What was found
CRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE. CRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE WAS REPAIRED PER REO: 670-54-22-181 REV- A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE. CRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE WAS REPAIRED PER REO: 670-54-22-181 REV- A.