What was found
(CAN) DURING ROUTINE INSPECTION CORROSION WAS FOUND IN THE FUSELAGE SKIN ABOVE THE MAIN CARGO DOOR BETWEEN BS 500 AND BS 540 AND FROM STRINGER S-3L TO S-4R (LEVEL 3 CORROSION).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING ROUTINE INSPECTION CORROSION WAS FOUND IN THE FUSELAGE SKIN ABOVE THE MAIN CARGO DOOR BETWEEN BS 500 AND BS 540 AND FROM STRINGER S-3L TO S-4R (LEVEL 3 CORROSION).