TASK 72-00-32-420-003-D00 LPC/Intermediate Case Module - Install The Tubes And Electrical Harness Raceways, Installation-003 - SBE 79-0087

DMC:V2500-A1-72-00-3200-03E-720A-B|Issue No:003.00|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-A1 and Post SBE 79-0087

Common Information

TASK 72-00-32-420-003-D00 LPC/Intermediate Case Module - Install The Tubes And Electrical Harness Raceways, Installation-003 - SBE 79-0087

General

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

TASK 72-00-32-420-001 (Page Block-401, INSTALLATION-001): Install the LP compressor/intermediate case brackets and the bifurcation panel.

TASK 72-00-32-420-002 (Page Block-401, INSTALLATION-002): Install the LP compressor/intermediate case components.

TASK 72-00-32-420-004-D00 (Page Block-401, INSTALLATION-004, config-004): SBE 79-0087: Install the LP compressor/intermediate case electrical harnesses.

TASK 72-00-32-420-005 (Page Block-401, INSTALLATION-005): 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.

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.

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 the SPM TASK 70-44-00-400-501.

For the torque tightening procedures, refer to the 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 the 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.

Loosely assemble the tubes together and the clip positions during the installation procedure. This will give flexibility and movement and not put strain on the tubes. Where access allows fully torque the tube nuts and then the clip positions when all the tubes are connected and installed. Torque the nuts securing the tubes at the bifurcation panel after all the tubes have been installed. Refer to each specific step for the torque values and procedure at the point of application.

Torque the tube nuts and clips so that the tubes are free of preload and have a minimum clearance of 0.10 in. (2.540 mm) with adjacent components and structure. Refer to the SPM TASK 70-42-01-400-501 to tighten tube end connectors. Make sure that the tubes always have support to prevent unwanted strain.

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

NameManufacturerPart Number / IdentificationQuantityRemark
IAE 1R18001 Wrench0AM53IAE 1R180011
IAE 1R18002 Wrench0AM53IAE 1R180021
IAE 1R18003 Wrench0AM53IAE 1R180031

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-003 SOLVENT, DELETEDX111XCoMat 01-003
CoMat 02-099 LINT-FREE CLOTHX222XCoMat 02-099
CoMat 02-126 LOCKWIREK6835CoMat 02-126
CoMat 02-274 SAFETY CABLE KITLOCALCoMat 02-274
CoMat 02-275 SAFETY CABLE KITLOCALCoMat 02-275
CoMat 04-019 Anti-sieze Thread CompoundIE539CoMat 04-019
CoMat 05-016 GARNET PAPER, 80-GRITLOCALCoMat 05-016
CoMat 05-017 GARNET PAPER, 60 GRITLOCALCoMat 05-017
CoMat 07-038 AIR DRYING ENAMEL00BB6CoMat 07-038
CoMat 08-013 COLD CURING SILICONE COMPOUNDX222XCoMat 08-013
CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANTX222XCoMat 08-014
CoMat 08-032 PRIMERK6835CoMat 08-032
CoMat 08-074 SEALANT, RTV SILICONELOCALCoMat 08-074
CoMat 10-038 PETROLEUM JELLYLOCALCoMat 10-038
CoMat 10-077 APPROVED ENGINE OILSX333XCoMat 10-077
CoMat 10-060 LIQUID PARAFFINLOCALCoMat 10-060
CoMat 10-073 SYNTHETIC GREASE, MoDISULFIDE0AM53CoMat 10-073

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Packing1

24-21-49, 01-106

Packing1

24-21-49, 03-514

Packing1

73-11-47, 02-108

Sealing ring1

73-11-49, 02-108

Sealing ring2

73-11-49, 02-498

Sealing ring1

73-11-49, 02-516

Sealing ring2

73-11-49, 03-098

Sealing ring1

73-11-49, 03-116

Sealing ring2

73-11-49, 03-498

Sealing ring2

73-11-49, 03-508

Packing1
Packing1

73-11-49, 07-508

Sealing ring1

79-21-49, 01-498

Sealing ring1

79-21-49, 02-096

Sealing ring1

79-21-49, 03-098

Sealing ring1

79-21-49, 03-496

Sealing ring1

79-22-49, 10-096

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-32-420-388 Install the EEC and Ignition Supply Harness Raceway (05-100)

    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 ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42, 05-090) at the flange FB with the bolt and the clipnut ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42, 05-101 and ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS 05-108).

    4. Torque the nut and the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    2. SUBTASK 72-00-32-420-389 Install the Vibration Harness Raceway (05-100)

    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 VIBRATION TRANSDUCER JUNCTION BOX 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).

    3. SUBTASK 72-00-32-420-390 Install the Vibration Transducer Raceway (05-300)

    1. Refer to Figure.

    2. Install the raceway to the bracket ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42, 05-830) at the flange FC with the bolt and the nut ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42, 05-309 and ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS 05-316).

    3. Install the raceway to the bracket ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42, 05-280) at the flange FB with the bolt and the nut ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42, 05-301 and ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS 05-308).

    4. Torque the nuts to 36 to 45 lbfin (4 to 5 Nm).

    4. SUBTASK 72-00-32-420-391 Install the Tubes 110 and 174, and the Hoses 175 and 176, the Power Plant Fuel Tubes and Hoses

    1. Refer to Figure, Figure, Figure, Figure and Figure.

    2. Lubricate the threads on the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (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 FUEL SYSTEM TUBES (RIGID)-POWER PLANT (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.

    4. Attach the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-114) to the mounting bracket FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 01-900) with the nut FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-110) and washer 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
      FUEL SYSTEM TUBES (RIGID)-POWER PLANT (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 N. 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 alternatives 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 FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 01-106) to the mounting bracket FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 01-900) with the nut FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 01-110) and washers FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 01-108). Torque the nut to 960 lbf.in to 1120 lbf.in (108 Nm to 135 Nm).

      NOTE

      The washers FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 01-108) are shown above the bracket, but can also be installed one on each side of the bracket as necessary.

    6. Connect the tube 110 to the union FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 01-106). Temporarily attach the tube 110 to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 packing FUEL SYSTEM TUBES (RIGID)-POWER PLANT (73-11-47, 02-108) 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 FUEL SYSTEM TUBES (RIGID)-POWER PLANT (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.

    5. SUBTASK 72-00-32-420-392-A00 Install the Tubes 172 and 117, the Fuel System Tubes (Pre SBE 73-0058)

    1. Refer to Figure and Figure.

    2. Lubricate the new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-485).

    4. Install the seal housing and the fire shield ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-485 and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE 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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-514). Torque the two bolts to 85 to 105 lbf.in (10 to 12 Nm).

    6. Install the restrictor ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-090) and the restrictor retaining ring ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-088) in the tube 117.

    7. Lubricate a new 73-11-49, 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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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. Refer to Figure.

    10. Pre SBE 73-0022 - Install the bolt, the washer, the nut and the clip at the clip position 0306. Refer to Figure.

    11. SBE 73-0022 - Install the bolt, the nut and the clip at the clip position 0306. Refer to Figure.

    12. Torque the tube 172 nut to 566 to 611 lbf.in (64 to 69 Nm) with theIAE 1R18003 Wrench 1 off.

    13. Torque the three bolts V2500-A5-73-11-49-01A-941A-D (73-11-49, 01-106) to 85 to 105 lbf.in (10 to 12 Nm).

    14. Torque the nut at the clip position 0306 to 36 to 45 lbf.in (4 to 5 Nm).

    15. NOTE

      Refer to TASK 72-00-60-420-002 to torque the clip positions 0302 and 0305 (during the tube 110 installation).

      Temporarily tighten the two bolts at the clip positions 0302 and 0305.

    16. Safety the tube 172 nut with CoMat 02-126 LOCKWIRE.

    6. SUBTASK 72-00-32-420-392-B00 Install the Tubes 172, 117 and (02-300), the Fuel System Tubes. (SBE 73-0058)

    1. SBE 73-0058: New tubes with a repositioned restrictor orifice.

    2. Refer to Figure and Figure.

    3. Lubricate the new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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.

    4. Lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-485).

    5. Install the seal housing and the fire shield ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-485 and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE 02-475) on the tube 172.

    6. 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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-514). Torque the two bolts to 85 to 105 lbf.in (10 to 12 Nm).

    7. Install the restrictor ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-288) and the restrictor retaining ring ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-290) in the tube ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-300) .

    8. 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.

    9. Install the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-305) and the three nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-306) which attach the tube ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-300) to the tube 117.

    10. 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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-300).

