DMC:V2500-A5-72-00-3200-03C-720A-B|Issue No:002|Issue Date:2019-05-01

Export Control

EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.

Copyright

© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).

Applicability

V2500-A5

Common Information

TASK 72-00-32-420-003-B00 LPC/Intermediate Case Module - Install The Tubes And Electrical Harness Raceways, Installation-003

General

Refer to the TASKS which follow for the other related procedures.

Install the LP compressor/intermediate case brackets and the bifurcation panel by TASK 72-00-32-420-001.

Install the LP compressor/intermediate case components by TASK 72-00-32-420-002.

Install the LP compressor/intermediate case electrical harnesses by TASK 72-00-32-420-004.

Install the pneumatic starter duct, the thermal anti-ice (TAI) duct, the hydraulic tubes, and the EEC cooling ducts to the LP compressor/intermediate case module by TASK 72-00-32-420-005.

Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.

Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS unless other lubricants are referred to in the procedure.

Refer to TASK 72-00-32-420-001 for the position on a raft or bracket of a particular clip position.

Transportation covers/blanks must be removed immediately before the installation of the tubes to the components or the other tubes.

For lockwire data refer to SPM TASK 70-42-05-400-501.

SBE 70-0813.

For safety cable data and procedures refer to SPM TASK 70-42-08-400-501.

Safety the threaded fasteners in the ATA Chapter/Section/Subject 73-22-49 as applicable with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT.

To identify, lubricate and install seal rings refer to SPM TASK 70-44-00-400-501.

For the torque tightening procedures, refer to SPM TASK 70-41-00-400-501 and the SPM TASK 70-41-01-400-501.

Special torque data and assembly tolerances are included in this procedure.

Special torque data is identified with the symbol * after the torque value.

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flanges and attach parts. Use the correct color of the air drying enamel. Refer to SPM TASK 70-38-21-380-501.

The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.

NOTE

To identify the consumable materials refer to the PCI.

SBE 70-0813: Announcement of introduction of safety cable as a preferred method to lockwire.

Safety the threaded fasteners in this TASK with safety cable for the ATA Chapter/Section/Subject detailed in 2. General.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

Name	Manufacturer	Part Number / Identification	Quantity
IAE 1R18001 Wrench	0AM53	IAE 1R18001	1
IAE 1R18002 Wrench	0AM53	IAE 1R18002	1
IAE 1R18003 Wrench	0AM53	IAE 1R18003	1

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 01-002 SOLVENT, DELETED.	X111X	CoMat 01-002
CoMat 02-099 LINT-FREE CLOTH	LOCAL	CoMat 02-099
CoMat 02-126 LOCKWIRE	LOCAL	CoMat 02-126
CoMat 02-274 SAFETY CABLE KIT	LOCAL	CoMat 02-274
CoMat 02-275 SAFETY CABLE KIT	LOCAL	CoMat 02-275
CoMat 04-019 Anti-sieze Thread Compound	IE539	CoMat 04-019
CoMat 05-016 GARNET PAPER, 80-GRIT	LOCAL	CoMat 05-016
CoMat 05-017 GARNET PAPER, 60 GRIT	LOCAL	CoMat 05-017
CoMat 07-038 AIR DRYING ENAMEL	k3504	CoMat 07-038
CoMat 08-013 COLD CURING SILICONE COMPOUND	X222X	CoMat 08-013
CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT	LOCAL	CoMat 08-014
CoMat 08-032 PRIMER	71984	CoMat 08-032
CoMat 08-074 SEALANT, RTV SILICONE	01139	CoMat 08-074
CoMat 10-038 PETROLEUM JELLY	LOCAL	CoMat 10-038
CoMat 10-039 ENGINE OIL	LOCAL	CoMat 10-039
CoMat 10-060 LIQUID PARAFFIN	LOCAL	CoMat 10-060
CoMat 10-073 SYNTHETIC GREASE, MoDISULFIDE	LOCAL	CoMat 10-073
CoMat 10-077 APPROVED ENGINE OILS	X333X	CoMat 10-077

Spares

Name	Manufacturer	Part Number / Identification	Quantity	Remark
Packing			1
Packing			1
Packing			1
Sealing ring			1
Sealing ring			2
Sealing ring			1
Sealing ring			2
Sealing ring			1
Sealing ring			2
Sealing ring			2
Packing			1
Packing			1
Sealing ring			1
Sealing ring			1
Sealing ring			1
Sealing ring			1
Sealing ring			1

