What was found
MAIN CABIN RT SIDE AT STA C59 BETWEEN 3R AND 4R SEAT TRACK FLOORBEAM HAS CRACK, AFT SIDE MIDDLE STIFFENER. REMOVED CRACK NDT VERIFIED NO CRACKS EXIST IAW NTM 51-10-08. INSTALLED REPAIR ANGLE IAW SRM 53-10-15, FIG 211.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN RT SIDE AT STA C59 BETWEEN 3R AND 4R SEAT TRACK FLOORBEAM HAS CRACK, AFT SIDE MIDDLE STIFFENER. REMOVED CRACK NDT VERIFIED NO CRACKS EXIST IAW NTM 51-10-08. INSTALLED REPAIR ANGLE IAW SRM 53-10-15, FIG 211.