What was found
FUSELAGE SKIN FROM BS 893 TO BS 895, STR 20 LT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN FROM BS 893 TO BS 895, STR 20 LT - LAP JOINT AREA WITH LOOSE MATERIAL DUE TO CORROSION. POSSIBLE CAUSE OF CRACK WAS SKIN FATIGUE. (X)