What was found
DURING HMV, A CRACK WAS FOUND ON INNER PAN BELOW STOP FITTING ON BEAM NR 3 FWD EDGE AT AFT CARGO COMPARTMENT DOOR. INNER PAN WAS STOP DRILLED AND DOUBLER INSTALLED IAW MD-88 SRM 52-05 FIG 50.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, A CRACK WAS FOUND ON INNER PAN BELOW STOP FITTING ON BEAM NR 3 FWD EDGE AT AFT CARGO COMPARTMENT DOOR. INNER PAN WAS STOP DRILLED AND DOUBLER INSTALLED IAW MD-88 SRM 52-05 FIG 50.