As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER T/O POWER WAS APPLIED, THE NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE AND N2 OVERLIMIT INDICATION DISPLAYED, PROMPTING THE CREW TO REJECT TAKE OFF AND RETURN THE ACFT TO THE BLOCK. TROUBLESHOOTING MANUAL, VSV ACTUATOR ON THE NR 1 ENGINE WAS REPLACED AND VSV MECHANISM WAS LUBRICATED IAW MM AND PERFORMED ALL REQUIRED TESTS WITHOUT FAILURE. IAW DATA OBTAINED, IT WAS DETERMINED THAT THE N2 OF THE NR 1 ENGINE DID NOT GO BEYOND LIMITS. THE AIRCRAFT WAS RETURNED TO SERVICE.