DMC:V2500-A5-72-00-3200-04D-720A-B|Issue No:003|Issue Date:2020-11-01

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-A5 and Post SBE 79-0088

Common Information

TASK 72-00-32-420-004-C00 LPC/Intermediate Case Module - Install The Electrical Harnesses, Installation-004 - SBE 79-0088

General

SBE 79-0088

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

TASK 72-00-32-420-001-B00 (INSTALLATION-001) - Install the LP compressor/intermediate case brackets and the bifurcation panel

TASK 72-00-32-420-002 (INSTALLATION-002) - Install the LP compressor/intermediate case components

TASK 72-00-32-420-003-C00 (INSTALLATION-003) - Install the LP compressor/intermediate case tubes and the electrical harness raceways

TASK 72-00-32-420-005-C00 (INSTALLATION-005) - Install the pneumatic starter duct, the thermal anti-ice (TAI) duct, and the hydraulic tubes, 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 SPM TASK 70-42-05-400-501.

SBE 70-0813
For safety cable data and procedures refer to SPM TASK 70-42-08-400-501.
Safety the threaded fasteners in the ATA Chapter/Section/Subject 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 SPM TASK 70-44-00-400-501.

For the torque tightening procedures, refer to SPM TASK 70-41-00-400-501, SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-410-501.

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 SPM TASK 70-43-01-400-501.

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

NOTE

To identify the consumable materials refer to the PCI.
SBE 70-0813: Announcement of introduction of safety cable as a preferred method to lockwire.
Safety the threaded fasteners in this TASK with safety cable for the ATA Chapter/Section/Subject detailed in 2. General.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

Name	Manufacturer	Part Number / Identification	Quantity	Remark
IAE 1R19416 EEC harness wrench	0AM53	IAE 1R19416	1

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 01-002 SOLVENT, DELETED.	X111X	CoMat 01-002
CoMat 01-003 SOLVENT, DELETED	X111X	CoMat 01-003
CoMat 02-126 LOCKWIRE	K6835	CoMat 02-126
CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)	LOCAL	CoMat 02-148
CoMat 02-159 LACING TAPE	LOCAL	CoMat 02-159
CoMat 02-184 LACING TAPE	LOCAL	CoMat 02-184
CoMat 02-274 SAFETY CABLE KIT	LOCAL	CoMat 02-274
CoMat 02-275 SAFETY CABLE KIT	LOCAL	CoMat 02-275
CoMat 06-086 TIES	18992	CoMat 06-086
CoMat 10-077 APPROVED ENGINE OILS	X333X	CoMat 10-077

Spares

Name	Manufacturer	Part Number / Identification	Quantity	Remark
Packing			1
Tape			1
Braid lacing			1

