As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK INSPECTION, THE FUSELAGE WAS FOUND TO BE CRACKED AT THE R1 DOOR LOWER AFT CORNER. THE CRACK WAS 2.5 TO 3 INCHES AND VERIFIED BY NDT. ALL REPAIRS HAVE BEEN ACCOMPLISHED ON NON ROUTINE 031033. TOTAL AIRCRAFT TIME 46985.2, TOTAL CYCLES 41351. (M)