As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN SUSTAINED DAMAGE BELOW L-2 DOOR AT BS 958 BETWEEN S22L AND S23L. THE DAMAGE WAS REPAIRED IAW ECRA 5330-03261. A DIP WAS ISSUED TO ACCOMPLISH AN EXTERNAL DETAIL VISUAL INSPECTION OF THE FILLER AND DOUBLER LOOKING FOR CRACKS AND LOOSE OR MISSING FASTENERS. INITIAL INSPECTION THRESHOLD IS 56,000 TOTAL AIRFRAME CYCLES WITH REPEAT INSPECTION EVERY 12,000 CYCLES.