What was found
CRACK ATTACHED ANGLE AT THE MID CABIN BS 717 RBL 3<[01] UPDATED STEP 2.;[02] REMOVED AND REPLACED WITH NEW CRACK ATTACHED ANGLE AT THE MID CABIN BS 717 RBL 3. HFEC INSPECTED AREA IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>CRACK NOTED. MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 07/2025. REMOVED ATTACHED ANGLE AT THE MID CABIN BS 717 RBL 3 PER SRM 51-40-02-0G-0. ANGLE FORMED; HEAT TREATED ON P.O# 857528/1. PO: 857528-SWA.<BR><BR>FABRICATED; LOCATED; DRILLED; DEBURRED NEW ATTACH ANGLE MID CABIN BS 717 RBL 3. (REF: DWG 273A9112 REV: -; 273A9111 REV: - ). APPLIED CHEMICAL CONVERSION COATING TO STRINGER CLIP PER SOPM 20-43-03<BR>APPLIED BMS10-11 PRIMER TO ATTACH ANGLE. PER AMM 51-21-72-370-804.INSTALLED ATTACH ANGLE AT THE MID CABIN BS 717 RBL 3 PER SRM 51-40-02; BOEING DWG# 273A9111 REV:-;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.