As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING UPPER REAR SPAR CAP HAS CORROSION ON AFT UPPER SURFACE AT XORS 480-490. [SUP 05-16-07] REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW FEDEX E.A. 8-57-109150 STEP 2 (LT WING CORROSION BETWEEN XORS=480-800)ALODINED AND PRIMED DC10 SRM 51-21-01 VOL II. MINOR REPAIR.