What was found
FOUND OVERWING FRAME INNER CHORD IS CRACKED AT BS 616L, JUST BELOW STR 17. MAJOR REPAIR ACCOMPLISHED: REPAIRED FRAME INNER CHORD AT STA 616L BELOW S17L WITH STIFFENER ANGLE AND FILLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND OVERWING FRAME INNER CHORD IS CRACKED AT BS 616L, JUST BELOW STR 17. MAJOR REPAIR ACCOMPLISHED: REPAIRED FRAME INNER CHORD AT STA 616L BELOW S17L WITH STIFFENER ANGLE AND FILLER.