What was found
VERTICAL FIN L/E FRONT SPAR FITTING FIX AFT EDGE SPRING ANGLE 2EA. CRACKS NOTED (DOT 223-VLE002). VERTICAL FIN L/E FRONT SPAR FITTING FIX FWD EDGE SPRING ANGLE 2EA. CRACKS NOTED (DOT 223-VLE002). / [01] REMOVED FWD SPRING ANGLE AT VERTICAL FIN L/E FRONT SPAR FITTING FIX AS PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW FWD SPRING ANGLE AT VERTICAL FIN L/E FRONT SPAR FITTING FIX AS PER B737-700 SRM 51-40-05-0G-0.;[03] VERIFIED STEPS #1 AND #2; REPLACEMENT FWD SPRING ANGLE LOCATED AND DRILLED.;[04] OK TO TREAT AND PRIME DRILLED HOLES.;[05] APPLIED ALODINE AND PRIMER AT NEW FWD SPRING ANGLE HOLES AT VERTICAL FIN L/E FRONT SPAR FITTING FIX AS PER B737-700 SRM 51-20-01-0G-0; AMM 51-21-72-370-801.;[06] VERIFIED STEP #5.<BR> OK TO INSTALL NEW FWD SPRING ANGLE.;[07] PARTIALLY INSTALLED NEW FWD SPRING ANGLE AT VERTICAL FIN L/E FRONT SPAR FITTING FIX AS PER B737-700 SRM 51-40-02-0G-0; DWG # 176A3001.;[08] (RII) VERIFIED STEP #7; FWD SPRING ANGLE PARTIALLY INSTALLED.;[09] COMPLETED INSTALLATION OF FWD SPRING ANGLE AT VERTICAL FIN L/E FRONT SPAR FITTING FIX AS PER B737-700 SRM 51-40-02-0G-0; DWG # 176A3001;[10] REMOVED AND REPLACED FWD SPRING ANGLE AT VERTICAL FIN L/E FRONT SPAR FITTING FIX AS PER B737-700 SRM 51-40-02-0G-0; DWG # 176A3001;[11] VERIFIED STEPS 9 AND 10