As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSP OF LT ENGINE INLET, MULTIPLE CRACKS WERE FOUND ALONG WITH SHEARED RIVET HEADS ON THE FWD ROW OF RIVETS AFT OF THE HEATED L/E. RIVETS WERE REPLACED AND CRACKS WERE TEMPORARILY REPAIRED PER EMBRAER ENGINEERING REPAIR DATA. PERMANENT REPAIR REQUIRED WITHIN 20 CYCLES.