What was found
CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW DC-10/MD-10 SRM 51-35-01 VOL II.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLG WHEEL WELL CAVITY, CORROSION ON FUSELAGE SKIN INTERIOR BETWEEN LONGERON 50R AND 49R, STA 1501 TO 1520. REMOVED AND REPLACED L51R END FITTINGS IAW DC-10/MD-10 SRM 51-35-01 VOL II.