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 2 CRACKS ALONG THE BONDED DOUBLER EDGES AT STRINGERS 22R & 23R. AN EXISTING REPAIR FOR A SIMILAR CRACK WAS LOCATED AT STRINGER 24R. THE EXISTING REPAIR WAS REMOVED, ALL CRACKS REMOVED WITH CUTOUTS, AND THE CUTOUTS REPAIRED WITH A SINGLE ALUMINUM DOUBLER/TRIPLER REPAIR. THE REPAIR WAS ACCOMPLISHED PER ER/A 089558-14, REV A.