TASK 72-00-32-420-004-D00 LPC/Intermediate Case Module - Install The Electrical Harnesses, Installation-004 - SBE 79-0087

DMC:V2500-A1-72-00-3200-04E-720A-B|Issue No:002.00|Issue Date:2013-11-01

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 SBE 79-0087

Common Information

TASK 72-00-32-420-004-D00 LPC/Intermediate Case Module - Install The Electrical Harnesses, Installation-004 - 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 72-00-32-420-003-D00 (Page Block-401, INSTALLATION-003, CONFIG-004): SBE 79-0087: Install the LP compressor/intermediate case tubes and the electrical harness raceways

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.

For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig/item number.

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.

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

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

Safety the threaded fasteners in the ATA Chapter/Section/Subject 71-51-41 and 73-22-49 as applicable with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT.

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

For standard torque data and procedures, refer to the SPM TASK 70-41-00-400-501, SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-400-501.

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

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

Transportation covers/blanks must be removed immediately before the connection of the hoses to the components.

For the connection of electrical connectors, refer to the SPM TASK 70-43-01-400-501.

For the installation of open wire harnesses, refer to the SPM TASK 70-43-02-400-501.

NOTE

  1. To identify the consumable materials refer to the PCI.

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

  3. 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 1R19416 EEC harness wrench0AM53IAE 1R194161

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-003 SOLVENT, DELETEDLOCALCoMat 01-003
CoMat 02-126 LOCKWIRELOCALCoMat 02-126
CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)LOCALCoMat 02-148
CoMat 02-159 LACING TAPELOCALCoMat 02-159
CoMat 02-184 LACING TAPELOCALCoMat 02-184
CoMat 02-202 GLASS CLOTH TAPE, ADHESIVELOCALCoMat 02-202
CoMat 02-274 SAFETY CABLE KITLOCALCoMat 02-274
CoMat 02-275 SAFETY CABLE KITLOCALCoMat 02-275
CoMat 06-086 TIES18992CoMat 06-086
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077
CoMat 01-002 SOLVENT, DELETED.0AM53CoMat 01-002
CoMat 10-039 ENGINE OILLOCALCoMat 10-039

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Packing1

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-32-420-420 Electrical Harness Installation Procedure

    1. Refer to Figure.

    2. During the installation procedure make sure the harnesses are held temporarily along their different lengths. Always install the datum clip positions when you install each electrical connector. This will give the correct installation of the different harnesses and prevent too much strain on the electrical connectors. It will also give the necessary drip loops (the drip loop makes sure moisture or fluids do not go into the electrical connector).

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

    4. Because of the differences between the harness diameters, the specified clip could be too large or too small. You can use a clip from a range of six clips (that have the same part numbers) refer to the IPC (70-40-10). If the harness diameter is between two of the clips in the range, use the larger clip. When you do this use CoMat 02-148 ADHESIVE TAPE (ELECTRICAL) to increase the harness diameter.

    5. Do not remove the special plastic caps from the electrical connectors and receptacles until immediately before they are installed. This will give protection from unwanted fluids or materials.

    6. For the data on the electrical connectors refer to the SPM TASK 70-43-00-400-501 and the SPM TASK 70-43-01-400-501.

    2. SUBTASK 72-00-32-420-421 Install the 400VC to IDG Cable Assembly (24-21-43,01-010)

    1. Refer to Figure, Figure and Figure.

    2. Temporarily attach the IDG cable connector to a safe position on the LP compressor/intermediate case with CoMat 06-086 TIES.

    3. Install the bolts, the washers, the clips and the nuts to attach the cables to the brackets at the clip positions 0883 to 0888. Do not tighten the nuts at this step.

    4. 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.

      Clean the mating faces of the brackets ELECTRICAL POWER-IDG CABLES (24-21-43,01-950), ELECTRICAL POWER-IDG CABLES (24-21-43,01-952) and the clamp ELECTRICAL POWER-IDG CABLES (24-21-43,01-030) with a clean lint free cloth made moist with CoMat 01-003 SOLVENT, DELETED.

    5. Install the clamp ELECTRICAL POWER-IDG CABLES (24-21-43,01-030) on the cables. Attach the clamp to the brackets ELECTRICAL POWER-IDG CABLES (24-21-43,01-950) and ELECTRICAL POWER-IDG CABLES (24-21-43,01-952) with the two bolts and the two nuts ELECTRICAL POWER-IDG CABLES (24-21-43,01-020) and ELECTRICAL POWER-IDG CABLES (24-21-43,01-040) at the clip position 0882.

    6. Clean the mating faces of the bracket ELECTRICAL POWER-IDG CABLES (24-21-43,01-940) and the cable terminals at the earth position with a clean lint free cloth made moist with CoMat 01-002 SOLVENT, DELETED..

    7. Install the two cable terminals to the earth position on the bracket ELECTRICAL POWER-IDG CABLES (24-21-43,01-940). Install the nut ELECTRICAL POWER-IDG CABLES (24-21-43,01-140) on the bracket. Refer to the view on A.

