What was found
CRACK INDICATIONS WERE FOUND AT THE FORWARD OUTBOARD BOLT HOLE LOCATION OF THE AFT PITCH LOAD FITTING, NR 1 PYLON. CRACK IS IN LOWER WING SKIN ALSO, AND REQUIRED SUBJECT HOLE TO BE OVERSIZED AND BUSHED BACK TO DIAMETER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INDICATIONS WERE FOUND AT THE FORWARD OUTBOARD BOLT HOLE LOCATION OF THE AFT PITCH LOAD FITTING, NR 1 PYLON. CRACK IS IN LOWER WING SKIN ALSO, AND REQUIRED SUBJECT HOLE TO BE OVERSIZED AND BUSHED BACK TO DIAMETER.