Lincoln Electric SVM208-A ROTOR “FLASHING” CIRCUIT TEST continued, 201A, 202A+, Procedure, F-18

Models: SVM208-A

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F-18

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F-18

TROUBLESHOOTING AND REPAIR

F-18

 

ROTOR “FLASHING” CIRCUIT TEST (continued)

FIGURE F.3 – BRUSH HOLDER LEADS 201(-) AND 202B (+)

201A(-)

SLIP

RINGS

202A(+)

PROCEDURE

1.With the 3/8” nutdriver, remove the 20 sheet metal screws that hold the top cover to the con- trol box. Remove the top cover.

2.Locate and remove lead #201A from the brush holder. See Figure F.3 for location.

3.Connect the negative (-) lead of the DC amme- ter to lead #201A and the positive (+) lead to the brush holder.

4.Remove lead #7 from field diode bridge rectifier D2. See Figure F.4. Electrically isolate the lead.

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FIGURE F.4 – DIODE BRIDGE LEAD ASSIGNMENTS

200

200C

7

+

 

201

 

 

 

 

 

 

 

9

 

 

 

 

 

 

 

201

BULLDOG® 140

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Lincoln Electric SVM208-A ROTOR “FLASHING” CIRCUIT TEST continued, 201A, 202A+, Troubleshooting And Repair, Procedure