What was found
DTW - DURING ROUTINE B-CHECK INSPECTION OF THE NR 1 ENGINE, A 6 INCH CRACK WAS AT THE 12 O'CLOCK POSITION ON THE AFT FLANGE OF THE INTERMEDIATE CASE (FORWARD ENGINE SLING ATTACH POINT). ENGINE WAS REMOVED FROM THE AIRCRAFT. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DTW - DURING ROUTINE B-CHECK INSPECTION OF THE NR 1 ENGINE, A 6 INCH CRACK WAS AT THE 12 O'CLOCK POSITION ON THE AFT FLANGE OF THE INTERMEDIATE CASE (FORWARD ENGINE SLING ATTACH POINT). ENGINE WAS REMOVED FROM THE AIRCRAFT. (M)