What was found
CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER FROM STA Y=1302 TO 1322 AND LONGERON 22L. CORROSION WAS REMOVED AND AREA OUT LIMIT WAS REPAIRED IAW ER/A 533315-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER FROM STA Y=1302 TO 1322 AND LONGERON 22L. CORROSION WAS REMOVED AND AREA OUT LIMIT WAS REPAIRED IAW ER/A 533315-14, REV ORIGINAL.