As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SJO - DURING C-CHECK, ROUTINE INSPECTION PER CARD NR J2C 51 2525, NOTED CRACK ON FUSELAGE FRAME AT BS 400 BETWEEN STR 25 AND 26 LT. CRACK WAS .250 INCH IN LENGTH. CRACK WS REPAIRED IAW SRM 53-10-4 FIG 6. COOPESA W.O. NR L1-0630, NR VAM 100-225, 208SDA006. (X)