As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AT FWD SIDE OF DOOR 311BL ON FUSELAGE. ACFT GROUNDED. REMOVED CORRROSION FROM FUSELAGE FWD OF DOOR 311BL ORIGINAL MATERIAL THICKNESS WAS .080 WITH .005 REMOVED .075 REMAINING FOUND TO BE IN LIMITS IAW SRM 53-80-01-1A-5 TREATED, PRIMED AND TOP COATED REPAIR AREA IAW SRM 51-21-01, TOOL T82250 DOT REMOVED.