As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING NR 2 ENGINE CHANGE, FOUND 7.5 INCH LONG CRACK IN THE TOP OF THE ''S'' DUCT ALONG THE LONGITUDINAL AXIS APPROXIMATELY 3 FEET IN FRONT OF THE ENGINE INLET. THERE IS ALSO A CRACK IN THE AFT ATTACHMENT FLANGE OF THE ANTI-ICE MANIFOLD ON THE TOP SIDE OF THE DUCT. THE MANUFACTURER HAS BEEN NOTIFIED AND ARE CURRENTLY WORKING WITH ENGINEERS TO EFFECT A REPAIR IF POSSIBLE. (X)