As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON JACK FITTING SUPPORT RH/LH SIDE FS 265 TO FS 280 BL 0 AT INTERNAL FUSELAGE. CORROSION ON JACK FITTING SUPPORT RH/LH SIDE FS 265 TO FS 280 BL 0 AT INTERNAL FUSELAGE WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01, JACK FITTING SUPPORT RH WAS EVALUATED WITHIN LIMITS AND JACK FITTING SUPPORT LH WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-10-001-001-A01 AND PER CRJ700 SRM 51-42-21-001-001-A01.