What was found
ETOPS-AT 1000' AFTER T/O ECAM AIR ENGINE 2 BLEED FAULT. PERFORMED ECAM ACTIONS AND OEB. CONTACTED MOC, RESET BLEED AFTER COOLING PERIOD. SYSTEM OPERATED NORMALLY FOR DURATION OF FLIGHT. POST FLIGHT SHOWS "PRESS REG-V (E2-4001HA)" 361152. REPLACED NR 2 ENGINE PRV, PER AMM 36-11-52. OPERATIONS AND LEAK CHECK OK. VALVE, BLEED, P OFF 43-3611-9-0002 02831 ON 43-3611-9-0002 03322.