As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT FUSELAGE WAS DENTED AT STA 218 BETWEEN LONGERON 18L AND 19L. LENGTH WAS 8 INCHES AND WIDTH 4 IN BY DEPTH 0.060. MADE AND INSTALLED NEW SHEAR TIE AT STA 218 PER SPM 6-70-01 PAGE 2 AND 3 AND DOUGLAS PRINT 9951888. INSTALLED SKIN REPAIR PER SRM.