As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FUSELAGE SKIN AT FS 159.24 AND WL 75.13 CRACKED TRANSVERSELY. CRACK LENGTH APPROXIMATELY 0.450 INCH. FABRICATED AND INSTALLED A 0.032 INCH BY 4.00 INCH BY 4.00 INCH SURFACE REPAIR DOUBLER TO AFFECTED AREA IAW FAIRCHILD SRM 51-90-04, PAGES 7-8, REV. 6-1-93. (X)