What was found
DURING 2C INSPECTION, FOUND FUSELAGE INNER SKIN FOUND CORRODED AT PAX DOOR CUTOUT, BENEATH BOTTOM FWD DOOR CUTOUT REINFORCEMENT DOUBLER. THE DAMGE WAS REPAIRED PER AERODESIGN REPORT NR 2118-1, REV IR, DATED 12-3-96.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 2C INSPECTION, FOUND FUSELAGE INNER SKIN FOUND CORRODED AT PAX DOOR CUTOUT, BENEATH BOTTOM FWD DOOR CUTOUT REINFORCEMENT DOUBLER. THE DAMGE WAS REPAIRED PER AERODESIGN REPORT NR 2118-1, REV IR, DATED 12-3-96.