What was found
DURING 8-DAY CHECK, A 3 3/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT RT TAIL AREA FORWARD OF OUTFLOW VALVE BS 927, STR 23 RT. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 229, DETAIL XI.