What was found
AIRCRAFT REJECTED TAKEOFF AT 120 KNOTS, DUE TO AN ABNORMAL VIBRATION IN THE LT MLG. PERFORMED HIGH ENERGY STOP INSPECTION & AIRFRAME VIBRATION CONDITION INSPECTION IAW AMM 05-51-07 & AMM 05-51-67, DETECTED LT MLG BRAKES & WHEELS NRS 1 & 2 DAMAGED, LT MLG AXLE DAMAGED & LT CTR & INNER MAIN GEAR DOORS MISSING. LT MLG & WHEELS NRS 1 & 2 REPLACED IAW AMM 32-41-41 & AMM 32-45-11, LT MLG AXLE REPLACED IAW AMM 32-11-85. THE MLG LOWER SIDE STRUT WAS FOUND WITH LIGHT TWIST, SO THE LOWER SIDE STRUT WAS REPLACED IAW AMM 32-11-61.