What was found
PANEL 195CL HAS A CRACK IN THE AFT EDGE LOWER RADIUS<[01] REPAIRED CRACK DAMAGE IN THE AFT EDGE LOWER RADIUS OF PANEL 195CL 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 195CL HAS A CRACK IN THE AFT EDGE LOWER RADIUS<[01] REPAIRED CRACK DAMAGE IN THE AFT EDGE LOWER RADIUS OF PANEL 195CL IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.