What was found
LEFT WW CTR WING BOX REAR SPAR VERTICAL PRESS WEB CRACK APPROX 7/8 INCHES IN LENGTH BETWEEN LBL 40 & 45.64. REPAIR CORRECTION TO THE RE INSPECTION SHOULD READ 56,000 FLIGHT CYCLE IAW SRM 57-10-10, REPAIR 3, FIG 204 & REPEAT AT 36,000 FLIGHT CYCLES INTERVALS, 57 DIP CONTROL NUMBER 28818.