    11. Install the tube ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-300) to the FCOC and connect the tube 172 to the tube 117. Install the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-316) which attach the tube ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-300) to FCOC.

    12. Install the bolts, the washers, the spacer, the clipnuts, the nut and the clips at the clip positions 0302 and 0305. Refer to Figure.

    13. Pre SBE 73-0022 - Install the bolt, the washer, the nut and the clip at the clip position 0306. Refer to Figure.

    14. SBE 73-0022 - Install the bolt, the nut and the clip at the clip position 0306. Refer to Figure.

    15. Torque the tube 172 nut to 566 to 611 lbf.in (64 to 69 Nm) with theIAE 1R18003 Wrench 1 off.

    16. Torque the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-316) and the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 02-305) to 85 to 105 lbf.in (10 to 12 Nm).

    17. Torque the nut at the clip position 0306 to 36 to 45 lbf.in (4 to 5 Nm).

    18. Temporarily tighten the two bolts at the clip positions 0302 and 0305.

    19. Safety the tube 172 nut with CoMat 02-126 LOCKWIRE.

      NOTE

      Refer to TASK 72-00-60-420-002 to torque the clip positions 0302 and 0305 (during the tube 110 installation).

    7. SUBTASK 72-00-32-420-393 Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    1. Refer to Figure, Figure and Figure.

    2. Lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 03-098) sealing ring 1 off with CoMat 10-077 APPROVED ENGINE OILS. Install the sealing ring on the tube 120.

    3. Pre SBE 71-0110 - 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. SBE 71-0110 - 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).

    5. Lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 03-496) sealing ring 1 off with CoMat 10-077 APPROVED ENGINE OILS. Install the sealing ring on the tube 114.

    6. Install the tube 114 to the FCOC with the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 03-506).

    7. Pre SBE 73-0058 - Install the bolt, the washer, the nut and the clips at the clip position 0304. Refer to Figure.

    8. SBE 73-0058 - Install the bolt, the washer, the nut, the spacer and the clips at the clip position 0304. Refer to Figure.

    9. Torque the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 03-506) to 85 to 105 lbf.in (10 to 12 Nm).

    10. Pre SBE 73-0058 - 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.

    11. SBE 73-0058 - Attach the tube 115 to the tubes 120 and 117 at the clip positions 0319 and 0759 with the bolts, the washers, the spacer, the nuts and the clips. Refer to Figure and Figure.

    12. 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.

    13. Attach the tube 113 to the flange FE bracket with the bolt, the washer, the clipnut and the clip at the clip position 0321 (refer to Figure. Connect the tube 114 to the tube 113.

    14. 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.

    15. Install the tube 177 to the bifurcation panel with the two bolts and the two nuts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 04-514 and OIL-PRESSURE OIL TUBES-ENGINE 04-510). Torque the two nuts to 85 to 105 lbf.in (10 to 12 Nm).

    16. 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.

    17. 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 theIAE 1R18002 Wrench 1 off. Safety the tube 113, 111 and 114 nuts with CoMat 02-126 LOCKWIRE.

    18. 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 and 0304 to 36 to 45 lbf.in (4 to 5 Nm).

    8. SUBTASK 72-00-32-420-394 Install the Tubes 96, 97, 98 and 99, the IDG Cooling Tubes

    1. Refer to Figure.

    2. Lubricate a new ELECTRICAL POWER-IDG OIL COOLING TUBES (24-21-49, 03-514) packing 1 off with CoMat 10-077 APPROVED ENGINE OILS.

    3. Lubricate a new ELECTRICAL POWER-IDG OIL COOLING TUBES (24-21-49, 01-106) packing 1 off with CoMat 10-077 APPROVED ENGINE OILS.

    5. Install the lubricated packing ELECTRICAL POWER-IDG OIL COOLING 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 ELECTRICAL POWER-IDG OIL COOLING 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 ELECTRICAL POWER-IDG OIL COOLING 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 lbfin (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 bolts, the washers, the nuts and the clips 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).

    9. SUBTASK 72-00-32-420-395 Install the Tubes 170 and 171, the Fuel System Tubes

    1. Refer to Figure.

    2. Lubricate the new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 03-485). Install the other sealing ring on the tube 170.

    3. Lubricate the new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 03-506) which attach the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 03-470) and the tube 170 to the IDG FCOC.

    7. Install the two bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 03-506) and the two bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (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 theIAE 1R18003 Wrench 1 off. Safety the tube nut with CoMat 02-126 LOCKWIRE.

    10. SUBTASK 72-00-32-420-396 Install the Tubes 244, 245, 246, 247 and 248, the Cooling Air Tubes (SBE 75-0010)

      SBE 75-0010: Dedicated alternator - Cooling air supply

    1. Refer to Figure, Figure and Figure.

    2. Install the tube 244 to the fan exit pressure boss ENGINE-FAN CASE (72-32-85, 02-100). Hand tighten the tube nut.

    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 positions 1103 and 1122. Torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure and Figure.

    10. Torque the tube 246 nut (at the tube 245) to 283 to 310 lbf.in (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).

    12. SBE 71-0110: Install the bolt, the washer, the nut and the clip at the clip position 0845. Torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

    13. Safety all tube nuts installed in this SUBTASK with CoMat 02-126 LOCKWIRE.

    11. SUBTASK 72-00-32-420-397 Install the Tubes 201, 202 and 203, the Pressure Oil Tubes

    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.

    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.

    9. Torque the tube 203 nuts to 135 to 145 * lbf.in (15.26 to 16.39 Nm).

    12. SUBTASK 72-00-32-420-398 Install the Tubes 205, 206, 207, 208 and 209, the Scavenge Oil Tubes

    1. Refer to 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. Pre SBE 79-0036: 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.

      SBE 79-0036: Connect the tubes 205 to the tube 206. Install the bolts, the washers, the nuts, the spacer and clips at 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. Pre SBE 71-0004: Install the bolts, the washers, the nuts, the clipnut and the clips at clip positions 0907 to 0913. Refer to Figure, Figure, Figure and Figure.

      SBE 71-0004: Install the bolts, the washers, the nuts, the clipnut and the clips at clip position 0907 to 0911, 0972 and 0913. Refer to Figure, 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 and 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).

    11. Install the bolts, the washers, the nut and the clips at the clip positions 0906 and 0904. Torque the nut and the bolt at the clip positions 0906 and 0904 to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

    13. SUBTASK 72-00-32-420-399 Install the Raceway (01-700)

    1. Refer to Figure.

    2. Install the raceway, the bolt and the clipnut at clip position 0556. Refer to Figure.

    3. NOTE

      The installation procedure for clip position 0558 is given in Step, during the installation of tube 149.

      Temporarily attach the raceway to the bracket with the bolt, the washer, the clip and the clipnut at clip position 0558. Tighten the nut. Refer to Figure.

    4. Torque the bolt clip position 0556 to 36 to 45 lbf.in (4 to 5 Nm).

    14. SUBTASK 72-00-32-420-400 Install the Tubes 95, 94, 109 and the Fuel Flow Transmitter to the Fuel System

    1. Refer to Figure. Figure and Figure.

    2. Install the tube 95 to the bifurcation panel with the two bolts and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 08-114 and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE 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. Install the tube 109 and the fuel flow transmitter ENGINE FUEL AND CONTROL-FUEL FLOWMETER (73-31-17, 01-100).

      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. 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. Refer to Figure.

      7. 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).

      8. Torque the six bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 07-506 and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE 07-106) to 85 to 105 lbf.in (10 to 12 Nm).

      9. NOTE

        The fuel flow transmitter bonding lead is attached during installation of the EEC fan harness at the clip position 1462.

        Refer to TASK 72-00-32-420-004-D00 ( INSTALLATION-004, CONFIG-004) for the procedure to install the fuel flow transmitter bonding lead to the raceway bonding lug.

    5. Torque the tube 95 nut to 398 to 434 lbf.in (45 to 49 Nm) with theIAE 1R18001 Wrench 1 off. Safety the tube nut with CoMat 02-126 LOCKWIRE.

    15. SUBTASK 72-00-32-420-401 Install the Electrical Harness Raceway (71-51-50,01-100)

    1. Refer to Figure and Figure.

    2. NOTE

      The installation procedure for clip position 0255 is given in TASK 72-00-60-420-002-A00 (INSTALLATION-003, CONFIG-001) during the installation of tube 103.

      Temporarily attach the raceway to the bracket with the bolt, the washer, the clip and the nut at clip position 0255. Tighten the nut.

