What was found
CABIN FLOOR PANEL 221AF SURFACE IS PEELING.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR><BR>FOUND 2 AREAS OF UPPER SURFACE SKIN DAMAGE; BOTH AREAS ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B.<BR><BR>REPAIRS TO BE ACCOMPLISHED PER SRM 53-00-50-2R-1.<BR><BR>REMOVED 3EA THROUGH INSERTS TO FACILITATE REPAIRS IAW SRM 53-00-50-2R-1 PARA 3B.<BR><BR>REMOVED ALL DAMAGE NOTED AND CLEANED AREAS; OK TO POT EXPOSED CORE IAW SRM 53-00-50-2R-1 PARA 3A-E.;;[07] INSTALLED REPAIR PLIES USING BMS8-201 TYPE 3 LOT#AK2EP8210K; VACUUM BAGGED; LEAK CHECKED GOOD USING VACUUM GAUGE ID:ATS2441 DUE:08/2023 IAW SRM 53-00-50-2R-1 PAR.3 K(1)(B-C)- L(1);[08] VERIFIED CORRECTIVE ACTION 7;[09] CURED REPAIR PLIES UNDER HEAT LAMP USING THERMOMETER ID: ATS2208 DUE:10/2023 IAW SRM 53-00-50-2R-1 PAR.3 M(1);[10] VERIFIED CORRECTIVE ACTION 9;[11] UNBAGGED AND TRIMMED REPAIR PLIES THEN INSTALLED 3EA THROUGH INSERTS USING BMS5-107 LOT#AK2KP8383K AND CURED INSERTS USING HEAT LAMP AND THERMOMETER IAW SRM 53-00-50-2R-1 PARA 3N AND BOEING DWG 141A5810-728. <BR><BR>CURES ACCOMPLISHED USING THERMOMETER ATS2208 CAL DUE DATE 10/2023.;[12] FINAL INSPECTION. JOB COMPLETE.