What was found
AT SCHEDULED INSPECTION DISCOVERED CORROSION FORWARD OF PANEL 510AL. REMOVED CORROSION. DETERMINED REMAINING THICKNESS BY ULTRASONIC INSPECTION. REMAINING THICKNESS DETERMINED TO BE ACCEPTABLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT SCHEDULED INSPECTION DISCOVERED CORROSION FORWARD OF PANEL 510AL. REMOVED CORROSION. DETERMINED REMAINING THICKNESS BY ULTRASONIC INSPECTION. REMAINING THICKNESS DETERMINED TO BE ACCEPTABLE.