As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVAL OF R2 DOOR SILL CORROSION WAS FOUND ON FR68 IN DOOR SILL ATTACH AREA. REPAIRED FR68 JUST ABOVE R2 DOOR SILL IAW ECRA 5310-07297 PART 1 STEPS 1-3. DIP CREATED TO ACCOMPLISH THE INITIAL INSPECTION PER PART 2 OF ECRA 5310-07297 ON OR BEFORE THE AIRCRAFT REACHES 39,728 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTION EVERY 10,700 AIRCRAFT FLIGHT CYCLES THEREAFTER.