What was found
ENG 1 BLEED LEAK, FOLLOWED BY APU AND ENG 2 BLEED LEAK ECAMS. - TOMC KROWN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM CHECK BLEED SYSTEM FOR POSSIBLE LEAKS AND CALL TOMC 847-700-9980 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM CHECK BLEED SYSTEM FOR POSSIBLE LEAKS AND CALL TOMC 847-700-9980 FOUND PNEUMATIC LEAK FROM CLAMP FORWARD OF OZONE CONVERTER ASSY RIGHT PACK PNEUMATIC CLAMP ADJUSTED AND TIGHTENED. LEAK CHECK GOOD. BMC 2 LAST LEG REPOT FAULTED X FEED VALVE 6HV. REMOVED AND INSTALLED CROSSBLEED VALVE 6HV IAW REFERENCE: 36-12-52/401. OPERATIONAL TESTED OF THE APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS REFERENCE: TASK 36-12-00-710-001-A OPS CHECK GOOD. VALVE, ISOLATIO OFF 31-3612-9-9001 0657 ON 31-3612-9-9001 5676 VALVE, ISOLATIO OFF 31-3612-9-9001 0657 ON 31-3612-9-9001 5676 PARTS USED: 31-3612-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1324223 SN OFF 0657 PRESSURIZED AIRCRAFT IAW PRESSURIZATION TEST FOR AIR LEAKAGE OR A DIFFERENTIAL PRESSURE OF 280 MBAR (4.06 PSI) REFERENCE: TASK 05-53-00-780-001-A. AIRCRFT PRESSURIZED NORMAL AND HELD STABLE PRESSURE. PACK 2 REINSPECTED AND FOUND NO OTHER LEAKS. NO ECAM MSGS. REVIEWED MAINT PERFORMED WITH TOMC AND OK TO RETURN TO SERVICE.