What was found
CRACKED ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207.<[01] NOT ALLOWABLE LIMITS APPLICABLE FOR SPECIFIC LOCATION PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207 I.A.W SRM 51-40-02-0G-0;[03] FABRICATED NEW ATTACH ANGLE FROM BAC1490-2883 7075-T0 CLAD LOT 1482272-1 AND HT ON R.O # 857528-SWA ALL I.A.W BOEING DWGS 273A9112;273A9110;273A9111 AND SRM 51-40-05-0G-0;[04] VERIFIED CORRECTIVE ACTION ITEM 1; 2; 3.<BR>OKAY TO TREAT AND PRIME PART GIVEN.<BR>VERIFIED MEASUREMENT TABLE COMPLETED.;[05] APPLIED CHEMICAL CONVERSION COAT AND PRIMED NEW ATTACH ANGLE ALL I.A.W SRM 51-20-01 AND SOPM 20-43-03. SOPM 20-41-02. AND BOEING DWG 273A9112 OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION ITEM 5.<BR>OKAY TO INSTALL ANGLE GIVEN.;[07] INSTALLED NEW ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207 I.A.W SRM 51-40-02-0G-0; BOEING DWGS 273A9112; 273A9110; 273A9111 COMPLETED TASK;[08] VERIFIED CORRECTIVE ACTION 7.