What was found
BIRD STRIKE ENGINE 2 AT TAKEOFF IN BGA HIGH VIBRATION DURING CLIMB N1 6.0. IN ACCORDANCE WITH AMM TASK 72-00-00-200 006-A AND SUBTASKS 72-00-00-220-172-A (B1) 72-00-00-280-057-A BOROSCOPE INSPECTION OF THE STAGE 4 LP TURBINE BLADES, HPC STAGES 1, 3 AND 8 CONBUSTION CHAMBER DOME ASSEMBLY WAS PERFORMED, NO DAMAGES WERE FOUND. IN ACCORDANCE WITH AMM 05-51-14-200-001-A, THE INSPECTION OF THE AIRFRAME AFTER A BIRD STRIKE ENGINE 2 WAS PERFORMED, AND AMM 72-00-00-200-006-A THE INSPECTION CHECK OF FOD WAS PERFORMED, AND NO ADDITIONAL DAMAGE FOUND. IN ACCORDANCE WITH AMM 71-00-00-710-009- THE VIBRATION CHECK WAS PERFORMED. THE VIBRATION VALVES ENGINE 2 MAX CLIMB 0.6% AND N2 0.3%.