUE the bolts (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF PRE SB 72-0113
     (f) POST SB 72-0113
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135), (153), (136), (152), (107), (156) and (100).
     (g) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold inlet supply bracket (155) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (h) Attach the inlet supply fuel manifold bracket (154) and the fuel manifold inlet supply bracket (155) with the bolt (153) and do as follows:
       1 TORQUE the bolt (153) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
     (i) Attach the bracket (108) to the bracket (110) with the bolt (152) and do as follows:
       1 TORQUE the bolt (152) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (j) Attach the bracket (112) to the bracket (110) with the bolt (156) and do as follows:
       1 TORQUE the bolt (156) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (k) Attach the tube (102) to the bracket (110) with the bolt (100) and loop clamp (103) and do as follows:
       1 TORQUE the bolt (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (l) Attach the oil supply tubes (104) and (99) to the brackets (110) and (112) with the bolts (107) and loop clamps (109) and (111) and do as follows:
       1 TORQUE the bolts (107) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
     (m) Attach the oil supply tube (101) to the bracket (112) with the bolt (100) and loop clamp (98) and do as follows:
       1 TORQUE the bolt (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0113
     (n) POST SB 72-0211
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (134), (153), (136), (113), (152), (107) and (100).
     (o) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold inlet supply bracket (155) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (p) Attach the inlet supply fuel manifold bracket (154) and the fuel manifold inlet supply bracket (155) with the bolt (153) and do as follows:
       1 TORQUE the bolt (153) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
     (q) Attach the bracket (108) to the bracket (110) with the bolt (152) and do as follows:
       1 TORQUE the bolt (152) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (r) Attach the oil supply tubes (102) and (104) to the bracket (110) with the bolts (113) and (100) and loop clamps (105) and (103) and do as follows:
       1 TORQUE the bolts (113) and (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (s) Attach the brackets (110) and (112) with the bolt (107) and do as follows:
       1 TORQUE the bolt (107) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
     (t) Attach the oil supply tube (99) to the brackets (110) and (112) with the bolt (100) and the loop clamp (106) and do as follows:
       1 TORQUE the bolt (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (u) Attach the oil supply tube (101) to the bracket (112) with the bolt (100) and the loop clamp (98) and do as follows:
       1 TORQUE the bolt (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0211
   (10) PRE AND POST SB 72-0133
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (72), (115), (26), (157), (123) and (121).
     (b) Attach the tube (126) to the bracket (125) with the loop clamp (73) and bolt (72) and do as follows:
       1 TORQUE the bolt (72) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
     (c) Attach the tube (117) to the bracket (114) with the loop clamp (116) and bolt (115) and do as follows:
       1 TORQUE the bolt (115) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
     (d) Attach together the bracket (114) and air tube bracket (124) with the bolts (157) and do as follows:
       1 TORQUE the bolts (157) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
     (e) Attach the 7th stage air tube (127) to the air tube bracket (124) with the retaining strap (25) and bolts (26) and do as follows:
       1 TORQUE the bolts (26) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (f) Attach the air tube (122) to the air tube bracket (124) with the retaining strap (95) and bolts (123) and do as follows:
       1 TORQUE the bolts (123) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (g) Attach the tube (118) to the bracket (114) with the loop clamp (46) and bolt (72) and do as follows:
       1 TORQUE the bolt (72) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
     (h) Attach the ignition lead (119) to the air tube bracket (124) with the loop clamp (120) and bolt (121) and do as follows:
       1 TORQUE the bolt (121) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF PRE AND POST SB 72-0133
   (11) PRE SB 72-0207
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (136) and (135).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF PRE SB 72-0207
     (c) POST SB 72-0207
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (163), (159), (136) and (135).
     (d) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (164) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (e) Attach together the inlet supply fuel manifold bracket (referred to as support bracket) (162) and fuel manifold support bracket (164) with the bolts (163) and do as follows:
       1 TORQUE the bolts (163) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (f) Attach the pilot primary and main supply hose tube (referred to as tube) (165) to the support bracket (162) with the loop clamp (160) and bolt (159) and do as follows:
       1 TORQUE the bolt (159) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (g) Attach the pilot primary main enriched supply fuel tube (referred to as tube) (161) to the support bracket (162) with the loop clamp (158) and bolt (159) and do as follows:
       1 TORQUE the bolt (159) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0207
   (12)      (a) PRE SB 72-0207
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (72), (135) and (136).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (c) Attach the tube (126) to the Low Pressure Turbine Active Clearance Control (LPTACC) support bracket (166) with the loop clamp (73) and bolt (72) and do as follows:
       1 TORQUE the bolt (72) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
END OF PRE SB 72-0207
     (d) POST SB 72-0207
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (72), (135), (136) and (169).
     (e) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (f) Attach the tube (126) to the tube support bracket (168) with the loop clamp (73) and bolt (72) and do as follows:
       1 TORQUE the bolt (72) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
     (g) Attach the pilot secondary supply fuel tube (referred to as tube) (167) to the tube support bracket (168) with the loop clamp (170) and bolt (169) and do as follows:
       1 TORQUE the bolt (169) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0207
   (13)      (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (135) and (136).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (145) and (138) and bolts (135) and (136) and do as follows:
       1 TORQUE the bolts (135) and (136) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