Safety Requirements

NONE

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-B00 (INSTALLATION-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 SPM TASK 70-43-00-400-501 and SPM TASK 70-43-01-400-501.
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 01-002 SOLVENT, DELETED. INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET 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 01-002 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. inhibited and stabilized trichloroethane.
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 lbfin to 45 lbfin (4 Nm 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).
1. Refer to Figure, Figure, Figure and Figure.
2. 1. Lightly lubricate a new Vibration Transducer (77-32-15,01-420) packing 1 off with CoMat 10-077 APPROVED ENGINE OILS.
  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 lbfin to 44 lbfin (3.9 Nm 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 EEC Fan Harness And Ignition Supply Harness (71-51-42,05-080) and EEC Fan Harness And Ignition 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 lbfin to 45 lbfin (4 Nm to 5 Nm).
  6. Torque the bolts at the clip positions 0870 to 0874 and the nut at clip position 0875 to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
3. 1. Pre SBE 71-0271: Install the bolts, the washers, the nuts and the clips at the clip positions 0876 to 0880.
  2. SBE 71-0271: Install the bolts, the washers, the nuts and the clips at the clip positions 0876 to 0880 and 1210.
  3. 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.
  4. Pre SBE 71-0271: Torque the nuts at the clip positions 0876 to 0880 to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
  5. SBE 71-0271: Torque the nuts at the clip positions 0876 to 0880 and 1210 to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
1. Refer to Figure, Figure, and Figure.
2. 1. Identify the correct datum clip positions as follows: 1075, 0781, 0764, 0550, 0818, 0819, 0822, 0800, 0801, 0802, 0809, 0863, 0864 and 0869. Refer to Fig. 72-00-32-811-004, Fig. 72-00-32-811-005, Fig. 72-00-32-811-006, Fig. 72-00-32-811-007, Fig. 72-00-32-811-008 and Fig. 72-00-32-811-009.
  2. Connect and torque the electrical connectors 4000KS-J1 and 4000KS-J7 to the EEC EEC And Terminal Block Assembly (73-22-34,01-280) with the IAE 1R19416 EEC harness wrench 1 off to 32 * lbfin (3.6 Nm).
  3. Temporarily attach the harnesses to the applicable bracket at the datum clip positions 1075, 0781 and 0764 with CoMat 06-086 TIES. Also datum clip position 0550 to the tube lug, Figure.
  4. Install the terminal module EEC And Terminal Block Assembly (73-22-34,01-560) to the hole No. 9 on the flange FB with the bolt and the nut EEC And Terminal Block Assembly (73-22-34, 01-240 and EEC And Terminal Block Assembly01-260). Torque the nut to 85 lbfin to 105 lbfin (10 Nm to 12 Nm). Refer to Figure.
    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.
  5. Install the harnesses at the datum clip positions 0818 and 0822. Temporarily attach the datum clip position 0819 to the bracket with CoMat 06-086 TIES. Refer to Figure and Figure.
  6. Install the remaining datum clip positions 0800, 0801, 0802, 0809, 0863, 0864 and 0869.
  7. Install the bolts, the washers, the nuts and the clipnuts, the spacers and the clips at the clip positions.
  8. Torque the bolts to 36 lbfin to 45 lbfin (4 Nm to 5 Nm) in the anchor/clipnuts at the clip positions. Refer to Fig.
  9. At the remaining clip positions, torque the nuts to 36 lbfin to 45 lbfin (4 Nm 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 step (9) or (10).
1. Refer to Figure, Figure and Figure.
2. 1. Identify the correct datum clip positions 0800, 0809, 0791, 0830 to 0834, 0881, 0852 to 0855, 0903, 0848, 0258, 0892, 0787, 0788 and 0922.
  2. Install the datum clip positions 0809 and 0800.
  3. 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 positions 0881 and 1408.
    4100KS-B to the relay box Ignition 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.
    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.
    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.
    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.
  4. Attach the terminals at GP1, GP2, GP3 and GP4 with the 24 bolts and the 24 washers General Services Harness (71-51-43, 01-010 and General Services Harness (71-51-43, 01-011). Install four of the bolts/washers at the positions which are not used. Torque the bolts to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
  5. 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 lbfin to 45 lbfin (4 Nm to 5 Nm). Refer to Figure and Figure.
  6. Install the remaining datum clip positions 0830, 0832 and 0834.
  7. Temporarily attach the datum clip positions 0892, 0787, 0258 and 0922 to the applicable brackets with CoMat 06-086 TIES. Refer to Figure.
  8. Install the bolts, the washers, the nuts, the clipnuts and the clips at the clip positions. Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.
