What was found
CRACK ON HOLES ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR 2024-780250 <[01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[02] UT EQUIPMENT USED P/N: EPOCH 600; S/N: 120357005; DUE DATE: 10-JUN-25;[03] REPAIRED ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.; [04] REPAIRED ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.