    8. Remove the CoMat 06-086 TIES which hold the IDG cable connector.

    9. Measure dimension B from the IDG cable connector to the clamp at the clip position 0882. Dimension B must be a minimum of 12.25 in. (311 mm) and a maximum of 12.52 in. (318 mm) for the cables T1 and T2. For the cables T3 and N, the minimum dimension B must be 11.8 in. (300 mm) and the maximum must be 12.07 in. (306 mm). Refer to the view on B.

    10. Torque the nuts at the clip positions to 36 to 45 lbfin. (4 to 5 Nm).

    11. Torque the nut ELECTRICAL POWER-IDG CABLES (24-21-43,01-140) at the earth position to 110 * lbfin. (12.4 Nm).

    3. SUBTASK 72-00-32-420-422 Install the Vibration Harnesses/Transducer

    1. Refer to Figure and Figure.

      2. Install the vibration transducer VIBRATION TRANSDUCER (77-32-15,01-100) as follows:

      1. Lightly lubricate a new VIBRATION TRANSDUCER (77-32-15,01-420) packing 1 off with CoMat 10-039 ENGINE OIL.

      2. Install the VIBRATION TRANSDUCER (77-32-15,01-420) Packing 1 off on the baseplate VIBRATION TRANSDUCER (77-32-15,01-410).

      3. Install the three bolts VIBRATION TRANSDUCER (77-32-15,01-400) through the transducer and the baseplate. Install the transducer assembly to the LP compressor/intermediate case. Torque the bolts to 35 to 44 lbfin (3.9 to 4.9 Nm).

      4. Install the bolts, washers, the nut, the clipnut and the clips at the clip positions 0870 to 0875.

      5. Install the transducer bracket to the flange brackets ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42,05-080) and ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42,05-090) with the two bolts and the two nuts VIBRATION TRANSDUCER (77-32-15,01-101) and VIBRATION TRANSDUCER (77-32-15,01-104). Torque the nuts to 36 to 45 lbfin (4 to 5 Nm).

      6. Torque the bolts at the clip positions 0870 to 0874 and the nut at clip position 0875 to 36 to 45 lbfin (4 to 5 Nm).

      3. Install the vibration harnesses VIBRATION TRANSDUCER JUNCTION BOX (77-32-43,01-100) and (77-32-15,02-100) as follows:

      1. Install the bolts, the washers, the nuts and the clips at the clip positions 0876 to 0880.

      2. Align the master keyways then connect and torque the electrical connectors P800 and P801 to J800 and J801 to 14 * lbfin (1.6 Nm), refer to the view on C.

      3. Torque the nuts at the clip positions 0876 to 0880 to 36 to 45 lbfin (4 to 5 Nm).

    4. SUBTASK 72-00-32-420-423 Install the EEC and Ignition Supply Harness (71-51-42,01-005) (Pre SBE 71-0019, Pre SBE 71-0070, SBE 71-0019 and SBE 71-0070)

      SBE 71-0019: Engine - Power Plant - EEC and Ignition Supply Harness, Clipping

      SBE 71-0070: Nacelle - Power Plant - EEC Cooling - Support Brackets - Removal/Replacement

      NOTE

      The EEC and ignition supply harness and the general services harness are previously attached to the terminal module. Refer to the Component Maintenance Manual (CMM-EHC-V2500-1IA) TASK 73-22-34-440-301. Install both these harnesses at the same time. Refer to Step.

    2. Identify the correct datum clip positions as follows:

      0550, 0764, 0781, 0800, 0801, 0802, 0809, 0818, 0819, 0822, 0826, 0863, 0864, 0869, 1001 and 1075.

    3. Connect and torque the electrical connectors 4000KS-J1 and 4000KS-J7 to the EEC ELECTRONIC ENGINE CONTROL (EEC) (73-22-34,01-280) with the IAE 1R19416 EEC harness wrench EEC harness wrench 1 off to 32* lbfin (3.6 Nm).

    4. Use CoMat 06-086 TIES and temporarily attach the harness to the applicable brackets at the clip positions that follow:

      Pre SBE 71-0019: 0550, 0764, 0781, 0800 to 0802, 0809, 0818 to 0823, 0826, 0867 to 0869, 0896, 0897, 1001 and 1075.

      SBE 71-0019 and Pre SBE 71-0070: 0550, 0764, 0781, 0800 to 0802, 0809, 0818 to 0823, 0826, 0867 to 0869, 0896, 0897, 1001 and 1075.

      SBE 71-0019 and SBE 71-007: 0550, 0764, 0781, 0800 to 0802, 0809, 0818 to 0823, 0867 to 0869, 0896, 0897, 1001 and 1075.

    5. Use CoMat 06-086 TIES and temporarily attach the harness to the applicable tube lugs at clip positions 0550 and 0863 to 0866.

      NOTE

      Hole No. 1 is at 12.5 degrees from the engine top position on the flange FB when you look from the rear of the engine.

    6. Install the terminal module ELECTRONIC ENGINE CONTROL (EEC) (73-22-34,01-560) to the hole No. 9 on the flange FB with bolt ELECTRONIC ENGINE CONTROL (EEC) (73-22-34,01-240) and nut ELECTRONIC ENGINE CONTROL (EEC) (73-22-34,01-260). Torque the nut to 85 to 105 lbfin (10 to 12 Nm).

    7. Remove the temporary ties and install the applicable bolts, washers, nuts or clipnuts, spacers and clips at all clip positions.

