What was found
LOWER FUSELAGE ACCESS PANEL 194E SEVERAL FASTENER HOLE ELONGATED / [01] ACCOMPLISHED VISUAL INSPECTION FOUND ALL HOLES DAMAGE AS PER B737 NTM 51-05-01 AND PREPARED AREA FOR DRY PROCCES AS PER B737 SRM 51-70-05-2R-0.;[02] VERIFIED STEP #1;[03] ACCOMPLISHED DRY PROCESS AT PANEL 194E AS PER B737 SRM 51-70-05-2R-0;[04] VERIFIED STEP 3<BR>OK TO INSTALL REPAIR;[05] INSTALLED THE REPAIR PLIES AT DAMAGED AREA ON ACCESS PANEL 194E. REF B737-700 SRM51-70-05-2R-8 PARAGRAPH 4 D;E;F AND G; REF B737-700 SRM 51-70-05-2R-0 PARAGRAPH 4.;[06] VERIFIED STEP 5;[07] APPLIED FINISH TOP COAT AT REPAIRED PANEL #194E; AS PER B737-7 AMM 51-21-73=370-803.;[08] VERIFIED STEP 7