   (14)      (a) PRE SB 72-0268
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (175), (181), (178) and (59).
     (b) Attach the left side core compartment cooling tube (referred to as tube) (179) to the core compartment cooling support bracket (176) with the loop clamp (180) and bolt (178) and do as follows:
       1 TORQUE the bolt (178) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (c) Attach the T3 sensor (173) to the T3 temperature sensor bracket (172) with the loop clamp (171) and bolt (175) and do as follows:
       1 TORQUE the bolt (175) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
     (d) Attach the T3 sensor (173) to the T3 temperature sensor bracket (174) and core compartment cooling support bracket (176) with the loop clamp (171) and bolt (175) and do as follows:
       1 TORQUE the bolt (175) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
     (e) Attach the T3 temperature sensor brackets (172) and (174) with the bolt (181) and do as follows:
       1 TORQUE the bolt (181) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (f) Attach the core compartment cooling support bracket (176) and T3 temperature sensor bracket (174) with the bolts (182) and do as follows:
       1 TORQUE the bolts (182) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (g) Attach the High Pressure Turbine Active Clearance Control (HPTACC) drain tube (referred to as tube) (177) to the core compartment cooling support bracket (176) with the loop clamp (60) and bolt (59) and do as follows:
       1 TORQUE the bolt (59) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
END OF PRE SB 72-0268
     (h) POST SB 72-0268
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (175) and (59).
     (i) Attach the tube (177) to the T3 temperature sensor bracket (174) with the loop clamp (60) and bolt (59) and do as follows:
       1 TORQUE the bolt (59) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
     (j) Attach the T3 sensor (173) to the T3 temperature sensor bracket (174) with the loop clamps (171) and bolts (175) and do as follows:
       1 TORQUE the bolts (175) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
END OF POST SB 72-0268
   (15)      (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (186) and (59).
     (b) Attach the Active Clearance Control (ACC) modulated turbine cooling fuel hydraulic manifold (referred to as manifold) (184) to the low pressure turbine fuel support bracket (referred to as support bracket) (183) with the fuel hydraulic support block (referred to as block clamp) (185) and bolts (186) and do as follows:
       1 TORQUE the bolts (186) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
     (c) Attach the tube (177) to the support bracket (183) with the loop clamp (60) and bolt (59) and do as follows:
       1 TORQUE the bolt (59) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
   (16) POST SB 72-0036
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (136), (153) and (135).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (138) and (145) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (c) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold inlet supply bracket (referred to as supply bracket) (188) with the loop clamps (138) and (140) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (d) Attach the inlet supply fuel manifold bracket (referred to as supply bracket) (187) and supply bracket (188) with the bolt (153) and do as follows:
       1 TORQUE the bolt (153) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
END OF POST SB 72-0036
     (e) POST SB 72-0133
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (136), (153), (123), (92) and (135).
     (f) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (138) and (145) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (g) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the supply bracket (188) with the loop clamps (138) and (140) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (h) Attach the 4th stage air manifold (94) to the support bracket (91) with the retaining strap (95) and bolts (123) and do as follows:
       1 TORQUE the bolts (123) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (i) Attach the support bracket (91) and support bracket (89) with the bolt (92) and do as follows:
       1 TORQUE the bolt (92) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (j) Attach the supply brackets (187) and (188) with the bolt (153) and do as follows:
       1 TORQUE the bolt (153) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
END OF POST SB 72-0133
     (k) POST SB 72-0205
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (136), (153), (96) and (135).
     (l) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (138) and (145) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (m) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the supply bracket (188) with the loop clamps (138) and (140) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (n) Attach the 4th stage air manifold (94) to the support bracket (91) and support bracket (89) with the retaining strap (95) and bolts (96) and do as follows:
       1 TORQUE the bolts (96) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (o) Attach together the supply brackets (187) and (188) with the bolt (153) and do as follows:
       1 TORQUE the bolt (153) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
END OF POST SB 72-0205
   (17)    (18) PRE SB 72-0133
     (a) Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (136), (135), (26) and (20).
     (b) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (138) and (145) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (c) Attach the right T48 harness (22) to the electrical harnesses 7th stage tube bracket (referred to as tube bracket) (189) with the loop clamp (21) and the bolt (20).
     (d) Attach the left T48 harness (19) to the tube bracket (189) with the loop clamp (21) and the bolt (20) and do as follows:
       1 TORQUE the bolt (20) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (e) Attach the 7th stage air manifold (24) to the tube bracket (189) with the retaining strap (50) and bolts (26) and do as follows:
       1 TORQUE the bolts (26) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
END OF PRE SB 72-0133
     (f) POST SB 72-0133
Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (136), (135) and (20).
     (g) Attach the primary fuel manifold (134) and secondary fuel manifold (139) to the fuel manifold support bracket (137) with the loop clamps (138) and (145) and bolts (136) and (135) and do as follows:
       1 TORQUE the bolts (136) and (135) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (h) Attach the right T48 harness (22) to the electrical harnesses support bracket (referred to as support bracket) (190) with the loop clamp (21) and the bolt (20).
     (i) Attach the left T48 harness (19) to the support bracket (190) with the loop clamp (21) and the bolt (20) and do as follows:
       1 TORQUE the bolt (20) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0133

