As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TASK CARD 900-54-430-300 LEFT AFT CORE COWL HAS CHAFING ON THE RUB STRIP. REMOVED DAMAGE FROM AFT CORE COWL RUB STRIP, LE TEE, IN A 11.5"X1" AREA. REMAINING THICKNESS .0876", MINIMUM ALLOWABLE THICKNESS .100", OUT OF LIMITS IAW SRM 54-13-00-201-005-A01. RECEIVED NEW AFT LT CORE COWL. NEW CORE COWL TO BE INSTALLED.