    8. At the clip positions that have clipnuts/anchor nuts, torque the bolts to 36 to 45 lbfin (4 to 5 Nm).

    9. At the remaining clip position, torque the nuts to 36 to 45 lbfin (4 to 5 Nm).

    10. Make sure that no harness length has too much strain on it. If it is necessary, loosen the bolt or nut at the applicable clip position. Adjust the harness and torque the bolt or nut to that given in the step above.

    5. SUBTASK 72-00-32-420-424 Install the General Services Harness

    1. Refer to Figure, Figure and Figure.

      2. Install the general services harness ELECT HARNESS-LIGHT DUTY-GEN SERVICES HARNESS (71-51-43, 01-005) as follows:

      1. Pre SBN 71-0166: Identify the correct datum clip positions that follow: 0258, 0786, 0787, 0788, 0790, 0791, 0800, 0805, 0809, 0828, 0830 to 0834, 0848, 0850, 0852 to 0855, 0881, 0892, 0903 and 0922.

        SBN 71-0166: Identify the correct datum clip positions that follow: 0258, 0786, 0787, 0788, 0790, 0791, 0800, 0805, 0809, 0830 to 0834, 0848, 0850, 0852 to 0855, 0881, 0892, 0903 and 0922.

      2. Pre SBN 29-0001, Pre SBE 71-0070, Pre SBE 71-0097 and Pre SBE 75-0010: Identify the correct clip positions that follow: 0800 to 0803, 0805 to 0819, 0826 to 0835, 0791, 0773, 0881 0554, 0838 to 0840, 0892, 0847 to 0862, 0258 and 0903.

        SBN 29-0001, SBE 71-0070, SBE 71-0097 and SBE 75-0010: identify the correct clip positions that follow: 0800 to 0803, 0805 to 0819, 0898, 0827 to 0835, 0791, 0773, 0881, 0554, 0838 to 0840, 0892, 0893, 0847 to 0849, 0851 to 0862, 0258 and 0903.

        SBN 71-0166: Identify the correct clip positions that follow: 0800, 0805, 0809, 0791, 1206, 0830 to 0834, 0881, 0852 to 0855, 0903, 0848, 0258 and 0892.

      3. Install the datum clip positions 0805, 0809 and 0800. Refer to Figure, Figure and Figure.

      4. Install the general services harness to the LP compressor/intermediate case, connect and torque the electrical connectors:

        4005EN-A to the No. 4 bearing pressure transducer OIL-NO.4 BEARING PRESSURE TRANSDUCER (79-33-16,01-100) to 12 * lbfin (1.4 Nm). Install the datum clip position 0881. Refer to Figure.

        4100KS-B to the relay box POWER PLANT-RELAY BOX (71-51-49,01-100) to 18 * lbfin (2.0 Nm). Temporarily attach the datum clip position 0791 to the tube lug with CoMat 06-086 TIES. Refer to Figure.

        4003EN-A to the oil pressure transmitter OIL-OIL PRESSURE TRANSMITTER (79-33-15,01-010) to 18 * lbfin (2.0 Nm). Install the datum clip positions 0852 and 0853. Refer to Figure.

        4000EN-A to the low oil pressure switch LOW OIL PRESSURE SWITCH (79-34-15,01-010) to 14 * lbfin (1.6 Nm). Install the datum clip position 0854. Refer to Figure.

        Pre SBN 29-0001: 1074GK-A to the hydraulic pressure switch HYDRAULIC POWER-HYDRAULIC PRESSURE SWITCH (29-11-17,01-010) to 14 * lbfin (1.6 Nm). Install the datum clip position 0850. Refer to Figure.

        SBN 29-0001: 1074GK-A to the hydraulic pressure switch HYDRAULIC POWER-HYDRAULIC PRESSURE SWITCH (29-11-17,01-010) to 14 * lbfin (1.6 Nm).

        4001EN-A to the scavenge filter differential pressure switch OIL-SCAVENGE FILTER DIFFERENTIAL PRESSURE SWITCH (79-35-16, 01-010)to 14 * lbfin (1.6 Nm). Install the datum clip position 0903. Refer to Figure.

      5. Attach the terminals at GP1, GP2, GP3 and GP4 with the 24 bolts and the 24 washers ELECT HARNESS-LIGHT DUTY-GEN SERVICES HARNESS (71-51-43, 01-010 and ELECT HARNESS-LIGHT DUTY-GEN SERVICES HARNESS01-011). Install four of the bolts/washers at the positions which are not used. Torque the bolts to 36 to 45 lbfin (4 to 5 Nm). Refer to Figure and Figure.

      6. Install the bolts, the washers, the clipnuts, the nut and the clips at the datum clip positions 0855, 0848, 0833 and 0831. Torque the bolts to 36 to 45 lbfin (4 to 5 Nm). Refer to Figure and Figure.

      7. Pre SBN 26-0005: Install the remaining datum clip positions 0828, 0830, 0832 and 0834.

        SBN 26-0005: Install the remaining datum clip positions 0830, 0832, 0834 and 1206.

        Refer to Figure, 72-00-32-990-648-016, 72-00-32-990-648-017 and Figure.

      8. Temporarily attach the datum clip positions 0892 and 0258 to the applicable brackets with CoMat 06-086 TIES. Refer to Figure.

