As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT SIDE OF AIRSTAIR AREA, INSIDE FUSELAGE TORQUE BOX, WEB AT BS.1223 HAS DRILL DAMAGE IN UPPER INBD CORNER. CUT OUT DAMAGE AREA DIM. 1" X 1" IAW SRM 51-40-2. FABRICATED FILLER PO 9009504 AND DOUBLER FROM PO 9008186. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-40-2. DTE REQUIRED WITHIN 12 MONTHS.