What was found
CRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1. REPLACED SUPPORT WEB LOCATED INBOARD FAN COWL ENGINE 1 IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND CMM 71-13-30 MEASURE OF CRACK IS L: 0.680 INCH;
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1. REPLACED SUPPORT WEB LOCATED INBOARD FAN COWL ENGINE 1 IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND CMM 71-13-30 MEASURE OF CRACK IS L: 0.680 INCH;