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 23-44-41-300-001 Maintenance Interphone Jack Cable - Replace The Connectors, Repair-001 (VRS2977)
General
This repair can be done on the harnesses during overhaul, or while they are installed on the engine. Replace only the parts of the connectors which are unserviceable.
To identify the consumable materials, refer to the PCI.
Part No. identified with (*) will have 387A before it.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Strap Wrench | LOCAL | Strap Wrench | TG-70 or BT-BS-611 | |
| Torque Wrench - 0 to 1000 lbf.in range | LOCAL | Torque Wrench | ||
| Extractor/inserter tool | LOCAL | Extractor/inserter tool | 16g or 20g |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-127 LOCKWIRE | LOCAL | CoMat 02-127 | ||
| CoMat 02-138 LOCKWIRE | LOCAL | CoMat 02-138 | ||
| CoMat 02-141 LOCKWIRE | LOCAL | CoMat 02-141 | ||
| CoMat 06-153 FELT TIP MARKER, RAPID DRYING | 0AM53 | CoMat 06-153 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Be careful not to cause damage to the lockwire holes.
Cut and remove the lockwire from the screws, the coupling nut, the shell and the connector.
Use the CoMat 06-153 FELT TIP MARKER, RAPID DRYING marking pen.
If the backshell is not a straight type, make a mark on the shell which aligns with the master keyway.
Remove the screws and the strain-relief clamp from the coupling nut.
Use the applicable Strap Wrench - (BT-BS-611 or TG-70).
Move the coupling nut and the grounding ferrule away from the shell.
Be careful not to cause damage to the ground-shields of the cables.
Remove the coupling nut from the shell.
Use the applicable Strap Wrench - (BT-BS-611 or TG-70).
Move the shell away from the connector.
Be careful not to cause damage to the ground-shields of the cables.
Remove the shell from the connector.
SUBTASK 23-44-41-350-053 Disassemble the Connector Assembly

WARNING
PUT ON PROTECTIVE GOGGLES WHEN YOU CUT THE LOCKWIRE. PIECES OF THE LOCKWIRE CAN CAUSE DAMAGE TO YOUR EYES.Refer to Figure.
Write on the tag the number of the connector hole from which the cable came.
Attach a temporary identification tag to each of the cables in the connector.
Use the applicable Extractor/inserter tool - (16g or 20g).
Put the cable in the groove of the tool.
Push the tool along the cable and into the rear of the connector, until it touches the contact (the tool will open the collet).
Hold the cable and the tool together and remove the contact from the rear of the connector.
Remove a contact from the connector.
Do Step again, for the remaining contacts.
Remove the remaining contacts from the connector.
SUBTASK 23-44-41-350-054 Remove the Contacts from the Connector
Be careful not to cause damage to the contacts of the ground-shields.
Remove the shell, the grounding ferrule and the coupling nut, from the harness.
SUBTASK 23-44-41-350-055 Remove the Components of the Connector Assembly
Refer to INSPECTION-001 TASK 23-44-41-200-301.
Reject the parts which are unserviceable.
Examine the connector, the contacts, the coupling nut, the grounding ferrule, the screws and the shell.
SUBTASK 23-44-41-220-054 Examine the Components
Refer to Figure.
Install the components in the sequence that follows: the coupling nut, the grounding ferrule and the shell.
Be careful not to cause damage to the contacts or the ground-shields.
Install the new, or serviceable, components to the harness.
SUBTASK 23-44-41-350-056 Install the Replacement Components of the Connector Assembly

CAUTION
THE REPLACEMENT COMPONENTS MUST HAVE THE SAME PART NUMBERS AS THE COMPONENTS WHICH WERE REMOVED. INCORRECT COMPONENTS CAN CAUSE DAMAGE TO THE SYSTEM.Refer to Figure.
You must install the contacts at the center of the connector first and work out.
Find the contact which must be installed in the center hole of the connector.
Use the applicable Extractor/inserter tool - (16g or 20g).
Put the cable in the groove of the tool.
Push the tool along the cable until it touches the flange of the contact.
Hold the cable and the tool together and use the tool to push the contact into the connector hole.
When the contact is in the correct position, in the connector hole, release the cable and remove the tool.
Lightly pull the cable to make sure that the contact is engaged correctly in the connector.
Install the center contact to the connector.
Do Step again, for the remaining contacts.
Make sure the contacts are installed in the positions noted, during their removal.
Install the contacts nearest to the center first.
Install the remaining contacts to the connector.
Remove the temporary tags, which were installed in Step.
Remove the identification tags from the cables.
SUBTASK 23-44-41-350-057 Install the Contacts to the Connector

CAUTION
THE CONTACTS MUST BE INSTALLED IN THEIR CORRECT POSITIONS IN THE CONNECTOR. IF THEY ARE INSTALLED IN THE INCORRECT POSITIONS, THE SYSTEM CAN BE DAMAGED.Refer to Figure.
Use the applicable Strap Wrench - (BT-BS-611 or TG-70), to tighten the shell.
If the backshell is not a straight type, align the mark (made in Step ) with the master keyway.
Install the shell to the connector.
Put the ground-shields and equal distance apart around the shell.
Push the ground ferrule along the harness, until it touches the ground-shields.
Put the ground-shields through the coupling nut.
Install the coupling nut to the shell.
Use the Torque Wrench - 0 to 1000 lbf.in range and the applicable Strap Wrench (BT-BS-611 or TG-70), to torque the coupling nut to 10 lbf in. (1.13 Nm).
Install the coupling nut to the shell.
Make sure that all of the twists and bends are out of the cables.
Attach the clamp to the coupling nut with the two screws.
Use the Torque Wrench - 0 to 1000 lbf.in range to torque the screws to between 10 and 20 lbf in. (1.13 and 2.26 Nm).
Install the strain-relief clamp to the coupling nut.
SUBTASK 23-44-41-350-058 Assemble the Connector Assembly
Refer to TASK 23-44-41-700-301.
Do the test for continuity and insulation.
SUBTASK 23-44-41-750-052 Do a Continuity and Insulation Test on the Connector Assembly
Refer to Figure.
Make sure that the connector, the shell, the coupling nut and the screws are all safetied.
Safety the connector assembly.
SUBTASK 23-44-41-350-059 Safety the Connector Assembly
Use the CoMat 06-153 FELT TIP MARKER, RAPID DRYING marking pen.
Put the repair scheme number VRS2977 on the identification sleeve of the harness, adjacent to the part number.
SUBTASK 23-44-41-850-053 Put the Repair Scheme Number on the Harness
Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

