What was found
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAMES 29-33, STRINGER 18R-22R.
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 RT SIDE FUSELAGE FRAMES 29-33, STRINGER 18R-22R.