What was found
FTW - NR 2 ENGINE AT 3:00 POSITION LE OF ACOUSTICAL PANEL SEPARATED 1.4 INCHES SPAN INLET COWL. REPAIR ACOUSTICAL PANEL PER MD80 SRM WITH EA 934 IAW MD80 SRM 54-04. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FTW - NR 2 ENGINE AT 3:00 POSITION LE OF ACOUSTICAL PANEL SEPARATED 1.4 INCHES SPAN INLET COWL. REPAIR ACOUSTICAL PANEL PER MD80 SRM WITH EA 934 IAW MD80 SRM 54-04. (M)