As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT CENTER WING FUSELAGE LONGERON 28 LOWER SIDE OF R3 DOOR STA 1256 FOUND WITH CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.250", REMOVED THICKNESS = 0.038", AND REMAINING THICKNESS = 0.212". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.