As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE AT LT WING LEADING EDGE ROOT AT BS 720D, 10" - 14" AT STRINGER 19L, LAP AREA IS WORN FROM PANEL CONTACT. BLENDED DAMAGED AREA REF 53-30-1 PAGE 2A. FOUND TO BE OUT OF LIMITS REF SRM 53-30-1 PG 2C. REPAIRED AREA WITH DOUBLER AND FILLER REF SRM 53-30-3 FIG 5. CLASSIFIED AS A MAJOR REPAIR.