What was found
AS THROTTLES WERE ADVANCED FOR TAKEOFF WITH THROTTLE POSITION EQUAL, ENGINE NR 1 N1 HUNG BACK AT 20 PERCENT WITH ENG NR 2 AT 70 PERCENT. UNABLE TO MAINTAIN RUNWAY CENTER LINE. REJECTED TAKEOFF AT LESS THAN 10 KTS. PERFORMED MAX POWER ASSURANCE RUN PER JRH 18.1 PG 5. PERFORMED ACCEL CHECK, FROM FLT IDLE TO T/O POWER WAS 6 SEC, THIS IS WITHIN LIMITS ALL IAW A300 M/M 71-00-00 PG 565.