As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV CRACKS WERE FOUND ON FUSELAGE SKIN AT STA Y=373.750 OF 0.046" LENGTH,Y=374.750 OF 0.046" LENGTH, Y=375.250 OF 0.031" LENGTH AND Y=376.0 OF 0.093" LENGTH OF THE FWD CARGO DOOR JAMB UPPER CORNER. DAMAGED SKIN WAS CUT OUT AND DOUBLERS INSTALLED IAW MD88 SRM 53-05 FIG 105.