As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SMALL CRACK NOTICED AT AFT INTERIOR FUSELAGE TAIL COMP. LEFT SIDE CANTED AREA STA 1178.225 BETWEEN LONG 13 AND 14 LEFT. INSTALLED FORMED ANGLE REPAIR ON LEFT FUSELAGE CANTED FRAME 1178 BETWEEN LONG 13 AND 14 LEFT PER B717 SRM 51-70-11 FIG 201.