As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-200435-01-1-002, SECONDARY FINDING DURING REMOVAL OF WIRE BUNDLE SUPPORT AT ENGINE 2, FOUND SUPPORT ATTACH HOLES OVERSIZED (2EA) AT ENGINE FLANGE B1 (BOLT HOLE LOCATION 79 AND 80).REPAIRED ENGINE 2 FLANGE B1 (BOLT HOLE LOCATION 79 AND 80) IAW CFM56-5B SERVICE BULLETIN 72-0892 PARAG 3A(2) AND REF CFM REPAIR DOCUMENT RD 840-422.53.NOTE: REINFORCEMENT PLATES WILL BE REMOVED AT NEXT ENGINE OVERHAUL IAW CFM REPAIR DOCUMENT RD 840-422.53. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1Q208 ITEM 4-91.