As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV, A CRACK WAS FOUND IN FWD SERVICE DOOR CUTOUT FUSELAGE SKIN FWD UPPER CORNER AT BS 175.75, CLOSE TO DOOR JAMB EDGE WITH THE LENGTH OF 0.055 INCH. DAMAGE AREA WAS CUT OUT AND REPAIRED DOUBLERS FILLER. INSTALLED IAW SRM 53-05 FIG 112.