As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 1.7 INCH CRACK IN WEB OF FRAME BS 328 BETWEEN S20R AND S21R WEB AREAS OF FRAME. INSTALLED DOUBLER OVER STOP DRILLED CRACKED AREA IN WEB, REPAIRED PER AIW SRM 51-40-2 AND BOEING PRING NR 65-45812. (M)