What was found
NR 4 MAIN TIRE BLEW ON LANDING. ANTI-SKID DID NOT RELEASE. CONNECTOR AT 18GG RECEPTICALS A & C AT CONNECTION ON NR 4 BRAKE SERVO VALVE INSTALLED IN WRONG POSITIONS. INSERTED WIRE (A)-4063 INTO A, AND INSERTED WIRE (C) -4062 INTO C IAW WDM 32-42-05, AND SCHEMATIC MANUAL 32-42-00, SCHEM 04 PG 101. PERFORMED A RIGHT MAIN GEAR BRAKES BLEEDING PROCEDURES MAIN GREEN SYSTEM AND ALT YELLOW SYST. REF AMM 32-42-00-3. ACCOMPLISHED ALL ADJUSTMENT AND TEST PROCEDURES FOR COMPONENTS REPLACED IAW AMM 32-42-00-05, NO LEAKS NOTED, REMOVED TEST EQUIPMENT FOM LEFT NOSE WHEEL REINSTALLED TACH WHEEL CAP ON LEFT NOSE TIRE IAW AMM 12-37-32-00-02. AIRCRAFT OK FOR SERVICE.