As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
3 RIVET HEADS WERE SHEARED AND METAL WAS BULGING UNDER REINFORCEMENT STRAP, UPPER SURFACE OF RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD OUTBOARD CORNER JUST OUTBOARD OF CEILING SERVICE LIGHT. WEB OUT OF LIMITS AFTER CORROSION REMOVAL MATERIAL LOSS 35%. REMOVED SHEARED FASTENERS AND REINFORCEMENT STRAP. REMOVED CORROSION. INSTALLED DOUBLER IAW ABX REA D853-53256.