As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE FRAME 28 GOUGED 3 EACH PLACES BETWEEN STR 9L AND STR 7L COMPLIED WITH FEDEX EA 6-5310-105185 TITLE FUSELAGE - MINOR NICKS IN FRAME 28 STRINGER 7L TO 9L REPAIR. BLENDED 3 AREAS WITH A MAXIMUM DEPTH OF .063 ON THE INBOARD CORNER AS NOTED IN FIGURE 1 ARE STRUCTURALLY ACCEPTABLE PROVIDED A MIN 63 MICRO FINISH IS MAINTAINTED TOUCH UP ALODINE AND FR PRIMER PER SRM CHAPTER 51.