As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IDENTICAL LEFT AND RIGHT SIDE AFT FUSELAGE SKIN CRACKS FOUND ON ANNUAL INSPECTION. EACH VERTICAL CRACK IS 1 1/2 INCH IN LENGTH AND IS LOCATED 1 1/2 INCH FORWARD OF STATION +222 BULKHEAD PN. 62443-00. AT THE LOWER OF TWO STRINGERS FOR SIDE SKIN ASSEMBLIES LEFT PN 99470-800, RIGHT PN 99470-01. EACH STRINGER IS CRACKED 1/2 INCH FORWARD OF STATION +222 BULKHEAD. NOTE: EACH STRINGER IS NOTCHED WHERE STRINGER PASSES OVER STATION +222 BULKHEAD. PICS ARE AVAILABLE.