What was found
SUPPLEMENTAL INFORMATION: PANEL 194E HAS 5 EACH SCREW HOLES CRACKED AT FWD END OF PANEL. PER GENERATING DOC REPAIR PER SRM 53-60-70. SIGN OF STEP 9 OF GENERATING DOC AFTER REPAIR (SEQ 168) ; DOT 8-25 / [01] MEASUREMENTS; [02] PERFORMED TAP TEST ON PANEL #194E ON DAMAGED AREA AND FOUND DELAMINATION ON MULTIPLE FASTENER HOLES AS PER B737 NDTM 51-05-01; [03] PREPARED DAMAGED AREA ON PANEL #194E FOR REPAIR AS PER B737 SRM 51-70-04-2R-9 AND SRM 53-40-70-2R-1; [04] VERIFIED 1-3.; [05] REPAIRED DAMAGED AREA AT PANEL 194E PER B737 SRM 51-70-04-2R-9 MATERIAL USED RESIN EY3804 PO#1753536 FIBERGLASS PO#1129190; [06] VERIFIED STEP 5 <BR>OK TO TOP COAT; [07] APPLIED TOP COAT FINISH PER AMM 51-21-73-370-803.; [08] REPAIRED DAMAGED AREAS; 5 EACH SCREW HOLES AT PANEL 194E PER B737 SRM 51-70-04-2R-9.; [09] CORRECTION TO STEP 3: PREPARED DAMAGED AREA ON PANEL #194E FOR REPAIR AS PER B737 SRM 51-70-04-2R-9 AND SRM 53-60-71-2R-1; [10] VERIFIED 7-9.