What was found
L/H WING T/E ACCESS PANEL 561AB INTERNAL SKIN SURFACE HAS CRACKS AROUND MULTIPLE FASTENER HOLES.<[01] MEASUREMENT;[02] CLEANED AND PREPARED AREA AT L/H WING ACCESS PANEL 561AB; REPAIRED DAMAGE AREAS AT L/W ACCESS PANEL #561AB AS PER SRM 51-70-04-2R-9 .MATERIAL USED BMS9-3-120TYD CL7 PO#1690463 PLUS EY3804 A/B PO# 2008859; APPLIED TOP COAT AT L/H WING T/E ACCESS PANEL 561AB INTERNAL SKIN SURFACE AS PER AMM-51-21-73-370-803; AND SRM 51-70-04-2R-9-REPAIR 9-REPAIR OF DAMAGE TO A FASTENER HOLE WITH LAMINATING RESIN AND CHOPPED FIBER.;[03] VERIFIED STEP 1 AND 2