Safety Requirements

NONE

Procedure

1. Refer to Figure.
2. Install the raceway to the bracket at the clip position 0890 with the bolt, the washer, the nut and the clip.
3. Install the raceway to the bracket EEC Fan Harness And Ignition Supply Harness (71-51-42, 05-090) at the flange FB with the bolt and the clipnut EEC Fan Harness And Ignition Supply Harness (71-51-42, 05-101 and 05-108).
4. Torque the nut and the bolt to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure.
2. Install the raceway to the bracket VIBRATION TRANSDUCER JUNCTION BOX (77-32-43, 05-080) at the flange FB with the bolt and the nut VIBRATION TRANSDUCER JUNCTION BOX (77-32-43, 05-109 and 05-116).
3. Install the raceway to the bracket at the clip position 0891 with the bolt, the washer, the clipnut and the clip.
4. Torque the two bolts to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure.
2. Install the raceway to the bracket EEC Fan Harness And Ignition Supply Harness (71-51-42, 05-830) at the flange FC with the bolt and the nut EEC Fan Harness And Ignition Supply Harness (71-51-42, 05-309 and 05-316).
3. Install the raceway to the bracket EEC Fan Harness And Ignition Supply Harness (71-51-42, 05-280) at the flange FB with the bolt and the nut EEC Fan Harness And Ignition Supply Harness (71-51-42, 05-301 and 05-308).
4. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. Lubricate the threads on the union Main Fuel Supply Fuel Tubes (73-11-47, 01-106), the tube end of the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-114) and the two nuts Main Fuel Supply Fuel Tubes (73-11-47, 01-110) and FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-110) with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY.
3. Lubricate the threads on the hose 175 and the hose end of the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-114) with CoMat 04-019 Anti-sieze Thread Compound liquid moly NV thread compound.
4. Attach the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-114) to the mounting bracket Main Fuel Supply Fuel Tubes (73-11-47, 01-900) with the nut FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-110) and washers FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-112) and FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-113). Torque the nut 240 lbf.in to 280 lbf.in (27 Nm to 32 Nm).
5. NOTE
  When the tube 110 is connected to the LP fuel pump (TASK 72-00-60-420-002) it can be necessary to make an adjustment of the bracket position, or install a washer between the mounting bracket and the unions Main Fuel Supply Fuel Tubes (73-11-47, 01-106) and FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-114). This is to reduce the possible clearance. Refer to Step for this procedure.
  NOTE
  The washers FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-112 and 02-113) are supplied in two different thicknesses and the two are alternative to each other. The washers are shown above the bracket, but can be installed one on each side of the bracket as necessary.
  Attach the union Main Fuel Supply Fuel Tubes (73-11-47, 01-106) to the mounting bracket Main Fuel Supply Fuel Tubes (73-11-47, 01-900) with the nut Main Fuel Supply Fuel Tubes (73-11-47, 01-110) and washer Main Fuel Supply Fuel Tubes (73-11-47, 01-108). Torque the nut to 960 lbf.in to 1120 lbf.in (108 Nm to 135 Nm).
  NOTE
  The washers Main Fuel Supply Fuel Tubes (73-11-47, 01-108) are shown above the bracket, but can be installed one on each side of the bracket as necessary.
6. Connect the tube 110 to the union Main Fuel Supply Fuel Tubes (73-11-47, 01-106). Temporarily attach the tube 110 to the bracket Control Fuel Tubes (73-11-49, 02-070) at the clip position 0302 (at the flange FC). Install the bolt, the washer, the clipnut and the clip. Tighten the bolt.
7. Tighten the tube 110 connector nut but do not torque the nut at this time.
8. Lubricate a new FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-108) packing 1 off with CoMat 10-060 LIQUID PARAFFIN, or CoMat 10-038 PETROLEUM JELLY. Install the packing on the tube 174.
9. Install the tube 174 to the fuel diverter and return valve Fuel Diverter and Return Valve (73-13-42, 01-100) with the three bolts FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-101). Connect the tube 174 to the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-114). Torque the three bolts to 85 to 105 lbf.in (10 to 12 Nm).
10. Tighten the tube 174 connector nut but do not torque the nut at this time.
11. Connect the hose 175 to the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-114). Tighten the hose 175 connector nut but do not torque the nut at this time.
12. Connect the hose 176 to the union Main Fuel Supply Fuel Tubes (73-11-47, 01-106). Tighten the hose 176 connector nut but do not torque the nut at this time.
13. Attach the hoses 175 and 176 together with the clamp assembly FUEL SYSTEM TUBES (FLEXIBLE)-POWER PLANT (73-11-48, 01-045).
14. Keep the four bolts FUEL SYSTEM TUBES (FLEXIBLE)-POWER PLANT (73-11-48, 01-020), the four washers FUEL SYSTEM TUBES (FLEXIBLE)-POWER PLANT (73-11-48, 01-021), the gasket FUEL SYSTEM TUBES (FLEXIBLE)-POWER PLANT (73-11-48, 01-030), the four bolts FUEL SYSTEM TUBES (FLEXIBLE)-POWER PLANT (73-11-48, 01-050), the four washers FUEL SYSTEM TUBES (FLEXIBLE)-POWER PLANT (73-11-48, 01-051) and the gasket FUEL SYSTEM TUBES (FLEXIBLE)-POWER PLANT (73-11-48, 01-060) for the installation of the hoses on the pylon.
15. Examine and adjust the mounting bracket installation. Do this step after the tube 110 is connected to the LP fuel pump (TASK 72-00-60-420-002). The remaining procedure to torque and adjust the power plant fuel tubes and hoses is given in TASK 72-00-60-420-002.
1. 1. Refer to Figure and Figure.
  2. Lubricate the new Control Fuel Tubes (73-11-49, 02-498) sealing ring 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the two sealing rings on the tube 172.
  3. Lubricate a new Control Fuel Tubes (73-11-49, 02-516) sealing ring 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing ring on the seal housing Control Fuel Tubes (73-11-49, 02-485).
  4. Install the seal housing and the fire shield Control Fuel Tubes (73-11-49, 02-485 and 02-475) on the tube 172.
  5. Install the tube 172 assembly to the fuel diverter and return valve Fuel Diverter and Return Valve (73-13-42, 01-100) with the two bolts Control Fuel Tubes (73-11-49, 02-514). Torque the two bolts to 85 to 105 lbf.in (10 to 12 Nm).
  6. Install the restrictor Control Fuel Tubes (73-11-49, 02-090) and the restrictor retaining ring Control Fuel Tubes (73-11-49, 02-088) in the tube 117.
  7. Lubricate a new73-11-49,02-108 sealing ring 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing ring on the tube 117.
  8. Install the tube 117 to the FCOC and connect the tube 172 to the tube 117. Install the three bolts Control Fuel Tubes (73-11-49, 02-106) which attach the tube 117 to FCOC.
  9. Install the bolts, the washers,the spacer, the clipnuts, the nut and the clips at the clip positions 0302 and 0305.
  10. Install the bolt, the nut and the clip at the clip position 0306.
  11. Torque the tube 172 nut to 566 to 611 lbf.in (64 to 69 Nm) with the IAE 1R18003 Wrench 1 off.
  12. Torque the three bolts Control Fuel Tubes (73-11-49, 02-106) to 85 to 105 lbf.in (10 to 12 Nm).
  13. Torque the nut at the clip position 0306 to 36 to 45 lbf.in (4 to 5 Nm).
  14. Temporarily tighten the two bolts at the clip positions 0302 and 0305.
  15. NOTE
    Refer to TASK 72-00-60-420-002 to torque the clip positions 0302 and 0305 (during the tube 110 installation).
  16. Safety the tube 172 nut with CoMat 02-126 LOCKWIRE.
1. 1. Refer to Figure, Figure and Figure.
  2. Lubricate the new Control Fuel Tubes (73-11-49, 02-498) sealing ring 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the two sealing rings on the tube 172.
  3. Lubricate a new Control Fuel Tubes (73-11-49, 02-516) sealing ring 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing ring on the seal housing Control Fuel Tubes (73-11-49, 02-485).
  4. Install the seal housing and the fire shield Control Fuel Tubes (73-11-49, 02-485 and 02-475) on the tube 172.
