What was found
INSPECTION TYPE:C LEFT WING FIXED WING FRONT SPAR ENCLOSURE APPROX STA XORS 506 UPPER SKIN FOUND CRACKED. CRACKED AREA TRIMMED OFF AS PER SRM 57-10-00 FIG.27V.1R.40. HFEC C/OUT IAW DA CNDTSPM R.13 PART 06-10-01.001, FOUND NO CRACK EVIDENT. REP ANGLES FAB USING 7075-0-0.063 MATL PER SRM 57-10-00 FIG 27 V.1R.40. REP ANGLES HEAT TREATED TO T6 COND PER DPS7.00-1 & HARDNESS OBTAINED HRB79.1, ACCEPTABLE PER DPS1-05-3. REP PARTS PROTECTED PER SRM 51-21-01V.2R.40. OK TO INSTALL.