What was found
DURING C-17 CHECK A 1 3/4 INCH CRACK WAS FOUND ON THE LOWER AFT END OF STIFFENER AT LT WING NR 3 FLAP FAIRING, WS 184.40 TO WS 191.00. MAINTENANCE REMOVED THE DAMAGED STIFFENER AT WS 184.40 TO WS 191.00, FABRICATED A NEW REPLACEMENT STIFFENER, AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 16-17, 38, FIG. 8, SRM 51-40-04, PG. 2, FIG. 1, AND SRM 51-40-05, PG. 7, FIG. 4.