What was found
EVIDENCE OF CRACK BETWEEN WR 200.8 & 192.0 BETWEEN LBL 36 & 42 CTR WING BOX REAR SPAR CERT. WEB LOCATED ON LT MLG WW AREA. REPAIRED IAW SRM 57-10-10 REPAIR 3 FIG 204 IAW FORM 44-0008. ISSUED DIP, CAT B REPAIR SUBJECT TO INSP IAW SRM 57-10-10 TABLE 20 4 REPAIR 3 & FIG 206 REPAIR 3 WITH HFEC INSP AT 56000 FLIGHT CYCLES AFTER INSTALL & INTERVAL OF 36000 FLIGHT CYCLES AFTER IAW NDT PART 6 51-00-00 PROCEDURE 4.