What was found
LEFT SIDE BODY OVERWING FAIRING ACCESS PANEL #195CL; SEVERAL SCREW HOLES ELONGATED/SURFACE BULGE AND INTERNAL WEAR NOTED. / [01] REMOVED LEFT SIDE BODY OVERSWING FAIRING ACCESS PANEL #195CL SRM51-40-02-0G-0.;[02] VERIFIED AND INSPECTED STEP#1.;[03] CLEANED AND PREPARED DAMAGE FASTENERS HOLES FOR REPAIR ;PERFORMED DRY OUT; NO WATER FOUND ON LEFT SIDE BODY OVER WING FAIRING ACCESS PANEL #195CL AS PER B737 SRM 51-70-04-2R-9;[04] OK TO INSTALL REPAIR.;[05] REPAIRED DAMAGE FASTENERS HOLES AND INTERNAL WEAR AREA AS MARKED WITH A PERMANENT REPAIR ON LEFT SIDE BODY OVER WING FAIRING ACCESS PANEL #195CL AS PER B737 SRM 51-70-04-2R-9; MATERIALS USED PO#1690463 AND PO#1774613;[06] PERFORMED TAP TEST ON REPAIRED AREA ;FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[07] VERIFIED STEPS #5 AND #6.<BR> OK TO PRIME AND TOP COAT ALL REPAIRED AREA.;[08] APPLIED TOP COAT REPAIR AREA AS PER AMM 51-21-73-370-803.;[09] VERIFIED TOP COAT APPLICATION AS PER STEP#8 .;[10] INSPECTION C/W AT FUS. TO UPPER LT./WING TRAILING EDGE BEHIND PNL. #195CL LOCATUION CIC /OK ; AREA READY FOR PNL./ INSTALLATION. OK TO INSTALL PNL. # 195CL ....;[11] REINSTALLED LEFT SIDE BODY OVERSWING FAIRING ACCESS PANEL #195CL SRM51-40-02-0G-0.;[12] VERIFIED STEP #11 ; ALL WORK COMPLETED...