What was found
NR 2 ENGINE FIRE LOOP HARNESS AT 6 O'CLOCK POSITION NEXT TO TRANSFER GEAR BOX OIL INLET TUBE IS CHAFED THROUGH. REMOVED & REPLACED THE FIRE LOOP HARNESS IAW MM 26-11-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE FIRE LOOP HARNESS AT 6 O'CLOCK POSITION NEXT TO TRANSFER GEAR BOX OIL INLET TUBE IS CHAFED THROUGH. REMOVED & REPLACED THE FIRE LOOP HARNESS IAW MM 26-11-02.