    3. Install the bolts, washers, clips, nuts and spacer at clip position 1457. Torque the bolts to 36 to 45 lbf.in (4 to 5 Nm).

      4. Install clip position 1463:

      1. WARNING

        WHEN YOU USE CoMat 01-003 SOLVENT, DELETED 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 BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN (71-51-50, 01-080) with CoMat 01-003 SOLVENT, DELETED. Use a clean lint free cloth moistened with the solvent.

      2. Clean the contact (washer) surfaces of the bolt, the nut and the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN (71-51-50, 01-087), BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN (71-51-50, 01-085) and BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN (71-51-50, 01-088) as given in step (1).

      3. Attach the bonding strap to the raceway with the bolt, the nut and the washer at clip position 1463. Torque the nut to 85 to 105 lbfin (10 to 12 Nm).

    16. SUBTASK 72-00-32-420-402 Install the Bifurcation Tubes 93, 106, 124, 168, 143 and 127

      2. Install the tube 93, the HP fuel servo tube:

      1. Install the tube 93 to the bifurcation panel with the two bolts and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 10-514) and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 10-501).

      2. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      3. Install the tube 106, the FMU fuel tube:

      1. Install the tube 106 to the bifurcation panel with the two bolts and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 20-106) and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 20-102).

      2. Install the bolts, the washers, the spacers, the nuts and the clips at the clip positions 0246, 1065 and 1460.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 0246, 1065 and 1460 to 36 to 45 lbf.in (4 to 5 Nm).

      4. Install the tube 124, the scavenge oil tube:

      1. 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 OIL-SCAVENGE OIL TUBES-ENGINE (79-22-49, 02-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).

      5. Install the Tube 168, the HP Bleed Air Tube:

      1. Install the tube 168 to the bifurcation panel with the two bolts and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 01-506) and AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 01-502).

      2. Install the bolt, the washer, the nut and the clip at the clip position 1435.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip position 1435 to 36 to 45 lbf.in (4 to 5 Nm).

      6. Install the tube 143, the No. 4 bearing cooling air tube.

      1. 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 AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 06-102).

      2. Install the bolt, the washer, the clips, the spacer and the nut at the clip position 1417.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip position 1417 to 36 to 45 lbf.in (4 to 5 Nm).

      7. Install the tube 127, the scavenge oil tube:

      1. Install the tube 127 to the bifurcation panel with the two bolts and the two nuts OIL-SCAVENGE OIL TUBES-ENGINE (79-22-49, 04-106) and OIL-SCAVENGE OIL TUBES-ENGINE (79-22-49, 04-102).

      2. Install the bolts, the washers, the clips and the nuts at the clip positions 1407, 1411, 1412 and 1453.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1407, 1411, 1412 and 1453 to 36 to 45 lbf.in (4 to 5 Nm).

    17. SUBTASK 72-00-32-420-403 Install the Tube 204, the Scavenge Oil Tube

    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 clips and the nuts at the clip positions 1406 and 1430.

    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 both tube nuts with CoMat 02-126 LOCKWIRE.

    7. Torque the nuts at the clip positions 1406 and 1430 to 36 to 45 lbf.in (4 to 5 Nm).

    18. SUBTASK 72-00-32-420-404 Install the Raceway (01-500) (SBE 79-0005)

      SBE 79-0005: Oil - Replace the clipping bracket on the air cooled oil cooler at CP 0533

    1. Refer to Figure.

    2. Pre SBE 79-0005 : Attach the raceway to the bracket OIL-AIR COOLED OIL COOLER (79-21-42, 01-086) with the bolt and the clipnut at the clip position 0533.

    3. SBE 79-0005 : Attach the raceway to the bracket OIL-AIR COOLED OIL COOLER (79-21-42, 01-070) with the bolt and the clipnut at the clip position 0533.

    4. Install the bolt, the washer, the clips, spacer and the nut at the clip position 1429. Refer to Figure.

    5. Torque the bolt at clip position 0533 to 36 to 45 lbf.in (4 to 5 Nm).

    6. Torque the nut at clip position 1429 to 36 to 45 lbf.in (4 to 5 Nm).

    19. SUBTASK 72-00-32-420-405-A00 Install the Bifurcation Tubes 145, 162, 156, 138, 153, 161, 166, 157, 243 and 216 (Pre SBE 73-0198)

      2. Install the tube 145, the HP7 bleed air tube:

      1. 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 AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 08-510).

      2. NOTE

        The nut at the clip position 1440 is torque tightened during the procedure to install tube 189 given in Step.

        Temporarily install the bolt, the washer, the clip and the nut at the clip position 1440.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Tighten the nut at the clip position 1440.

      3. Install the tube 162, the turbine cooling air tube:

      1. 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 AIR-TURBINE COOLING CONTROLLED AIR TUBES (75-23-48, 02-510).

      2. Install the bolt, the washer, the clip and the nut at the clip position 1445.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip position 1445 to 36 to 45 lbf.in (4 to 5 Nm).

      4. Install the tube 156, the HP7 bleed air tube:

      1. 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 AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 12-110).

      2. Install the bolts, the washers, the clips, the spacers and the nuts at the clip positions 1433 and 1436.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip positions 1433 and 1436 to 36 to 45 lbf.in (4 to 5 Nm).

      5. Install the tube 138, the Pb air tube:

      1. Install the tube 138 to the bifurcation panel with the two bolts and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 06-106) and ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 06-102). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).

      6. Install the tube 153, the IP/HP cabin air tube:

      1. Install 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 PNEUMATIC-TUBES-HP BLEED CONTROL AIR (36-11-47, 01-502). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).

      7. Install the tube 161, the HP7 bleed air tube:

      1. Install the tube 161 to the bifurcation panel with the two bolts and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 10-514) and AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 10-510).

      2. Install the bolt, the washer, the clip and the nut at the clip position 1431.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip position 1431 to 36 to 45 lbf.in (4 to 5 Nm).

      8. Install the tube 166, the HP10 bleed air tube:

      1. 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 AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 04-510).

      2. Install the bolts, the washers, the clips, spacers and the nuts at the clip positions 1418 and 1420.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1418 and 1420 to 36 to 45 lbf.in (4 to 5 Nm).

      9. Install the tube 157, the P4.9 air tube:

      1. Install the tube 157 to the bifurcation panel with the two bolts and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 02-506) and ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 02-502).

      2. Install the bolts, the washer, the clips, the spacers and the nuts at the clip positions 1415, 1416, 1427 and 1446.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1415, 1416, 1427 and 1446 to 36 to 45 lbf.in (4 to 5 Nm).

      10. Install the tube 243, the P2.5 air tube:

      1. Install the tube 243 to the bifurcation panel with the two bolts and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 10-106) and ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 10-102).

      2. Install the bolts, the washer, the clips, the spacers and the nuts at the clip positions 1413, 1419 and 1426.

      3. Torque the two nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1413, 1419 and 1426 to 36 to 45 lbf.in (4 to 5 Nm).

      11. Install the tube 216, the core drain tube:

      1. Install the tube 216 to the bifurcation panel with the two bolts and the two nuts POWER PLANT-FUEL DRAIN TUBES-POWER PLANT (71-71-48, 03-410) and POWER PLANT-FUEL DRAIN TUBES-POWER PLANT (71-71-48, 03-415).

      2. Install the bolts, the washer, the clips and the nuts at the clip positions 1454 and 1455.

      3. Torque the two nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1454 and 1455 to 36 to 45 lbf.in (4 to 5 Nm).

    20. SUBTASK 72-00-32-420-405-B00 Install the Bifurcation Tubes 145, 162, 156, 138, 153, 161, 166, 157, 243 and 216 (SBE 73-0198)

      SBE 73-0198: Engine fuel and control - Introduction of re-routed burner to Engine Electronic Controller (EEC) pressure (PB) sense line tube assemblies

    1. Refer to Figure, Figure, Figure, Fig. 72-00-32-990-919-007, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.

      2. Install the tube 145, the HP7 bleed air tube:

      1. Install the tube 145 to the bifurcation panel with the two bolts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 08-514) and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 08-510).

      2. NOTE

        The nut at the clip position 1440 is torque tightened during the procedure to install tube 189 given in Step.

        Temporarily install the bolt, the washer, the clip and the nut at the clip position 1440.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Tighten the nut at the clip position 1440.

      3. Install the tube 162, the turbine cooling air tube:

      1. Install the tube 162 to the bifurcation panel with the two bolts AIR-TURBINE COOLING CONTROLLED AIR TUBES (75-23-48, 02-514) and the two nuts AIR-TURBINE COOLING CONTROLLED AIR TUBES (75-23-48, 02-510).

