What was found
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT FUSELAGE LOWER BELT FRAME RELIEF RADIUS AT FS 144 AND BL 8. STOP DRILLED THE CRACK AND INSTALLED A DOUBLER AND STIFFENER IAW SRM 53-90-20. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT FUSELAGE LOWER BELT FRAME RELIEF RADIUS AT FS 144 AND BL 8. STOP DRILLED THE CRACK AND INSTALLED A DOUBLER AND STIFFENER IAW SRM 53-90-20. (M)