What was found
AFTER REMOVAL OF STOP FITTING NR 4, ONE CRACK WAS FOUND ON THE PAN AT THE MID CARGO DOOR FWD EDGE. THE PAN WAS REPAIRED IAW SRM 52-30-02, FIG 2, VOL I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF STOP FITTING NR 4, ONE CRACK WAS FOUND ON THE PAN AT THE MID CARGO DOOR FWD EDGE. THE PAN WAS REPAIRED IAW SRM 52-30-02, FIG 2, VOL I.