What was found
DURING BLOCK INSPECTION AT MSP, FOUND CRACK IN BELT FRAME RELIEF RADIUS AT FS 212.27 DUE TO A CRACK. REPAIRS WERE COMPLETED USING A DOUBLER AND STIFFENER IAW FAC SRM 53-90-20 REPAIR NR 20. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING BLOCK INSPECTION AT MSP, FOUND CRACK IN BELT FRAME RELIEF RADIUS AT FS 212.27 DUE TO A CRACK. REPAIRS WERE COMPLETED USING A DOUBLER AND STIFFENER IAW FAC SRM 53-90-20 REPAIR NR 20. (W)