TASK 72-00-32-450-001 LPC/Intermediate Case Module Components - Installation Of The Electronic Engine Control (EEC), Installation-008

DMC:V2500-A0-72-00-3250-00A-720A-B|Issue No:002.00|Issue Date:2016-08-01

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

All

Common Information

TASK 72-00-32-450-001 LPC/Intermediate Case Module Components - Installation Of The Electronic Engine Control (EEC), Installation-008

General

This TASK gives the procedure to install the electronic engine control (EEC) on the LP compressor/intermediate case module.

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

For installation of preformed packings, refer to SPM TASK 70-44-01-400-501.

For the connection of electrical plugs during engine maintenance, refer to SPM TASK 70-43-00-400-501.

For installation and the reuse of self-locking fasteners, refer to SPM TASK 70-42-01-400-501.

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

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

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

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

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 application Chapter/Section/Subject comes before the Fig/item number.

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
IAE 1R19416 EEC harness wrench0AM53IAE 1R194161

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-126 LOCKWIRELOCALCoMat 02-126
CoMat 02-141 LOCKWIRELOCALCoMat 02-141
CoMat 02-274 SAFETY CABLE KITLOCALCoMat 02-274
CoMat 02-275 SAFETY CABLE KITLOCALCoMat 02-275
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Seal ring1
Seal ring1
Seal ring1
Seal ring2

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-32-450-066 Remove the Protective Covers

    1. Remove the protective covers from all the openings on the EEC.

    2. SUBTASK 72-00-32-450-067 Prepare the Replacement EEC

    1. Refer to Figure

      2. Install the seal rings on the adaptors and unions.

      1. NOTE

        Do not apply white petrolatum to the new seal rings V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-271, V2500-A5-73-22-34-01A-941A-D 73-22-34, 01-275, V2500-A5-73-22-34-01A-941A-D 73-22-34, 01-278 or V2500-A5-73-22-34-01A-941A-D 73-22-34, 01-282).

        Install the seal ring V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-271) 1 off, on the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-270).

      2. Install the seal ring V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-275) 1 off, on the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-274).

      3. Install the seal ring V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-278) 1 off, on the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-277).

      4. Install the seal rings V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-282) 2 off, on the adapters V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-284).

    3. NOTE

      Do not apply lubricant to the threads.

      Install the adapters and unions into their related openings in the bottom of the EEC.

      4. Torque the adapters and unions.

      1. Torque the adapters V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-284) to 221 lbfin to 239 lbfin (25 Nm to 27 Nm).

      2. Torque the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-277) to 248 lbfin to 265 lbfin (28 Nm to 30 Nm).

      3. Torque the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-274) to 195 lbfin to 212 lbfin (22 Nm to 24 Nm).

      4. Torque the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-270) to 168 lbfin to 181 lbfin (19 Nm to 20.5 Nm).

    3. SUBTASK 72-00-32-450-068 Install the EEC

    1. WARNING

      BE CAREFUL DURING THE INSTALLATION OF THE EEC. IT WEIGHS APPROXIMATELY 41 LBS (18.6 KG).

      Refer to Figure.

    2. Apply clean CoMat 10-077 APPROVED ENGINE OILS to the threads of the four bolts V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-300).

    3. Install the four washers V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-305) on the bolts.

    4. Install the EEC V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-280) on the mount brackets.

    5. Install the bolts and the washers.

    6. Torque the bolts to 180 lbfin to 220 lbfin (20 Nm to 25 Nm).

    7. Apply clean CoMat 10-077 APPROVED ENGINE OILS to the threads of the bolt V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-340).

    8. Install the bolt through the ground cable V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-320) in to the EEC.

    9. Torque the bolt to 85 lbfin to 105 lbfin (10 Nm to 12 Nm).

    4. SUBTASK 72-00-32-450-069 Install the Vent Plug Assembly

    1. Refer to Figure

    2. Apply clean CoMat 10-077 APPROVED ENGINE OILS to the threads of the vent plug assembly V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-290).

