What was found
FUSELAGE FORWARD SKIN CORRODED AT BS 887, BETWEEN STR 23L TO STR 26L. REPAIRED SKIN PER ER & EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FORWARD SKIN CORRODED AT BS 887, BETWEEN STR 23L TO STR 26L. REPAIRED SKIN PER ER & EA.