What was found
CRACKED INTERNAL STRUCTURE PAN FORWARD EDGE BETWEEN BEAMS 3 AND 4, FORWARD CARGO DOOR. PAN WAS REPAIRED IAW SRM 51-03-D, FIG 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED INTERNAL STRUCTURE PAN FORWARD EDGE BETWEEN BEAMS 3 AND 4, FORWARD CARGO DOOR. PAN WAS REPAIRED IAW SRM 51-03-D, FIG 8.