What was found
DURING ROUTINE C CHECK INSPECTION, NR 2 ENGINE, T/R LT INTERNAL PART FRAME CRACKED 2 AT 10 O’CLOCK POSITION, YN 208.000. REMOVED DEFLECTION FAIRING SEAL, PERFORMED STOP HOLE OF 0.06 IAW CFM 56-2 MM 78-31-41 REP. 016 PAGE 2. FAB`D STIFFENER (STEEL SHEET 0.080 AMS 5504) IAW CFM 56-2 MM 78-31-41 REP. 016 PAGE 2. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW STIFFENER WITH BLIND BOLTS AND REINSTALLED DEFLECTION FAIRING SEAL IAW CFM 56-2 MM 78-31-41 REP 016 PAGE 2.