As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A C-CHECK IN MCN, THE RADIUS OF FUSELAGE SKIN FORWARD OF THE NOSE LANDING GEAR DOOR WAS SUSPECTED OF BEING CRACKED BEYOND LIMITS. S/D - MAINTENANCE REPAIRED THE FUSELAGE SKIN RADIUS RH AND LHS, AT FS 235, IAW ASA EO 600-53-0122. (M)