F. External Hardware Installation

CAUTION: BEFORE YOU INSTALL THE TUBES, DUCTS AND MANIFOLDS, REMOVE ALL THE PLUGS OR CAPS FROM THE OPEN HOLES. IF YOU DO NOT REMOVE THE PLUGS OR CAPS, THEY CAN GO INTO TUBES, DUCTS AND MANIFOLDS. THIS CAN CAUSE DOMESTIC OBJECT DAMAGE AND/OR BLOCKAGE OF THE AIR/OIL/FUEL SYSTEM.

CAUTION: REMOVE ALL THE PLUGS/CAPS OR COVERS FROM THE PORTS, OPENINGS AND MATING SURFACES OF THE CASES. IF YOU DO NOT REMOVE THEM, THEY CAN GO INTO THE ENGINE. THIS CAN CAUSE DOMESTIC OBJECT DAMAGE AND/OR BLOCKAGE OF THE AIR/OIL/FUEL SYSTEM WITH FOREIGN MATERIAL.

CAUTION: BEFORE YOU APPLY TORQUE TO THE B-NUTS, MAKE SURE THAT THE FUEL NOZZLE FITTINGS ARE CORRECTLY ENGAGED AND FULLY INSTALLED. IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE PARTS CAN OCCUR.

CAUTION: USE TWO WRENCHES WHEN YOU CONNECT THE DUCTS AND TUBES: - ONE WRENCH TO HOLD THE NIPPLE, AND - THE SECOND WRENCH TO TIGHTEN THE DUCT/TUBE COUPLING NUT. IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE PARTS CAN OCCUR.

