What was found
ENGINE NR 1 RT CORE COWL UPPER STRIP STRUCTURE CORRODED. CORRODED PART REMOVED AND NEW WEAR STRIP, PN 224-2301-122 WAS INSTALLED USING RIVETS IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE NR 1 RT CORE COWL UPPER STRIP STRUCTURE CORRODED. CORRODED PART REMOVED AND NEW WEAR STRIP, PN 224-2301-122 WAS INSTALLED USING RIVETS IAW SRM 51-40-02.