      2. Install the bolt, the washer, the clip and the nut at the clip position 1445.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip position 1445 to 36 to 45 lbf.in (4 to 5 Nm).

      4. Install the tube 156, the HP7 bleed air tube:

      1. Install the tube 156 to the bifurcation panel with the two bolts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 12-114) and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 12-110).

      2. Install the bolts, the washers, the clips, the spacers and the nuts at the clip positions 1433 and 1436.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip positions 1433 and 1436 to 36 to 45 lbf.in (4 to 5 Nm).

      5. Install the tube 166, the HP bleed air tube:

      1. Install the tube 166 to the bifurcation panel with the two bolts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 04-514) and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 04-510). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).

      6. Install the tube 153, the IP/HP cabin air tube:

      1. Install the tube 153 to the bifurcation panel with the two bolts PNEUMATIC-TUBES-HP BLEED CONTROL AIR (36-11-47, 01-506) and the two nuts PNEUMATIC-TUBES-HP BLEED CONTROL AIR (36-11-47, 01-502). Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).

      7. Install the tube 161, the HP7 bleed air tube:

      1. Install the tube 161 to the bifurcation panel with the two bolts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 10-514) and the two nuts AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 10-510).

      2. Install the bolt, the washer, the clip and the nut at the clip position 1431.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nut at the clip position 1431 to 36 to 45 lbf.in (4 to 5 Nm).

      8. Install the tube 138, the PB air tube:

      1. Install the tube 138 to the bifurcation panel with the two bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 06-106) and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 06-102).

      2. Torque the nuts to 85 to 105 lbf.in (10 to 12 Nm).

      3. Install the bolts, the washers, the clips, spacers and the nuts at the clip positions 1418, 1420 and 1480.

      4. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      5. Torque the nuts at the clip positions 1418, 1420 and 1480 to 36 to 45 lbf.in (4 to 5 Nm).

      9. Install the tube 157, the P4.9 air tube:

      1. Install the tube 157 to the bifurcation panel with the two bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 02-506) and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 02-502).

      2. Install the bolts, the washer, the clips, the spacers and the nuts at the clip positions 1415, 1416, 1427 and 1446.

      3. Torque the nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1415, 1416, 1427 and 1446 to 36 to 45 lbf.in (4 to 5 Nm).

      10. Install the tube 243, the P2.5 air tube:

      1. Install the tube 243 to the bifurcation panel with the two bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 10-106) and the two nuts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 10-102).

      2. Install the bolts, the washer, the clips, the spacers and the nuts at the clip positions 1413, 1419 and 1426.

      3. Torque the two nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1413, 1419 and 1426 to 36 to 45 lbf.in (4 to 5 Nm).

      11. Install the tube 216, the core drain tube:

      1. Install the tube 216 to the bifurcation panel with the two bolts POWER PLANT-FUEL DRAIN TUBES-POWER PLANT (71-71-48, 03-410) and the two nuts POWER PLANT-FUEL DRAIN TUBES-POWER PLANT (71-71-48, 03-415).

      2. Install the bolts, the washer, the clips and the nuts at the clip positions 1454 and 1455.

      3. Torque the two nuts at the bifurcation panel to 85 to 105 lbf.in (10 to 12 Nm).

      4. Torque the nuts at the clip positions 1454 and 1455 to 36 to 45 lbf.in (4 to 5 Nm).

    21. SUBTASK 72-00-32-420-406-A00 Install the Bottom Right Side Tubes 188, 192, 155, 160, 236, 165, 144, 137, 158, 242 and 163 (Pre SBE 73-0198)

      2. Install the tube 188, the ACOC fuel tube:

      1. NOTE

        The nuts at the clip positions 1438 and 1439 are torque tightened during the procedure to install tube 189 given in Step.

        Temporarily attach the tube 188 to the tube 143 at the clip positions 1438 and 1439. Install the bolts, the washers, the clips, the spacers and the nuts at the clip positions 1438 and 1439. Tighten the nuts.

      3. Install the tube 192, the ACOC fuel tube:

      1. Connect the tube 192 to the tube 106.

      2. Install the bolt, the washer, the clip and the nut at the clip position 1443.

      3. Torque the tube 192 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at the clip position 1443 to 36 to 45 lbf.in (4 to 5 Nm).

      4. Install the tube 155, the HP7 bleed air tube:

      1. Connect the tube 155 to the tube 156.

      2. Install the bolt, the washer, the clips, the spacer and the nut at the clip position 1444.

      3. Torque the tube 155 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at the clip position 1444 to 36 to 45 lbf.in (4 to 5 Nm).

      5. Install the tube 160, the HP7 bleed air tube:

      1. Connect the tube 161 to the tube 160.

      2. NOTE

        The nut at the clip position 0589 is torque tightened during the procedure to install tube 242 given in SUBTASK 72-00-32-420-406.

        Temporarily attach the tube 160 to the bracket OIL-AIR COOLED OIL COOLER (79-21-42, 01-350) at the clip position 0589. Install the bolt, the washer, the clips, the spacer and the clipnut at the clip position 0589. Tighten the nut.

      3. Torque the tube 161 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      6. Install the tube 236, the IP/HP cabin air tube:

      1. Connect the tube 236 to the tube 153.

      2. Install the bolt, the washer, the clips and the spacer at the clip position 0581.

      3. Install the bolt, the washer, the clips, the spacer and the nut at the clip position 1432.

      4. Torque the tube 236 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      5. Torque the bolt at the clip position 0581 to 36 to 45 lbf.in (4 to 5 Nm).

      6. Torque the nut at the clip position 1432 to 36 to 45 lbf.in (4 to 5 Nm).

      7. Install the tube 165, the HP10 bleed air tube:

      1. Connect the tube 166 to the tube 165.

      2. Install the bolt, the washer, the clips, the spacer and the nut at the clip position 1409.

      3. Torque the tube 166 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at the clip position 1409 to 36 to 45 lbf.in (4 to 5 Nm).

      8. Install the tube 144, the HP7 bleed air tube:

      1. Connect the tube 145 to the tube 144.

      2. Install the bolt, the washer, the clip and the nut at the clip position 1434.

      3. Torque the tube 145 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at the clip position 1434 to 36 to 45 lbf.in (4 to 5 Nm).

      9. Install the tube 137, the Pb air tube:

      1. Connect the tube 137 to the tube 138.

      2. Install the bolt, the washer, the clips, the spacer and the clipnut at the clip position 0587.

      3. Torque the tube 137 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the bolt at the clip position 0587 to 36 to 45 lbf.in (4 to 5 Nm).

      10. Install the tube 158, the P4.9 air tube:

      1. Connect the tube 157 to the tube 158.

      2. Install the bolt, the washer, the clips, the spacer and the clipnut at the clip position 0588.

      3. Install the bolts, the washers, the clips and the nuts at the clip positions 1422 and 1441.

      4. Torque the tube 157 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      5. Torque the bolt at the clip position 0588 to 36 to 45 lbf.in (4 to 5 Nm).

      6. Torque the nut at the clip positions 1422 and 1441 to 36 to 45 lbf.in (4 to 5 Nm).

      11. Install the tube 242, the P2.5 air tube:

      1. Connect the tube 242 to the tube 243.

      2. Install the bolts, the washers, the clips, the spacers and the clipnut at the clip positions 0584, 0586 and 0589.

      3. Torque the tube 242 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the bolt at the clip positions 0584, 0586 and 0589 to 36 to 45 lbf.in (4 to 5 Nm).

      12. Install the tube 163, the turbine cooling air tube:

      1. Connect the tube 162 to the tube 163.

      2. Install the bolts, the washers, the clips and the spacers at the clip positions 0582, 0583 and 0585.

      3. Install the bolts, the washers, the clips, the spacers and the nuts at the clip positions 1424 and 1428.

      4. Torque the tube 162 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      5. Torque the bolts at the clip positions 0582, 0583 and 0585 to 36 to 45 lbf.in (4 to 5 Nm).

      6. Torque the nuts at the clip positions 1424 and 1428 to 36 to 45 lbf.in (4 to 5 Nm).

    22. SUBTASK 72-00-32-420-406-B00 Install the Bottom Right Side Tubes 188, 192, 155, 160, 236, 165, 144, 137, 158, 242 and 163 (SBE 73-0198)

      SBE 73-0198: Engine fuel and control - Introduction of re-routed burner to Engine Electronic Controller (EEC) pressure (PB) sense line tube assemblies

      2. Install the tube 188, the ACOC fuel tube:

      1. NOTE

        The nuts at the clip positions 1438 and 1439 are torque tightened during the procedure to install tube 189 given in Step.

