What was found
DURING SCHEDULED HC2 CHECK, NR 2 ENGINE HAS 2 EACH COMPRESSOR SPOOL BLADE TIP CORNERS MISSING MATERIAL BEYOND LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED HC2 CHECK, NR 2 ENGINE HAS 2 EACH COMPRESSOR SPOOL BLADE TIP CORNERS MISSING MATERIAL BEYOND LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.