   (1) Install the external components at the bottom of the engine, 6:00 o’clock position, aft looking forward, as follows:
     (a)        1 Apply a layer of synthetic beeswax (Material No.CP2635) to a new EIPC 72-00-02-35-160 METAL SEAL RING (128) to hold it in position during installation.
       2 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (130).
       3 Attach the 7th stage air tube (127) to the HPT case with the metal seal ring (128), bolts (130) and 7th stage air retainers (129). Tighten the bolts (130) but do not torque them at this time.
       4 Attach the 7th stage air tube (127) to the air tube bracket (124) with the bolts (26) and retaining strap (25). Tighten the bolts (26) but do not torque them at this time.
       5 TORQUE the bolts (130) that connect the 7th stage air tube (127) to the HPT case to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       6 TORQUE the bolts (26) that connect the 7th stage air tube (127) to the air tube bracket (124) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (b)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (72), (115), (26), (123) and (121).
       2 Install the bolt (72) that attaches the loop clamp (73) and the tube (126) to the bracket (125) and do as follows:
         a TORQUE the bolt (72) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
       3 Install the bolt (115) and the loop clamp (116) that attach the tube (117) to the bracket (114) and do as follows:
         a TORQUE the bolt (115) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
       4 Attach the 7th stage air tube (127) to the air tube bracket (124) with the bolts (26) and retaining strap (50) and do as follows:
         a TORQUE the bolts (26) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       5 Install the bolt (72) and the loop clamp (46) that attach the tube (118) to the bracket (114) and do as follows:
         a TORQUE the bolt (72) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
       6 Attach the air tube (122) to the air tube bracket (124) with the bolts (123) and retaining strap (37) and do as follows:
         a TORQUE the bolts (123) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       7 Attach the ignition lead (119) to the air tube bracket (124) with the bolt (121) and loop clamp (120) and do as follows:
         a TORQUE the bolt (120) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
     (c)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (100) and (107).
       2 Install the bolt (107) and the loop clamp (109) that attach the tube (104) to the bracket (110).
       3 Install the bolt (100) and the loop clamp (103) that attach the tube (102) to the bracket (110).
       4 Install the bolt (100) and the loop clamp (98) that attach the tube (101) to the bracket (110).
       5 Install the bolt (107) and the loop clamp (111) that attach the tube (99) to the brackets (110) and (112) and do as follows:
         a TORQUE the bolts (107) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
         b TORQUE the bolts (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF PRE SB 72-0211
     (d)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (100) and (113).
       2 Install the bolt (100) and the loop clamp (98) that attach the tube (101) to the bracket (112).
       3 Install the bolt (100) and the loop clamp (106) that attach the tube (99) to the brackets (110) and (112).
       4 Install the bolt (100) and the loop clamp (103) that attach the tube (102) to the bracket (110).
       5 Install the bolt (113) and the loop clamp (105) that attach the tube (104) to the bracket (110) and do as follows:
         a TORQUE the bolts (113) and (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0211
     (e)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (100).
       2 Install the bolt (100) and the loop clamp (105) that attach the tube (104) to the bracket (97).
       3 Install the bolt (100) and the loop clamp (103) that attach the tube (102) to the bracket (97).
       4 Install the bolt (100) and the loop clamp (98) that attach the tube (101) to the bracket (97).
       5 Install the bolt (100) and the loop clamp (98) that attach the tube (99) to the bracket (97) and do as follows:
         a TORQUE the bolts (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF PRE SB 72-0211
     (f)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (100).
       2 Install the bolt (100) and the loop clamp (105) that attach the tube (104) to the bracket (97).
       3 Install the bolt (100) and the loop clamp (103) that attach the tube (102) to the bracket (97).
       4 Install the bolt (100) and the loop clamp (98) that attach the tube (101) to the bracket (97).
       5 Install the bolt (100) and the loop clamp (106) that attach the tube (99) to the bracket (97).
       6 TORQUE the bolts (100) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
END OF POST SB 72-0211
   (2) Install the external components at the LH side of the engine, aft looking forward, as follows:
     (a)        1 For POST SB 72-0036 and PRE SB 72-0133 configurations, do as follows:
         a Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (88) and (90).
         b Install the two bolts (90) to the support brackets (87) and (89):

• TORQUE the bolts (90) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
  

         c Install the two bolts (88) and the block clamp (86) that attach the support bracket (89):

• TORQUE the bolts (88) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
  END OF POST SB 72-0036 AND PRE SB 72-0133
  

