As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MDC FLOOR STRUCTURE, BRACKET SUPPORT IS CRACKED AT THE L/H SIDE OF FUSELAGE AT FR 38. REMOVED COVER ANGLE AT MDC FLOOR STRUCTURE FROM FR34 TO FR 38 LT SIDE OF FUSELAGE. IAW SRM 51-40-21-001. REMOVED BRACKET SUPPORT (DOG BONE) AT MDC FLOOR STRUCTURE, LT SIDE OF FUSELAGE AT FR 38 IAW SRM 51-40-21-001. RE-INSTALLED COVER ANGLE AT MDC FLOOR STRUCTURE FROM FR34 TO FR 38 LH SIDE OF FUSELAGE IAW SRM 51-40-21-001.