As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DENT ON LT FWD FUSELAGE STARTING AT EDGE OF FRAME 10 TO SKIN SPLICE BETWEEN FRAMES 9 - 10, STRINGERS 17L-18L. PERFORMED PERMANENT REPAIR BY CUT OUT AND SKIN DOUBLER AT FWD FUSELAGE SKIN LH SIDE BETWEEN FRAMES 9L-10L STGR 17L-18L IN ACCORDANCE WITH REFERENCE ETD2019-170-012810 REV C. SEE EAMS W/O H6968 TASK 2232 FOR WORK DETAILS.