What was found
R WING DEFLECTION CONTROL RIB HAS 2EA ELONGATED FASTENER HOLES.(MARKED)<[01] INSPECTED DEFLECTION CONTROL RIB UPPER TAB ELONGATED FASTENER HOLES AND FOUND TO BE OUT-OF-LIMITS PER SRM 57-51-02-1A-1;[02] VERIFIED DEFLECTION CONTROL RIB UPPER TAB FOUND BE OUT OF LIMITS;[03] CUT AND REMOVED DAMAGE FROM DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-4.;[04] VERIFIED WORK ACCOMPLISHED IN C/A #3;[05] PERFORMED HFEC SURFACE INSPECTION ON THE CUTOUT PER BOEING NDT MANUAL PART 6 51-00-00 PROCEDURE 23. PERFORMED A HFEC HOLE PROBE ON THE DEFLECTIION RIB PER BOEING NDT MANUAL PART 6 51-00-00 PROCEDURE 16. NO DEFECTS FOUND.;[06] FABRICATED -2 FILLER PER SRM 57-51-02-2R-4.;[07] INSPECTED C/A 6.;[08] LOCATED; DRILLED AND DEBURRED REPAIR PARTS PER SRM 57-51-02-2R-4.;[09] INSPECTED C/A 8.;[10] TREATED; PRIMED AND APPLIED ENAMEL FINISH TO REPAIR FILLER AND REPAIR AREA PER SRM 57-51-02-2R-4.;[11] VERIFIED CORRECTIVE ACTION #10;[12] OK TO INSTALL;[13] INSTALLED REPAIR PARTS PER SRM 57-51-02-2R-4.;[14] VERIFIED CORRECTIVE ACTION #13;[15] INSPECTED DEFLECTION CONTROL RIB UPPER TAB ELONGATED FASTENER HOLES AND FOUND TO BE OUT-OF-LIMITS PER SRM 57-51-02-1A. CUT AND REMOVED DAMAGE FROM DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-4. INSTALLED REPAIR PARTS PER SRM 57-51-02-2R-4. SEE ATTACHED SIGN OFFS FOR ALL WORK PERFORMED.;[16] SEE INDIVIDUAL SIGN OFFS FOR WORK COMPLETED<BR>INSPECTED AS REQUIRED