What was found
R/W FRONT SPAR INFERNAL UPPER CHORD FWD TIE-DOWN CLIP CRACKED ABOVE ACCESS PANEL621EB DEFUELING STATION MKD DOT<[01] REMOVED ACCESS PANEL # 621FB GAINED ACCESS TO REPAIR REF B 737-700 SRM 51-40-01;[02] PARTIAL REMOVED FASTENERS AT R/W UPPER CHORD FWD TIE DOWN ABOVE ACCESS PANEL 621EB REF B737-700 SRM 57-40-01;[03] REMOVED NOSE BEAM F/P AT R/W T/E SS 150.81 AND SS 48.97 IN REF SRM 51-40-02-0G-0;[04] LOCATED AND DRILED NEW NOSE BEAM P/N 116A5640Y18 REF. B737-700 SRM 51-40-05-0G-0;[13] PARTIALLY INSTALLED FASTENERS. 70% AT NOSE BEAM R/W FRONT SPAR ABOVE ACCESS PANEL 621 REF. B737-700SRM 51-40-02-0G-0;[14] COMPLETED INSTALLATION OF NOSE BEAM R/W FRONT SPAR ABOVE ACCESS PANEL 621EB 100% FASTENERS INSTALLED PER REF 51-40-02-0G-0 AND DWG 116A5640.;[21] (FINAL) REMOVED ACCESS PANEL # 621FB TO GAIN ACCESS TO NOSE BEAM REPLACEMENT; LOCATED; DRILLED; TREATED; PRIMED AND TOPCOAT NEW NOSE BEAM (P/N 116A5640Y18). INSTALLED NEW NOSE BEAM AND APPLIED CIC AND INSTALLED ACCESS PANEL # 621FB.;[22] VERIFIED STEPS 20 AND 21