What was found
FOLLOW UP TO NR 33, RT WING REAR SPAR WEB HAS A CIRCUMFERENTIAL DAMAGE AROUND FASTENER BORE LOCATED 4" INBD FROM INBD LOWER STUD, ON THE SECOND LOWER ROW OF PULLED FASTENERS. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY, NR FOR ADDITIONAL INFORMATION 035-0001:5710-01110-05/013 00035. REPAIR IAW PRI 548718-14, REV 2, ER/A 548718-14AD, REV A.