What was found
CRACK ON PAN, AFT EDGE BETWEEN BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR. REPAIRED IAW SRM 52-05 FIG. 26A, SRM 51-30-2 AND SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON PAN, AFT EDGE BETWEEN BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR. REPAIRED IAW SRM 52-05 FIG. 26A, SRM 51-30-2 AND SRM 51-30-5.