What was found
FAULT - CRACK, CENTER WING FRONT SPAR STIFFENR AT STA 785.9 LBL 11 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-10-2R-2 REV.91 AND EGAT WORK SHEET NO. 50137, UPS SREO-58151-REQ001 REV1, BOEING DWG NO. 111T5200 SH 2 REV: B, 140T0520 SH 23 REV: -, 111T2000 SH 20 REV: F, SH 21 REV: J AND SH 22 REV: G. PAPER FINAL CHECK COMPLETED.