As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
*** SUPPLEMENTAL SDR *** FAULT- TWO SCRATCHES 0N THE RIGHT SIDE FUSELAGE SKIN AT STA 320, S-14R. DOT 8-001 AFTER FURTHER EVALUATION NO DAMAGE WAS FOUND. ONLY TOP COAT WAS AFFECTED. CLEANED AREA PER SOPM 20-30-03. NO MATERIAL LOST. VERIFIED WITH TR T17807 + TR89336. ORIGINAL THICKNESS 0.090.