What was found
C2 INSPECTION FOUND A SMALL AREA OF CORROSION ON FWD FUSELAGE STRINGER 21L BETWEEN FS 3293 AND 3596.5. THE DAMAGED AREA OF THE STRINGER WAS REMOVED AND REPAIRED PER AERODESIGN REPORT NR 1990-3, REV IR, DATED 10-26-96.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C2 INSPECTION FOUND A SMALL AREA OF CORROSION ON FWD FUSELAGE STRINGER 21L BETWEEN FS 3293 AND 3596.5. THE DAMAGED AREA OF THE STRINGER WAS REMOVED AND REPAIRED PER AERODESIGN REPORT NR 1990-3, REV IR, DATED 10-26-96.