What was found
FUSELAGE SKIN CRACKED AT APPROXIMATELY BS 870 AND STRINGER 24R. MAINTENANCE ROUTED OUT CRACK AT BS 870 AND STRINGER 24R THEN FABRICATED DOUBLER IAW AIRBUS SRM 53-00-01 FIGURE 229. INSTALLED DOUBLER, FILLET WAS SEALED AND DOUBLER PAINTED IN REFERENCE TO AIRBUS SRM 53-00-01 FIGURE 229. DAMAGE AREA WAS PLACED ON MONITOR, CONTROL NR 250645, AND WILL BE RE-INSPECTED AT 60,000 CYCLES WITH REPLACEMENT OF SKIN TERMINATING THE MONITOR.