What was found
(CAN) #3 MAIN WHEEL TIRE CAP SEPARATION ON TAKEOFF. AIR TURN BACK TO AIRPORT. AIRCRAFT SUSTAINED DAMAGE TO #2 ENGINE FAN BLADES, ENGINE INTAKE ACOUSTIC PANELS, R/H INBOARD TRAILING EDGE FLAP. ONE LINE OF THE YELLOW HYDRAULIC SYSTEM BROKE IN AREA OF R/H MAIN LANDING GEAR AREA. THE R/H HORIZONTAL STABILIZER DENTED AND HOLE ON THE UPPER SURFACE OF THE R/H WING ABOVE THE MAIN LANDING GEAR (R/H).REPAIRS WILL BE ACCOMPLISHED AFTER ENGINEERING EVALUATION.FINAL REEPORT FOR FIXES WILL BE PRODUCED AT A LATER DATE.