What was found
DURING TRANSIT CHECK, FIVE BLADES WERE DETECTED DAMAGED DUE TO A FOD IN LT ENGINE. (4) BLADES WERE DETECTED WITH NICKS ON BLADES LEADING EDGE AND WERE REWORKED IAW MM 72-33-21 BEING WITHIN LIMITS. ONE BLADE WAS DETECTED WITH DENT WITH DEPTH OF 0.135 INCHES AND 5 INCHES FROM BLADE LEADING EDGE TO BLADE ROOT AND WAS REWORKED IAW MM 72-33-21 PARAGRAPH B-3B, CONDITIONED TO 24 FLIGHT HOURS. A BOROSCOPE INSPECTION TO 6TH AND 7TH STAGE COMPRESSOR WERE PERFORMED IAW MM 72-00-00, PAGE 635, NO DAMAGES WERE FOUND. (2) BLADES SETS OF FAN STAGE WERE REPLACED IAW MM 72-33-21 AND LT ENGINE WAS TESTED IAW 71-00-00, ALL CORRECT.