As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:SEG4 RIGHT WHEEL WELL FWD BULKHEAD, JUST BELOW APU LOAD CONTROL VLV, HAS A 3.5 INCH CRACK TO 4 INCH CRACK CRACKED THROUGH. STOP DRILLED CRACK AS PER B72 7 SRM 51-10-01, ACCOMPLISHED HFEC 51-000-00 FIG 4 NDT INSP CRACK CONTAINMENT CONFIRMED. INSTALLED DOUBLERS AND FILLERS AS PER B727 SRM 53-10-9 FIG 5. REPLACED KEEL BEAM SUPPORT ANGLE AT BS 870 AS PER BOEING DRAWING NR 66-12638.