What was found
(CAN) NR 2 AC GEN CAUTION ON LANDING. INITIAL RUN SHOWED NO LOAD ON NR 1 AC GEN BUSS, ALL THE LOAD WAS BEING HANDLED BY THE NR 2 GEN (INDICTATED AS 116 VOLTS ON ALL THREE PHASES ON NR 1 WITH LOAD OF 0.01, ON NR 2 VOLTAGE WAS 114 VOLTS WITH A LOAD OF 0.19 ON ALL PHASES) WHEN POWER LEVER WAS BROUGHT FROM FLIGHT IDLE TO DISC OR DISC TO FLIGHT IDLE, NR 2 AC GEN CAUTION LIGHT ILLUMINATED AND NR 2 LOAD FELL TO ZERO ON ALL PHASES AND NR 1 LOAD CLIMBED TO 0.21 WITH VOLTAGE REMAINING AT 116 VOLTS. SWAPPED GCUÏ¿½S ,NO CHANGE. SWAPPED BACK REPLACED #2 AC GENERATOR AND RAN A/C AGAIN, GOT BETTER SHARING OF OUTPUT LOADS ON EACH INDIVIDUAL BUS BUT THE SAME RESULT WITH THE POWER LEVER ADVANCEMENT OR RETARDING WITH THE NR 2 AC GEN CAUTION LIGHT, STILL ILLUMINATING AND LOAD INDICATION ON ELECTRICAL PAGE. UPON FUTHER TROUBLESHOOTING FOUND PIN C OF CONNECTOR 9811-718 SHORTING TO GND. SHIELD TERMINATION SOLDER SLEEVE REMOVED FROM WIRE AND FOUND WIRE EXPOSED AND SHORTING THROUGH THE SOLDER SELEEVE TO GROUND. WIRE W20002B-12-1 IS TO BE RETERMINATED AT CONNECTOR 9811-P718.