       2 For POST SB 72-0133 and PRE SB 72-0205 configurations, do as follows:
         a Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (92), (90) and (93).
         b Install the bolt (92) that attaches the support brackets (91) and (89):

• TORQUE the bolts (92) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
  

         c Install the two bolts (90) that attach the support brackets (87) and (89):

• TORQUE the bolts (90) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
  

         d Install the two bolts (93) that attach the block clamp (86) to the support bracket (89):

• TORQUE the bolts (93) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
  END OF POST SB 72-0133 AND PRE SB 72-0205
  

       3 For POST SB 72-0205 configuration, do as follows:
         a Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (96), (90) and (93).
         b Install the two bolts (96) that attach the retaining strap (95) and the 4th stage air manifold (94) to the support brackets (91) and (89):

• TORQUE the bolts (96) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
  

         c Install the two bolts (90) that attach the support brackets (87) and (89):

• TORQUE the bolts (90) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
  

         d Install the two bolts (93) that attach the block clamp (86) to the support bracket (89):

• TORQUE the bolts (93) to between 59 and 51 lbf.in (0.67 and 0.58 m.daN ) .
  END OF POST SB 72-0205
  

     (b)        1 Install the PRSOV 1 (83) and the air duct (80) as a module package.
       2 If the PRSOV 1 (83) and the air duct (80) were removed separately, install the air duct (80) first, then install the PRSOV 1 (83).
       3 Wait to perform the required test and/or inspection until the end of this AMM task.
     (c)        1 Install the HPTACC and LPTACC valves (82) and (81), brackets and flex ducts as a module package.
       2 Wait to perform the required test and/or inspection until the end of this AMM task.
     (d)        1 Slowly and carefully install the four case bolts (78).
       2 Do a visual inspection of all seal and flange sealing surfaces before installation to make sure that there are no scratches, cut, pits or foreign material.
   (3) Install the external components at the RH side of the engine, aft looking forward as follows:
     (a)        1 Triple-torque the B-nut (131) as follows:
         a TORQUE the B-nut (131) to between 307 and 263 lbf.in (3.47 and 2.97 m.daN ) .
         b Loosen the B-nut (131) until it turns freely.
         c TORQUE the B-nut (131) to between 307 and 263 lbf.in (3.47 and 2.97 m.daN ) .
         d TORQUE the B-nut (131) again to between 307 and 263 lbf.in (3.47 and 2.97 m.daN ) .
         e Tightly attach the B-nut (131) to the nipple connection with CP8006safety cable 0.032 in. (0.8 mm) or safetywire (Material No.CP8002) .
END OF PRE SB 72-0190 AND POST SB 72-0190
     (b)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of two bolts (76).
       2 Attach the air duct bracket (33) to the combustion case (6) pad with the bolts (76).
       3 TORQUE the bolts (76) to between 389 and 331 lbf.in (4.40 and 3.74 m.daN ) .
     (c)        1 Apply engine oil (Material No.CP2442) on the threads of the bolts (59), (68), (32) and (65).
       2 Put the start bleed valve support bracket (34) in position on the engine.
       3 Install the bolt (68) that attaches the loop clamp (69) to the PS3 air tube (67) and support bracket (42) and do as follows:
         a TORQUE the bolt (68) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
       4 Install the bolt (68) that attaches the loop clamp (69) to the PS3 air tube (67) and start bleed valve support bracket (34) and do as follows:
         a TORQUE the bolt (68) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
       5 Install the bolt (59) that attaches the drain tube (62) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the bolt (59) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
       6 Install the four bolts (32) that attach the start bleed valve support bracket (34) to the support bracket (42) and do as follows:
         a TORQUE the four bolts (32) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       7 Install the two bolts (32) that attach the start bleed valve support bracket (34) to the air duct bracket (33) and do as follows:
         a TORQUE the two bolts (32) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       8 Install the two bolts (32) that attach the start bleed tube duct (70) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the two bolts (32) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       9 Install the two bolts (32) that attach the start bleed valve support bracket (34) to the booster anti-ice air tube (75) and do as follows:
