As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE OUTBOARD REVERSER EXTERIOR SKIN HAS A 7.5 INCH BY 6.0 INCH DENT IN UPPER AREA OF TRANSLATING COWL. PERMANENT REPAIR ACCOMPLISHED AS PER GE CF6-50 ENGINE MANUAL 78-32-01, REPAIR 003. ALSO, REFERENCE ATLAS AIR XEO NR 78-082907.