As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) FUSELAGE SKIN AT STA 183.0, LBL 24.75 - 28.0 FOUND CRACKED. THE CRACK APPEARS TO HAVE ORIGINATED ON THE LEFT HAND EDGE OF THE SKIN AND PROPAGATED INBOARD CLEAR OF THE LONGTITUDINAL AND LATERAL FLANGE ANGLES. NO EVIDENCE OF MECHANICAL DAMAGE OR CORROSION EVIDENT. AIRCRAFT TT: 2,322 HOURS.