  5. Install the tube 172 assembly to the fuel diverter and return valve Fuel Diverter and Return Valve (73-13-42, 01-100) with the two bolts Control Fuel Tubes (73-11-49, 02-514). Torque the two bolts to 85 to 105 lbf.in (10 to 12 Nm).
  6. Install the restrictor Control Fuel Tubes (73-11-49, 02-288) and the restrictor retaining ring Control Fuel Tubes (73-11-49, 02-290) in the tube Control Fuel Tubes (73-11-49, 02-300) .
  7. Lubricate a new 73-11-49,02-308 sealing ring 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing ring on the tube 117.
  8. Install the three bolts Control Fuel Tubes (73-11-49, 02-305) and the three nuts Control Fuel Tubes (73-11-49, 02-306) which attach the tube Control Fuel Tubes (73-11-49, 02-300) to the tube 117.
  9. Lubricate a new 73-11-49,02-314 sealing ring 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing ring on the tube Control Fuel Tubes (73-11-49, 02-300).
  10. Install the tube Control Fuel Tubes (73-11-49, 02-300) to the FCOC and connect the tube 172 to the tube 117. Install the three bolts Control Fuel Tubes (73-11-49, 02-316) which attach the tube Control Fuel Tubes (73-11-49, 02-300) to FCOC.
  11. Install the bolts, the washers,the spacer, the clipnuts, the nut and the clips at the clip positions 0302 and 0305.
  12. Install the bolt, the nut and the clip at the clip position 0306.
  13. Torque the tube 172 nut to 566 to 611 lbf.in (64 to 69 Nm) with theIAE 1R18003 Wrench 1 off.
  14. Torque the three bolts Control Fuel Tubes (73-11-49, 02-316) and the three bolts Control Fuel Tubes (73-11-49, 02-305) to 85 to 105 lbf.in (10 to 12 Nm).
  15. Torque the nut at the clip position 0306 to 36 to 45 lbf.in (4 to 5 Nm).
  16. Temporarily tighten the two bolts at the clip positions 0302 and 0305.
  17. NOTE
    Refer to TASK 72-00-60-420-002 to torque the clip positions 0302 and 0305 (during the tube 110 installation).
  18. Safety the tube 172 nut with CoMat 02-126 LOCKWIRE.
1. Refer to Figure, Figure, Figure, Figure, Figure and Fig. 72-00-32-990-269-006
2. Lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49,03-098) sealing ring 1 off with CoMat 10-039 ENGINE OIL. Install the sealing ring on the tube 120.
3. Install the tube 120 to the FCOC with the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 03-114). Torque the three bolts to 85 to 105 lbf.in (10 to 12 Nm).
4. Lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49,03-496) sealing ring 1 off with CoMat 10-039 ENGINE OIL. Install the sealing ring on the tube 114.
5. Install the tube 114 to the FCOC with the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 03-506).
6. Install the bolt, the washer, the nut and the clips at the clip positions 0304, 1186 and 1187. Refer to Figure and Figure.
7. Torque the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 03-506) to 85 to 105 lbf.in (10 to 12 Nm).
8. Attach the tube 115 to the tubes 120 and 117 at the clip positions 0319 and 0759 with the bolts, the washers, the nuts and the clips. Refer to Figure.
9. Connect the tube 115 to the tube 114. Torque the tube 115 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
10. Attach the tube 113 to the flange FE bracket with the bolt, the washer, the clipnut and the clip at the clip position 0321. Connect the tube 114 to the tube 113. Refer to Figure and Figure.
11. Connect the tube 111 to the tube 113. Install the bolt, the washer, the clipnut and the clip at the clip position 0288 to attach the tube 111 to the flange FE bracket. Refer to Figure.
12. Install the tube 177 to the bifurcation panel with the two bolts and the two nuts Engine Pressure Oil Tubes (79-21-49, 04-514 and Engine Pressure Oil Tubes 04-510). Torque the two nuts to 85 to 105 lbf.in (10 to 12 Nm). Refer to Figure.
13. Connect the tube 113 to the tube 177. Torque the tube 113 nut to 398 to 434 lbf.in (45 to 49 Nm) with the IAE 1R18001 Wrench 1 off.
14. Torque the tube 111 nut to 283 to 310 lbf.in (32 to 35 Nm). Torque the tube 114 nut to 478 to 513 lbf.in (54 to 58 Nm) with the IAE 1R18002 Wrench 1 off. Safety the tube 113, 111 and 114 nuts with CoMat 02-126 LOCKWIRE.
15. NOTE
  The nuts at the clip positions 0319 and 0759 are torque tightened during the procedure given in Step.
  Torque the bolts and the nut at the clip positions 0321, 0288, 1186, 1187 and 0304 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure
2. Lubricate a new ELECTRICAL POWER-IDG OIL COOLING TUBES (24-21-49,03-514) packing 1 off with CoMat 10-039 ENGINE OIL.
3. Lubricate a new IDG Cooling Oil Tubes (24-21-49,01-106) packing 1 off with CoMat 10-039 ENGINE OIL.
4. Lubricate the shanks of the six bolts IDG Cooling Oil Tubes (24-21-49, 01-102 and 03-510) with CoMat 10-073 SYNTHETIC GREASE, MoDISULFIDE.
5. Install the lubricated packing IDG Cooling Oil Tubes (24-21-49, 01-106) on the tube 98. Install the lubricated packing ELECTRICAL POWER-IDG OIL COOLING TUBES (24-21-49, 03-514) on the tube 99.
6. Install the tube 98 and the bracket IDG Cooling Oil Tubes (24-21-49, 01-070) to the IDG FCOC Electrical Power-Fuel Cooled IDG Oil Cooler (24-21-42, 01-100) with the three bolts IDG Cooling Oil Tubes (24-21-49, 01-102). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
7. Install the tube 99 and the bracket ELECTRICAL POWER-IDG OIL COOLING TUBES (24-21-49, 03-470) to the IDG FCOC with the three bolts ELECTRICAL POWER-IDG OIL COOLING TUBES (24-21-49, 03-510). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
8. Connect the tube 96 to the tube 98. Torque the tube 96 nut to 855 to 945 * lbf.in (96.62 to 106.79 Nm).
9. Connect the tube 97 to the tube 99. Torque the tube 97 nut to 620 to 680 * lbf.in (70.10 to 76.84 Nm).
10. Install the bolts, the washers, the clips and the clipnuts at the clip positions 0929 and 0930. Refer to Figure.
11. Install the bolt, the washer, the nut and the clip at the clip position 0289. Refer to Figure.
12. Torque the bolts and the nuts at the clip positions to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure.
2. Lubricate the new Control Fuel Tubes (73-11-49,03-508) sealing ring 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install one of the sealing rings on the seal housing Control Fuel Tubes (73-11-49, 03-485). Install the other sealing ring on the tube 170.
3. Lubricate the new Control Fuel Tubes (73-11-49,03-498) sealing ring 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing rings on the tube 170.
4. Install the seal housing Control Fuel Tubes (73-11-49, 03-485) on the tube 170.
5. Install the tube 170 assembly to the IDG FCOC Electrical Power-Fuel Cooled IDG Oil Cooler (24-21-42, 01-100) and the fuel diverter and return valve Fuel Diverter and Return Valve (73-13-42, 01-100).
6. Install the three bolts Control Fuel Tubes (73-11-49,03-506) which attach the bracket Control Fuel Tubes (73-11-49,03-470) and the tube 170 to the IDG FCOC.
7. Install the two bolts Control Fuel Tubes (73-11-49, 03-514) which attach the seal housing and the tube 170 to the fuel diverter and return valve.
8. Torque the three bolts Control Fuel Tubes (73-11-49,03-506) and the two bolts Control Fuel Tubes (73-11-49,03-514) to 85 to 105 lbf.in (10 to 12 Nm).
9. Install the bolt, the washer, the clipnut and the clip at the clip position 0755 to attach the tube 115 to the bracket Control Fuel Tubes (73-11-49, 03-470). Torque the nuts at the clip positions 0319, 0759 and the bolt at the clip position 0755 to 36 to 45 lbf.in (4 to 5 Nm).
10. Lubricate the new Control Fuel Tubes (73-11-49,03-098) sealing ring 2 off with CoMat to 10-060 liquid paraffin or CoMat 10-038 PETROLEUM JELLY. Install the sealing rings on the tube 171.
11. Lubricate a new Control Fuel Tubes (73-11-49, 03-116) sealing ring 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing ring on the seal housing Control Fuel Tubes (73-11-49, 03-085).
12. Install the seal housing on the tube 171.
13. Install the tube 171 assembly to the IDG FCOC. Connect the tube 171 to the tube 117.
14. Install the three bolts Control Fuel Tubes (73-11-49, 03-114) which attach the tube 171 assembly to the IDG FCOC. Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).
15. Torque the tube 171 nut to 566 to 611 lbf.in (64 to 69 Nm) with the IAE 1R18003 Wrench 1 off. Safety the tube nut with CoMat 02-126 LOCKWIRE.