      9. Install the bolts, the washers, the nuts, the clipnuts and the clips at the remaining clip positions.

        Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Fig. 72-00-32-990-648-021.

      10. Torque the bolts to 36 to 45 lbfin (4 to 5 Nm) in the anchor/clipnuts at the clip positions.

      11. At the remaining clip positions torque the nuts to 36 to 45 lbfin (4 to 5 Nm).

      3. Install the terminal module, refer to Figure.

      1. Refer to Step.

      4. Examine the harness.

      1. Make sure that no harness length has too much strain on it. If it is necessary, loosen the bolt or nut at the applicable clip position. Adjust the harness and torque the bolt or the nut to that given in step A. (10) or (11).

    6. SUBTASK 72-00-32-420-425 Install the EEC Harness (SBE 71-0109)

      SBE 71-0109: Provide improved routing and clipping of the EEC and Ignition supply harness and raceway

      NOTE

      Install the ignition supply harness with the EEC harness. Refer to Step.

      1. Install the EEC harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-005) as follows.

      2. Pre SBE 71-0107: Identify the correct datum clip positions 1075, 0783, 0761, 0764, 1015, 1021, 1022, 0539, 0529, 0792, 1009, 0256, 0325, 0753, 0295, 1032 and 0778.

      3. SBE 71-0107: Identify the correct datum clip positions 1075, 0783, 0761, 0764, 1015, 1021, 1022, 0529, 0792, 1009, 0256, 0325, 0753, 0295, 1032 and 0778.

      4. Pre SBE 73-0040: Identify the correct datum clip positions 1075, 0783, 0761, 0764, 1015, 1021, 1022, 0529, 0792, 1009, 0256, 0753, 0295, 1032 and 0778.

      5. Connect and torque the electrical connectors 4000KS-J2 to -J5 and 4000KS-J8 to -J11 to the EEC ELECTRONIC ENGINE CONTROL (EEC) (73-22-34,01-280) with theIAE 1R19416 EEC harness wrench 1 off to 32* lbfin (3.6 Nm).

      6. Install the datum clip position 0783, refer to Figure. Temporarily attach the harness at the datum clip position 0764 with CoMat 06-086 TIES.

      7. Install the electrical harness receptacle 4000VC, attached to the EEC harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41,01-005), to the bracket POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41,05-940) with the four bolts and the four assembled washer nuts POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-027 and POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN01-025). Make sure the master keyway is in the outboard direction. Refer to the detail on B, refer to Figure. Install the datum clip position 0761, refer to Figure.

      8. Torque the assembled washer nuts to 10 to 14 lbfin (1.1 to 1.6 Nm).

      9. Pre SBE 71-0070: Connect the electrical connector 4000VC-A ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42,01-005) to the harness receptacle 4000VC, align the master keyway. Torque the connector to 46 * lbfin (5.2 Nm). Refer to Fig. 72-00-32-990-023-002and Fig. 72-00-32-990-026-011. Remove the temporary ties and install the datum clip positions 0764 and 0826, refer to Figure and Figure.

        SBE 71-0070: Connect the electrical connector 4000VC-A ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42,01-005) to the harness receptacle 4000VC, align the master keyway. Torque the connector to 46 * lbfin (5.2 Nm). Refer to Fig. 72-00-32-990-023-002and Fig. 72-00-32-990-026-004. Remove the temporary ties and install the datum clip position 0764, refer to Figure.

      10. Install the electrical harness receptacle 4001VC, attached to the EEC harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41,01-005), to the bracket POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41,06-560) with the four bolts and the four assembled washer nuts POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-022 and POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN 01-020). Make sure the direction of the master keyway is at the top (in relation to the bracket). Refer to the detail on A, refer to Figure. Remove the temporary ties and install the datum clip position 1075, refer to Figure.

      11. Torque the assembled washer nuts to 10 to 14 lbfin (1.1 to 1.6 Nm).

      12. Connect the electrical connector 4001VC-A ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42,01-005) to the harness receptacle 4001VC, align the master keyway. Torque the connector to 46 * lbfin (5.2 Nm). Refer to Figure and Figure.

      13. Remove the temporary ties and install the datum clip position 0819, refer to Figure, Figure and Figure.

        NOTE

        Refer to TASK 72-00-32-420-005 and TASK 72-00-60-420-003 for the procedure for clip positions 0529 and 0778.

    2. Connect and torque the electrical connectors (Right side):

      4100KS-E and 4100KS-A to the relay box POWER PLANT-RELAY BOX (71-51-49,01-100) to 21 * lbfin (2.4Nm). Install the datum clip position 1015, refer to Figure.

      4016KS-A to the ACOC oil temperature thermocouple OIL-ACOC OIL TEMPERATURE THERMOCOUPLE (79-32-15,01-200) to 18 * lbfin (2.0 Nm). Install the datum clip position 1022, refer to Figure.

      4029KS-A to the HP stage 7 and 10 air solenoid valve STAGE 10 AIR SOLENOID VALVE (36-11-57,01-100) to 18 * lbfin (2.0 Nm).

