What was found
FUSELAGE SKIN INTERNAL SURFACE CHAFED AT BS 282, BETWEEN STR 2L TO STR 3L. REPAIRED SKIN PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN INTERNAL SURFACE CHAFED AT BS 282, BETWEEN STR 2L TO STR 3L. REPAIRED SKIN PER SRM.