1. Refer to Figure, Figure and Figure.
2. Install the tube 244 to the fan exit pressure boss ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 03-200). Hand tighten the tube nut. Refer to Figure.
3. Install the bolts, the washers, the clipnuts and the clips at the clip positions 1100, 1114 and 1115. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.
4. Torque the tube 244 nut (at the fan exit pressure boss) to 230 to 248 lbf.in (26 to 28 Nm).
5. Connect the tube 245 to the tube 244. Hand tighten the tube nut.
6. Install the bolts, the washers, the clipnuts and the clips at the clip positions 1101 and 1102. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.
7. Torque the tube 245 nut (at the tube 244) to 283 to 310 lbf.in (32 to 35 Nm).
8. Connect the tube 246 to the tube 245. Hand tighten the tube nut.
9. Install the bolt, the washer, the nut and the clip at the clip position 1103. Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).
10. Torque the tube 246 nut (at the tube 245) to 283 to 310 lbfin (32 to 35 Nm).
11. Connect the tube 247 to the tube 246 and connect the tube 248 to the tube 247 and to the dedicated alternator stator Dedicated Alternator Stator (73-22-38, 01-100). Torque the tube 247 and the tube 248 tube nuts to 283 to 310 lbf.in (32 to 35 Nm). Refer to Figure.
12. Safety all tube nuts installed in this SUBTASK with CoMat 02-126 LOCKWIRE.
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. Install the tube 244 to the fan exit pressure boss ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 03-200). Hand tighten the tube nut. Refer to Figure.
3. Install the bolts, the washers, the clipnuts and the clips at the clip positions 1114 and 1115. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.
4. Torque the tube 244 nut (at the fan exit pressure boss) to 230 to 248 lbf.in (26 to 28 Nm).
5. Connect the tube 246 to the tube 244. Hand tighten the tube nut.
6. Install the bolts, the nut and the clipnuts at the clip positions 1180, 1181 and 1179. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
7. Torque the tube 246 nut (at the tube 245) to 283 to 310 lbf.in (32 to 35 Nm).
8. Connect the tube 247 to the tube 246. Hand tighten the tube nut.
9. Install the bolts, washer, spacer and the nuts at the clip positions 1182 and 1122. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
10. connect the tube 248 to the tube 247 and to the dedicated alternator stator Dedicated Alternator Stator (73-22-38, 01-100). Refer to Figure.
11. Install the bolt, washer and the nut at the clip position 0845. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).
12. Torque the tube 247 and the tube 248 tube nuts to 283 to 310 lbf.in (32 to 35 Nm).
13. Safety all tube nuts installed in this SUBTASK with CoMat 02-126 LOCKWIRE.
1. Refer to Figure, Figure and Figure.
2. Connect the tube 202 to the low oil pressure switch LOW OIL PRESSURE SWITCH (79-34-15, 01-010).
3. Connect the tube 201 to the tube 113 and the tube 202 to the tube 201.
4. Install the bolt, the spacer, the washer, the nut and the clip at the clip position 0914. Refer to Figure.
5. Torque the tube 201 nut (at the tube 113) to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube 201 nut with CoMat 02-126 LOCKWIRE. Refer to Figure.
6. Torque the tube 202 nuts to 135 to 145 * lbf.in (15.26 to 16.39 Nm).
7. Torque the nut at the clip position 0914 to 36 to 45 lbf.in (4 to 5 Nm).
8. Connect the tube 203 to the oil pressure transmitter OIL-OIL PRESSURE TRANSMITTER (79-33-15, 01-010) and the tube 202. Refer to Figure.
9. Torque the tube 203 nuts to 135 to 145 * lbf.in (15.26 to 16.39 Nm).
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure and Figure.
2. Connect the tube 206 to the low oil pressure switch LOW OIL PRESSURE SWITCH (79-34-15, 01-010).
3. Connect the tube 205 to the tube 206. Install the bolts, the washers, the nuts and the clips at the clip positions 0926, 0923 and 0918. Refer to Figure and Figure.
4. Install the bolt, the washer, the clipnut and the clip at the clip position 0917. Refer to Figure.
5. Connect the tube 207 to the tube 206 and the oil pressure transmitter OIL-OIL PRESSURE TRANSMITTER (79-33-15, 01-010).
6. Install the bolts, the washers, the nuts, the clipnut and the clips at the clip positions 0907 to 0913 and 0972. Refer to Figure. Figure and Figure.
7. Torque the tube 206 nut and the tube 205 nut to 135 to 145 * lbf.in (15.26 to 16.39 Nm).
8. Torque the tube 207 nut at the transmitter to 135 to 145 * lbf.in (15.26 to 16.39 Nm). Torque the nut which connects the tube 207 to the tube 206 to 135 to 145 * lbf.in (15.26 to 16.39 Nm).
9. Torque the bolts at the clip positions 0909/0917 and the nuts at the remaining clip positions to 36 to 45 lbf.in (4 to 5 Nm).
10. Connect the tubes 208 and 209 to the scavenge filter differential pressure switch OIL-SCAVENGE FILTER DIFFERENTIAL PRESSURE SWITCH (79-35-16, 01-010). Torque the tube nuts to 135 to 145 * lbf.in (15.26 to 16.39 Nm).
  Refer to Figure.
11. Install the bolt, the washer, the nut and the clips at the clip position 0906. Install the bolt, the washer, the spacer and the clips at the clip position 0904. Torque the nut and the bolt at the clip positions 0906 and 0904 to 36 to 45 lbfin (4 to 5 Nm).
  Refer to Figure.
1. Refer to Figure and Figure.
2. Attach the raceway to the bracket Air Cooled Oil Cooler (ACOC) And Inlet Duct (79-21-42, 01-070) with the bolt and the clipnut at the clip position 0533. Refer to Figure.
3. NOTE
  The installation procedure for the clip position 0246 is given in Step or 72-00-32-420-198-B00, during the installation of the tube 106.
  Attach the raceway to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-070) with the bolt, the washer and the nut at the clip position 0255. Refer to Figure. Tighten the nut.
4. WARNING
  WHEN YOU USE COMAT 01-002 INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.
  Remove the grease, the fingerprints and the unwanted material from the mating surfaces of the raceway lug and the bonding strap Fan Harness Support Raceways (71-51-50, 01-080) with CoMat 01-002 SOLVENT, DELETED.. Use a clean lint free cloth moistened with the solvent.
5. Clean the contact (washer) surfaces of the bolt, the nut and the washer Fan Harness Support Raceways (71-51-50, 01-087 , 01-085 and 01-088) as given in Step.
6. Attach the bonding strap to the raceway with the bolt, the nut and the washer. Torque the nut to 85 to 105 lbf.in (10 to 12 Nm).
7. Torque the bolt at the clip positions 0533 and 0255 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. Install the tube 127 to the bifurcation panel with the two bolts and the two nuts Engine Scavenge Oil Tubes (79-22-49, 04-106 and 04-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
3. Temporarily attach the tube 127 to the bracket Control Fuel Tubes (73-11-49, 22-470) at the clip position 0560, Figure.
4. Install the tube 124 to the bifurcation panel with the two bolts and the two nuts OIL-SCAVENGE OIL TUBES-ENGINE (79-22-49, 02-106 and 02-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
5. Temporarily attach the tube 124 clip to the tube 127 lug at the clip position 0565.
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. Install the tube 168 to the bifurcation panel with the two bolts and the two nuts HPC Bleed Control Air Tubes (75-32-49, 01-506 and 01-502). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm). Refer to Figure.
3. Connect the tube 167 to the tube 168. Temporarily attach the tube 167 to the bracket Control Fuel Tubes (73-11-49, 22-470) at the clip position 0560.
4. Attach the tube 236 to the tube 124 at the clip position 1079 with the bolt, the washer, the spacer and the nut. Refer to Figure.
5. NOTE
  The installation procedure for the two bolts and the two nuts which attach the tube 153 to the bifurcation panel and the tube 236 to the tube 153 is given in TASK 72-00-32-420-004.
  Connect the tube 236 to the tube 153. Temporarily attach the tube 153 to the bifurcation panel with the two bolts and the two nuts PNEUMATIC-TUBES-HP BLEED CONTROL AIR (36-11-47, 01-506 and 01-502).
6. Install the tube 138 to the bifurcation panel with the two bolts and the two nuts Fuel System Air Tubes (73-22-49, 06-106 and 06-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm). Refer to Figure.
