As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING BASIC CHECK, INSPECTION FOUND THE AFT FUSELAGE LT LOWER SKIN PANEL TO HAVE A PROTRUDING DENT AND CRACK DAMAGE CAUSED BY IMPACT DAMAGE FROM A DOOR RIG BALANCE WEIGHT. THE DAMAGE IS LOCATED BETWEEN FRAMES 85 & 86 AND STRINGERS 25-26L. MAJOR REPAIR.