         a TORQUE the two bolts (32) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       10 Install the two bolts (65) that attach the support bracket (66) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the two bolts (65) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN ) .
END OF POST SB 72-0190
     (d)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (63), (59), (58), (53), (32), (65), (40) and (56).
       2 If the module package was installed loosely, TORQUE all the bolts (bracket to bracket) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       3 Install the bolt (63) that attaches the loop clamp (60) and the drain tube (62) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the bolt (63) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
       4 Install the bolt (59) that attaches the loop clamp (60) and the drain tube (62) to the support bracket (61) and do as follows:
         a TORQUE the bolt (59) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
       5 Install the bolt (58) that attaches the loop clamp (57) and the drain tube (62) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the bolt (58) to between 67 and 57 lbf.in (0.76 and 0.64 m.daN ) .
       6 Install the bolt (53) that attaches loop clamp (54) and core compartment cooling right side tube (55) to core compartment cooling bracket (52) and do as follows:
         a TORQUE the bolt (53) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
       7 Install the bolt (53) that attaches the loop clamp (54) and core compartment cooling right side tube (55) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the bolt (53) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
       8 Install the two bolts (32) that attach the start bleed valve support bracket (34) to the start bleed valve support bracket (47).
       9 Install the two bolts (32) that attach the start bleed valve support bracket (34) to the air duct bracket (33).
       10 Install the two bolts (32) that attach the start bleed valve support bracket (34) to the start bleed valve support bracket (43).
       11 Install the two bolts (32) that attach the start bleed valve support bracket (34) to the start bleed valve support bracket (48):
         a TORQUE the bolts (32) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       12 Install the two bolts (65) that attach the bracket (61) to the support bracket (66) and do as follows:
         a TORQUE the two bolts (65) to between 37 and 33 lbf.in (0.42 and 0.37 m.daN ) .
       13 Install the two bolts (40) that attach the support bracket (64) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the bolts (40) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
       14 Install the bolt (56) that attaches the loop clamp (54) and support bracket (64) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the bolt (56) to between 70 and 60 lbf.in (0.79 and 0.68 m.daN ) .
     (e)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (40).
       2 Install the two bolts (40) that attach the support bracket (41) to the start bleed valve support bracket (34) and do as follows:
         a TORQUE the two bolts (40) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (f)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (32), (44) and (26).
       2 Attach the support bracket (42) to the start bleed valve support bracket (47) and the support bracket (34) with four bolts (32) and do as follows:
         a TORQUE the two bolts (32) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       3 Attach the support bracket (42) to the support leg bracket (49) and the start bleed valve support bracket (43) with two bolts (44) and do as follows:
         a TORQUE the bolts (44) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       4 Install the retaining strap (50) and 7th stage air tube (51) to the support bracket (42) with two bolts (26) and do as follows:
         a TORQUE the bolts (26) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
     (g)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of the bolts (30), (35), (29), (27) and (32).
       2 If the module package (valve support bracket (31), support bracket (13), support bracket (39) and air duct bracket (33)) was installed loosely, TORQUE all the bolts (bracket to bracket) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       3 Attach the support bracket (31) to the combustion case (6) pad, between fuel nozzles (14) No. 1 and No. 2, with the bolts (30) and do as follows:
         a TORQUE the bolts (30) to between 388 and 332 lbf.in (4.38 and 3.75 m.daN ) .
       4 Attach the air duct bracket (33) to the combustion case (6) pad, between fuel nozzles (14) No. 3 and No. 4, with the bolts (30) and do as follows:
         a TORQUE two bolts (30) to between 388 and 332 lbf.in (4.38 and 3.75 m.daN ) .
       5 Attach the start bleed valve support bracket (34) to the support bracket (33) with two bolts (32) and do as follows:
