As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ERA 605623-14 ISSUED FOR CRACK TO #2 PYLON FWD UPPER SPAR WEB BE TWEEN STA 221.25 AND 237.5. DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: PER ER/A 605623-14 REV A, DTE ANALYSIS FOR THE SECTION I REPAIR COMPLETED. DAMAGE TOLERANCE ASSESSMENT HAS ESTABLISHED THAT THIS IS A CATEGORY 'A' PERMANENT REPAIR WITH NO ADDITIONAL REQUIREMENTS.