What was found
DURING INSPECTION AS REQUIRED BY EO 4453A301 REV C A CRACK WAS FOUND AT 1 FASTENER HOLE ON BS 760 LT TENSION TIE, FORWARD CHANNEL. (THE DAMAGE WAS REPAIRED IAW STEP 6 OF PART 1 OF EO 4453A301 REV C. INITIAL INSPECTION REQUIRED AT 20,000 FLIGHT CYCLES AND REPEAT INSPECTION EVERY 3,000 FLIGHT CYCLES THERE AFTER IAW PART 2 OF EO 4453A673. )