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TROUBLESHOOTING AND REPAIR

F-17

CONTROL CABLE CONTINUITY TEST (continued)

FIGURE F.3 – CONTROL CABLE CONTINUITY TEST POINTS.

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CONTROL

CABLE

AMPHENOL

PLUG

D

E

TEST PROCEDURE

1.Disconnect the control cable amphenol plug from the welding power source and the wire feeder.

2.Using a multimeter, measure the resistance of the control cable wiring from the amphenol plug on the wire feeder end to the terminal connectors or amphenol plug on the welding power

C

B CONNECTOR LETTERING

SEQUENCE AS

VIEWED FROM

CAVITY END

A OF CONNECTOR

F

source end. Refer to the Wiring Diagrams in Section G, Table F.2, and Figure F.3 for wire designations.

3.If the conductor resistance measures greater than 1.0 Ohm, the cable is faulty and should be replaced. If the resistance between conductors is less than 0.5 MOhm, the cable is faulty and should be replaced.

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TABLE F.2 – CONTROL CABLE PIN AND LEAD DESIGNATIONS

SIX PIN AMPHENOL

LEAD NUMBERS

FOURTEEN PIN

WIRE FEEDER END

MACHINE END

AMPHENOL MACHINE END

 

 

 

A

4

D

B

2

C

C

32

A

D

31

J

E

CASE GROUND

B

F

21

H

 

 

 

LN-7 GMA WIRE FEEDER

Page 81
Image 81
Lincoln Electric SVM 106-A Control Cable Continuity Test, Connector Lettering Sequence AS Viewed from Cavity END