7. Install the bolts, the washers, the nuts and the clips at the clip positions 0544, 0561, 0565 and 1118.
  Refer to Figure, Figure and Figure.
8. Install the tube 157 to the bifurcation panel with the two bolts and the two nuts Fuel System Air Tubes (73-22-49, 02-506 and 02-502). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
9. Install the tube 243 to the bifurcation panel with the two bolts and the two nuts Fuel System Air Tubes (73-22-49, 10-106 and 10-102). Torque the two nuts to 85 to 105 lbf.in (10 to 12 Nm).
10. Install the bolt, the washer, the two spacers, the nut and the clips at the clip position 0566. Refer to Figure.
11. Install the bolt, the washer, the spacer, the nut and the clips at the clip position 0569. Refer to Figure.
12. Install the bolt, the washers, the nut and the clips at the clip position 1080. Refer to Figure.
13. Torque the nuts at the clip positions to 36 to 45 lbf.in (4 to 5 Nm).
14. Install the tube 162 to the bifurcation panel with the two bolts and the two nuts AIR-TURBINE COOLING CONTROLLED AIR TUBES (75-23-48, 02-514 and 02-510). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm). Temporarily attach the tube 162 to the tube 127 at the clip position 0564.
1. Refer to Figure, Figure and Figure.
2. Install the tube 95 to the bifurcation panel with the two bolts and the two nuts Control Fuel Tubes (73-11-49, 08-114 and 08-110). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
3. Connect the tube 95 to the tube 94.
4. 1. Lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49,07-508) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY.
  2. Lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49,07-108) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY.
  3. Install the packing ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-508) on the tube 94.
  4. Install the packing ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-108) on the tube 109.
  5. Install the fuel flow transmitter and the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-470) to the tube 94 with the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-506).
  6. NOTE
    The fuel flow transmitter bonding lead is installed during the installation of the EEC fan case harness at clip position 1141.
    Refer to TASK 72-00-32-420-004-B00 (INSTALLATION-004, CONFIG-002) for the procedure to install the fuel flow transmitter bonding lead.
  7. Attach the tube 96 and 97 clips to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-470) at the clip position 0965 with the bolt, the washer and the nut, Figure.
  8. Install the tube 109 and the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-070) to the fuel flow transmitter with the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-106).
  9. Torque the six bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-506 and 07-106) to 85 to 105 lbf.in (10 to 12 Nm).
5. Torque the tube 95 nut to 398 to 434 lbf.in (45 to 49 Nm) with the IAE 1R18001 Wrench 1 off. Safety the tube nut with CoMat 02-126 LOCKWIRE.
1. Refer to Figure and Figure.
2. Connect the tube 205 to the tube 204. Connect the tube 204 to the tube 127.
3. Torque the tube 205 nut (which connects to the tube 204) to 135 to 145 * lbf.in (15.26 to 16.39 Nm).
4. Torque the tube 204 nut (which connects to the tube 127) to 159 to 177 lbf.in (18 to 20 Nm).
5. Safety the tube 204 nut (at the tube 127) with CoMat 02-126 LOCKWIRE.
1. Refer to Figure, Figure and Figure.
2. Connect the tube 205 to the tube 204. Connect the tube 204 to the tube 127.
3. Install the bolts, the washers, the spacers, the nuts and the clips at clip positions 1397 and 1398. Refer to Figure.
4. Torque the tube 205 nut (which connects to the tube 204) to 135 to 145 * lbf.in (15.26 to 16.39 Nm).
5. Torque the tube 204 nut (which connects to the tube 127) to 159 to 177 lbf.in (18 to 20 Nm).
6. Safety the tube 204 nut (at the tube 127) with CoMat 02-126 LOCKWIRE.
7. Torque the nuts at the clip positions to 36 to 45 lbfin (4 to 5 Nm).
1. Refer to Figure, Figure and Figure.
2. Install the tube 106 to the bifurcation panel with the two bolts and the two nuts Control Fuel Tubes (73-11-49, 20-106 and 20-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
3. Install the tube 93 to the bifurcation panel with the two bolts and the two nuts Control Fuel Tubes (73-11-49, 10-514 and 10-510). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
4. Install the bolts, the washers, the spacers, the nuts and the clips at the clip positions 1065 and 0246. Refer to Figure and Figure.
5. Install the bolts, the washers, the nuts and the clips at the clip positions 0758, 0928, 0602 and 0564. Refer to Figure and Figure.
6. Connect the tube 192 to the tube 106. Torque the tube 192 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
7. Torque the nuts at the clip positions 0758, 0928, 1065, 0246, 0602 and 0564 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure and Figure.
2. Install the tube 106 to the bifurcation panel with the two bolts and the two nuts Control Fuel Tubes (73-11-49, 20-106 and 20-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
3. Install the tube 93 to the bifurcation panel with the two bolts and the two nuts Control Fuel Tubes (73-11-49, 10-514 and 10-501). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
4. Install the bolts, the washers, the spacers, the nuts and the clips at the clip positions 1065 and 0246. Refer to Figure and Figure.
5. Install the bolts, the washers, the nuts and the clips at the clip positions 0248, 0758, 1399, 0602, 0564 and 1168. Refer to Figure, Figure and Figure.
6. Connect the tube 192 to the tube 106. Torque the tube 192 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
7. Torque the nuts at the clip positions 0248, 0758, 1399, 1065, 0246, 0602, 0564 and 1168 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure, Figure, Figure and Figure.
2. Refer to Figure, Figure and Figure. Install the tube 143 to the bifurcation panel with the two bolts and the two nuts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 06-106 and 06-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
3. Install the tube 161 to the bifurcation panel with the two bolts and the two nuts HPC Bleed Control Air Tubes (75-32-49, 10-514 and 10-510). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
4. Install the tube 156 to the bifurcation panel with the two bolts and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 12-114 and 12-110). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
5. Install the bolt, the washer, the spacer, the nut and the clips at the clip position 0573. Refer to Figure.
6. Install the bolts, the washers, the nuts and the clips at the clip positions 0570 and 1037. Refer to Figure.
7. Install the tube 166 to the bifurcation panel with the two bolts and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 04-514 and 04-510). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
8. Install the tube 145 to the bifurcation panel with the two bolts and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 08-514 and 08-510). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).
9. Safety the tube 32, 63, 48, 64 and 65 nuts with CoMat 02-126 LOCKWIRE.
10. Install the bolts, the washers, the nuts and the clips at the clip positions 0572, 0574, 1067 and 1171. Refer to Figure and Figure.
11. Torque the nuts at the clip positions to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure and Figure.
2. Install the bolt, the washer, the nut and the clip at the clip position 0563. Refer to Figure.
3. Torque the tube 167 nut to 283 to 310 lbf.in (32 to 35 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
4. Torque the nut at the clip position 0563 to 36 to 45 lbf.in (4 to 5 Nm).
5. Connect the tube 194 to the tube 143.
6. Install the bolt, the washer, the nut and clips at the clip position 0562. Refer to Figure.
7. Torque the tube 194 nut to 204 to 221 lbf.in (23 to 25 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
8. Torque the nut at the clip position 0562 to 36 to 45 lbf.in (4 to 5 Nm).
9. NOTE
  During the installation procedure for the tube 137 hold the tube temporarily at the clip position 0586.