      4020KS1-A to the HP compressor stage 7 solenoid valve (51.9 degrees) AIR-HPC STAGE 7 SOLENOID VALVE (75-32-51,01-100) to 18 * lbfin (2.0 Nm). Install the datum clip position 1021, refer to Figure.

      4020KS3-A to the HP compressor stage 7 solenoid valve (228 degrees) AIR-HPC STAGE 7 SOLENOID VALVE (75-32-51,01-100) to 18 * lbfin (2.0 Nm).

      4020KS2-A to the HP compressor stage 7 solenoid valve (108.8 degrees) AIR-HPC STAGE 7 SOLENOID VALVE (75-32-51,01-100) to 18 * lbfin (2.0 Nm).

      4028KS-A to the stage 10 air solenoid valve AIR-STAGE 10 AIR SOLENOID VALVE (75-23-52,01-100) to 18 * lbfin (2.0 Nm).

      4023KS-A to the HP compressor stage 10 solenoid valve AIR-HPC STAGE 10 SOLENOID VALVE (75-32-53,01-400) to 18 * lbfin (2.0 Nm).

      Pre SBE 71-0107 - 4019KS-A and 4019KS-B to the ACOC air modulating valve OIL-AIR COOLED OIL COOLER MODULATING VALVE (79-21-51,01-100) to 18 * lbfin (2.0 Nm). Install the datum clip positions 1009, 0792 and 0539. Temporarily attach the datum clip positions 0529 and 0778 with CoMat 06-086 TIES.

      SBE 71-0107 - 4019KSA and 4019KS-B to the ACOC air modulating valve OIL-AIR COOLED OIL COOLER MODULATING VALVE (79-21-51,01-100) to 18 * lbfin (2.0 Nm). Install the datum clip positions 1009, 0792 and 0540. Temporarily attach the datum clip positions 0529 and 0778 with CoMat 06-086 TIES.

      3. Route the harness at the bifurcation panel.

      1. Remove the two nuts and the two bolts which temporarily attach the tube 153 to the bifurcation panel.

      2. Route the harness from the right side of the engine and between the tubes 153 and 138. This is the bundle attached with the bundle for the electrical connector 4009VC-A.

      3. Put the electrical connector 4008VC-A (from the left side of the engine) between the tubes 153 and 138.

      4. Attach the bundles together at the datum clip position 0256.

      5. Attach the tube 153 to 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 01-502).

      6. Torque the tube 236 nut (attached to the tube 153) to 159 to 177 lbfin (18 to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.

      7. Torque the two nuts PNEUMATIC-TUBES-HP BLEED CONTROL AIR (36-11-47,01-502) to 85 to 105 lbfin (10 to 12 Nm).

    4. Connect and torque the electrical connectors (Left side):

      4015KS-A to the IDG FCOC ELECTRICAL POWER-FUEL COOLED IDG OIL COOLER (24-21-42,01-100) to 18 * lbfin (2.0 Nm).

      Install the datum clip position 0325, refer to Figure.

      4017KS-A to the fuel temperature thermocouple FUEL TEMPERATURE THERMOCOUPLE (73-35-15,01-100) to 18 * lbfin (2.0 Nm).

      4018KS-A to the fuel diverter and return valve FUEL DIVERTER AND RETURN VALVE (73-13-42,01-100) to 20 * lbfin (2.3 Nm). Install the datum clip position 0295, refer to Figure.

      4018KS-B to the fuel diverter and return valve FUEL DIVERTER AND RETURN VALVE (73-13-42,01-100) to 24 * lbfin (2.7 Nm). Install the datum clip position 0753, refer to Figure.

      5. Install split sleeves POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-514 and POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN01-490) and the bonded clips at the clip positions 1447, 1448, 1449 and 1450.

        1. Stage 1: Attach the EEC harness and the ignition supply harness ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS (71-51-44, 01-005) together.

          1. Step 1: Secure the end of the reinforced silicone rubber tape POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 03-964) in the cable wire of the harness.

          1. Wind the tape around the harness bundle and along the length of harness. Use a sufficient length of the tape to reduce the diameter of the harnesses to give the dimensions on Figure.

          2. At the start of the wrapping wrap the tape around the harness twice, to give two complete turns. Wind the tape so there is a 50 percent width overlap as it is wrapped around the harness.

          2. Step 2 : Build-up the harness diameter to match the inside diameter of the split sleeves.

          1. Wrap the 0.750 in. tape POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-492) around the harness at the raceway lug clip positions 1450, 1449, 1448 and 1447 to give the dimensions on Figure.

          2. Lightly clamp the split sleeves around the harness and measure the outside diameter of the split sleeves. The diameter must be between 1.5 in. and 1.505in. (38.10 to 38.77mm). This is to allow the bonded clips to be installed.

          3. Step 3: Secure the ends of the silicone rubber tape.

          1. Wrap the 1 in. wide tape POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 03-966) twice around the harness at both ends of the silicone rubber tape to hold it securely to give the dimensions on Figure.

        2. Stage 2 : Attach the split sleeves POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-514 and POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN01-490) to the harness.

        1. Do the following procedure to install both the split sleeve assemblies to the harness.

          2. Steps 1 and 2 :

          1. Position and attach the lower split sleeve to the harness with lacing tape number 1 POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-491) as given in Figure. Use a length of 31.5 in (800mm) or longer.

