What was found
CHAFED RUB STRIP, NR 2 ENG RT CORE COWL INNER FACE T/E UPPER SIDE. REMOVED DAMAGE RUB STRIP IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHAFED RUB STRIP, NR 2 ENG RT CORE COWL INNER FACE T/E UPPER SIDE. REMOVED DAMAGE RUB STRIP IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.