        Temporarily attach the tube 188 to the tube 143 at the clip positions 1438 and 1439. Install the bolts, the washers, the clips, the spacers and the nuts at the clip positions 1438 and 1439. Tighten the nuts.

      3. Install the tube 192, the ACOC fuel tube:

      1. Connect the tube 192 to the tube 106.

      2. Install the bolt, the washer, the clip and the nut at the clip position 1443.

      3. Torque the tube 192 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at the clip position 1443 to 36 to 45 lbf.in (4 to 5 Nm).

      4. Install the tube 155, the HP7 bleed air tube:

      1. Connect the tube 155 to the tube 156.

      2. Install the bolt, the washer, the clips, the spacer and the nut at the clip position 1444.

      3. Torque the tube 155 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at the clip position 1444 to 36 to 45 lbf.in (4 to 5 Nm).

      5. Install the tube 160, the HP7 bleed air tube:

      1. Connect the tube 161 to the tube 160.

      2. NOTE

        The nut at the clip position 0589 is torque tightened during the procedure to install tube 242 given in step K.

        Temporarily attach the tube 160 to the bracket OIL-AIR COOLED OIL COOLER (79-21-42, 01-350) at the clip position 0589. Install the bolt, the washer, the clips, the spacer and the clipnut at the clip position 0589. Tighten the nut.

      3. Torque the tube 161 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      6. Install the tube 236, the IP/HP cabin air tube:

      1. Connect the tube 236 to the tube 153.

      2. Install the bolt, the washer, the clips and the spacer at the clip position 0581.

      3. Install the bolt, the washer, the clips, the spacer and the nut at the clip position 1432.

      4. Torque the tube 236 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      5. Torque the bolt at the clip position 0581 to 36 to 45 lbf.in (4 to 5 Nm).

      6. Torque the nut at the clip position 1432 to 36 to 45 lbf.in (4 to 5 Nm).

      7. Install the tube 165, the HP10 bleed air tube:

      1. Connect the tube 166 to the tube 165.

      2. Install the bolts, the washesr, the clips and the nuts at the clip positions 0587 and 1422.

      3. Torque the tube 166 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the nuts at the clip position 0587 and 1422 to 36 to 45 lbf.in (4 to 5 Nm).

      8. Install the tube 144, the HP7 bleed air tube:

      1. Connect the tube 145 to the tube 144.

      2. Install the bolt, the washer, the clip and the nut at the clip position 1434.

      3. Torque the tube 145 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the nut at the clip position 1434 to 36 to 45 lbf.in (4 to 5 Nm).

      9. Install the tube 137, the Pb air tube:

      1. Connect the tube 137 to the tube 138.

      2. Install the bolt, the washer, the clips, the spacer and the clipnut at the clip position 1409.

      3. Torque the tube 137 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the bolt at the clip position 1409 to 36 to 45 lbf.in (4 to 5 Nm).

      10. Install the tube 158, the P4.9 air tube:

      1. Connect the tube 157 to the tube 158.

      2. Install the bolt, the washer, the clips, the spacer and the clipnut at the clip position 0588.

      3. Install the bolt, the washer, the clip and the nut at the clip position 1422.

      4. Torque the tube 157 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      5. Torque the bolt at the clip position 0588 to 36 to 45 lbf.in (4 to 5 Nm).

      6. Torque the nut at the clip position 1422 to 36 to 45 lbf.in (4 to 5 Nm).

      11. Install the tube 242, the P2.5 air tube:

      1. Connect the tube 242 to the tube 243.

      2. Install the bolts, the washers, the clips, the spacers and the clipnut at the clip positions 0584, 0586 and 0589.

      3. Torque the tube 242 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      4. Torque the bolt at the clip positions 0584, 0586 and 0589 to 36 to 45 lbf.in (4 to 5 Nm).

      12. Install the tube 163, the turbine cooling air tube:

      1. Connect the tube 162 to the tube 163.

      2. Install the bolts, the washers, the clips and the spacers at the clip positions 0582, 0583 and 0585.

      3. Install the bolts, the washers, the clips, the spacers and the nuts at the clip positions 1424 and 1428.

      4. Torque the tube 162 nut to 159 to 177 lbf.in (18 to 20 Nm). Safety the tube nuts with CoMat 02-126 LOCKWIRE.

      5. Torque the bolts at the clip positions 0582, 0583 and 0585 to 36 to 45 lbf.in (4 to 5 Nm).

      6. Torque the nuts at the clip positions 1424 and 1428 to 36 to 45 lbf.in (4 to 5 Nm).

    23. SUBTASK 72-00-32-420-407-A00 Install the Hose 220 and the Tubes 142, 135 and 159 the Fuel System Air Tubes (Pre SBE 73-0198)

    1. Refer to Figure, Figure, Figure and Figure.

    2. Attach the tube 142 at the clip positions 1053, 1054, 1055, 0794, 0793 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).

    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 ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-800) with the locknut ENGINE FUEL AND CONTROL-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 ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-800) with the locknut ENGINE FUEL AND CONTROL-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.

    7. Torque the locknut ENGINE FUEL AND CONTROL-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 ENGINE FUEL AND CONTROL-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 ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 07-110) and ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 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).

    24. SUBTASK 72-00-32-420-407-B00 Install the Hose 220 and the Tubes 142, 135 and 159, the Fuel System Air Tubes (SBE 73-0198)

      SBE 73-0198: Engine fuel and control - Introduction of re-routed burner to Engine Electronic Controller (EEC) pressure (PB) sense line tube assemblies

    2. Attach the tube 142 at the clip positions 1053, 1054, 1055, 0794, 0793 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).

    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. Attach the tube 135 to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-848) with the bolt, the washer, the clip and the nut at the clip position 1482. Connect the tube 135 to the tube 137.

    5. Install the bolt, the washer, the clip and the nut at the clip position 1481.

    6. Install the bolt, the spacer, the clip and the nut at the clip position 1017.

    7. Install the tube 159 to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-800) with the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-510). Connect the tube 158 to the tube 159.

    8. Torque the locknut ENGINE FUEL AND CONTROL-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 158 nuts to 159 to 177 lbf.in (18 to 20 Nm).

    10. Safety the hose 220, 158 nuts and the locknuts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-510) with CoMat 02-126 LOCKWIRE.

    11. Torque the nuts at the clip position 1017, 1481 and 1482 to 36 to 45 lbf.in. (4 to 5 Nm).

    25. SUBTASK 72-00-32-420-408 Install the Tubes 169 and 125, the Scavenge Oil Tubes

    1. Refer to Figure.

    2. Lubricate a new OIL-SCAVENGE OIL TUBES-ENGINE (79-22-49, 10-096) sealing ring 1 off with CoMat 10-077 APPROVED ENGINE OILS. Install the sealing ring on the tube 169.

    3. Remove the three bolts ENGINE-LP COMP/INTERMEDIATE CASE 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 ENGINE-LP COMP/INTERMEDIATE CASE 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 ENGINE-LP COMP/INTERMEDIATE CASE 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.

    26. SUBTASK 72-00-32-420-409 Install the Right Side Tubes 164, 195, 196, 197, 151, 154 and 241

    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. 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. Install the bolts, the washers, the nuts, the clipnuts and the clips at the clip positions 1024, 1030, 1029 and 0590.

    5. Connect the tube 144 to the tube 196. Connect the tube 196 to the HPC stage 7 solenoid valve (108.8 degrees) AIR-HPC STAGE 7 SOLENOID VALVE (75-32-51, 01-100).

    6. Connect the tube 197 to the tube 160 and the HPC stage 7 solenoid valve (228 degrees) AIR-HPC STAGE 7 SOLENOID VALVE (75-32-51, 01-100).

    7. Install the bolt, the washer, the clipnut and the clips at the clip position 0599.

    8. Connect the tube 154 to the tube 155 and the HPC stage 7 solenoid valve (51.9 degrees) AIR-HPC STAGE 7 SOLENOID VALVE (75-32-51, 01-100).

    9. Connect the tube 236 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).

    10. Install the bolt, the washer, the nut and the clips at the clip position 0591.

    11. Connect the tube 241 to the tube 242, attach the tube 242 to the bracket ENGINE FUEL AND CONTROL-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).

    12. Install the bolts, the washers, the nuts and the clipnut at the clip positions 1051, 0594 and 1026.

    13. 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).

