As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SJO - DURING C-CHECK, FOUND EXTERNAL FUSELAGE, BS 952, BETWEEN STRINGER 23 AND 24 RIGHT SKIN WITH OIL CAN. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 943 TO BS 958, BETWEEN STRINGER 21 AND 25 RIGHT DUE TO OIL CAN IAW SRM 53-30-3 FIG 17 DETAIL V. (M)