What was found
CORROSION. ** R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE O/B OF FLAP TRACK # 8 ; / [01] REMOVER NUT PLATE FOR ACCESS AT R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE IAW B737 SRM 51-40-02-0G -0.; [02] REMOVED CORROSION AT R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE IAW B737 SRM51-10-02-0G-0.; [03] CORRECTION STEP1. REMOVED NUT PLATE FOR ACCESS AT R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE IAW B737 SRM 51-40-02-0G -0.; [04] (AMENDING STEP 1) REMOVED NUT PLATE FOR ACCESS AT R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE O/B OF FLAP TRACK #8 IAW B737 SRM 51-40-02-0G -0.; [05] AMENDING STEP2. REMOVED CORROSION AT R/W REAR SPAR FIXED T/E LOWER SUPPORT ANGLE O/B OF FLAP TRACK #8 IAW B737 SRM 51-10-02-0G-0; [09] REWORK EVALUATION; FOUND LOWER PANEL SUPPORT ANGLE OUT OF LIMITS AS PER B737-7 SRM 57-51-02-1A-1 SEC 4B. DET D. <BR>MATERIAL REMOVED 0.014''; MAT REMAINING 0.066''; ORIGINAL MATERIAL 0.080''.; [10] REWORK EVALUATION; FOUND LOWER PANEL SUPPORT ANGLE OUT OF LIMITS AS PER B737-7 SRM 57-51-02-1A-1 SEC 4B. DET D. <BR>MATERIAL REMOVED 0.014''; MAT REMAINING 0.066''; ORIGINAL MATERIAL 0.080''.;HT WING REAR SPAR FIXED T/E LOWER SUPPORT ANGLE FLAP TRACK #8.; [14] FABRICATED NEW ANGLE AND LOCATED AND DRILLED AND COUNTERSINK AT R/WING REAR SPAR FIXED T/E LOWER SUPPORT ANGLE O/B FLAP TRACK IAW SRM51-40-05-0G-0 AND SRM51-40-08-0G-0.