What was found
FUSELAGE SKIN FROM BS 720B TO BS 720C STR 26LT, LAP JOINT. POSSIBLE CAUSE OF THE CORROSION WAS FATIGUE. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN FROM BS 720B TO BS 720C STR 26LT, LAP JOINT. POSSIBLE CAUSE OF THE CORROSION WAS FATIGUE. (X)