What was found
CRACK ON OUTBOARD FAN COWL SKIN 1 INCHES OF UPPER EDGE AND 2 INCHES OF FWD EDGE ENG 1 2024-340205<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23379002; DUE DATE: 18-FEB-25.;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 28-NOV-24;[03] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTE 600D. S/N: 220272712. DUE DATE: 28-NOV-24.;[04] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25.;[05] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 20-JUN-24 WAS USED ON STEP 18;[06] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811019; DUE DATE: 23-JAN-25.;[07] PERFORMED PERMANENT REPAIR ON ENGINE 1 OUTB FAN COWL SKIN PANEL AT UPPER FORWARD CORNER IAW B737-800 SRM 54-20-01-2R-13 REPAIR 13 AND EA #24-171-01532-WIP1 REV: 2<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[08] PERFORMED PERMANENT REPAIR ON ENGINE 1 OUTB FAN COWL SKIN PANEL AT UPPER FORWARD CORNER IAW B737-800 SRM 54-20-01-2R-13 REPAIR 13 AND EA #24-171-01532-WIP1 REV: 2; SEE INDIVIDUAL SIGNS-OFF BELOW.