What was found
RIGHT HAND FUSELAGE SKIN DAMAGED STA 37 TO STA 110. INSTALLED NEW SKIN PANEL FROM STA 37 TO STA 110, BETWEEN L18R AND L27R AS PER DWG 5911400 AND B717 SRM 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT HAND FUSELAGE SKIN DAMAGED STA 37 TO STA 110. INSTALLED NEW SKIN PANEL FROM STA 37 TO STA 110, BETWEEN L18R AND L27R AS PER DWG 5911400 AND B717 SRM 51-40-2.