As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHECK DENT AT STA NR 896 W/L236 ACFT GROUNDED. CHECKED LIMITS ON FUSELAGE SKIN AT STA 896 W/L 236 ORIGINAL THICKNESS IS .100 WIDTH IS .650 AND LENGTH IS 3 DEPTH IS .020 W/Y=32.5 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01 TOPCOAT IAW AMM 51-21-44.