As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL WING TO FUSELAGE SUPPORT STRUCTURE ANGLE IS CRACKED AT FS 909.00. TRIMMED FWD DIAPHRAGM AND ANGLE TO COMPLETELY ELIMINATE CRACK, FABRICATED AND VERIFIED MATERIALS AND INSTALLED REPAIR PARTS IAW REO 670-53-82-478 REV A DATED 2014-11-12.