As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PASSENGER DOOR UPPER SILL JUST AFT OF FS 280 HAS CRACKED SUPPORT ANGLE, CRACK IS CRACKED 75 PERCENT THROUGH THE ANGLE. PASSENGER DOOR UPPER SILL FAILS INSPECTION IAW NDTM 53-21-126, PART 9, STEPS 5 THROUGH STEP 6. ALL SKINS OF CRACKS ON PASSENGER DOOR SILLS MEMBERS ARE CAUSE FOR REJECTION. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-06.