What was found
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN. FOUND CORROSION AT FRAME 17-19, STRINGERS 5L-19L.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN. FOUND CORROSION AT FRAME 17-19, STRINGERS 5L-19L.