  Connect the tube 138 to the tube 137.
10. Install the bolt, the washers, the nut and the clips at the clip position 0560. Refer to Figure.
11. Torque the tube 138 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
12. Torque the nut at the clip position 0560 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. Connect the tube 145 to the tube 144. Temporarily attach the tube 144 clip at the clip position 0586. Refer to Figure.
3. Connect the tube 157 to the tube 158. Install the bolt, the washer, the spacer, the clipnut and the clips at the clip position 0588. Refer to Figure.
4. Connect the tube 166 to the tube 165. Temporarily attach the tube 165 clip at the clip position 0586. Refer to Figure.
5. Install the bolt, the washers,the spacer, the nut and the clips at the clip position 0537.
  Refer to Figure.
6. Connect the tube 242 to the tube 243. Install the bolts, the washers, the spacers and the clips at the clip positions 0586, 0584 and 0582. Refer to Figure.
7. Install the bolt, the washer, the spacer, the clipnut and the clips at the clip position 0587.
  Refer to Figure.
8. Connect the tube 161 to the tube 160. Refer to Figure.
9. Install the bolt, the washer, the spacer, the clipnut and the clip at the clip position 0589. Refer to Figure.
10. Connect the tube 155 to the tube 156. Refer to Figure.
11. Connect the tube 152 to the tube 236. Temporarily attach the tubes 155 and 152 at the clip position 0585.
12. Connect the tube 192 to the tube 191.
13. Attach the tube 188 to the tube 191 with the bolts, the washers, the nuts and the clips at the clip positions 0578 and 1036.
14. Pre SBE 75-0081: Connect the tube 162 to the tube 163. Refer to Figure. Temporarily attach the tube 163 at the clip position 0585.
15. Install the bolt, the washer, the two spacers, the nut and the clips at the clip position 0576.
16. Install the bolt, the washers, the nut and the clips at the clip position 0577.
17. Install the bolts, the washers and the clips at the clip positions 0585, 0583 and 0581. Refer to Figure.
18. Torque the tube 145, 157, 166, 242, 161, 155, 152, 192 and 162 nuts to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.
19. Torque the bolts at the clip positions 0581 to 0589 to 36 to 45 lbf.in (4 to 5 Nm).
20. Torque the nuts at the clip positions 0537, 0576 to 0578 and 1036 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Fig. 72-00-32-990-277-008.
2. Attach the tube 188 to the tube 192 with the bolt, the washers, the nut and the clip at the clip position 1048. Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure, Figure, Figure and Figure.
2. Attach the tube 142 at the clip positions 1053, 1054, 1055, 0793, 0794 and 0603 with the bolts, the washers, the nuts, the clipnuts and the clips. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure and Figure.
3. Connect the hose 220 to the tube 142. Torque the hose nut to 135 to 145 * lbf.in (15.26 to 16.39 Nm). Temporarily attach the tube 142 to the flange FA bracket with the clip, the two washers and the nut at the clip position 0793. Refer to TASK 72-00-32-420-005 for the configuration of this clip position.
4. Install the tube 135 to the bracket Fuel System Air Tubes (73-22-49, 03-800) with the locknut Fuel System Air Tubes (73-22-49, 07-110). Connect the tube 135 to the tube 137.
5. Install the tube 159 to the bracket Fuel System Air Tubes (73-22-49, 03-800) with the locknut Fuel System Air Tubes (73-22-49, 03-510). Connect the tube 158 to the tube 159.
6. Install the bolts, the washers, the nut, the clipnut and the clips at the clip positions 1027 and 1028. Refer to Figure.
7. Torque the locknut Fuel System Air Tubes (73-22-49, 07-110) to 38 to 42 * lbf.in (4.3 to 4.7 Nm).
8. Torque the locknut Fuel System Air Tubes (73-22-49, 03-510) to 58 to 62 * lbf.in (6.5 to 7.0 Nm).
9. Torque the tube 135 and 158 nuts to 159 to 177 lbf.in (18 to 20 Nm).
10. Safety the hose 220, tube 135, 158 nuts and the locknuts Fuel System Air Tubes (73-22-49, 07-110 and 03-510) with CoMat 02-126 LOCKWIRE.
11. Torque the nut at the clip position 1028 and the bolt at the clip position 1027 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. Lubricate a new Engine Scavenge Oil Tubes (79-22-49, 10-096) sealing ring 1 off with CoMat 10-039 ENGINE OIL. Install the sealing ring on the tube 169.
3. Remove the three bolts LP Compressor (LPC) - Intermediate Structure Module (72-32-00, 01-130) from the LP compressor/intermediate case module.
4. Install the tube 169 to the module and the hot vent tube INTERMEDIATE STRUCTURE OIL & AIR TRANSFER TUBES (72-32-96, 01-100) with the three bolts LP Compressor (LPC) - Intermediate Structure Module (72-32-00, 01-130).
5. Install the bolt, the washer, the clipnut and the clip at the clip position 1016. Refer to Figure.
6. Torque the three bolts LP Compressor (LPC) - Intermediate Structure Module (72-32-00, 01-130) to 85 to 105 lbf.in (10 to 12 Nm).
7. Torque the bolt at the clip position 1016 to 36 to 45 lbf.in (4 to 5 Nm).
8. Connect the tube 125 to the tube 169.
9. Torque the tube 125 nut to 566 to 611 lbf.in (64 to 69 Nm) with the IAE 1R18003 Wrench 1 off. Safety the tube nut with CoMat 02-126 LOCKWIRE.
1. Refer to Figure, Figure, Figure and Figure.
2. Connect the tube 164 to the tube 165 and the HPC stage 10 solenoid valve (81.9 degrees) AIR-HPC STAGE 10 SOLENOID VALVE (75-32-53, 01-400).
3. Pre SBE 75-0081: Connect the tube 163 to the tube 195. Connect the tube 195 to the stage 10 air solenoid valve AIR-STAGE 10 AIR SOLENOID VALVE (75-23-52, 01-100).
4. Pre SBE 75-0081: Install the bolts, the washers, the nuts, the clipnuts and the clips at the clip positions 1024, 1030, 1029 and 0590. Refer to Figure and Figure.
5. SBE 75-0081: Install the bolts, the washers, the nuts, the clipnuts and the clips at the clip positions 1403, 1030, 1029 and 0590. Refer to Figure and Figure.
6. Connect the tube 144 to the tube 196. Connect the tube 196 to the HPC stage 7 solenoid valve (108.8 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100).
7. Connect the tube 197 to the tube 160 and the HPC stage 7 solenoid valve (228 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100).
8. Install the bolt, the washer, the clipnut and the clips at the clip position 0599. Refer to Figure.
9. Connect the tube 154 to the tube 155 and the HPC stage 7 solenoid valve (51.9 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100).
10. Connect the tube 152 to the tube 151. Connect the tube 151 to the HPC stage 7 and 10 air solenoid valve STAGE 10 AIR SOLENOID VALVE (36-11-57, 01-100).
11. Install the bolt, the washer, the nut and the clips at the clip position 0591. Refer to Figure.
12. Connect the tube 241 to the tube 242, attach the tube 242 to the bracket Fuel System Air Tubes (73-22-49, 03-800) with the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 11-110).
13. Install the bolts, the washers, the nuts and the clipnut at the clip positions 1051, 0594 and 1026. Refer to Figure and Figure.
14. Torque the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 11-110) to 38 to 42 * lbf.in (4.3 to 4.7 Nm).
15. Pre SBE 75-0081: Torque the tube 164, 163, 195, 144, 196, 197, 154, 152 and 241 nuts to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts and the locknut with CoMat 02-126 LOCKWIRE.
16. SBE 75-0081: Torque the tube 164, 195, 144, 196, 197, 154, 152 and 241 nuts to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts and the locknut with CoMat 02-126 LOCKWIRE.
17. Torque the tube 151 nut to 204 to 221 lbf.in (23 to 25 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
18. Pre SBE 75-0081: Torque the nuts at the clip positions 1024, 0590, 0594 and 1051 and the bolts at the clip positions 1026, 1029, 1030 and 0599 to 36 to 45 lbf.in (4 to 5 Nm).
19. SBE 75-0081: Torque the nuts at the clip positions 1403, 0590, 0594 and 1051 and the bolts at the clip positions 1026, 1029, 1030 and 0599 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. NOTE
  It could be necessary to make an adjustment to the position of the tube 188 at the clip positions 1036 and 0578.
  Connect the tube 189 to the ACOC air modulating valve Air Cooled Oil Cooler (ACOC) Modulating Valve (79-21-51, 01-100) and the tube 188.