          2. Take one half of the split sleeves and push the lacing tape number 1 and 2 through the slit of the split sleeve, step 1 Figure.

          3. Take one end of the lacing tape and turn it around the harness four times. Make sure the lacing is tight and that it does not go out of the sleeve slit, step 2 Figure.

        3. Steps 3 to 8 : Tie and secure the sleeve half to the harness as shown in Figure.

        4. Step 9 : Do the procedure in steps 2 to 8 for lacing tape number 2, Figure.

        5. Take the other half of the sleeve and install and secure it with lacing tape numbers 3 and 4 as given in the procedure in stage 2, steps 1 through 9.

        6. Position the sleeve so that at least one CAUTION identification label can be read when it is installed, refer to stage 3 for the completed view, Figure.

        7. Check the gap between the split sleeves after assembly, the gap must be between zero to 0.1in. (0 to 2.54 mm).

        3. Clean the fayed surfaces, sleeves and bonded clips.

        1. Do this operation immediately before the assembly of the clips and sleeves to the raceway.

        2. 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.

          Clean the outer surface of the split sleeves POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-490 and POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN01-514), the bonded clips POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 02-822 , POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN02-814, POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN02-806 and POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN02-798) earth fingers, the clip and the raceway lugs with CoMat 01-003 SOLVENT, DELETED. Use a clean cloth made moist with the solvent. Refer to the SPM TASK 70-11-26-300-503 for the procedure to locally swab clean components.

        4. Stage 3 : Install the bonded clips around the harnesses, refer to Figure.

        1. Install the bolts, the washers and the nuts at the clip positions 1447, 1448, 1449 and 1450. Refer to Figure.

        2. Install the bonded clips to get the dimensions in Figure.

        3. Torque the four nuts at the clip positions 1447 to 1450 to 85 to 105 lbfin (10 to 12 Nm).

        5. Check the electrical continuity.

        1. After the installation of the harness to the raceway at the clip positions 1447 to 1450 to the raceway check the electrical continuity.

        2. Check the continuity between the sleeves and the bonding clips attached to the raceway with an ohmeter. The electrical resistance between each sleeve and racway that the clip is attached to must not be more than 15 milliohms.

      6. Install clip position 1462, refer to Figure.

      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 BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN (71-51-50, 01-100) bonding lug, the fuel flow transmitter bonding lead 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 two washers at clip position 1462.

      3. Install the bolt, washers, clip, bonding lead and nut to attach the EEC harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41,01-005) and the Ignition Supply harness ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS (71-51-44,01-005) to the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN (71-51-50,01-100) at clip position 1141. Torque the nut to 36 to 45 lbfin (4 to 5 Nm).

      7. Install the remaining clip positions.

        NOTE

        Install the clip positions 0766 and 0767 during the procedure given in Step.

      1. Install the bolts, the washers, the spacers, the nuts or the clipnuts and the clips at the remaining clip positions.

      2. Torque the bolts to 36 to 45 lbfin (4 to 5 Nm) in the anchor nuts and the clipnuts.

      3. Torque the nuts at the remaining clip positions to 36 to 45 lbfin (4 to 5 Nm).

      4. Make sure that no harness length has too much strain on it. If it is necessary loosen the bolt or nut at the applicable clip position. Adjust the harness and torque the bolt or the nut to 36 to 45 lbfin (4 to 5 Nm) or if applicable to 85 to 105 lbfin (10 to 12 Nm), refer to step E.(9).

    7. SUBTASK 72-00-32-420-426 Install the Ignition Supply Harness

    1. Refer to Figure and Figure.

      2. Install the ignition supply harness ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS (71-51-44, 01-005) as follows:

      1. Identify the correct datum clip positions 0791, 0550 and 1007.

      2. Connect the electrical connectors 4100KS-D and 4100KS-C to the relay box POWER PLANT-RELAY BOX (71-51-49,01-100). Torque the electrical connectors to 18 * lbfin (2.0 Nm).

      3. Install the electrical harness receptacles.

      1. Attach the electrical harness receptacle 4002VC (attached to the ignition supply harness) to the bracket POWER PLANT-RELAY BOX (71-51-49,01-330) with the four bolts and the four assembled washer nuts ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS (71-51-44, 01-022 and ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS01-020). Make sure the master keyway is in the outboard direction, refer to the detail on E. Refer to Figure.

        Remove the temporary ties and install the datum clip position 0550 and the clip position 0207. Refer to Figure.

      2. Attach the receptacle 4003VC to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49,03-800) with the four bolts and the four assembled washer nuts ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS (71-51-44, 01-027 and ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS01-025). Make sure the master keyway is in the outboard direction, refer to the detail on D. Refer to Figure.

        Install the datum clip position 1007. Refer to Figure and Figure.

      3. Torque the assembled washer nuts installed in (1) and (2) to 6 to 8 lbfin (0.70 to 0.90 Nm).

      4. Connect and torque the electrical connectors, as follows:

      1. 4002VC-A and 4003VC-A ELECT HARNESS-LIGHT DUTY-EEC/IGN SUPPLY HARNESS (71-51-42,01-005) to the receptacles, align the master keyways. Refer to Figureand Figure. Torque the electrical connectors to 14 * lbfin (1.6 Nm).

