As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKE OFF, CAPTAIN REPORTED STRONG VIBRATION IN MLG. MX PERSONNEL DETECTED TREAD LOSS IN THE WHEEL POSITION NR 1 IN THE LT MLG, CRACK IN THE LT FLAP LOWER SKIN AT STA 261 AND A DENT OF 8 IN LONG X 4 IN WIDTH 0.200” DEPTH IN THE LOWER ACCESS PANEL 511JB OF LEADING EDGE OF SLAT N7. THE WHEEL WAS REPLACED IAW AMM 32-45-01.