TASK 78-32-77-300-002 Right C-Duct Electrical Harness - Replace The Connector, Repair-002 (VRS2129)

DMC:V2500-A0-78-32-7700-01A-920A-C|Issue No:002.00|Issue Date:2015-08-01

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 78-32-77-300-002 Right C-Duct Electrical Harness - Replace The Connector, Repair-002 (VRS2129)

Effectivity

FIG/ITEM

PART NO.

01-150

740W0288-503

General

Price and availability - refer to Rohr Inc.

Repair may be done by removal and replacement of the damaged connector(s).

Equivalent equipment may be used.

To identify the consumable materials refer to the PCI.

Repair Parts

FIG/ITEM

PART NO.

PART IDENT

QTY

01-210

S700Y0847

Plug, Sealing

1

01-240

S700Y0838

Receptacle

1

01-270

D38999-26KA98SN

Plug

1

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Contact removal/insertion toolLOCALContact removal/insertion tool
Connector pliersLOCALConnector pliers

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPERLOCALCoMat 02-002
CoMat 02-176 LOCKWIRELOCALCoMat 02-176
CoMat 02-177 MASKING TAPE (GLASS CLOTH)LOCALCoMat 02-177
CoMat 06-131 MARKING PEN0AM53CoMat 06-131

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 78-32-77-350-052 Remove the Damaged Connector

    1. Refer to Figure.

      2. Remove the strain relief

      1. Remove the lockwire from the strain relief screws and the strain relief.

      2. Remove the screws and the strain relief clamping bars from the strain relief.

      3. Remove the strain relief from the backshell and move it along the harness away from the backshell.

      4. Remove the tape from the harness under the clamping bar locations.

      3. Remove the grounding ferrule from the backshell

      1. Remove the grounding ferrule from under the braided wire shields and move it along the harness away from the backshell.

      2. Do not damage the braided wire shields.

      4. Remove the backshell from the connector

      1. Remove the lockwire from the backshell nut and the backshell.

      2. Remove the backshell from the connector.

      5. Identify the contacts

      1. Put a piece of CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER general purpose paper masking tape on the wire to which contacts are connected.

      2. Make a mark on the tape to identify the connector holes in which the contacts are installed.

      6. Remove the contacts

      1. Use the Contact removal/insertion tool to remove the contacts from the connector.

    2. SUBTASK 78-32-77-350-053 Install the New Connector

    1. Refer to Figure.

      2. Install the contacts in the connector

      1. Install the contacts in the connector with the Contact removal/insertion tool. Install the sealing plugs in to the rear of the contacts which are not attached to wires.

      2. Push on the contacts from the front of the connector to make sure that they are fully installed.

      3. They are fully installed if they do not move rearward when you push them from the front of the connector.

      4. Remove the tape markers from the wires.

      3. Install the backshell on the connector

      1. Install the backshell on the connector.

      2. Tighten the backshell nut by hand plus one eighth turn with the Connector pliers.

      3. Safety the backshell nut with CoMat 02-176 LOCKWIRE.

      4. Install the grounding ferrule

      1. Move the grounding ferrule toward the backshell and under the braided wire shields.

      2. Put the braided wire shields evenly over the grounding ferrule.

      3. Push the grounding ferrule in to the backshell. Shape the braided wire shields over the top of the grounding ferrule and along the outer jacket of the harness.

      4. The braided wire shields must end at the aft end of the strain relief.

      5. Install the strain relief on the backshell

      1. Put enough CoMat 02-177 MASKING TAPE (GLASS CLOTH) on the electrical harness and over the ends of the braided wire shields so that the strain relief clamping bars will fit tight on the wire harness.

      2. It is not necessary for the clamping bars to fit tight against the strain relief.

      3. Install the strain relief on the backshell.

      4. Tighten the strain relief until firmly gripped connector pliers slip on the strain relief.

      5. Install the clamping bars on the strain relief with the screws.

      6. Torque the screws to between 12 and 15 lbfin (1 and 2 Nm).

      7. Safety the screws with CoMat 02-176 LOCKWIRE.

    3. SUBTASK 78-32-77-220-053 Examine the Completed Repair

      1. Visually examine

      1. Examine the completed repair to make sure all the requirements of this repair procedure are done.

    4. SUBTASK 78-32-77-750-052 Test the Left C-Duct Electrical Harness

      1. Test the harness

      1. Refer to Testing-001 TASK 78-32-47-700-301.

    5. SUBTASK 78-32-77-350-054 Identify the Repair

      1. Make a mark VRS2129 adjacent to the assembly number.

      1. Use CoMat 06-131 MARKING PEN of a color that contrasts.

    6. Figure: Right C-Duct Electrical Harness Connector Replacement

    Right C-Duct Electrical Harness Connector Replacement

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised note to remove "materials or".(PSAF 15VC314)

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
Manufacturer Code:LOCAL
Supply Number:CoMat 02-002
Type:sp01
Supply Short Name:CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER
Supply Name:CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER
Specification Groups:
Doc NumberType
JCR-198SCOTCH 202 PREMIUM GRADE (A-A-883 TYPE I)
OMAT: 237SCOTCH 202 PREMIUM GRADE (A-A-883 TYPE I)
Suppliers:
ManufacturerRemarks
LOCAL
94960
K0993
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 02-176
Type:sp01
Supply Short Name:CoMat 02-176 LOCKWIRE
Supply Name:CoMat 02-176 LOCKWIRE
Specification Groups:
Doc NumberType
AIA/NAS NASM20995 Part Number MS20995N20 (0.5 MM)
Suppliers:
ManufacturerRemarks
LOCAL
V508V
Manufacturer Code:LOCAL
Supply Number:CoMat 02-177
Type:sp01
Supply Short Name:CoMat 02-177 MASKING TAPE (GLASS CLOTH)
Supply Name:CoMat 02-177 MASKING TAPE (GLASS CLOTH)
Specification Groups:
Doc NumberType
SCOTCHBOY NO. 361
Suppliers:
ManufacturerRemarks
LOCAL
76381
Manufacturer Code:0AM53
Supply Number:CoMat 06-131
Type:sp01
Supply Short Name:CoMat 06-131 MARKING PEN
Supply Name:CoMat 06-131 MARKING PEN
Suppliers:
ManufacturerRemarks
0AM53
Link not Found
Manufacturer Code:LOCAL
Tool Number:Contact removal/insertion tool
Tool Name:Contact removal/insertion tool