As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REAR FUSELAGE 2, SKIN AT FR78 AND BETWEEN STGR 6R-7R AROUND A RIVET HEAD HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2 SKIN AT FR78 AND BTWEEN STGR 6R/7R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0385.