What was found
DURING A SCHEDULED INSPECTION AN 1.5 INCH STRESS CORROSION CRACK WAS FOUND AT XCW=58.5 RIGHT LOWER TEE CAP OUTBOARD RADIUS, BETWEEN STRINGER 13 AND 14, (EF SB 57-98 R8). PERFORMED SB 57-98 R8 TEE CAP INSPECTION, BY REMOVING BOLTS AND BARREL NUTS, CLEANED HOLES, VISUAL INSPECTION FOUND NO DISCREPANCIES IN BOLT HOLES. RE-INSTALLED BOLTS AND BARREL NUTS. NDT VERIFIED CRACK BETWEEN STRINGER 13-14 RIGHT LOWER INST CLIP REPAIR IAW AERO EO 96-407 TO BE RE-INSPECTED AT INTERVALS NOT TO EXCEED. (M)