      2. Remove the temporary ties and install the datum clip position 0791. Refer to Figure.

      5. Install the harness at the remaining clip positions.

      1. Route the harness with the EEC harness at the given clip positions. Refer to SUBTASK 72-00-32-420-xxx.

      2. Install the bolts, the washers, the spacer, the nuts and the clips at the clip positions 1421 and 1414 (at the bifurcation panel). Refer to Figure and Figure.

      3. Remove the retaining lockwire from the combined fume and fireseal. Assemble and install the assembly to the bifurcation panel with the four bolts, the four nuts and the two flame trap brackets ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS (71-51-44, 01-032 , ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS01-030 and ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS01-034). Tighten the four nuts to 36 to 45 lbfin (4 to 5 Nm). Refer to Figure.

      4. Remove the temporary ties and install the clip positions 0892 and 0258. Refer to Figure, Figure and Figure.

      5. Torque the bolts at the clip positions to 36 to 45 lbfin (4 to 5 Nm).

        NOTE

        Refer to TASK 72-00-40-420-006 for the installation of the ignition supply harness to the core engine.

      6. Torque the nuts at the remaining clip positions to 36 to 45 lbfin (4 to 5 Nm).

    8. SUBTASK 72-00-32-420-427 Install the EEC Flexible Hoses and the Tube 235 (SBE 71-0108)

      SBE 71-0108: Provide a P2/T2 line bracket with lockwire holes

    1. Refer to Figure.

    2. Connect the hose 238 to the EEC union and the tube 239. Torque the hose nuts to 142 to 150 lbfin (16 to 17 Nm).

    3. Connect the hose 134 to the EEC union and the tube 135. Torque the hose nuts to 142 to 150 lbfin (16 to 17 Nm).

    4. Attach the tube 235 to the bracket POWER PLANT-RELAY BOX (71-51-49,01-390) with the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49,08-310). Connect the tube 142 to the tube 235. Torque the locknut to 70 to 80 * lbfin (7.9 to 9.0 Nm).

    5. Install the bolts, the washers, the clips and the nuts at the clip positions 0766 and 0767. Refer to Figure.

    6. Connect the hose 133 to the EEC union and the tube 235. Torque the hose 133 nuts to 182 to 199 * lbfin (20.5 to 22.5 Nm). Torque the tube 142 nut to 159 to 177 lbfin (18 to 20 Nm).

    7. Connect the hose 240 to the EEC union and the tube 241. Torque the hose nuts to 142 to 150 lbfin (16 to 17 Nm).

    8. Connect the hose 129 to the EEC union and the tube 159. Torque the hose nut at the EEC to 182 to 199 * lbfin (20.5 to 22.5 Nm). Torque the hose nut at the tube 159 to 159 to 177 lbfin (18 to 20 Nm).

    9. SBE 71-0108 : Safety the hose 133 and the locknut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49,08-310) separately to the bracket POWER PLANT-RELAY BOX (71-51-49,01-390) with CoMat 02-126 LOCKWIRE. Refer to the view on A and B, Figure.

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

    11. Safety the hose 238 nut to the bracket ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49,03-790) with CoMat 02-126 LOCKWIRE.

    12. Torque the nuts at the clip positions 0766 and 0767 to 36 to 45 lbfin (4 to 5 Nm).

    9. SUBTASK 72-00-32-220-126 Measure the Harness Clearance and Examine the Routing

    1. Refer to Figure and Figure.

      2. Measure the clearance between all the different harnesses and engine parts.

      1. Do a check on the clearance. Push the harness with a light pressure of the thumb then release. The harness must spring back and give the minimum clearance. If the pressure moves the harness through the adjacent clips, change the clip or adjust the harness thickness. Refer to Step.

      2. The general clearance must be a minimum of 0.250in. (6.35 mm).

        3. A minimum clearance of 0.100in. (2.5 mm) is necessary as follows:

        1. For a harness length which has Spirap protection around it. Each end of the Spirap must be held with a clip position.

        2. Pre SBE 71-0107 - Between the harness bundle breakout at the clip position 0539 and the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-FAN (71-51-50,01-100).

        3. Between the harness adjacent to the clip position 0753 and the tubes 114 and 170.

        4. Between the harness and the flange FC, adjacent to the clip position 0820.

        5. The harness length between the clip positions 1075 and 0897 and the flange FD.

      4. Make sure that the harness loop below the clip position 0257 is forward of a line taken from the rear of the clip. This will prevent a foul of the loop in the left side C-duct door. Attach the loop to the adjacent harness with CoMat 02-159 LACING TAPE to make the loop as small as possible.

      5. The harness can touch the smooth parts of brackets and rafts if the harness is clipped to them. Make sure the harness is held to prevent movement between the harness and the bracket or raft.

      3. Adjust the harness.

      1. Adjust the harness to get the minimum clearances. Refer to Step.

    4. Torque the bolt or nut, as necessary, to the value given in the applicable installation SUBTASK for each of the harnesses.

      5. Examine the harness wire bundle breakouts.

      1. Make sure each harness wire bundle breakout curves smoothly from its primary harness. It must go to the component to which it attaches and not across the primary harness.

