What was found
LOWER FUSELAGE HAS EVIDENCE OF A CRACK JUST AFT OF THE RT LANDING GEAR DOOR. COMPLETED NDT INSPECTION IAW NDT MM PART 6, 51-00-19. FOUND A 1.1 INCH CRACK IN RADIUS AT WING TO BODY FAIRING SUPPORT ATTACH ANGLE, BS 1139, RBL 10.5. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, PG 4, PAR 7, & DWG 149N7528.