3. Connect the tube 191 to the tube 190. Connect the tube 190 to the ACOC air modulating valve.
4. Install the bolt, the washer, the clips and the clipnut at the clip position 0579. Refer to Figure.
5. Torque the tube 189 nut (at the ACOC air modulating valve) to 142 to 150 lbf.in (16 to 17 Nm).
6. Torque the tube 189 nut (which connects to the tube 188) and the tube 190 and 191 nuts to 159 to 177 lbf.in (18 to 20 Nm).
7. Torque the bolt at the clip position 0579 to 36 to 45 lbf.in (4 to 5 Nm).
8. Safety the tube nuts with CoMat 02-126 LOCKWIRE.
1. Refer to Figure and Figure.
2. Connect the tube 149 to the tube 167 and the HPC stage 7 solenoid valve (51.9 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100).
3. Install the bolt, the washer, the clips and the nut at the clip position 0580. Refer to Figure.
4. Torque the tube 149 nut (which connects to the tube 167) to 283 to 310 lbf.in (32 to 35 Nm).
5. Torque the tube 149 nut (at the solenoid valve) to 204 to 221 lbf.in (23 to 25 Nm).
6. Torque the nut at the clip position 0580 to 36 to 45 lbf.in (4 to 5 Nm).
7. Safety the tube nuts with CoMat 02-126 LOCKWIRE.
1. Refer to Figure.
2. Connect the tube 150 to the tube 149 and the stage 10 air solenoid valve AIR-STAGE 10 AIR SOLENOID VALVE(75-23-52, 01-100). Torque the tube 150 nuts to 204 to 221 lbf.in (23 to 25 Nm).
3. Safety the tube nuts with CoMat 02-126 LOCKWIRE.
1. Refer to Figure and Figure
2. Connect the tube 147 to the HPC stage 10 solenoid valve (81.9 degrees) AIR-HPC STAGE 10 SOLENOID VALVE (75-32-53, 01-400) and the tube 149.
3. Connect the tube 148 to the HPC stage 7 and 10 air solenoid valve STAGE 10 AIR SOLENOID VALVE (36-11-57, 01-100) and the tube 149.
4. Install the bolt, the washer, the nut and the clip at the clip position 1025. Refer to Figure.
5. Connect the tube 198 to the HPC stage 7 solenoid valve (108.8 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100) and the tube 149.
6. Connect the tube 146 to the HPC stage 7 solenoid valve (228 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100) and the tube 149.
7. Torque the tubes 146 to 148 and 198 nuts to 204 to 221 lbf.in (23 to 25 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.
8. Torque the nut at the clip position 1025 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. Lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 02-096) sealing ring 1 off with CoMat 10-039 ENGINE OIL. Install the sealing ring on the tube 119.
3. Lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 01-498) sealing ring 1 off with CoMat 10-039 ENGINE OIL. Install the sealing ring on the tube 122.
4. Install the tube 119 to the ACOC Air Cooled Oil Cooler (ACOC) And Inlet Duct (79-21-42, 01-100) with the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 02-106).
5. Install the tube 122 to the ACOC with the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 01-514).
6. Install the bolts, the washers, the nuts and the clips at the clip position 0220 and 1031.
7. Torque the six bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 02-106 and 79-21-49, 01-514) to 85 to 105 lbf.in (10 to 12 Nm).
8. Torque nuts at the clip positions 0220 and 1031 to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. Connect the tube 128 to the tube 194. Torque the tube 128 nut to 204 to 221 lbf.in (23 to 25 Nm).
3. Safety the tube nut with CoMat 02-126 LOCKWIRE.
4. Connect the tube 127 to the tube 126.
5. Install the bolts, the washers, the nuts and the clips at the clip positions 0555, 0557, 0558 and 1035. Refer to Figure.
6. Connect the tube 193 to the No.4 bearing oil pressure transducer OIL-NO.4 BEARING PRESSURE TRANSDUCER (79-33-16, 01-100) and the tube 126.
7. Torque the tube 127 nut to 566 to 611 lbf.in (64 to 69 Nm) with the IAE 1R18003 Wrench 1 off.
8. Torque the tube 193 nuts to 159 to 177 lbf.in (18 to 20 Nm).
9. Safety the tube nuts with CoMat 02-126 LOCKWIRE.
10. Torque the bolt at the clip position 0558 and the nuts at the remaining clip positions to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. Remove the top two bolts of the three bolts Fuel System Air Tubes (73-22-49, 03-805) which attach the bracket Fuel System Air Tubes (73-22-49, 03-800) to the bracket Ignition Relay Box (71-51-49, 01-370).
3. Attach the bracket Fuel System Air Tubes (73-22-49, 03-790) to the bracket Fuel System Air Tubes (73-22-49, 03-800) with the two bolts Fuel System Air Tubes (73-22-49, 03-805). Torque the two bolts to 85 to 105 lbf.in (10 to 12 Nm).
4. Attach the tube 239 to the flange brackets at the clip positions 1059, 1068, 1073 and 1074 with the bolts, the washers, the nuts and the clipnut. Refer to Figure.
5. Connect the tube 239 nut to the No. 1 outer strut tube connection.
6. Attach the tube 239 to the bracket Fuel System Air Tubes (73-22-49, 03-790) with the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 12-110).
7. Torque the tube 239 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
8. Torque the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49,12-110) to 38 to 42 * lbf.in (4.3 to 4.7 Nm). Safety the locknut to the bracket Fuel System Air Tubes (73-22-49, 03-790) with CoMat 02-126 LOCKWIRE.
9. Torque the bolts at the clip position 1074 and the nuts at the remaining clip positions to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure and Figure.
2. Attach the tube 239 to the flange brackets at the clip positions 1059, 1068, 1073 and 1074 with the bolts, the washers, the nuts and the clipnut. Refer to Figure.
3. Connect the tube 239 nut to the No. 1 outer strut tube connection.
4. NOTE
  Refer to TASK 72-00-32-420-001-B00, SUBTASK 72-00-32-420-278-B00 for the installation of bracket Fuel System Air Tubes (73-22-49, 03-790).
  Attach the tube 239 to the bracket Fuel System Air Tubes (73-22-49, 03-790) with the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 12-110).
5. Torque the tube 239 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
6. Torque the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 12-110) to 38 to 42 * lbfin (4.3 to 4.7 Nm). Safety the locknut to the bracket Fuel System Air Tubes (73-22-49, 03-790) with CoMat 02-126 LOCKWIRE.
7. Torque the bolts at the clip position 1074 and the nuts at the remaining clip positions to 36 to 45 lbf.in (4 to 5 Nm).
1. Refer to Figure.
2. Clean the surface of the joint faces at the bifurcation panel, number 6 strut and the tube joint connections.
3. Refer to the SPM TASK 70-11-26-300-503 for the procedure to locally swab clean.
4. Hand clean the specified surfaces with CoMat 05-016 GARNET PAPER, 80-GRIT or CoMat 05-017 GARNET PAPER, 60 GRIT.
5. Locally swab clean the areas again, refer to the SPM TASK 70-11-26-300-503.
6. NOTE
  Make sure that there are no remaining cleaners in clearances between the bifurcation panel and the fuel tube connectors. The surfaces to be filled must be dry and free from grease, oil and dust.
  Use dry compressed air or CoMat 02-099 LINT-FREE CLOTH , dry the cleaned areas.
7. NOTE
  For CoMat 08-013 COLD CURING SILICONE COMPOUND compound use CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT. For CoMat 08-074 SEALANT, RTV SILICONE use CoMat 08-032 PRIMER.
  Use a soft brush and apply a thin layer of primer to the cleaned areas. You must apply the primer immediately after the surface has been cleaned. You must use the correct sealant with each primer.
8. 1. For CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT air dry for 30 minutes.
  2. For CoMat 08-032 PRIMER air dry for 60 to 90 minutes.
9. 1. Use a spatula to apply the CoMat 08-013 COLD CURING SILICONE COMPOUND compound or CoMat 08-074 SEALANT, RTV SILICONE.
  2. NOTE
    You must apply the sealant in a thin layer, less than 0.120 in. (3.0 mm) diameter.
    Press the sealant into the joint clearances at the specified locations.
10. 1. NOTE
    The surface of the compound can be touched after 12 hours.
    Do not apply a load during this time.
    For CoMat 08-013 COLD CURING SILICONE COMPOUND cold cure at 68 deg F (20 deg C) for 48 hours.
  2. NOTE
    The surface of the sealant can be touched after 1 or 2 hours.
    Do not apply a load during this time.
    For CoMat 08-074 SEALANT, RTV SILICONE cure at 77 deg F (35 deg C) for 24 hours.