    3. Install the vent plug assembly in to the vent plug opening on the bottom of the EEC.

    4. Torque the vent plug assembly to 90 lbfin to 100 lbfin (10.17 Nm to 11.30 Nm) and safety with CoMat 02-141 LOCKWIRE.

    5. SUBTASK 72-00-32-450-070 Connect the Electrical Connectors to the Front and Rear Sides of the EEC

    1. Connect the 4000KS-J5, 4000KS-J7, 4000KS-J8, 4000KS-J9 and 4000KS-J10 electrical connectors to its related receptacle on the rear side of the EEC. Torque the connectors to 32 * lbfin (3.6 Nm). Use theIAE 1R19416 EEC harness wrench 1 off.

    2. Connect the 4000KS-J11, 4000KS-J1, 4000KS-J2, 4000KS-J3 and 4000KS-J4 electrical connectors to its related receptacle on the front side of the EEC. Torque the connectors to 32 * lbfin (3.6 Nm). Use the IAE 1R19416 EEC harness wrench 1 off.

    3. Connect the data entry plug assembly to the receptacle J6 on the rear side of the EEC. Torque the connector 32 * lbfin (3.6 Nm). Use the IAE 1R19416 EEC harness wrench 1 off.

    6. SUBTASK 72-00-32-450-071 Connect the Flexible Hoses

    1. Refer to Figure.

    2. Remove the protective covers from the flexible hoses.

      3. Connect the flexible hose to the adapters and unions on the bottom of the EEC and torque the nuts.

      1. Connect the flexible hose ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49,12-500) to the adapter V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-284) and torque the nut to 142 lbfin to 150 lbfin (16 Nm to 17 Nm).

      2. Connect the flexible hose Fuel System Air Tubes (73-22-49, 08-500) to the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-277) and torque the nut to 182 lbfin to 199 lbfin (20.5 Nm to 22.5 Nm).

      3. Connect the flexible hose Fuel System Air Tubes (73-22-49, 04-100) to the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-274) and torque the nut to 182 lbfin to 199 lbfin (20.5 Nm to 22.5 Nm).

      4. Connect the flexible hose Fuel System Air Tubes (73-22-49, 07-500) to the union V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-270) and torque the nut to 142 lbfin to 150 lbfin (16 Nm to 17 Nm).

      5. Connect the flexible hose ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 11-500) to the adapter V2500-A5-73-22-34-01A-941A-D (73-22-34, 01-284) and torque the nut to 142 lbfin to 150 lbfin (16 Nm to 17 Nm).

    7. SUBTASK 72-00-32-750-053-A00 V2500-A1: Do a Test of the EEC

    1. Refer to TASK 71-00-00-700-052-A00 (TESTING-000, CONFIG-001).

    8. SUBTASK 72-00-32-750-053-B00 V2500-A5: Do a Test of the EEC

    1. Refer to TASK 71-00-00-700-052-B00 (TESTING-000, CONFIG-002).

    9. SUBTASK 72-00-32-210-055 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 SPM TASK 70-42-05-400-501.

    10. SUBTASK 72-00-32-210-056 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.

    1. NOTE

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

      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.

    4. Examine EEC ground strap ends to ensure strap is securely fastened at (2) crimping locations. Refer to Figure.

      NOTE

      Replace the strap if wire crimp is found disconnected or moveable.

    11. Figure: Installation of the Electronic Engine Control (EEC)

    Sheet 1

    Legend
    Installation of the Electronic Engine Control (EEC)

    Sheet 1

    Close

    Figure: Installation of the electronic engine control (EEC)

    Sheet 2

    Legend
    Installation of the electronic engine control (EEC)

    Sheet 2

    Close

    Figure: Visually inspect the backshells and cable clamps

    Visually inspect the backshells and cable clamps

    Figure: Ground Cable

    Ground Cable

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised procedural step 10 to examine EEC ground strap and added figure 4. (16VC056)

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:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
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 02-141
Type:sp01
Supply Short Name:CoMat 02-141 LOCKWIRE
Supply Name:CoMat 02-141 LOCKWIRE
Specification Groups:
Doc NumberType
AS3214-02 (0.8 mm)AMS 5689
Suppliers:
ManufacturerRemarks
LOCAL
81343
IE508
58401
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: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