What was found
AFTER T/O THRUST WAS APPLIED AT 50 PERCENT POWER SET, POWER DROP TO 21.1 PERCENT ON RIGHT ENGINE, AIRCRAFT TURN TO THE RIGHT, REJECTED T/O WAS EXCECUTED. IAW TSM 77-00-00-810-852, OPERATIONAL TEST OF THE FADEC ON GROUND WITH ENGINE NON-MOTORING PERFORMED, IAW AMM 73-21-50-210-002, VISUALLY CHECK OF J9/J10 HARNESS CONNECTORS WERE PERFORMED SATISFACTORY, AND IAW AMM 71-00-00-710-025 ACELERATION CHECK OF ENGINE 2 PERFORMED SATISFACTORY.