What was found
RT WING #8 SLAT LWR SURFACE HAS A SUSPECTED CRACK AT I/B HILOCK 2ND FROM FWD FASTENER SLAT STA 451.50. 8-9 / [01] PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK CONFIRMED EMANATING FROM I/B AFT FASTENER. CRACK LENGTH : 0.748';[17] INSTALLED ACCESS PANELS #625EB; 625CB; 625DAB; 625DBB; AND FLEX SKIN PANEL AT R/W. SLAT #8 AS PER B-737-700 SRM.51-40-02-0G-0;[18] ACCOMPLISHED PERMANENT REPAIR AT R/W. SLAT #8 AS PER B-737-700 SRM. 57-42-01-2R-8;[19] VERIFIED STEPS 17 AND 18.