What was found
INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 1620-1640, S21R, JUST BELOW AND FORWARD OF R-3 DOOR. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 214. A DIP WAS ISSUED TO INSPECT FASTENERS EVERY 1,000 FLIGHT CYCLES AND TO PERFORM A PERMANENT REPAIR AT 3,000 FLIGHT CYCLES.