What was found
BIRDSTRIKE ON BASE-TO-FINAL TURN FOR PHL RWY 27R. POST-FLIGHT REVEALED EXTENSIVE DAMAGE TO RH WING LEADING EDGE INBOARD OF #3 ENGINE. INSTALLED R/H WING #2 SLAT PER AMM 27-80-20-400-802 , PERFORMED ADJUSTMENT PER AMM 27-80-20-820-802 NO ISSUES NOTED AT THIS TIME. PERFORMED INSPECTION OF THE INBOARD SLAT CONTROL SURFACES AND TEST OF THE SLAT RANGE OF MOVEMENT PER AMM 27-80-20-200-801 AND 27-80-20-710-802. INSPECTION AND FUNCTION TEST GOOD. C/W AMM 27-80-20-820-802 VERIFIED TORQUE AND OPS TEST GOOD.