What was found
FUSELAGE SKIN FROM BS 880 TO BS 890, STR 25RT , LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN CORROSION. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN FROM BS 880 TO BS 890, STR 25RT , LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN CORROSION. (X)