What was found
FAULT - CRACK - ANGLE, MAIN EQUIPMENT CENTER LEFT SIDE AT STA 246 LBL 49.3.(REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-05 REV. 88. PERFORMED THE HEAT TREATMENT FROM 7075-O-063 CLAD TO T62 CONDITION. I.A.W. WORK SHEET NO.:40034 WORK INSTRUCTIONS STEP 3 AND SPWPS-HT-008 REV.:31 AND SPDS-HT-005 REV.:33 (REFER TO SHOP LOG NO:2024-017). FABRICATE P/N: 141T5146 PER BOEING DWG NO: 141T5146 SH. 15 REV."B"; PL REV."F"; PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV. 6 REQUIREMENT. 2. INSTALL FABRICATED PART I.A.W SRM 51-40-02-0G REV. 88 AND BOEING DWG NO. 141T5600 SH. 2 REV. E. 3. JOB COMPLETED. REVIEWED