What was found
ON 2C INSPECTION, THE FUSELAGE PASSENGER DOOR SURROUND STRUCTURE INNER SKIN WAS FOUND CORRODED BETWEEN FRAMES 15 AND 15A, JUST ABOVE STRINGER 17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED PER AERODESIGN REPORT NR 2118-2, REV IR, DATED 2-8-97.