What was found
ON PRE-FLIGHT INSP SUSPECT CRACK RT WING LE PANEL INBD RADIUS OF SLAT DRIVE MECHANISM DOOR CUT OUT. VERIFIED AREA TO BE CRACKED IAW NDT SPM PART 6. CRACK IS MARKED WITH PERMANENT MARKER. CUT OUT DAMAGE IAW SRM 57-40-02. NEED NDT TO INSPECT FOR DAMAGE REMOVAL. HFEC INSPECTED DAMAGE CUT OUT IAW NDT SPM 06-10-01, NO DEFECTS NOTED. FABRICATED DOUBLER FROM .063" 6AL4V TI MP2338177 & FILLER FROM .090" 7075-T6 AL MP1681501 IAW SRM 57-40-02 REPAIR 7. NEED OK TO INSTALL. REPAIRED IAW SRM 57-40-02 FIGURE 202.