    14. Torque the tube 164, 163, 195, 144, 196, 197, 154 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.

    15. Torque the tube 236 nut to 204 to 221 lbf.in (23 to 25 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.

    16. 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).

    27. SUBTASK 72-00-32-420-410 Install the Tubes 189 and 190, the Fuel System Tubes

    2. NOTE

      It could be necessary to make an adjustment to the position of the tube 188 at the clip positions 1438, 1439 and 1440.

      Connect the tube 189 to the ACOC air modulating valve OIL-AIR COOLED OIL COOLER MODULATING VALVE (79-21-51, 01-100) and the tube 188.

    3. Connect the tube 192 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.

    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 192 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. Torque the nuts at the clip positions 1438, 1439 and 1440 to 36 to 45 lbf.in (4 to 5 Nm).

    9. Safety the tube nuts with CoMat 02-126 LOCKWIRE.

    28. SUBTASK 72-00-32-420-411 Install the Tube 149, the HP Compressor Bleed Air Tube

    2. Connect the tube 149 to the tube 168 and the HPC stage 7 solenoid valve (51.9 degrees) AIR-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.

    4. Install the bolt, the washer, the clipnut and the clips at the clip position 0558.

    5. Torque the tube 149 nut (which connects to the tube 168) to 283 to 310 lbf.in (32 to 35 Nm).

    6. Torque the tube 149 nut (at the solenoid valve) to 204 to 221 lbf.in (23 to 25 Nm).

    7. Torque the nut at the clip position 0580 to 36 to 45 lbf.in (4 to 5 Nm).

    8. Torque the bolt at the clip position 0558 to 36 to 45 lbf.in (4 to 5 Nm).

    9. Safety the tube nuts with CoMat 02-126 LOCKWIRE.

    29. SUBTASK 72-00-32-420-412 Install the Tube 150 to the Turbine Cooling Controlled Air Tube System

    1. Refer to Figure, Figure, Figure, Figure and 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.

    30. SUBTASK 72-00-32-420-413 Install the Tubes 198 and 146 to 148, the HP Compressor (HPC) Bleed Air Tubes

    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.

    5. Connect the tube 198 to the HPC stage 7 solenoid valve (108.8 degrees) AIR-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) AIR-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).

    31. SUBTASK 72-00-32-420-414 Install the Tubes 119 and 122, the Pressure Oil Tubes

    1. Refer to Figure.

    2. Lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 02-096) sealing ring 1 off with CoMat 10-077 APPROVED ENGINE OILS. 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 10-077 APPROVED ENGINE OILS. Install the sealing ring on the tube 122.

    4. Install the tube 119 to the ACOC OIL-AIR COOLED OIL COOLER (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 OIL-PRESSURE OIL TUBES-ENGINE 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).

    32. SUBTASK 72-00-32-420-415 Install the Tubes 128, 126 and 193, the Scavenge Oil Tubes

    1. Refer to Figure, Figure, Figure, Figure and Figure.

    2. Connect the tube 128 to the tube 143.

    3. Connect the tube 127 to the tube 126.

    4. Install the bolts, the washers, the nuts and the clips at the clip positions 0555, 0557 and 1035.

    5. 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 127 tee adapter.

    6. Install the bolt, the washer, the nut and the clip at the clip position 1425.

    7. Torque the tube 128 nut to 204 to 221 lbf.in (23 to 25 Nm).

    8. Torque the tube 127 nut to 566 to 611 lbf.in (64 to 69 Nm) with the IAE 1R18003 Wrench 1 off.

    9. Torque the tube 193 nuts to 159 to 177 lbf.in (18 to 20 Nm).

    10. Safety the tube nuts with CoMat 02-126 LOCKWIRE.

    11. Torque the nuts at the clip positions 0555, 0557, 1035 and 1425 to 36 to 45 lbfin (4 to 5 Nm).

    33. SUBTASK 72-00-32-420-416-A00 Install the Tube 239, the Fuel System Air Tube (Pre SBE 73-0140)

    1. Refer to Figure.

    2. Remove the top two bolts of the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES(73-22-49, 03-805) which attach the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-800) to the bracket POWER PLANT-RELAY BOX (71-51-49, 01-370).

    3. Attach the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-790) to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-800) with the two bolts ENGINE FUEL AND CONTROL-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 ENGINE FUEL AND CONTROL-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 ENGINE FUEL AND CONTROL-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).

    34. SUBTASK 72-00-32-420-416-B00 Install the Tube 239, the Fuel System Air Tube (SBE 73-0140)

      SBE 73-0140: Engine fuel and control - Fuel system air tubes - Introduction of revised EEC pipe-support bracket.

    1. Refer to 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-A00, SUBTASK 72-00-32-420-279-A00 for the installation of bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 03-790).

      Attach the tube 239 to the bracket ENGINE FUEL AND CONTROL-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 lbfin (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 * lbf.in (4.3 to 4.7 Nm). Safety the locknut to the bracket ENGINE FUEL AND CONTROL-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).

    35. SUBTASK 72-00-32-420-417 Fully Torque the Fancase Externals

    1. Fully tighten and torque all the nuts which attach the tubes at the bifurcation panel. Refer to each applicable step in this procedure for the specific torque value.

    2. Fully tighten and torque all the tube nut end connections. Safety all the applicable tube nuts with lockwire. Refer to each applicable step in this procedure.

    3. Fully tighten and torque all the nuts and bolts as applicable for all the clip positions.

    36. SUBTASK 72-00-32-420-418 Seal the Tube Connections at the Bifurcation Panel. (SBE 72-0193)

      SBE 72-0193: Core to fancase interface sealing of the bifurcation panel.

    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.

    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. Dry the primer:

      2. For CoMat 08-032 PRIMER air dry for 60 to 90 minutes.

      9. Apply the sealant:

      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. Cure the sealant:

      1. NOTE

        1. The surface of the compound can be touched after 12 hours.

        2. 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

        1. The surface of the sealant can be touched after 1 or 2 hours.

        2. 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.

    37. 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

    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

    Figure: Install the Tubes 110, 117 and 172

    Install the Tubes 110, 117 and 172

    Figure: Install the Tubes 110, 117 and 172

    Install the Tubes 110, 117 and 172

    Figure: Install the Tubes 110, 117 and 172

    Sheet 3

    Legend
    Install the Tubes 110, 117 and 172

    Sheet 3

    Close

    Figure: Install the Tubes 111, 113, 114, 115, 120 and 177 Pressure Oil Tubes

    Sheet 1

    Legend
    Install the Tubes 111, 113, 114, 115, 120 and 177 Pressure Oil Tubes

    Sheet 1

    Close

    Figure: Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 2

    Legend
    Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 2

    Close

    Figure: Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 3

    Legend
    Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 3

    Close

    Figure: Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 4

    Legend
    Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 4

    Close

    Figure: Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 5

    Legend
    Install the Tubes 111, 113, 114, 115, 120 and 177, the Pressure Oil Tubes

    Sheet 5

    Close

    Figure: Install the Tubes 96 to 98, the IDG Cooling Tubes

    Sheet 1

    Legend
    Install the Tubes 96 to 98, the IDG Cooling Tubes

    Sheet 1

    Close

    Figure: Install the Tubes 96 to 98, the IDG Cooling Tubes

    Sheet 2

    Legend
    Install the Tubes 96 to 98, the IDG Cooling Tubes

    Sheet 2

    Close

    Figure: Install the Tubes 170 and 171, the Fuel System Tubes

    Install the Tubes 170 and 171, the Fuel System Tubes

    Figure: SBE 71-0110: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 1

    Legend
    SBE 71-0110: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 1

    Close

    Figure: SBE 75-0010: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 2

    Legend
    SBE 75-0010: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 2

    Close

    Figure: SBE 75-0010: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 3

    Legend
    SBE 75-0010: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 3

    Close

    Figure: SBE 75-0010: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 4

    Legend
    SBE 75-0010: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 4

    Close

    Figure: Install the Dedicated Alternator Cooling Air Tubes

    Sheet 5

    Legend
    Install the Dedicated Alternator Cooling Air Tubes

    Sheet 5

    Close

    Figure: Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 1

    Legend
    Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 1

    Close

    Figure: Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 2

    Legend
    Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 2

    Close

    Figure: Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 3

    Legend
    Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 3

    Close

    Figure: Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 4

    Legend
    Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 4

    Close

    Figure: Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 5

    Legend
    Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 5

    Close

    Figure: Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 6

    Legend
    Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 6

    Close

    Figure: Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 7

    Legend
    Install the Pressure/Scavenge Oil Tubes to the Left Side of the LP Compressor/Intermediate Case

