What was found
VERTICAL FIN FRONT SPAR FITTING; FIX LEADING EDGE SPRING ANGLE CRACK NOTED. ; / [01] REMOVED FIX LEADING EDGE SPRING ANGLE AT VERTICAL FIN FRONT SPAR FITTING IAW SRM 51-40-02-0G-0.; [02] VERIFIED STEP #1; [03] LOCATED AND DRILLED NEW FITTING FIX LEADING EDGE VERTICAL FIN FRONT SPAR SPRING ANGLE IAW B737-700 SRM 51-40-05-0G-0 AND DWG# 176A3101.; [04] (RII) VERIFIED STEP #3; [05] OK TO INSTALL NEW REPLACEMENT FIX L/E SPRING ANGLE.; [06] MIXED 0870C080BM654SKN40 SEALANT 17:00 12-01-21 SQUEEZE OUT TIME BY 03:00 12-05-21; [07] INSTALLED NEW FITTING FIX LEADING EDGE VERTICAL FIN FRONT SPAR SPRING ANGLE IAW B737-700 SRM 51-40-02-0G-0AND DWG# 176A3101; [08] (FINAL) REMOVED FIX LEADING EDGE SPRING ANGLE AT VERTICAL FIN FRONT SPAR FITTING IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW FITTING FIX LEADING EDGE VERTICAL FIN FRONT SPAR SPRING ANGLE IAW B737-700 SRM 51-40-05-0G-0 AND DWG# 176A3101. INSTALLED NEW FITTING FIX LEADING EDGE VERTICAL FIN FRONT SPAR SPRING ANGLE IAW B737-700 SRM 51-40-02-0G-0AND DWG# 176A3101; [09] (RII) FINAL INSPECTION; FIX L/E SPRING ANGLE REPLACED.