As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER INSPECTION PER FEDEX EO, F-5310-E0329085 P-6 STEP 3A CRACK WAS FOUND AT FRAME 1640 R/H S-14R. COMPLIED WITH EA # F-5310-T0380850 P1 TITLE; FUSELAGE - MAIN FRAME - RH STA 1640 - TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9R AND S-20R, THIS IS A MAJOR REPAIR.