         a TORQUE the two bolts (32) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       6 Attach the two loop clamps (28) to the support bracket (13) with two bolts (29) and do as follows:
         a TORQUE the two bolts (29) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN ) .
       7 Attach the two bolts (27) to the support bracket (38), support bracket (13) and support bracket (39) and do as follows:
         a TORQUE the two bolts (27) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       8 Install the two bolts (35) that attach the retaining strap (37), 4th stage air manifold (36) and support bracket (39) to the support bracket (13) and do as follows:
         a TORQUE the two bolts (35) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
END OF PRE SB 72-0190
     (h)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of two nuts (17) and bolts (20).
       2 Install the support bracket (15) on the forward side of the combustion case (6) with the nuts (17) and bolts (16) at bolt holes No. 4 and No. 7, aft looking forward and do as follows:
         a TORQUE the nuts (17) to between 243 and 207 lbf.in (2.75 and 2.34 m.daN ) .
       3 Install the two bolts (20) and two loop clamps (21) that attach the left T48 harness (19) to the support bracket (15). Tighten the bolts (20) with your hand.
       4 Install the two bolts (20) and two loop clamps (21) that attach the right T48 harness (22) to the support bracket (15). Tighten the bolts (20) with your hand.
       5 Install the two bolts (20) and two loop clamps (23) that attach the turbine center frame accelerometer (18) to the support bracket (15). Tighten the bolts (20) with your hand.
       6 TORQUE the bolts (20) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN ) .
END OF PRE SB 72-0133
     (i)        1 Apply a layer of engine oil (Material No.CP2442) to the threads of two nuts (17) and the bolts (20).
       2 Install the support bracket (15) on the forward side of the combustion case (6) with the nuts (17) and bolts (16) at bolt holes No. 3 and No. 7, aft looking forward and do as follows:
         a TORQUE the nuts (17) to between 243 and 207 lbf.in (2.75 and 2.34 m.daN ) .
       3 Install the three bolts (20) and three loop clamps (21) that attach the left T48 harness (19) to the support bracket (15). Tighten the bolts (20) with your hand.
       4 Install the two bolts (20) and two loop clamps (21) that attach the right T48 harness (22) to the support bracket (15). Tighten the bolts (20) with your hand.
       5 Install the two bolts (20) and two loop clamps (23) that attach the turbine center frame accelerometer (18) to the support bracket (15). Tighten the bolts (20) with your hand.
       6 TORQUE the bolts (20) to between 38 and 32 lbf.in (0.43 and 0.36 m.daN ) .
END OF POST SB 72-0133
     (j)        1 Apply a layer of engine oil (Material No.CP2442) to the bolts (5) and (11).
       2 Apply a layer of CP2961tiodize grease T8E-H grease/anti-seize to the bolts (9).
       3 Use a small quantity of synthetic beeswax (Material No.CP2635) to hold the new EIPC 72-00-02-05-350 METAL SEAL RING (7) in the groove of the transient bleed air tube (10) forward flange.
       4 Make sure that the orifice plate (8) is installed on the combustion case (6) pad.
       5 Attach the transient bleed air tube (10) to the combustion case (6) with the four bolts (9) and do as follows:
         a Slowly and carefully install the four bolts (9).
         b TORQUE the four bolts (9) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       6 Attach the transient bleed air tube (10) to the support bracket (13) with four bolts (5) and do as follows:
         a TORQUE the four bolts (5) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
       7 Attach the transient bleed air tube (10) to the support bracket (12) with two bolts (11) and do as follows:
         a TORQUE the two bolts (11) to between 124 and 106 lbf.in (1.40 and 1.20 m.daN ) .
END OF PRE SB 72-0190
     (k)        1 Wait to perform the required test and/or inspection until the end of this AMM task.
     (l) For PRE SB 72-0190 and POST SB 72-0190 configurations, do as follows:
       1          a Wait to perform the required test and/or inspection until the end of this AMM task.
END OF PRE SB 72-0190 AND POST SB 72-0190
     (m)        1 Install the TBV (3) (Ref. AMM TASK 75-33-05-400-801) and do as follows:
         a Wait to perform the required test and/or inspection until the end of this AMM task.
END OF PRE SB 72-0190 AND POST SB 72-0190
     (n) For PRE SB 72-0190 and POST SB 72-0190 configurations, do as follows:
       1          a Only if necessary, use the PLIERS - JAWED, SOFT to connect the HJ8A harness (1).
END OF PRE SB 72-0190 AND POST SB 72-0190
     (o) For PRE SB 72-0190 and POST SB 72-0190 configurations, do as follows:
       1          a Only if necessary, use the PLIERS - JAWED, SOFT to connect the HJ8A harness (1).
END OF PRE SB 72-0190 AND POST SB 72-0190