What was found
CRACK INNER PAN BETWEEN FWD UPPER CORNER AND BEAM5 OF MID CARGO COMPARTMENT DOOR. CRACK ON INNER PAN BETWEEN FWD UPPER CORNER AND BEAM NR 5 WAS REPAIRED IAW SRM 52-03D, FIG 8 HFEC WAS PERFORMED AND NO CRACK WERE FOUND.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INNER PAN BETWEEN FWD UPPER CORNER AND BEAM5 OF MID CARGO COMPARTMENT DOOR. CRACK ON INNER PAN BETWEEN FWD UPPER CORNER AND BEAM NR 5 WAS REPAIRED IAW SRM 52-03D, FIG 8 HFEC WAS PERFORMED AND NO CRACK WERE FOUND.