As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MODIFICATION AND INSPECTION OF AFT CARGO DOOR STRUCTURE AT FR60A REVEALED THE TOP TWO HOLES MOST OUTBOARD ROW, BETWEEN THE LOCK PLATE AND TORSION BOX PLATE HAVE CRACK INDICATIONS. (REFERENCE ITEM 18B OF WORK CARD) CARGO LATCH INTERNAL STRUCTURE. REPAIRED IAW FEDEX EA 6-5320-T0348097-P1.