As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN LOWER PANEL WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-003-A02, FIG. 53-61-01-991-806, ITEM 1 AND ITEM F (REV.38 DATED 9 JUL 2021 ). DEFECT LOCATION: FS 1000- FS 10L5 AND STRG 25R AND STRG 26R