What was found
PERFORMED DETAIL VISUAL INSP. OF THE OUTER WING, UPPER SPAR CAP (P/N ARB7413-2) FROM STATIONS XORS-1041.500 THROUGH XORS-1044.000 PER FOLLOW UP E.A. 1-5720-87643 AND W/C SEQ. #000806, W/C #T-1-5720-87643 P2. FOUND CORROSION BETWEEN AREAS X0RS- 1035.500 THROUGH X0RS-1044.000. 5121818: CONSIGNADO, FREDERICK J - 12-FEB-2020 18:10 REF E.A 1-5710-T0351904 " WINGS - BASIC WING STRUCTURE - RH WING REAR SPAR UPPER GAP AFT LEG - REWORK" REMOVED CORROSION AND REPAIRED TOP WING SPAR PER EA T1-5710-Y0351904. WORKED ACCOMPLISHED ON N/R 1206 & N/R 507 "MAJOR REPAIR" AMT# EA 5082867, RII: QC# 5156615, 02/11/20 JPF ITEM 1: EMP: NMS 911637, RII: RII, OPEN WORK ITEM; CORROSION IN INDICATED AREA RE REQUIRES BLEEDING CORRECTIVE ACTION: BLENDED CORROSION IAW SRM 57-00-00-2R., MECH: NMS 911637, INSP: QC# 97952, 11/06/20 ITEM 2: EMP: NMS 911637, RII: RII, OPEN WORK ITEM: REQUEST NDT CHECK BLENDED AREA FO FOR REMAINING MATERIAL THICKNESS CORRECTIVE ACTION: PERFORMED UT THICKNESS MEASUREMENT PER NDTSPM TP-MDC- 93K0393 MINIMUM THICKNESS MEASURED IS .035 INCH MAXIMUM THICKNESS MEASURED I IS .115 INCH. MECH: N/A QC 97952, INSP; QC# 97952, 11/07/19