As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STABILIZER, CRACKS (3EA'S) ON VERTICAL STABILIZER DORSAL FIN LEADING EDGE ACCESS PANEL CUTOUT 6301A. DAMAGE AREA WAS REPAIRED PER SRM 55-05 FIGURE 3 SHEET 1. PERFORM DECAL CONDITION VISUAL INSPECTION EVERY "C" CHECK PER TOPP 30-10-70 PAR I PG 14.