As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L-1 DOOR LOWER SILL WEB CREASE BEAM ATTACH ANGLE CORROSION AROUND FASTENER HOLES / REMOVED CORROSION FROM L-1 DOOR LWR SILL CREASE BEAM ATTACH ANGLE. ATTACH ANGLE ORIGINAL THICKNESS IS .080'; REMOVED .067' MATERIAL LOSS; REMAINING THICKNESS .013'. L-1 CREASE BEAM ATTACH ANGLE OUT OF LIMITS. REMOVED CORRODED ATTACH ANGLE AND INSTALLED NEW ATTACH ANGLE. I.A.W BOEING DWG. NO.