As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON THE SKIN AROUND THE EMERGENCY EXIT DOOR ON R/H SIDE OF FUSELAGE. BLENDED SIGNS OF CORROSION FROM 2 SPOTS ON THE E-EXIT OUTER SKIN. REMAINING MATERIAL THICKNESS IN THE BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS SPECIFIED IN SR-680-ATA52-18636 REV - DATED 03/01/2019 AND 8100-9. THIS IS IN SUPPORT OF A MAJOR REPAIR. SEE DUNCAN AVIATION WORK ORDER R0EPA SQUAWK 47 FOR DETAILS.