What was found
MAIN CABIN STA 940 FWD SIDE OF AFT FRAME, ANGLE APPROX 2' UP FROM CREASE BEAM WEB CORRODED. CORRODED FAILSAFE CHORD FOUND OUT OF LIMITS IAW SRM 53-00-07, PG 103, FIG 101, DETAIL II. ORIG. MAT .125 AFTER REWORK .111, MAT. LOSS .014 (1/2"X3/4") STA 940, S-16R TO S-17R. R & R FAILSAFE CHORD PN 1441120-35 AT STA 940, S-9R TO S-17R IAW SRM 51-40-02 AND BOEING DWG NR 1441120, SHT 50 OF 124. MAJOR REPAIR.