As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FRAME ON THE C-1 DOORWAY WAS FOUND TO BE CRACKED APPROX 6 BELOW THE LOWER STOP FITTING. THE CRACK IS LOCATED WHERE FRAME WAS GOUGED. A 1.10 DIAMETER HOLE WAS REQUIRED TO CLEAN UP THE DAMAGE TO THE WEB. MATERIAL IS 0.071 7075-T6. THE CRACK WILL BE REPAIRED PER THE INSTRUCTIONS OF AD 93-14-10 AND SB 737-53-1096, REV 5 (DAL SI 3-55297-12AD).