As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE PYLON L/E PANEL INNER SURFACE AT UPPER AND LOWER O/B EDGE CHAFED PARTS RACK DL198. BLENDED CHAFED AREA IAW DC9 SRM 54-01 FIG ORIG MAT .070 TITANIUM DMS1536 IAW DC9 SRM 54-30-0 FIG 1. MAT REMOVED .030 MAT REMAINS .040 FOUND OUT OF LIMITS IAW DC9 SRM 54-01 FIG 1. AREA WORKED .5 X 5.5 2 EA PLACES. REPAIRED IAW DC9 SRM 54-01 FIG 4.