What was found
LEFT WING FIXED T/E WIGGLE PANEL I/B FWD STRUTS UPPER SUPPRT HAS 2EA ELONGATED HOLES ; / [01] STRIPPED FINISH FROM BOTTOM WING SKIN IN AREA OFWIGGLE PANEL PER BOEING SOPM 20-30-02.; [02] REMOVED WIGGLE PLATE AS PER B737-700 SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED NEW WIGGLE PLATE AS PER B737-700 SRM 51-40-05-0G-0.; [04] VERIFIES WORK PERFORMED; [05] OK TO TREAT; PRIME AND TOP COAT HOLES; [06] OK TO TREAT; PRIME AND TOP COAT WING SURFACE AREA; [07] APPLIED ALODINE; PRIMER; AND TOPCOAT TO HOLES AND WING SKIN AS PER B737-700 SRM 51-20-01-0G-0.; [08] VERIFIED WORK PERFORMED; [09] OK TO INSTALL; [10] INSTALLED NEW WIGGLE PLATE AS PER B737-700 SRM 51-40-02-0G-0.; [11] REPLACED WIGGLE PLATE AT L/W FIXED T/E WIGGLE PANEL I/B FWD STRUTS UPPER SUPPORT AS PER B737-700 SRM 51-40-02-0G-0.; [12] VERIFIED WORK PERFORMED