What was found
(CAN) 1.5 INCH CRACK FOUND ON COMPRESSOR SCROLL STARTING ALONG AFT RADIUS OF SCROLL PROGRESSING TOWARD DISCHARGE ELBOW AND TURNING TO MIDDLE OF OUTSIDE FACE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) 1.5 INCH CRACK FOUND ON COMPRESSOR SCROLL STARTING ALONG AFT RADIUS OF SCROLL PROGRESSING TOWARD DISCHARGE ELBOW AND TURNING TO MIDDLE OF OUTSIDE FACE.