What was found
AT D-CHECK, FUSELAGE INTERIOR FRAME CORRODED AT BS 620 INNER FLANGE ABOVE FLOOR LEVEL. REMOVED AND REPLACED SPLICE PLATE PER SRM 51-40-3 . PLATE 6 INCHES BY 7 INCHES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D-CHECK, FUSELAGE INTERIOR FRAME CORRODED AT BS 620 INNER FLANGE ABOVE FLOOR LEVEL. REMOVED AND REPLACED SPLICE PLATE PER SRM 51-40-3 . PLATE 6 INCHES BY 7 INCHES.