  9. Torque the bolts to 36 lbfin to 45 lbfin (4 Nm to 5 Nm) in the anchor/clipnuts at the clip positions.
  10. At the remaining clip positions torque the nuts to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
3. 1. Refer to Step.
4. 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).
1. 1. For the installation of (open wire) harnesses, refer to SPM TASK 70-43-02-400-501.
    NOTE
    Install the ignition supply harness with the EEC harness. Refer to Step.
2. 1. Identify the correct datum clip positions 1075, 0783, 0761, 0764, 1015, 1021, 1022, 1451, 0529, 0792, 1009, 0256, 0325, 0753, 0754, 0295 and 0778.
  2. Connect and torque the electrical connectors 4000KS-J2, -J3, J4, -J5 and 4000KS-J8, -J9, -J10, -J11 to the EEC EEC And Terminal Block Assembly (73-22-34, 01-280) with the IAE 1R19416 EEC harness wrench 1 off to 32* lbfin (3.6 Nm). Refer to Figure.
  3. Install the datum clip position 0783, refer to Figure. Temporarily attach the harness at the datum clip position 0764 with CoMat 06-086 TIES.
  4. Install the electrical harness receptacle 4000VC, attached to the EEC harness EEC Fan Harness (71-51-41, 01-005), to the bracket EEC Fan Harness (71-51-41, 05-935) with the four bolts and the four assembled washer nuts EEC Fan Harness (71-51-41, 01-027 and EEC Fan Harness01-025). Make sure the master keyway is in the outboard direction. Refer to the detail on B, Figure and Figure. Install the datum clip position 0761, refer to Figure.
  5. Torque the assembled washer nuts to 10 lbfin to 14 lbfin (1.1 Nm to 1.6 Nm).
  6. Connect the electrical connector 4000VC-A EEC Fan Harness And Ignition 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 Figureand Figure. Remove the temporary ties and install the datum clip positions 0764, refer to Figure.
  7. Install the electrical harness receptacle 4001VC, attached to the EEC harness EEC Fan Harness (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 EEC Fan Harness (71-51-41, 01-022 and EEC Fan Harness01-020). 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 and Figure. Remove the temporary ties and install the datum clip position 1075, refer to Figure.
  8. Torque the assembled washer nuts to 10 lbfin to 14 lbfin (1.1 Nm to 1.6 Nm).
  9. Connect the electrical connector 4001VC-A EEC Fan Harness And Ignition 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 Figureand Figure.
  10. Remove the temporary ties and install the datum clip position 0819, Figure and Figure.
3. Connect and torque the electrical connectors (Right side):
  4100KS-E and 4100KS-A to the relay box Ignition Relay Box (71-51-49, 01-100) to 21 * lbfin (2.4Nm). Install the datum clip position 1015, refer to Figure and Figure.
  4016KS-A to the ACOC oil temperature thermocouple ACOC Oil Temperature Thermocouple (79-32-15, 01-200) to 18 * lbfin (2.0 Nm). Install the datum clip position 1022, refer to Figure and 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), refer to Figure, 72-00-32-990-815-006 and Figure.
  4020KS1-A to the HP compressor stage 7 solenoid valve (51.9 degrees) 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, 72-00-32-990-815-006, 72-00-32-990-815-007 and Figure.
  4020KS3-A to the HP compressor stage 7 solenoid valve (228 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100) to 18 * lbfin (2.0 Nm), refer to Figure, 72-00-32-990-815-006 and Figure.
  4020KS2-A to the HP compressor stage 7 solenoid valve (108.8 degrees) HPC Stage 7 Solenoid Valve (75-32-51, 01-100) to 18 * lbfin (2.0 Nm), refer to Figure, Figure and Figure.
  Pre SBE 75-0081: 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), refer to Figure and Figure.
  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), refer to Figure, Figure and Figure.
  4019KSA and 4019KS-B to the ACOC air modulating valve Air Cooled Oil Cooler (ACOC) Modulating Valve (79-21-51, 01-100) to 18 * lbfin (2.0 Nm), refer to Figure, 72-00-32-990-815-006 and Figure. Install the datum clip positions 1009, 0792 and 1451, refer to Figure, 72-00-32-990-815-030 and Figure. Temporarily attach the datum clip positions 0529 and 0778 with CoMat 06-086 TIES.
4. 1. CAUTION
    YOU MUST ROUTE THE EEC HARNESS AND THE IGNITION SUPPLY HARNESS NEXT TO EACH OTHER TO THE ELECTRICAL CONNECTOR 4009VC-A. FOLLOW THE ROUTING PROCEDURE TO KEEP THE RIGHT SIDE EEC HARNESS FROM TOUCHING THE RIGHT SIDE C DUCT AND ADJACENT TUBE INSTALLATIONS.
    Route the right side EEC harness and the right side ignition supply harness next to each other to the electrical connection 4009VC-A as follows:
    Remove the two nuts and the two bolts which temporarily attach the tube 153 to the bifurcation panel.
    Route the EEC 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.
    Put the electrical connector 4008VC-A (from the left side of the engine) between the tubes 153 and 138.
    Attach the bundles together at the datum clip positions 1451 and 0256. Refer to Figure and Figure.
    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 AIR01-502).
