What was found
AFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL. ROUGH-CUT FLOOR PANEL USING BMS4-17 TYPE VI LOT 1531501-1 AND DETERMINED INSERT HOLE LOCATIONS; WORK PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 4 AND BOEING DRAWING 147A5810 SHEET 8.;[02] UPSIZED INSERT HOLE LOCATIONS TO 1/2' DIAMETERS; INSTALLED INSERTS WITH BMS5-107 LOT 1538621-1 RESIN AND CURED A RESIN UNDER A HEAT LAMP USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023; WORK PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A.(1) AND TABLE 204; ALSO IAW BOEING DRAWING 147A5810-8.;[03] VERIFIED CORRECTIVE ACTION 1 & 2 AND MEASUREMENTS TABLE.;[04] AFT FLOOR PANEL 241AAF WITH UPPER SKIN PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-0.;[05] VERIFIED FLOOR PANEL 241AAF REPAIRED VIA FABRICATION PER SRM 53-00-50-2R-0 PARAGRAPH 4 AND BOEING DRAWING 147A5810 SHEET 8.