As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORRSION ON ACCESS PANEL 832DL ON THE PASSENGER DOOR. CORROSION ON THE ACCESS PANEL WAS REMOVED IAW SRM 51-21-06-001-001-A01 PAR. 1 TO 5.B. (1) AND REWORKED AREA WAS MEASURED AS FOLLOW 832DL ORIGINAL THICKNESS: .050"" AND REMAINING THICKNESS: .044"" THEREFORE IT IS WITHIN OF LIMITS PER CRJ 900 S.R.M. 52-11-32-101-001-A01 TABLE 1.