What was found
PANEL 195CL OUTER COMPOSITE PUNCTURED 12-13 INCHES FORWARD OF AFT EDGE 4-5 INCHES UP FROM BEND. REPAIRED PUNCTURE ON PANEL 195CL, IAW SRM 51-70-04-2R-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 195CL OUTER COMPOSITE PUNCTURED 12-13 INCHES FORWARD OF AFT EDGE 4-5 INCHES UP FROM BEND. REPAIRED PUNCTURE ON PANEL 195CL, IAW SRM 51-70-04-2R-10.