    Torque the tube 236 HP Bleed Control Air Tubes (36-11-47, 02-100) nut (attached to the tube 153) to 159 lbfin to 177 lbfin (18 Nm to 20 Nm). Safety the tube nut with CoMat 02-126 LOCKWIRE.
    Torque the two nuts PNEUMATIC-TUBES-HP BLEED CONTROL AIR (36-11-47,01-502) to 85 lbfin to 105 lbfin (10 Nm to 12 Nm).
5. 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), refer to Fig. 72-00-32-815-002.
  Install the datum clip position 0325, refer to Fig. 72-00-32-815-036.
  Refer to Step or Step for the installation procedure for the electrical connector 4017KS-A.
  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), refer to Fig. 72-00-32-815-002. Install the datum clip position 0295, refer to Fig. 72-00-32-815-036.
  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), refer to Fig. 72-00-32-815-002. Install the datum clip position 0753, refer to Fig. 72-00-32-815-037.
6. 1. Attach the EEC harness and the ignition supply harness Ignition Supply Harness (71-51-44, 01-005) together with the EEC Fan Harness (71-51-41, 03-964) tape 1 off.
  2. Attach one end of the tape between the cables, in the center of the harness bundle at the clip positions 1449, 1450 and 1448, 1447. Use a sufficient length of the tape to reduce the diameter of the harnesses.
  3. Hold the split sleeves together at both positions around the harness and measure the diameter of the split sleeves. The diameter must not be more than 1.5 in. (38 mm).
  4. WARNING
    WHEN YOU USE CoMat 01-002 SOLVENT, DELETED. INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.
    Clean the split sleeves EEC Fan Harness (71-51-41, 01-490 and EEC Fan Harness01-514), the bonded clip EEC Fan Harness (71-51-41, 01-489 , EEC Fan Harness01-497, EEC Fan Harness01-513 and EEC Fan Harness02-224) earth fingers, the clip and the raceway lugs with CoMat 01-002 SOLVENT, DELETED.. Use a clean cloth made moist with the solvent.
  5. Install the split sleeve EEC Fan Harness (71-51-41, 01-490) around the harnesses. Make sure the CAUTION label on one of the split sleeves can be seen when the installation procedure is complete. Attach them with CoMat 02-184 LACING TAPE as follows:
    Put one end of the braid lacing, minimum length 31.5 in. (800 mm), through the harness cables. Put both ends of the lacing through the slot of the split sleeve. Step 1.
    Wind the longest end of the lacing four times around the harness/sleeve assembly. Make sure the lacing is tight and does not go out of the slot. Step 2.
    Make a clove hitch (at the bottom of the slot) with the longest end of the lacing. Step 3.
    Pull both ends of the lacing tight. Make a reef knot. Steps 4 and 5.
    Make one more hitch. Steps 6 to 9.
    Attach the split sleeve at the other slot with the braid lacing, refer to the paragraphs (a) to (e).
    Install the remaining split sleeve with two more pieces of braid lacing refer to paragraphs (a) to (f). Make the hitch at the top of the split sleeve. Steps 1 to 10.
  6. Install the split sleeve EEC Fan Harness (71-51-41, 01-514) around the harnesses, refer to paragraph (5).
  7. Measure the diameter of the harnesses. The diameter must not be more than 1.5 in. (38 mm).
  8. Install the bonded clips around the harnesses.
  9. Install the bolts, the washers and the nuts at the clip positions 1449, 1450, 1447 and 1446. Torque the four nuts to 85 lbfin to 105 lbfin (10 Nm to 12 Nm).
7. 1. Stage 1: Attach the EEC harness and the ignition supply harness Ignition Supply Harness (71-51-44, 01-005) together.
    Step 1: Secure the end of the reinforced silicone rubber tape EEC Fan Harness (71-51-41, 03-964) in the cable wire of the harness.
    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.
    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.
    Step 2: Build-up the harness diameter to match the inside diameter of the split sleeves.
    Wrap the 0.750 in. (19.050 mm) tape EEC Fan Harness (71-51-41, 01-492) around the harness at the raceway lug clip positions 1449, 1450, 1447 and 1446 to give the dimensions on Figure.
    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. to 1.505 in. (38.10 mm to 38.77 mm). This is to allow the bonded clips to be installed.
    Step 3: Secure the ends of the silicone rubber tape.
    Wrap the 1 in. (25.4 mm) wide tape EEC Fan Harness (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 EEC Fan Harness (71-51-41, 01-514) and EEC Fan Harness (71-51-41, 01-490) to the harness.
    Do the following procedure to install both the split sleeve assemblies to the harness.
    Steps 1 and 2:
    Position and attach the lower split sleeve to the harness with lacing tape number 1 EEC Fan Harness (71-51-41, 01-491) as given in Figure. Use a length of 31.5 in. (800 mm) or longer.
    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.
    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.
    Steps 3 to 8: Tie and secure the sleeve half to the harness as shown in Figure.
    Step 9: Do the procedure in steps 2 to 8 for lacing tape number 2, Figure.
    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.
    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 and Figure.
    Check the gap between the split sleeves after assembly, the gap must be between 0 in. to 0.1 in. (0 mm to 2.54 mm).
  3. Clean the fayed surfaces, sleeves and bonded clips.
    Do this operation immediately before the assembly of the clips and sleeves to the raceway.
    WARNING
    WHEN YOU USE CoMat 01-003 SOLVENT, DELETED INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.
    Clean the outer surface of the split sleeves EEC Fan Harness (71-51-41, 01-490) and EEC Fan Harness (72-51-41, 01-514), the bonded clips EEC Fan Harness (71-51-41, 02-822), EEC Fan Harness (71-51-41, 02-814), EEC Fan Harness (71-51-41, 02-806) and EEC Fan Harness (71-51-41, 02-798) earth fingers, the clip and the raceway lugs with CoMat 01-003 SOLVENT, DELETED inhibited and stabilized trichloroethane. Use a clean cloth made moist with the solvent. Refer to 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.
    Install the bolts, the washers and the nuts at the clip positions 1447, 1448, 1449 and 1450. Refer to Figure.
    Install the bonded clips to get the dimensions in Figure and Figure.
    Torque the four nuts at the clip positions 1447, 1448, 1449 and 1450 to 85 lbfin to 105 lbfin (10 Nm to 12 Nm).
  5. Check the electrical continuity.
    After the installation of the harness to the raceway at the clip positions 1447, 1448, 1449 and 1450 to the raceway check the electrical continuity.
    Check the continuity between the sleeves and the bonding clips attached to the raceway with an ohmeter. The electrical resistance between each sleeve and raceway that the clip is attached to must not be more than 15 milliohms.
8. 1. WARNING
    WHEN YOU USE CoMat 01-002 SOLVENT, DELETED. INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.
    Remove the grease, the fingerprints and the unwanted material from the mating surfaces of the raceway Fan Harness Support Raceways (71-51-50, 01-100) bonding lug, the fuel flow transmitter bonding lead with CoMat 01-002 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 EEC Fan Harness (71-51-41, 01-005) and the Ignition Supply harness Ignition Supply Harness (71-51-44, 01-005) to the raceway Fan Harness Support Raceways (71-51-50, 01-100) at clip position 1462. Torque the nut to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
9. 1. Install the bolts, the washers, the spacers, the nuts or 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, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.
  2. Torque the bolts to 36 lbfin to 45 lbfin (4 Nm to 5 Nm) in the anchor nuts and the clipnuts.
  3. Torque the nuts at the remaining clip positions to 36 lbfin to 45 lbfin (4 Nm 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 lbfin to 45 lbfin (4 Nm to 5 Nm) or to 85 lbfin to 105 lbfin (10 Nm to 12 Nm) at the clip positions 1447, 1448, 1449 and 1450, refer to steps E and F.
1. Refer to Figure.
2. Connect the 4017 KS-A to the fuel temperature thermocouple FUEL TEMPERATURE THERMOCOUPLE (73-35-15, 01-100) and torque the connector to 18 * lbfin (2.0 Nm).
3. Adjust the harness in the datum clip position 0295 as necessary to obtain the correct clearance and drip loop, refer to Figure. Torque the clip bolt to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
1. Refer to Figure and Figure.
2. 1. If the thermocouple is not to be removed, remove and install the thermocouple securing bolts one at a time. Refer to Figure.
  2. Remove the two bolts FUEL TEMPERATURE THERMOCOUPLE (73-35-15,01-110) that secure the thermocouple to the FCOC Fuel Cooled Oil Cooler (FCOC) (79-21-43,01-100).
  3. WARNING
    WHEN YOU USE CoMat 01-002 SOLVENT, DELETED. INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.
    Remove the grease, the fingerprints and the unwanted material from the mating surfaces of the ground terminals and thermocouple earth positions with CoMat 01-002 SOLVENT, DELETED.. Use a clean lint free cloth moistened with the solvent.
  4. Install the harness ground terminal connectors to the two bolts. Install the two bolts and torque to between 85 lbfin and 105 lbfin (10 Nm to 12 Nm).
  5. CAUTION
    YOU MUST NOT EXCEED THE RECOMMENDED TORQUE VALUES. OVER TORQUING CAN RESULT IN FRACTURE OF THE THERMOCOUPLE STUDS.
    Install channel A and B thermocouple lead assemblies EEC Fan Harness (71-51-41, 04-900) to the fuel temperature thermocouple studs. Install the two nuts FUEL TEMPERATURE THERMOCOUPLE (73-35-15, 01-140) to the top studs and torque to between 18 lbfin and 22 * lbfin (2.03 Nm to 2.48 Nm). Install the two nuts FUEL TEMPERATURE THERMOCOUPLE (73-35-15, 01-130) to the bottom studs and torque to between 15 lbfin and 18 * lbfin (1.69 Nm to 2,03 Nm).
  6. Adjust the harness in the datum clip position 0295 as necessary to obtain the correct clearance and drip loop, refer to Figure. Torque the clip bolt to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
1. 1. Refer to Figure, Figure and Figure.
