What was found
CRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] STEP 1 CORRECTED REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.