What was found
CRACK AT FORWARD BOTTOM EDGE OF FORWARD ENTRY DOOR BELOW BOTTOM HINGE BRACKET. REPAIRED CRACK PAN WITH REPAIR IAW DC9 SRM 52-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK AT FORWARD BOTTOM EDGE OF FORWARD ENTRY DOOR BELOW BOTTOM HINGE BRACKET. REPAIRED CRACK PAN WITH REPAIR IAW DC9 SRM 52-05.