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F-16

TROUBLESHOOTING AND REPAIR

F-16

 

ROTOR RESISTANCE TEST (continued)

 

FIGURE F.2 – LOCATION OF ROTOR SLIP RINGS

-+

Lead 219

Lead 200A

 

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TEST PROCEDURE

1.With the 5/16” nut driver, remove the 6 sheet metal screws from the case top.

2.Remove the rubber gasket (cover seal) from the lift bail.

3.Remove the fuel cap. The rubber gasket for the fill tube will come off with the case top.

4.Remove the case top, then replace the fuel cap.

5.With the 5/16” nut driver, remove the 5 screws holding the right case side.

6.Remove the right case side by lifting up and out.

7.Conduct the test with the gasoline engine OFF.

8.Remove the spark plug wires to prevent acci- dental engine kickback or starting.

9.Isolate the rotor electrically by removing the generator brush leads. Refer to Figure F.2 as you perform the remaining steps.

10.Remove lead 219 from the negative brush.

11.Remove lead 200A from the positive brush.

12.Measure the resistance across the rotor slip rings.

A.Set the ohmmeter on the low scale (X1).

B.Place one meter probe on one of the rotor slip rings. Place the other probe on the other slip ring.

C.Check the resistance across the slip rings. It should read between 4 and 5 ohms.

EAGLE™ 10,000

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Lincoln Electric SVM192-A service manual Rotor Resistance Test, Remove the case top, then replace the fuel cap

SVM192-A specifications

Lincoln Electric's SVM192-A is a standout model in the sphere of welding machines, renowned for its advanced technology and versatility, making it a preferred choice among welding professionals and industrial applications. This single-phase inverter-based machine balances performance and portability, providing users with a reliable solution for a variety of welding tasks.

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