    Sheet 7

    Close

    Figure: Install the Raceway (71-51-50,01-700)

    Sheet 1

    Legend
    Install the Raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN(71-51-50,01-700)

    Sheet 1

    Close

    Figure: Install the Raceway (71-51-50,01-700)

    Sheet 2

    Legend
    Install the Raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN(71-51-50,01-700)

    Sheet 2

    Close

    Figure: Install the Tubes and the Fuel Flow Transmitter to the Fuel System

    Sheet 1

    Legend
    Install the Tubes and the Fuel Flow Transmitter to the Fuel System

    Sheet 1

    Close

    Figure: Install the tubes and the fuel flow transmitter to the Fuel System

    Install the tubes and the fuel flow transmitter to the Fuel System

    Figure: Install the raceway (71-51-50, 01-100)

    Install the raceway (71-51-50, 01-100)

    Figure: Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 1

    Legend
    Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 1

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 2

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 2

    Close

    Figure: SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 3

    Legend
    SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 3

    Close

    Figure: Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 4

    Legend
    Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 4

    Close

    Figure: SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 5

    Legend
    SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 5

    Close

    Figure: Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 6

    Legend
    Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 6

    Close

    Figure: SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 7

    Legend
    SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 7

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 8

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 8

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 9

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 9

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 10

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 10

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 11

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 11

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 12

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 12

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 13

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 13

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 14

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 14

    Close

    Figure: Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 15

    Legend
    Pre SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 15

    Close

    Figure: SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 16

    Legend
    SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 16

    Close

    Figure: SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 17

    Legend
    SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 17

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 18

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 18

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 19

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 19

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 20

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 20

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 21

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 21

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 22

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Tubes at the Bifurcation Panel

    Sheet 22

    Close

    Figure: Install the Tubes at the Bifurcation Panel

    Sheet 23

    Legend
    Install the Tubes at the Bifurcation Panel

    Sheet 23

    Close

    Figure: Install the raceway (71-51-50, 01-500)

    Install the raceway (71-51-50, 01-500)

    Figure: Install the raceway (71-51-50, 01-500)

    Install the raceway (71-51-50, 01-500)

    Figure: Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 1

    Legend
    Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 1

    Close

    Figure: SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 2

    Legend
    SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 2

    Close

    Figure: Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 3

    Legend
    Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 3

    Close

    Figure: Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 4

    Legend
    Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 4

    Close

    Figure: SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 5

    Legend
    SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 5

    Close

    Figure: SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 6

    Legend
    SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 6

    Close

    Figure: Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 7

    Legend
    Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 7

    Close

    Figure: SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 8

    Legend
    SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 8

    Close

    Figure: Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 9

    Legend
    Pre SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 9

    Close

    Figure: SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 10

    Legend
    SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 10

    Close

    Figure: Install the Bottom Right Side Tubes

    Sheet 11

    Legend
    Install the Bottom Right Side Tubes

    Sheet 11

    Close

    Figure: Install the Bottom Right Side Tubes

    Sheet 12

    Legend
    Install the Bottom Right Side Tubes

    Sheet 12

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 13

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 13

    Close

    Figure: Install the Bottom Right Side Tubes

    Sheet 14

    Legend
    Install the Bottom Right Side Tubes

    Sheet 14

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 15

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 15

    Close

    Figure: Install the Bottom Right Side Tubes

    Sheet 16

    Legend
    Install the Bottom Right Side Tubes

    Sheet 16

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 17

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 17

    Close

    Figure: Install the Bottom Right Side Tubes

    Sheet 18

    Legend
    Install the Bottom Right Side Tubes

    Sheet 18

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 19

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 19

    Close

    Figure: Install the Bottom Right Side Tubes

    Sheet 20

    Legend
    Install the Bottom Right Side Tubes

    Sheet 20

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 21

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Bottom Right Side Tubes

    Sheet 21

    Close

    Figure: Install the Bottom Right Side Tubes

    Sheet 22

    Legend
    Install the Bottom Right Side Tubes

    Sheet 22

    Close

    Figure: Pre SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 1

    Legend
    Pre SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 1

    Close

    Figure: SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 2

    Legend
    SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 2

    Close

    Figure: Pre SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 3

    Legend
    Pre SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 3

    Close

    Figure: SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 4

    Legend
    SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 4

    Close

    Figure: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 5

    Legend
    Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 5

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 6

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 6

    Close

    Figure: SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 7

    Legend
    SBE 73-0198: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 7

    Close

    Figure: Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 8

    Legend
    Install the Tubes 159, 135 and 142, the Fuel System Air Tubes and the Hose 220

    Sheet 8

    Close

    Figure: Install the Tubes 125 and 169, the Scavenge Oil Tubes

    Sheet 1

    Legend
    Install the Tubes 125 and 169, the Scavenge Oil Tubes

    Sheet 1

    Close

    Figure: Install the Tubes 125 and 169, the Scavenge Oil Tubes

    Sheet 2

    Legend
    Install the Tubes 125 and 169, the Scavenge Oil Tubes

    Sheet 2

    Close

    Figure: Install the Right Side Tubes

    Sheet 1

    Legend
    Install the Right Side Tubes

    Sheet 1

    Close

    Figure: Pre SBE 73-0198: Install the Right Side Tubes

    Sheet 2

    Legend
    Pre SBE 73-0198: Install the Right Side Tubes

    Sheet 2

    Close

    Figure: SBE 73-0198: Install the Right Side Tubes

    Sheet 3

    Legend
    SBE 73-0198: Install the Right Side Tubes

    Sheet 3

    Close

    Figure: Pre SBE 73-0198: Install the Right Side Tubes

    Sheet 4

    Legend
    Pre SBE 73-0198: Install the Right Side Tubes

    Sheet 4

    Close

    Figure: SBE 73-0198: Install the Right Side Tubes

    Sheet 5

    Legend
    SBE 73-0198: Install the Right Side Tubes

    Sheet 5

    Close

    Figure: Install the Right Side Tubes

    Sheet 6

    Legend
    Install the Right Side Tubes

    Sheet 6

    Close

    Figure: Install the Right Side Tubes

    Sheet 7

    Legend
    Install the Right Side Tubes

    Sheet 7

    Close

    Figure: Install the Right Side Tubes

    Sheet 8

    Legend
    Install the Right Side Tubes

    Sheet 8

    Close

    Figure: Install the Right Side Tubes

    Sheet 9

    Legend
    Install the Right Side Tubes

    Sheet 9

    Close

    Figure: Pre SBE 73-0198 and SBE 73-0198: Install the Right Side Tubes

    Sheet 10

    Legend
    Pre SBE 73-0198 and SBE 73-0198: Install the Right Side Tubes

    Sheet 10

    Close

    Figure: Install the Right Side Tubes

    Sheet 11

    Legend
    Install the Right Side Tubes

    Sheet 11

    Close

    Figure: Install the Right Side Tubes

    Sheet 12

    Legend
    Install the Right Side Tubes

    Sheet 12

    Close

    Figure: Install the Right Side Tubes

    Sheet 13

    Legend
    Install the Right Side Tubes

    Sheet 13

    Close

    Figure: Install the Right Side Tubes

    Sheet 14

    Legend
    Install the Right Side Tubes

    Sheet 14

    Close

    Figure: Install the Right Side Tubes

    Sheet 15

    Legend
    Install the Right Side Tubes

    Sheet 15

    Close

    Figure: Install the Right Side Tubes

    Sheet 16

    Legend
    Install the Right Side Tubes

    Sheet 16

    Close

    Figure: Install the Tubes 119 and 122, the Pressure Oil Tubes

    Sheet 1

    Legend
    Install the Tubes 119 and 122, the Pressure Oil Tubes

    Sheet 1

    Close

    Figure: Install the Tubes 119 and 122, the Pressure Oil Tubes

    Sheet 2

    Legend
    Install the Tubes 119 and 122, the Pressure Oil Tubes

    Sheet 2

    Close

    Figure: Pre SBE 73-0140: Install the Tube 239, the fuel System Air Tube

    Sheet 1

    Legend
    Pre SBE 73-0140: Install the Tube 239, the fuel System Air Tube

    Sheet 1

    Close

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

    Sheet 2

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

    Sheet 2

    Close

    Figure: Install the tube 239, the Fuel System Air Tube

    Sheet 3

    Legend
    Install the tube 239, the Fuel System Air Tube

    Sheet 3

    Close

    Figure: Seal the Bifurcation Panel and Tubes

    Seal the Bifurcation Panel and Tubes

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the procedure to update note and figure. (17VN302)

