As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
fuselage frame inner chord cracked at FLOORBEAM attach point left side BS 616. cut out damaged area; FABBED repair angle and filler; drilled, treated, primed and installed repair IAW BOEING S/B 737-53-1182 and AWA ER 03-5311-01127-KB1.