What was found
DURING INSPECTION AS REQUIRED BY EO 4453A301 REV C CRACKS WERE FOUND AT 2 FASTENER HOLES AT BS 760 RT TENSION TIE, FORWARD CHANNEL (THE DAMAGE WAS REPAIRED AS IAW STEP 6 OF PART 2 OF EO 4453A301 REV C. PART 2 OF EO 4453A674 REQUIRES AND INITIAL INSPECTION AT 20,000 FLIGHT CYCLES AND REPEAT INSPECTIONS AT EVERY 3,000 FLIGHT CYCLES THEREAFTER.)