What was found
ENG 2 COMPRESSOR VANE ECAM ON INITIAL T/O/ROLL CONNECTOR. ANY QUESTIONS PLEASE CALL TOMC EMC DESK. R. TOTH 15JUN2023. REFERENCE MT TIP 75-002 - COMPRESSOR VANE MESSAGE RESULTING IN AHM ALSO SHOWING 2.5 BLEED FAULT MESSAGE ASSOCIATED WITH VSV REMOVED AND REPLACED VSV ACTUATOR AT #2 ENGINE AS PER AMM PERFORMED TEST #3 AS PER MM71-00-00-710-012 AND TEST 11 AS PER ABORTED TAKEOFF. WILL REQUIRE REPLACEMENT OF THE VSVA. ACTUATOR. ALONG WITH REPLACING THE VSV ACTUATOR PLEASE CHECK J3 75-32-41. NEED TO PEFORM OPS AND LEAK CHECK. PARTS USED: MM-71-00-00-710-012. ALL CHECS GOOD ON # 2 ENGINE MAINTENANCE POST FLIGHT REPORT ATTACHED. CONNECTOR AT EEC FOR ANY DISCREPANCIES OR BENT PINS. THAT 31-7532-9-0002,QTY :1 COMPONENT ALONG WITH THE VSV IS ASSOCIATED WITH THAT J3 ADD EMP:U214924 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1723100 SN OFF 8276 ACTUATOR, VARIA OFF 31-7532-9-0002 8276 ON 31-7532-9-0002 9864 PERFORMED IDLE LEAK CHECK ON ENG 2 VSV ACTUATOR. HIGH POWER ASSURANCE TEST GOOD.