What was found
CORROSION ON RIGHT WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING JUMPER IFSS119. MARKED<[01] VERIFIED APLICABILITY SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3;[02] REMOVED CORROSION ON R/H WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING JUMPER PER SRM 57-20-10-1A-3;[03] DO A FLOURESCENT PENETRANT INSPECTION OF REWORKED AREA;[04] VISUALLY INSPECTED THE REWORK AREA ON THE FRONT SPAR BOOST PUMP UPPER BONDING JUMPER POINT. NO CORROSION NOTED VISUALLY.;[05] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO DEFECTS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2504-A; B; C CAL DUE: 05/23;[06] UT REQUEST AT REWORKED AREA TO VERIFY REMAINING THICKNESS; ORIGINAL THICKNESS 0.480 IAW SRM 57-20-10-1A-3; SEE GRID MAP ATTACHED 0.250' X 0.250';[07] ACCOMPLISHED UT THICKNESS INSPECTION IAW 737 NDTM PART 4 CHAPTER 51-00-00 PROCEDURE 2.<BR>REMAINING MINIMUM MATERIAL 0.286' SEE ATTACHED GRID.<BR><BR>EQUIPMENT USED: EPOCH 650 ID: ATS2342 CAL DUE: 07/2023;[08] PERFORMED FLAP PEEN AT REWORKED AREAS AT FRONT SPAR AROUND BOOST PUMP UPPER AND LOWER BONDING JUMPER IAW 57-20-10-1A-3<BR>FLAP PEEN KIT ID: ATS 2771 S/N 22181705 DUE: 07/2023.<BR>TACHOMETER ID: ATS 127 S/N: 1372941 DUE: 03/2023;[09] VERIFIED CORRECTIVE ACTION 8.;[10] VERIFIED THE MEASUREMENT TABLE.;[21] THE DAMAGE WAS REPAIRED PER 737-700 SRM 57-20-10; ALLOWABLE DAMAGE 3 AND EA 23-157-00357;