What was found
CRACK ACCESS PANEL 194HL BODY FAIRING AT FUSELAGE EXTERIOR 2024-766342<[01] TOOL USED: HOTBONDER: P/N: HCS9200B S/N: 18185847 DUE DATE: 01-OCT-25;[02] TOOL USED ON STEP 10: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 600; S/N: 120357005; DUE DATE: 10-JUN-25;[03] TOOL USED: SCALE: P/N: SPX621 S/N:8340225489 DUE DATE: 22-FEB-25.;[04] TOOL USED MULTIMETER P/N: FLUKE 87 ; S/N: 42180179 ; DUE DATE: 26-MAR-25 ; HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH8P3 ; S/N: 19104817 ; DUE DATE: 21-MAR-25.;[05] REPAIRED ACCESS PANEL 194HL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[06] REPAIRED ACCESS PANEL 194HL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10. REFER TO INDIVIDUALS SIGNOFFS BELOW.