As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK AT FS 727D JUST ABOVE STRINGER 23R RUNNING ALONG THE BONDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A 4 X 1 INCH CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385208-14, REV B.