Link not Found
Manufacturer Code:00BB6
Enterprise Name:INDESTRUCTIBLE PAINT INC
BU Name:INDESTRUCTIBLE PAINT INC
Street:1 INDEPENDENCE DRIVE
City:MONROE
State:CT
Zip Code:06468
Country:USA
Phone Number:1-203-880-9130
Fax Number:1-203-880-9133
Email:dave@indestructiblepaint.com
Internet:www.indestructiblepaint.com
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: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:K6835
Enterprise Name:MED-LAB LTD
BU Name:MED-LAB LTD
Street:COPELAND ST
City:DERBY
Zip Code:DE1 2PU
Country:GREAT BRITAIN
Phone Number:44-1332-349094
Fax Number:44-1332-371237
Email:sales@med-lab.co.uk
Internet:www.med-lab.co.uk
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X111X
Enterprise Name:N/A – DELETED CONSUMABLE MATERIAL
Manufacturer Code:X222X
Enterprise Name:N/A – REFER TO APPLICABLE COMAT SUFFIX
Manufacturer Code:X333X
Enterprise Name:REFER TO V2500 SB ENG-79-0108
Link not Found
Manufacturer Code:X111X
Supply Number:CoMat 01-003
Type:sp01
Supply Short Name:CoMat 01-003 SOLVENT, DELETED
Supply Name:CoMat 01-003 SOLVENT, DELETED
Specification Groups:
Doc NumberType
wiring harnesses. Where CoMat 01‐003 is specified to clean mechanical components, use one or more of the solvents that SPM TASK 70‐11‐26‐300‐503 specifies as applicable.DELETED. Where CoMat 01‐003 is specified to clean electrical contacts or wiring harnesses, use one or more of the solvents that SPM TASK 70‐11‐57‐110‐501 specifies to clean electrical contacts or
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:X222X
Supply Number:CoMat 02-099
Type:sp01
Supply Short Name:CoMat 02-099 LINT-FREE CLOTH
Supply Name:CoMat 02-099 LINT-FREE CLOTH
Specification Groups:
Doc NumberType
WHERE COMAT 02-099 IS SPECIFIED WITH NO SUFFIX, USE COMAT 02-099A OR COMAT 02-099B.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:K6835
Supply Number:CoMat 02-126
Type:sp01
Supply Short Name:CoMat 02-126 LOCKWIRE
Supply Name:CoMat 02-126 LOCKWIRE
Specification Groups:
Doc NumberType
DTD 189A, 0.028 TO 0.032 IN DIA
Suppliers:
ManufacturerRemarks
K6835
KB362
LOCAL
U06C8
Manufacturer Code:LOCAL
Supply Number:CoMat 02-274
Type:sp01
Supply Short Name:CoMat 02-274 SAFETY CABLE KIT
Supply Name:CoMat 02-274 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
SAE AS3510-0218K (DIA 0,032 IN LENGTH 18IN)
Suppliers:
ManufacturerRemarks
LOCAL
11851
U0419
70958
H7503
SA221
V384V
Manufacturer Code:X111X
Supply Number:CoMat 02-275
Type:sp01
Supply Short Name:CoMat 02-275 SAFETY CABLE KIT
Supply Name:CoMat 02-275 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
Deleted. Use CoMat 02-274.
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:IE539
Supply Number:CoMat 04-019
Type:sp01
Supply Short Name:CoMat 04-019 Anti-sieze Thread Compound
Supply Name:CoMat 04-019 Anti-sieze Thread Compound
Specification Groups:
Doc NumberType
Liqui-Moly NV Thread Compound (MIL-A-907)
Suppliers:
ManufacturerRemarks
IE539
Manufacturer Code:0KHE3
Supply Number:CoMat 05-016
Type:sp01
Supply Short Name:CoMat 05-016 GARNET PAPER, 80-GRIT
Supply Name:CoMat 05-016 GARNET PAPER, 80-GRIT
Specification Groups:
Doc NumberType
GARNET PAPER, CAMI GRIT SIZE 80 GRADE 0 (ANSI B74.18)
Suppliers:
ManufacturerRemarks
0KHE3
1E1X8
LOCAL
C4347
K0993
K2F42
K6835
V571V
Manufacturer Code:0KHE3
Supply Number:CoMat 05-017
Type:sp01
Supply Short Name:CoMat 05-017 GARNET PAPER, 60 GRIT
Supply Name:CoMat 05-017 GARNET PAPER, 60 GRIT
Specification Groups:
Doc NumberType
GARNET PAPER, CAMI GRIT SIZE 60 GRADE 1/2 (ANSI B74.18)
Suppliers:
ManufacturerRemarks
0KHE3
1E1X8
C4347
LOCAL
K0993
K6835
Manufacturer Code:00BB6
Supply Number:CoMat 07-038
Type:sp01
Supply Short Name:CoMat 07-038 AIR DRYING ENAMEL
Supply Name:CoMat 07-038 AIR DRYING ENAMEL
Specification Groups:
Doc NumberType
OMAT:7/22B (RR REF)IP9138 R1
JCR-029 (JAEC REF)
Suppliers:
ManufacturerRemarks
00BB6
K3504
Manufacturer Code:X222X
Supply Number:CoMat 08-013
Type:sp01
Supply Short Name:CoMat 08-013 COLD CURING SILICONE COMPOUND
Supply Name:CoMat 08-013 COLD CURING SILICONE COMPOUND
Specification Groups:
Doc NumberType
If CoMat 08-013 is specified without an asterisk or a letter suffix, use one of the letter suffix alternative materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:X222X
Supply Number:CoMat 08-014
Type:sp01
Supply Short Name:CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT
Supply Name:CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT
Specification Groups:
Doc NumberType
Use the applicable letter suffix material. Refer to SPM TASK 70-36-02-360-501.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:X222X
Supply Number:CoMat 08-032
Type:sp01
Supply Short Name:CoMat 08-032 PRIMER
Supply Name:CoMat 08-032 PRIMER
Specification Groups:
Doc NumberType
DELETED. USE ONE OF THE COMAT 08-032 LETTER SUFFIX ALTERNATIVE MATERIALS.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:CoMat 08-074
Type:sp01
Supply Short Name:CoMat 08-074 SEALANT, RTV SILICONE
Supply Name:CoMat 08-074 SEALANT, RTV SILICONE
Specification Groups:
Doc NumberType
N/A
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:K6835
Supply Number:CoMat 10-038
Type:sp01
Supply Short Name:CoMat 10-038 PETROLEUM JELLY
Supply Name:CoMat 10-038 PETROLEUM JELLY
Specification Groups:
Doc NumberType
SILKOLENE 775 CERTIFIED TO DEF STAN 91-38 GRADE PX-7 OR TO NATO S-743
Suppliers:
ManufacturerRemarks
K6835
U1757
Manufacturer Code:LOCAL
Supply Number:CoMat 10-060
Type:sp01
Supply Short Name:CoMat 10-060 LIQUID PARAFFIN
Supply Name:CoMat 10-060 LIQUID PARAFFIN
Specification Groups:
Doc NumberType
OMAT:CoMat 1020BP TECHNICAL WHITE OIL
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:X222X
Supply Number:CoMat 10-073
Type:sp01
Supply Short Name:CoMat 10-073 SYNTHETIC GREASE, Mo DISULFIDE
Supply Name:CoMat 10-073 SYNTHETIC GREASE, MoDISULFIDE
Specification Groups:
Doc NumberType
DELETED. USE ONE OF THE COMAT 10-073 LETTER SUFFIX ALTERNATIVE MATERIALS.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:X333X
Supply Number:CoMat 10-077
Type:sp01
Supply Short Name:CoMat 10-077 APPROVED ENGINE OILS
Supply Name:CoMat 10-077 APPROVED ENGINE OILS
Specification Groups:
Doc NumberType
For V2500-A1/A5/D5 models - Refer to V2500 Service Bulletin ENG-79-0108
For V2500-E5 model - Refer to Service Bulletin E5-79-0001
Suppliers:
ManufacturerRemarks
X333X
Manufacturer Code:0AM53
Tool Number:IAE 1R18001
Tool Name:IAE 1R18001 Wrench
Manufacturer Code:0AM53
Tool Number:IAE 1R18002
Tool Name:IAE 1R18002 Wrench
Manufacturer Code:0AM53
Tool Number:IAE 1R18003
Tool Name:IAE 1R18003 Wrench