What was found
REMOVED EXISTING FASTENERS, STIFFENERS, ANGLE AND A SECTION OF THE WEB. REMOVED AND DISCARDED REINFORCING ANGLE, DOUBLER AND A SECTION OF THE WEB. DRILL AND COLD WORKED THE HOLES IN THE CHORD. INSTALLED SPLICE ANGLE AND STIFFENERS WITH FASTENERS SHOWN IN SECTION A-A. INSTALLED THE ANGLE, REINFORCING ANGLE, FILLER DOUBLER, SPLICE PLATES AND THE WEB WITH FASTENERS FROM THE KIT. APPLIED ALODINE, BMS 10-11 TYPE 1 PRIMER AND TYPE 11 ENAMEL TO ANY BARE SURFACE. COMPLETED REPAIR IAW ECO 2223, FIGURES 4 AND 9. AIRCRAFT RETURNED TO SERVICE. (M)