What was found
EGPR INTERNAL DOUBLER CRACKED AT FWD LOWER CORNER.<[01] REMOVED PAINT BY STRIPPING AT FUSELAGE SKIN R/H SIDE EGPR AREA REF B737-700 AMM 51-21-11-150-810.; LOCATED AND DRILLED NEW EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-05-0G-0.;[07] TREATED AND PRIMED DRILLED HOLES ON NEW EGPR INTERNAL DOUBLER REF B737-700 SRM 51-20-01-0G-0.;[08] VERIFIED STEPS 6 AND 7. OK TO INSTALL NEW EGPR DOUBLER.;[09] MIXED BMS 5-95 SEALANT 22:00 2/1/23. SQUEEZE OUT TIME BY 06:00 2/5/23.;[10] INSTALLED 90% OF FASTENERS AT EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 146A0640.;[11] COMPLETED INSTALLATION OF EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 146A0640.;[12] VERIFIED STEP # 10 AND 11;[13] VERIFIED STEP #9; SQUEEZE OUT TIME 100%; ALL FASTENERS INSTALLED.;[14] CORRECTION STEP 11 : COMPLETED INSTALLATION OF EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A0640 AND 141A3702.;] APPLIED TOP COAT AT FUSELAGE SKIN ON EGPR AREA REF B737-700 AMM 51-21-73-370-803.;[18] VERIFIED DRAWINGS STEP 14-15.;[19] VERIFIED 16-17.;[20] REMOVED AND REPLACED EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A0640.;[21] FINAL 20.