What was found
REPEAT WRITE UP ANTISKID CAUTION LT ILLUMINATEDTOMC LOCKS FOR TSING AND REPAIR. ANTISKID INOP REPEAT. 2 HISTORY ITEMS ON 13TH. CREW DEBRIEF - CREW STATED ANTISKID LIGHT ILLUMINATED AFTER GEAR RETRACTION. LIGHT WENT ON AND OFF THROUGHOUT THE WHOLE FLIGHT. UPON LANDING LIGHT STAYED ILLUMINATED. LABOR HOURS UDATED ALONG WITH GROUND TIME . NORM ANTISKID" AND ALTN ANTISKID" STATUS MESSAGES PRESENT ON EICAS. PERFORMED ANTISKID AUTOBRAKE CONTROL UNIT BITE PROCEDURE IN REFERENCE TO 32-42 FAULT TREE 815 AND THE FOLLOWING MESSAGES WERE FLAGGED: XDCR 7, BOX 4-8, AND XDCR 8. REMOVED AND REPLACED AACU REFERENCE ELB PAGE NO 3536146 FOR WORK PERFORMED. PERFORMED RESISTANCE CHECKS ON #7 AND #8 TRANSDUCER AND FOUND THEM TO BE WITHIN LIMITS IN REFERENCE TO 32-42 FAULT TREE 815. PERFORMED RESISTANCE CHECK FROM THE AACU CONNECTOR (D2372A) PINS A5 AND A6 TO THE #8 TRANSDUCER CONNECTOR (D2026) PINS 1 AND 3 AND FOUND THE RESISTANCE VALUES TO BE SATISFACTORY. ALSO PERFORMED RESISTANCE CHECK FROM THE AACU (D2372A) PINS A12 AND A13 TO THE #7 TRANSDUCER CONNECTOR D2024 PINS 1 AND 3 AND FOUND THE RESISTANCE TO BE 354OHMS REFERENCE WDM 32-42-11-1. DISCONNECTED CONNECTOR D6993P AT THE J6 JUNCTION BOX AND PINS 1 AND 3 ON CONNECTOR D2026 RREF WDM 32-42-22-1 FOUND OPEN WIRE W1524-204R-20. RE-TERMINATE WIRE ON D5032P. CLEANED CONNECTIONS AND RAN TESTS FOR WHEEL SPIN UP TEST REF AMM 32-42-00 AND ANTISKID SYSTEM OPERATIONAL TEST. ALL TESTS PASSED, ANTISKID SYSTEM RETURNED TO OPERATION.