What was found
NUMBER 1 ENGINE LEFT PYLON UPPER TORQUE BOX SKIN HAS POSSIBLE CRACK AT AFT OUTBOARD AND FORWARD INBOARD NUT PLATE LOCATIONS FOR GENERATOR FEEDER CABLE PASS THRU. INSTALLED DOUBLE REPAIR PER AARD 54-52-01-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMBER 1 ENGINE LEFT PYLON UPPER TORQUE BOX SKIN HAS POSSIBLE CRACK AT AFT OUTBOARD AND FORWARD INBOARD NUT PLATE LOCATIONS FOR GENERATOR FEEDER CABLE PASS THRU. INSTALLED DOUBLE REPAIR PER AARD 54-52-01-1.