What was found
DURING C-CHECK, NOSE WHEELWELL, RT SIDE PRESSURE WEB, FOUND CRACKED BELOW ACCESS PANEL, STA 241. CUT OUT DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER 17 INCHES BY 21 INCHES AT STA 241 PER BOEING SRM 51-40-2. TAT: 59,690.0 HRS. TAC: 43,708.