As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER INSPECTION PER ED F-5310-E0329085DP5 STEP 3, A CRACK WAS FOUND AT FR-1640 LH, S- 14. COMPLIED WITH FEDEX E.A. # F -5310-T0380418 P1 TITLE: FUSELAGE- MAINFRAME - LH STA 1640 - TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9L AND S-20L.