What was found
ON 2C CHECK, THE FUSELAGE STRINGER 18L WAS FOUND TO BE CORRODED NEAR FRAME 16, THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-5, REV IR, DATED 1-28-97.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON 2C CHECK, THE FUSELAGE STRINGER 18L WAS FOUND TO BE CORRODED NEAR FRAME 16, THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-5, REV IR, DATED 1-28-97.