What was found
CABIN FLOOR PANEL 241 AF HAS FIBERS PEELING UPPER SURFACE CENTER A225-006 / [01] EVALUATED UPPER SURFACE DAMAGED FIBERS ON FLOORBOARD PANEL (241-AF) AND FOUND DAMAGE TO BE IN REPAIRABLE LIMITS I/A/W B737-800 SRM 53-00-50-2R-1 (3) A-N <BR>(REV 74);[02] CLEANED AND PREPPED UPPER SURFACE AT DAMAGED FIBERS AREA TO FLOORBOARD PANEL (241-AF) FOR WET-LAYUP REPAIR I/A/W B737-800 SRM 53-00-50-2R-1 (3) E-G (REV 74);[03] VERIFIED MATERIALS FOR REPAIR<BR>FABRIC BMS9-3TY H3 (A13437)<BR>RESIN EPOCAST 50A1/946 (E82891)<BR>I/A/W B737-800 SRM 53-00-50-2R-1 (2)A(1) REV 74;[04] NEED OK TO BOND FIBERGLASS REPAIR ON UPPER SURFACE OF FLOORBOARD PANEL (241-AF);[05] VERIFIED STEPS 1 THRU 4;[06] OK GIVEN TO BOND REPAIR;[07] BONDED REPAIR ON UPPER SURFACE TO DAMAGED FIBERS WITH WET LAY-LAYUP ON FLOORBOARD PANEL (241-AF) I/A/W B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 74);[08] REPAIRED UPPER SURFACE DAMAGED FIBERS ON FLOORBOARD PANEL<BR>(241-AF) WITH WET-LAYUP REPAIR I/A/W B737-800 SRM<BR>53-00-50-2R-1 (3) A-N (REV 74).;[09] VERIFIED STEPS 7 AND 8;[10] JOB COMPLETE; AUDIT C/W