  2. Identify the correct datum clip positions 0791, 0550 and 1007, refer to Figure and Figure.
  3. Connect the electrical connectors 4100KS-D and 4100KS-C to the relay box Ignition Relay Box (71-51-49, 01-100). Torque the electrical connectors to 18 * lbfin (2.0 Nm). Remove the temporary ties and install the datum clip position 0791.
2. 1. Attach the electrical harness receptacle 4002VC (attached to the ignition supply harness) to the bracket Ignition Relay Box (71-51-49,01-330) with the four bolts and the four assembled washer nuts Ignition Supply Harness (71-51-44, 01-022) and Ignition Supply Harness (71-51-44, 01-020). Make sure the master keyway is in the outboard direction, refer to the detail on E, refer to Figure and Figure.
  2. Remove the temporary ties and install the datum clip position 0550 and the clip position 0207, refer to Figure.
  3. Attach the receptacle 4003VC to the bracket Fuel System Air Tubes (73-22-49, 03-800) with the four bolts and the four assembled washer nuts Ignition Supply Harness (71-51-44, 01-027 and Ignition Supply Harness (71-51-44, 01-025). Make sure the master keyway is in the outboard direction, refer to the detail on D, refer to Figure and Figure.
  4. Install the datum clip position 1007, refer to Figure.
  5. Torque the assembled washer nuts installed in (1) and (2) to 6 lbfin to 8 lbfin (0.70 Nm to 0.90 Nm).
3. 1. 4002VC-A and 4003VC-A EEC Fan Harness And Ignition Supply Harness (71-51-42, 01-005) to the receptacles, align the master keyways. Refer to Figure and Figure. Torque the electrical connectors to 14 * lbfin (1.6 Nm).
  2. Remove the temporary ties and install the datum clip position 0781. Refer to Figure.
4. 1. Route the harness with the EEC harness at the given clip positions. Refer to Step.
  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, Figure, 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 Ignition Supply Harness (71-51-44, 01-032 , Ignition Supply Harness01-030 and Ignition Supply Harness (71-51-44, 01-034). Tighten the four nuts to 36 lbfin to 45 lbfin (4 Nm to 5 Nm). Refer to Figure.
  4. Remove the temporary ties and install the clip positions 0892 and 0258. Refer to Figure, Figure, 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-C00 (INSTALLATION-009) for the installation of the ignition supply harness to the core engine.
  6. Torque the nuts at the remaining clip positions to 36 lbfin to 45 lbfin (4 Nm to 5 Nm).
1. Refer to Figure.
2. Connect the hose 238 to the EEC union and the tube 239. Torque the hose nuts to 142 lbfin to 150 lbfin (16 Nm to 17 Nm).
3. Connect the hose 134 to the EEC union and the tube 135. Torque the hose nuts to 142 lbfin to 150 lbfin (16 Nm to 17 Nm).
4. Attach the tube 235 to the bracket Ignition Relay Box (71-51-49, 01-390) with the locknut Fuel System Air Tubes (73-22-49, 08-310). Connect the tube 142 to the tube 235. Torque the locknut to 70 lbfin to 80 * lbfin (7.9 Nm 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 lbfin to 199 * lbfin (20.5 Nm to 22.5 Nm). Torque the tube 142 nut to 159 lbfin to 177 lbfin (18 Nm to 20 Nm).
7. Connect the hose 240 to the EEC union and the tube 241. Torque the hose nuts to 142 lbfin to 150 lbfin (16 Nm 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 lbfin to 199 * lbfin (20.5 Nm to 22.5 Nm). Torque the hose nut at the tube 159 lbfin to 177 lbfin (18 Nm to 20 Nm).
9. Safety the hose 133 and the locknut Fuel System Air Tubes (73-22-49, 08-310) separately to the bracket Ignition Relay Box (71-51-49, 01-390) with CoMat 02-126 LOCKWIRE.
10. Safety the tube/hose nuts with CoMat 02-126 LOCKWIRE.
11. Safety the hose 238 nut to the bracket 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 lbfin to 45 lbfin (4 Nm to 5 Nm).
1. 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 0.250 in. (6.35 mm).
  3. A minimum clearance of 0.100 in. (2.5 mm) is necessary as follows:
    For a harness length which has spiral wrapping/sleeving (Spirap) protection around it. Each end of the Spirap must be held with a clip position.
    Between the harness bundle breakout at the clip positions 1451 and the raceway Fan Harness Support Raceways (71-51-50, 01-100).
    Between the harness and the tubes 114/170 adjacent to the clip position 0913 and 0753.
    Between the harness bundle breakouts and the flange FC, between the clip positions 0819 and 0820.
    The harness length between the clip positions 1075 and 0897 and the flange FD.
  4. 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.
2. 1. Adjust the harness to get the minimum clearances. Refer to Step.
3. Torque the bolt or nut, as necessary, to the value given in the applicable installation SUBTASK for each of the harnesses.
4. 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.
5. 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.
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.
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 SPM TASK 70-42-05-400-501.
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 SPM TASK 70-42-08-400-501.

