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Table 2-4. Troub leshooting - continued
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TM-5-6115-612-34 Gas Turbine Engine Driven Aviation Generator Set Manual
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Table 2-4. Troub leshooting - continued

ARMY TM  5-6115-612-34 MARINE CORPS TM 6115-34/8 AIR  FORCE TO  35C2-3-471-2 NAVY AG-320BO-MME-OOO 2-3. GENERAL. (cont) Table 2-4. Troubleshooting - continued MALFUNCTION TEST  OR  INSPECTION CORRECTIVE   ACTION Step 2. Connect voltmeter to P1-11(+). Release MASTER SWITCH to RUN. If voltage is less than 1.5 Vdc, replace microprocessor circuit  card  (paragraph  10-2b). If voltage is 1.5 Vdc or greater, connect voltmeter positive(+) to switch circuit card TB1-2. If voltage is less than 20 Vdc, replace switch card (paragraph 10-2b). If voltage is 20 Vdc or greater, check continuity. P2-20 to K2-X1 K2-A2 to E2 K2-X1 to E1 (ground) K2-A1 to J5-K Repair or replace as necessary. If continuity is present, replace  relay  K2  (paragraph  10-2g). 4. ENGINE  OVERTEMP  MALFUNCTION  -  PROBLEM  ISOLATED  TO  EECM. Step  1. Inspect and check continuity of wires from J5-R and J5-S to microprocessor  board  P2-6  and  P2-7. Repair  or  replace  wires  as  necessary. Step  2. Connect EECM under test to EECM tester. Short EGT input terminals   together. Move MASTER SWITCH to RUN position. Connect voltmeter to P1-8(+) and E1(-) ground terminal. If voltage is less than 1.5 Vdc, replace microprocessor circuit  card  (paragraph  10-2b). If voltage is 1.5 Vdc or greater, connect voltmeter positive(+) to switch circuit card Q1-C. If voltage is 19 Vdc  or  less,  replace  switch  circuit  card  (paragraph  10-2b). 5. OVERSPEED MALFUNCTION INDICATOR - PROBLEM ISOLATED TO EECM. Step 1. Inspect and check continuity of wires from J5-G to micro- processor  board  P2-5  and  from  J5-F  to  microprocessor  board  P2-8. If  no  continuity,  repair  or  replace  wires  as  necessary. If continuity present, go to Step 2. 2-43

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