As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK SUPPORT WEB LOCATED INBOARD FAN COWL ON ENGINE 1. REPLACED SUPPORT WEB AND FASTENERS LOCATED ON INBOARD FAN COWL AT ENGINE 1 IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 PAGE 10090. MEASUREMENT OF CRACK: 1.317 INCH.