What was found
INSPECTION TYPE: C2, RT WING HAS A CRACKED LONGERON 64 END FITTING-STRAP, AND LOWER SPAR IS CRACKED 1/2 INCH FROM EDGE OF SPAR TO FASTENER HOLE AT XRS 450. NDT VERIFIED 1/2 INCH CRACK AT XRS 450 FROM EDGE OF SPAR TO FASTENER HOLE, REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRAP IAW DWG. 3644046 AND OVERSIZED HOLE AT CRACK LOCATION AND INSTALLED FASTENER AND STRAP IAW SAA SK 779-634 AND UPS EO DC8-5710-17626-A.