As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT HMV-1, INSPECTION FOUND THE CHORD ANGLE CRACKED AT STA 134248 SECTION HORIZONTAL CHORD ANGLE LOC ABOVE S-DUCT. IT IS CRACKED JUST I/B OF RT FIN TERMINAL FITTING. CHORD HAS BEEN PREVIOUSLY STOP DRILLED, CRACK APPEARS TO HAVE CONTINUED PAST STOP DRILL HOLES. REPAIRED CRACK PER M/M 53-11-0 PG 808.