What was found
INSPECTION TYPE:C LT WING FRONT SPAR ENCLOSURE APPROX STA XORS 514 UPPER SKIN FOUND CRACKED. CRACK AREA TRIM OFF PER EN1007-08. HFEC CARRIED OUT IAW DAC NDT SPM R.13 PART06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB USING 7075-0-0.063" MAT`L PER SRM57-10-00 FIG 27V.1R.40 AND EN1007-08. FASTENER HOLES DRILLED ON REPAIR PARTS PER SRM 57-10-00 FIG 27 V.1R.40 AND EN1007-08. REPAIR PARTS PROTECTED PER SRM 51-21-01V.2R.40. OK TO INSTALL.