Installation of the Fuel Nozzle for DAC Engines [CFMB]

C. Installation of the HPTACC manifold:
   (1) Remove the protective covers from the open ends of the HPTACC manifold, the open pads of the combustion case and the open ports of the HPTACC valve.
   (2) Install a serviceable C-seal on the upper combustion case pad. Align the holes in the C-seal with the holes in the combustion case pad.
   (3) Install a serviceable C-seal on the lower combustion case pad. Align the holes in the C-seal with the holes in the combustion case pad.
   (4) Put the manifold in position on the upper and lower combustion case pads.
   (5) Apply a thin layer of graphite grease (Material No.CP2101) to the threads and friction surfaces of the bolts.
   (6) Temporarily install the bolts in the manifold and the upper and lower combustion case pads. Do not tighten the bolts at this time.
   (7) Install the bolts, nuts, serviceable gaskets and plate between the forward 4-bolt pad of the HPTACC manifold and the air manifold. Ensure that one gasket is installed on each side of the plate and that the bolt heads are on the forward side. TORQUE the bolts to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (8) Install the V-clamp and a serviceable seal between the large forward port of the HPTACC manifold and the discharge port of the HPTACC valve at 3 o'clock. TORQUE to between 80 and 70 lbf.in (0.90 and 0.79 m.daN ) .
   (9) TORQUE the bolts at the upper combustion case pad to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (10) TORQUE the bolts at the lower combustion case pad to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (11) Wirelock the bolts at the upper combustion case pad with CP8001lockwire 0.032 in. (0.8 mm) dia. or CP8002lockwire 0.032 in. (0.8 mm) dia
   (12) Wirelock the bolts at the lower combustion case pad with CP8001lockwire 0.032 in. (0.8 mm) dia. or CP8002lockwire 0.032 in. (0.8 mm) dia.
   (13) Put the strap clamp on the HPTACC manifold and the support bracket assembly at the fuel nozzle in position 6. Install the bolts, washers and nuts.
   (14) TORQUE the bolts to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (15) Put the strap clamp on the HPTACC manifold at the bracket between flange R and flange S. Install the bolts.
   (16) TORQUE the bolts to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (17) Put the strap clamp on the HPTACC manifold at the bracket at the combustion case end of the upper RH LPT cooling tube. Install the bolts, washers and nuts.
   (18) TORQUE the bolts to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (19) Put the strap clamp on the HPTACC manifold at the bracket at the combustion case end of the lower RH LPT cooling tube. Install the bolts, washers and nuts.
   (20) TORQUE the bolts to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (21) If removed, install the LPTACC tube as follows:
     (a) Remove the protective covers from the open ends of the LPTACC tube and the open end of the LPTACC valve.
     (b) Ensure that the piston ring is installed on the aft end of the LPTACC tube.
     (c) Carefully engage the aft end of the LPTACC tube in the LPTACC air manifold.
     (d) Attach the forward end of the LPTACC tube to the LPTACC valve with the clamp assembly. Hand tighten the nut on the clamp assembly.
     (e) Apply a thin layer of graphite grease (Material No.CP2101) to the threads and friction surfaces of the bolt.
     (f) Attach the LPTACC tube to the support bracket assembly at the fuel nozzle in position 6 with bolt, nut and washer.
     (g) TORQUE the nut to between 110 and 98 lbf.in (1.24 and 1.11 m.daN ) .
     (h) TORQUE the nut on the clamp assembly to between 53 and 47 lbf.in (0.60 and 0.53 m.daN ) .
   (22) If removed, install the start bleed tube as follows:
     (a) Remove the protective covers from the open ends of the start bleed tube, the open pad of the combustion case and the open port of the RACSB valve.
     (b) Apply a thin layer of graphite grease (Material No.CP2101) to the threads and friction surfaces of the bolts.
     (c) Install a serviceable seal on the combustion case pad. Align the holes in the seal with the holes in the pad.
     (d) Put the start bleed tube in position on the combustion case pad. Temporarily install the bolts. Do not torque the bolts at this time.
     (e) Install a serviceable gasket between the end of the start bleed tube and the RACSB valve.
     (f) Install the bolts that attach the start bleed tube to the RACSB valve.
     (g) TORQUE the bolts that attach the start bleed tube to the combustion case pad to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
     (h) TORQUE the bolts that attach the start bleed tube to the RACSB valve to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
     (i) Safety the bolts with CP8001lockwire 0.032 in. (0.8 mm) dia. or CP8002lockwire 0.032 in. (0.8 mm) dia.
     (j) Install the bolts, strap clamp, washers (350) and nuts that attach the start bleed tube to the start bleed tube bracket.
     (k) TORQUE the bolts to between 70 and 55 lbf.in (0.79 and 0.62 m.daN ) .
   (23) If removed, install the strap clamps that attach the LPT cooling tubes, to the LPT cooling brackets at fuel nozzles in positions 3, 8, 13, and 18 as follows:
     (a) Apply a thin layer of graphite grease (Material No.CP2101) to the threads and friction surfaces of the bolts.
     (b) Install the bolts, strap clamps, washers and nuts on the LPT cooling brackets at the nozzle.
   (24) If removed or displaced, install the ignition leads and spark igniters as follows:
     (a) Install the left ignition lead into the clip on the support bracket at the fuel nozzle in position 11.
   (25) If removed, install the right ignition lead into the hinged clamps on the core engine. Turn the attachment bolt of the hinged clamp a quarter of a turn to engage the locking feature, and continue to torque until the ignition lead no longer moves in the clamp .
   (26) Remove protective covers and install the spark igniter (Ref. AMM TASK 74-21-30-400-002).
     (a) If removed, install the engine bleed air ducts (Ref. AMM TASK 36-11-49-400-044) or (Ref. AMM TASK 36-11-49-400-045) or (Ref. AMM TASK 36-11-49-400-046) or (Ref. AMM TASK 36-11-49-400-048).