What was found
FUSELAGE SKIN AT BS 787, STR 14 LT - LAP JOINT AREA, UPPER ROW WITH HOLE CRACKED. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT BS 787, STR 14 LT - LAP JOINT AREA, UPPER ROW WITH HOLE CRACKED. POSSIBLE CAUSE OF THE CORROSION WAS SKIN FATIGUE. (X)