Identify the Clip Location

Install the 400VC to IDG Cable Assembly

Install the Vibration Harnesses/Transducer

Install the EEC and Ignition Supply Harness

SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

Install the EEC and Ignition Supply Harness

SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

SBE 71-0165: Install the EEC and Ignition Supply Harness

Install the General Services Harness

Install the Terminal Module

Install the EEC Harness

Pre SBE 75-0081: Install the EEC Harness

SBE 75-0081: Install the EEC Harness

Install the EEC Harness

SBE 73-0071: Install the EEC Harness

Install the EEC Harness

SBE 73-0071: Install the EEC Harness

Install the EEC Harness

SBE 73-0071: Install the EEC Harness

Install the EEC Harness

SBE 73-0071: Install the EEC Harness

Install the EEC Harness

SBE 73-0071: Install the EEC Harness

Install the EEC Harness

SBE 73-0071: Install the EEC Harness

Install the EEC Harness

Pre SBE 75-0081: Install the EEC Harness

SBE 75-0088: Install the EEC Harness

Install the EEC Harness

Install the ignition supply Harness

Install the Ignition Supply Harness

Install the EEC Flexible Hoses and the Tube 235

Visually Inspect the Backshells and Cable Clamps

Requirements After Job Completion

Follow-On Conditions

NONE

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:	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:	0AM53
Tool Number:	IAE 1R19416
Tool Name:	IAE 1R19416 EEC harness wrench

