As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND FUSELAGE SKIN GOUGED BETWEEN STA 620 AND 640 AT S16L AND S17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 204. A DIP WAS ISSUED TO INSPECT BLIND RIVETS EVERY 2500 FLIGHT CYCLES AND TO REPLACE THE REPAIR NO LATER THAN 12,00 FLIGHT CYCLES PER SRM 53-00-01, FIGURE 204.