What was found
DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE ON FUSELAGE SKIN, BS 440, BETWEEN STRINGERS 27R- 28R. REPAIRED SKIN PER DALFORT XEA X2-53-255.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE ON FUSELAGE SKIN, BS 440, BETWEEN STRINGERS 27R- 28R. REPAIRED SKIN PER DALFORT XEA X2-53-255.