What was found
REMOVED EXISTING FASTENERS, STIFENERS, FILLERS, AND DAMAGED SECTION OF WEB AS SHOWN ON FIGURE 5. FABRICATED A .050 INCH THICK REINFORCING DOUBLER FROM 7075-T6. ALODINE AND APPLIED BMS 10-11 TYPE 1 PRIMER TO ALL BARE SURFACES. INSTALLED RE-ENFORCING DOUBLER, WEB, STIFFENERS, AND FILLERS WITH NEW FASTENERS IAW ECO 2223 FIGURE 5 AND FIGURE 7. AIRCRAFT RETURNED TO SERVICE. (M)