As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CREW DOOR AT MIDDLE TO LOWER SIDE HAS AFT EDGE DAMAGE. BLENDED AREA ON CREW DOOR AT MIDDLE TO LOWER SIDE HAS AFT EDGE IAW A300-600 SRM 51-73-10, ORIGINAL THICKNESS IS 0.098" MAXIMUM LOSS OF MATERIAL 0.003" AND THE MAXIMUM PERMIT REWORKED IS 0.009" THEREFORE IS WITHIN LIMITS IAW A300-600 SRM 52-11-00 TABLE 102.