As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) SEVERE CORROSION FOUND DURING ANNUAL INSPECTION. EXFOLIATION CORROSION FOUND AT LT FLAP 3 AND 4 HINGE BRACKET. INTERGRANULAR CORROSION FOUND AT LT MAIN GEAR LINK ATTACHMENT TO MAIN WING SPAR BRACKET. AT THE LT AND RT FUSELAGE TUBING ATTACHMENT TO MAIN WING LOWER SPAR, THE STEEL TUBING IS RUSTED RIGHT THROUGH. ALSO, GENERAL SURFACE CORROSION WAS DISCOVERED IN THE CABIN FLOOR AREA.