Install the EEC and Ignition Supply Harness Raceway

Install the Vibration Harness Raceway

Install the Vibration Transducer Raceway

Install the Tubes 174 and 110, the Power Plant Fuel Tubes

Install the Tubes 110, 117 and 172

Sheet 2

Sheet 3

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 1

Sheet 2

Install the Tubes 170 and 171, the Fuel System Tubes

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 7

Sheet 1

Sheet 2

Sheet 1

Sheet 2

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 7

Sheet 8

Sheet 9

Sheet 10

Sheet 11

Sheet 12

Sheet 13

Sheet 14

Sheet 15

Sheet 16

Sheet 17

Sheet 18

Sheet 19

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 7

Sheet 8

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 1

Sheet 2

Sheet 1

Sheet 2

Sheet 1

Sheet 2

Sheet 3

Sheet 4

Sheet 5

Sheet 6

Sheet 7

Sheet 8

Sheet 9

Sheet 10

Sheet 11

Sheet 12

Sheet 13

Sheet 14

Sheet 1

SBE 73-0140: Install the Tube 239, the Fuel System Air Tube

Sheet 3

Seal the Tube Connections at the Bifurcation Panel.

Requirements After Job Completion

Follow-On Conditions

NONE

Manufacturer Code:	01139
Enterprise Name:	MOMENTIVE PERFORMANCE MATERIALS, INC
BU Name:	MOMENTIVE PERFORMANCE MATERIALS, INC
Street:	260 HUDSON RIVER RD
City:	WATERFORD
State:	NY
Zip Code:	12188
Country:	UNITED STATES OF AMERICA

Manufacturer Code:	0AM53
Enterprise Name:	IAE INTERNATIONAL AERO ENGINES AG
BU Name:	NULL
Building:	SUITE 400
Street:	628 HEBRON AVENUE
City:	GLASTONBURY
State:	CT
Zip Code:	06033
Country:	USA

Manufacturer Code:	71984
Enterprise Name:	DOW SILICONES CORP
BU Name:	DOW SILICONES CORP
Street:	2200 W SALZBURG RD
City:	MIDLAND
State:	MI
Zip Code:	48611
Country:	UNITED STATES OF AMERICA
Phone Number:	1-800-248-2481, 1-989-496-7881, 1-989-496-6000
Fax Number:	1-989-496-6731, 1-989-496-5956
Internet:	www.dowcorning.com

Manufacturer Code:	IE539
Enterprise Name:	THE LOCKREY COMPANY
BU Name:	THE LOCKREY COMPANY
P.O. Box:	1269
City:	Merchantville
Zip Code:	08109
Country:	New Jersey
Phone Number:	856 665 4794

Manufacturer Code:	LOCAL
Enterprise Name:	LOCALLY SUPPLIED

Manufacturer Code:	0AM53
Tool Number:	IAE 1R18001
Tool Name:	IAE 1R18001 Wrench

TASK 72-00-32-420-003-B00 LPC/Intermediate Case Module - Install The Tubes And Electrical Harness Raceways, Installation-003

Export Control

Copyright

Applicability

Common Information

TASK 72-00-32-420-003-B00 LPC/Intermediate Case Module - Install The Tubes And Electrical Harness Raceways, Installation-003

General

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-00-32-420-182 Install the EEC and Ignition Supply Harness Raceway (05-100)

SUBTASK 72-00-32-420-183 Install the Vibration Harness Raceway (05-100)

SUBTASK 72-00-32-420-184 Install the Vibration Transducer Raceway (05-300)

SUBTASK 72-00-32-420-185 Install the Tubes 110 and 174, and the Hoses 175 and 176, the Power Plant Fuel Tubes and Hoses

NOTE

NOTE

NOTE

SUBTASK 72-00-32-420-186-A00 Install the Tubes 172 and 117, the Fuel System Tubes. (Pre SBE 73-0078)

NOTE

SUBTASK 72-00-32-420-186-B00 Install the Tubes 172, 117 and (02-300) the Fuel System Tubes (SBE 73-0078)

NOTE

SUBTASK 72-00-32-420-187 Install the Tubes 120, 115, 114, 113, 111 and 177, the Pressure Oil Tubes

NOTE

SUBTASK 72-00-32-420-188 Install the Tubes 96, 97, 98 and 99, the IDG Cooling Tubes

SUBTASK 72-00-32-420-189 Install the Tubes 170 and 171, the Fuel System Tubes

SUBTASK 72-00-32-420-190-A00 Install the Tubes 244, 245, 246, 247 and 248, the Cooling Air Tubes (Pre SBE 72-0160)

SUBTASK 72-00-32-420-190-B00 Install the Tubes 244, 246, 247 and 248, the Cooling Air Tubes (SBE 72-0160)

SUBTASK 72-00-32-420-191 Install the Tubes 201, 202 and 203, the Pressure Oil Tubes

SUBTASK 72-00-32-420-192 Install the Tubes 205, 206, 207, 208 and 209, the Scavenge Oil Tubes

SUBTASK 72-00-32-420-193 Install the Electrical Harness Raceway (01-100)

NOTE

WARNING

SUBTASK 72-00-32-420-194 Install the Tubes 127 and 124, the Scavenge Oil Tubes

SUBTASK 72-00-32-420-195 Install the Bifurcation Panel Tubes

NOTE

SUBTASK 72-00-32-420-196 Install the Tubes 95, 94, 109 and the Fuel Flow Transmitter to the Fuel System

NOTE

SUBTASK 72-00-32-420-197-A00 Install the Tube 204, the Scavenge Oil Tube (Pre SBE 79-0047)

SUBTASK 72-00-32-420-197-B00 Install the Tube 204, the Scavenge Oil Tube (SBE 79-0047)

SUBTASK 72-00-32-420-198-A00 Install the Tubes 192, 93 and 106 to the Fuel System (Pre SBE 79-0047)

SUBTASK 72-00-32-420-198-B00 Install the Tubes 192,93 and 106 to the Fuel System (SBE 79-0047)

SUBTASK 72-00-32-420-199 Install the Bifurcation Panel Tubes

SUBTASK 72-00-32-420-200 Install the Tubes 137 and 194, the Bottom Right Side Tubes

NOTE

SUBTASK 72-00-32-420-201 Install the Right Side Tubes (Pre SBE 75-0081 and SBE 75-0081)

SUBTASK 72-00-32-420-202 Install the Clip Position 1048

SUBTASK 72-00-32-420-203 Install the Hose 220 and the Tubes 142, 135 and 159, the Fuel System Air Tubes

SUBTASK 72-00-32-420-204 Install the Tubes 169 and 125, the Scavenge Oil Tubes

SUBTASK 72-00-32-420-205 Install the Right Side Tubes (Pre SBE 75-0081 and SBE 75-0081)

SUBTASK 72-00-32-420-206 Install the Tubes 189 and 190, the Fuel System Tubes

NOTE

SUBTASK 72-00-32-420-207 Install the Tube 149, the HP Compressor Bleed Air Tube

SUBTASK 72-00-32-420-208 Install the Tube 150 to the Turbine Cooling Controlled Air Tube System (Pre SBE 75-0081)

SUBTASK 72-00-32-420-209 Install the Tubes 198 and 146 to 148, the HP Compressor (HPC) Bleed Air Tubes

SUBTASK 72-00-32-420-210 Install the Tubes 119 and 122, the Pressure Oil Tubes

SUBTASK 72-00-32-420-211 Install the Tubes 128, 126 and 193, the Scavenge Oil Tubes

SUBTASK 72-00-32-420-212-A00 Install the Tube 239, the Fuel System Air Tube (Pre SBE 73-0140)

SUBTASK 72-00-32-420-212-B00 Install the Tube 239, the Fuel System Air Tube (SBE 73-0140)

NOTE

SUBTASK 72-00-40-420-290 Seal the Tube Connections at the Bifurcation Panel (SBE 72-0193)

NOTE

NOTE

NOTE

NOTE

NOTE

Figure: Install the EEC and Ignition Supply Harness Raceway

Install the EEC and Ignition Supply Harness Raceway

Figure: Install the Vibration Harness Raceway

Install the Vibration Harness Raceway

Figure: Install the Vibration Transducer Raceway

Install the Vibration Transducer Raceway

Figure: Install the Tubes 174 and 110, the Power Plant Fuel Tubes

Install the Tubes 174 and 110, the Power Plant Fuel Tubes

Figure: Install the Tubes 174 and 110, the Power Plant Fuel Tubes

Install the Tubes 174 and 110, the Power Plant Fuel Tubes