As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER FUSELAGE 1 EXTERNAL SKIN HAS DAMAGE AREA FROM PREVIOUS BLEND OUT BETWEEN FR22 AND FR23 AND BETWEEN STGR 19R AND STGR 20R. INSTALLED FABRICATED DOUBLER AND FILLER FOR REPAIR ON CENTER FUSELAGE 1 EXTERNAL SKIN FROM PREVIOUS BLEND OUT BETWEEN FR22 AND FR23 AND BETWEEN STGR 19R AND STGR 20R. IAW EMB 145 SRM 53-21-01RE FIGURE 204 AND PIEDMONT EO1-53-26-0173.