      2. If the primary harness and the wire bundle breakout touch each other you must attach them together. Both harness bundles must not move in relation to each other. Refer to Step.

      6. Examine the harness routing.

      1. If one harness goes across or it is parallel with a different harness (and they can touch) you must attach them together. Each harness must not move in relation to each other. Refer to Step.

    10. SUBTASK 72-00-32-420-428 Attach the Harnesses Together

    1. Attach the wire bundle breakout to the primary harness with CoMat 02-159 LACING TAPE to prevent movement of them in relation to each other.

    2. Attach the parallel harnesses and those which go across each other together. If it is necessary wrap CoMat 02-148 ADHESIVE TAPE (ELECTRICAL) around the harness to prevent abrasion. Then attach the harnesses together with the lacing tape.

    11. SUBTASK 72-00-32-210-089 Visually Inspect the Electrical Backshells and Cable Clamps

    1. Refer to Figure.

    2. Make sure that all the applicable connectors, backshells and cable clamps are secure.

    3. Make sure that all the applicable backshells and cable clamps are safetied with CoMat 02-126 LOCKWIRE. Refer to the SPM TASK 70-42-05-400-501.

    12. SUBTASK 72-00-32-210-090 Visually Inspect the EEC Harness (01-005) Electrical Backshells and Cable Clamps (SBE 70-0813)

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

      NOTE

      Use this procedure to safety the EEC harness backshells and cable clamps with safety cable.

    1. Refer to Figure.

    2. Make sure that all the EEC harness connectors, backshells and cable clamps are secure.

    3. Make sure that all the EEC harness backshells and cable clamps are safetied. Safety with CoMat 02-274 SAFETY CABLE KIT or with CoMat 02-275 SAFETY CABLE KIT. Refer to the SPM TASK 70-42-08-400-501.

    13. Figure: Electrical Harness Installation Procedure

    Electrical Harness Installation Procedure

    Figure: Install the 400VC to IDG Cable Assembly

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    Figure: Install the Vibration Harnesses/Transducer

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    Figure: Install the Terminal Module

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    Figure: Install the Ignition Supply Harness

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    Sheet 3

    Close

    Figure: Install the Ignition Supply Harness

    Sheet 4

    Legend
    Install the Ignition Supply Harness

    Sheet 4

    Close

    Figure: Install the EEC Harness

    Sheet 5

    Legend
    Install the EEC Harness

    Sheet 5

    Close

    Figure: Install the Ignition Supply Harness

    Sheet 6

    Legend
    Install the Ignition Supply Harness

    Sheet 6

    Close

    Figure: Install the Ignition Supply Harness

    Install the Ignition Supply Harness

    Figure: Install the Ignition Supply Harness

    Install the Ignition Supply Harness

Requirements After Job Completion

Follow-On Conditions

NONE
Link not Found
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:18992
Enterprise Name:HANSCOM INC
BU Name:HANSCOM INC
Street:331 MARKET STREET
P.O. Box:364
City:WARREN
State:RI
Zip Code:02885
Country:USA
Phone Number:1-401-247-1999, 1-800-725-6788
Fax Number:1-401-247-4575
Internet:www.hanscominc.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Manufacturer Code:X111X
Supply Number:CoMat 01-002
Type:sp01
Supply Short Name:CoMat 01-002 SOLVENT, DELETED.
Supply Name:CoMat 01-002 SOLVENT, DELETED.
Specification Groups:
Doc NumberType
wiring harnesses. Where CoMat 01‐002 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 01‐002 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: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: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 02-148
Type:sp01
Supply Short Name:CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)
Supply Name:CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)
Specification Groups:
Doc NumberType
OMAT: 296SCOTCH NO. 69 (WHITE)
Suppliers:
ManufacturerRemarks
LOCAL
76381
94960
K0993
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 02-159
Type:sp01
Supply Short Name:CoMat 02-159 LACING TAPE
Supply Name:CoMat 02-159 LACING TAPE
Specification Groups:
Doc NumberType
T085 OMAT: 274
Suppliers:
ManufacturerRemarks
LOCAL
IE218
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 02-184
Type:sp01
Supply Short Name:
Supply Name:CoMat 02-184 LACING TAPE
Specification Groups:
Doc NumberType
718 G MIL-T-43435B
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:LOCAL
Supply Number:CoMat 02-202
Type:sp01
Supply Short Name:CoMat 02-202 GLASS CLOTH TAPE, ADHESIVE
Supply Name:CoMat 02-202 GLASS CLOTH TAPE, ADHESIVE
Specification Groups:
Doc NumberType
NO.69-3/4 IN WIDE MIL-I-19166-C JCR-275
Suppliers:
ManufacturerRemarks
LOCAL
81349
76381
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:18992
Supply Number:CoMat 06-086
Type:sp01
Supply Short Name:CoMat 06-086 TIES
Supply Name:CoMat 06-086 TIES
Specification Groups:
Doc NumberType
PMC 4272SPECIAL WIRE TIES
Suppliers:
ManufacturerRemarks
18992
Manufacturer Code:LOCAL
Supply Number:CoMat 10-039
Type:sp01
Supply Short Name:
Supply Name:CoMat 10-039 ENGINE OIL
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
LOCAL
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 1R19416
Tool Name:IAE 1R19416 EEC harness wrench