TASK 72-00-32-420-004-C00 LPC/Intermediate Case Module - Install The Electrical Harnesses, Installation-004 - SBE 79-0088

Export Control

Copyright

Applicability

Common Information

TASK 72-00-32-420-004-C00 LPC/Intermediate Case Module - Install The Electrical Harnesses, Installation-004 - SBE 79-0088

General

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-00-32-420-534 Electrical Harness Installation Procedure

SUBTASK 72-00-32-420-535 Install the 400VC to IDG Cable Assembly (24-21-43, 01-010)

WARNING

SUBTASK 72-00-32-420-536 Install the Vibration Harnesses/Transducer (Pre SBE 71-0271 and SBE 71-0271)

SUBTASK 72-00-32-420-537 Install the EEC and Ignition Supply Harness (71-51-42, 01-005) (Pre SBE 71-0165, SBE 71-0165 and SBE 71-0177)

NOTE

NOTE

SUBTASK 72-00-32-420-538 Install the General Services Harness (71-51-43, 01-005)

SUBTASK 72-00-32-420-539 Install the EEC Harness (71-51-41, 01-005) (Pre SBE 75-0081 and SBE 75-0081)

NOTE

CAUTION

WARNING

WARNING

WARNING

NOTE

SUBTASK 72-00-32-420-540-A00 Connect the EEC Harness Connector 4017 KS-A (Pre SBE 73-0071 and Pre SBE 71-0183)

SUBTASK 72-00-32-420-540-B00 Connect the EEC Harness Terminal Connector 4017 KS-A (SBE 73-0071 and SBE 71-0183)

WARNING

CAUTION

SUBTASK 72-00-32-420-541 Install the Ignition Supply Harness (71-51-44, 01-005)

NOTE

SUBTASK 72-00-32-420-542 Install the EEC Flexible Hoses and the Tube 235

SUBTASK 72-00-32-220-128 Measure the Harness Clearance and Examine the Routing

SUBTASK 72-00-32-420-543 Attach the Harnesses Together

SUBTASK 72-00-32-210-091 Visually Inspect the Electrical Backshells and Cable Clamps

SUBTASK 72-00-32-210-092 Visually Inspect the EEC Harness (01-005) Electrical Backshells and Cable Clamps (SBE 70-0813)

NOTE

Figure: Identify the Clip Location

Identify the Clip Location

Figure: Install the 400VC to IDG Cable Assembly

Install the 400VC to IDG Cable Assembly

Figure: Install the 400VC to IDG Cable Assembly

Install the 400VC to IDG Cable Assembly

Figure: Install the 400VC to IDG Cable Assembly

Install the 400VC to IDG Cable Assembly

Figure: Install the Vibration Harnesses/Transducer

Install the Vibration Harnesses/Transducer

Figure: Install the Vibration Harnesses/Transducer

Install the Vibration Harnesses/Transducer

Figure: Install the Vibration Harnesses/Transducer

Install the Vibration Harnesses/Transducer

Figure: Install the Vibration Harnesses/Transducer

Install the Vibration Harnesses/Transducer

Figure: Install the EEC and Ignition Supply Harness

Install the EEC and Ignition Supply Harness

Figure: Install the EEC and Ignition Supply Harness

Install the EEC and Ignition Supply Harness

Figure: SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

Figure: Install the EEC and Ignition Supply Harness

Install the EEC and Ignition Supply Harness

Figure: Install the EEC and Ignition Supply Harness

Install the EEC and Ignition Supply Harness

Figure: Install the EEC and Ignition Supply Harness

Install the EEC and Ignition Supply Harness

Figure: SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

Figure: SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

SBE 71-0165 and SBE 71-0177: Install the EEC and Ignition Supply Harness

Figure: SBE 71-0165: Install the EEC and Ignition Supply Harness

SBE 71-0165: Install the EEC and Ignition Supply Harness

Figure: Install the General Services Harness

Install the General Services Harness

Figure: Install the General Services Harness

Install the General Services Harness