As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER INSPECTION PER EO F-5310-E0329085 D P5 STEP: 3 FIG: 1 CIRCLE: 1 CRACK WAS FOUND AT FRAME BS 1640 LH S-14. COMPLIED WITH FEDEX E.A. #: F-5310-T0379541(P1), TITLE: FUSELAGE-MAINFRAME-LH STA 1640- TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9L AND S-20L.