As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE BELLY SKIN AT STA 520, BETWEEN STRINGERS 28L & 28R HAS A CRACK WHICH COMES OUT OF THE FORWARD L CORNER OF THE EXTERNAL AIR CONDITION ACCESS DOOR CUTOUT. PERFORMED HFEC AND SURFACE CONTOUR. CUT OUT, FABRICATED AND INSTALLED REPAIR DOUBLER .080 2024-T3 IN REFERENCE TO ASI SOLUTIONS DRAWING 5330840-1 REV IR.