As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRAP THAT ATTACHES FUSELAGE PANEL 195DL/196DR IS CORRODED. (C-CHECK RO 4/1/2021) REMOVED DAMAGE FROM STRAP THAT ATTACHED FUSELAGE PANEL 195DL/196DR BY BLENDING AND EVALUATED IAW CRJ700 SRM 53-00-00-101-001-A01. MEASURED ORIGINAL THICKNESS AT 0.063", REMAINING THICKNESS IS 0.063". NO MATERIAL LOSS. WITHIN LIMITS.