As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INBD UPPER LONGERON IS CRACKED AT THE FWD END. CRACK IS 1.3 INCH LONG AND IS IN THE INBD RADIUS. IT TRAVELS FROM THE FWD END, BELOW THE FIRST RIVET AND TO THE SECOND RIVET. INSTALLED RIVETS THRU VERTICAL LEG OF REPAIR ANGLE. REPAIRED IAW EO8-54 10-0007.