What was found
PANEL 195CR HAS CRACK TO AFT LOWER CORNER EDGEBAND ON INNER SURFACE<[01] CRACK AT AFT LOWER CORNER EDGEBAND ON INNER SURFACE OF PANEL 195CR WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 195CR HAS CRACK TO AFT LOWER CORNER EDGEBAND ON INNER SURFACE<[01] CRACK AT AFT LOWER CORNER EDGEBAND ON INNER SURFACE OF PANEL 195CR WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.