What was found
DURING C-14 CHECK A .25 INCH CRACK WAS FOUND ON ANGLE AT LT POSITION OF NR 2 PYLON AFT KEEL, ABOVE TURBINE FIRE SLEEVE NAC STA 254.52. REMOVED DAMAGED ANGLE AT LT POSITION OF NR 2 PYLON AFT KEEL NAC STA 254.52; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 PG 4, FIG 2 & SRM 51-40-02 PG 3 - 4 & 38, FIG 8.