What was found
PANEL BREAK CRACKED AT BS 538; RBL 1; WL 208<[01] ALL STEPS COMPLETED REMOVED PASSENGER CABIN FLOOR PANEL 231UF PER AMM 53-21-00-000-801.REMOVED PANEL BREAK AT BS 538; RBL 1; WL 208 PER SRM 51-40-02LOCATED AND DRILLED NEW PANEL BREAK AT BS 538; RBL 1; WL 208 PER SRM 51-40-05-0G-0 BOEING DWG 143A0060 SHEET #64 BOEING DWG 143A5240 SHEET #14.INSTALLED PANEL BREAK ASSY AT BS 538; RBL 1; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 143A0060.INSTALLED PANEL 231UF PER AMM 53--21-00-400-801<BR><BR>TORQUE GUN ID# ATS1699 DATE : 04-24;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE