As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN AVIONICS COMPARTMENT FWD LT DOOR FITTING ON FUSELAGE IS GOUGED. BLENDED DAMAGE IAW SRM 51-12-00 BLEND AREA IS .5" WIDE X .2" T. ALL MATERIAL REMOVED IS .017" MEASURED USEING MACT 3100. SUBMITTED TO STS ENGINEERING FOR PERMANENT DISPOSITON REF SRM 51-13-00-01. COMPLIED WITH EA 32-2016-020.