As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 616L FRAME WEB IS CRACKED IN 2 HOLES COMMON TO INBD CHORD ANGLE. UPPER HOLE IS 0.5 INCH BELOW STRINGER S-17L AND LOWER HOLE IN WEB IS 7 INCH BELOW STRINGER S-17L. MAJOR REPAIR ACCOMPLISHED: REAMED HOLES & ACCMP NDT FOR CRACK CONTAINMENT. FABRICATED & INSTALLED FREEZE PLUG.