What was found
FUSELAGE UPPER LOBE, CORROSION ON FRAME INNER AND OUTER FLANGE, AT BS 720A BETWEEN STR 1 TO STR 4 RT. REPAIRED FRAME PER SRM 53-10-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE UPPER LOBE, CORROSION ON FRAME INNER AND OUTER FLANGE, AT BS 720A BETWEEN STR 1 TO STR 4 RT. REPAIRED FRAME PER SRM 53-10-4.