What was found
SUPPLEMENTAL INFORMATION: PANEL 195CL HAS CRACK ON AFT END IN THE RADIUS OF THE BEND. / APPLIED REPAIR PLIES AND BONDED PER SRM 51-70-05 REPAIR 6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUPPLEMENTAL INFORMATION: PANEL 195CL HAS CRACK ON AFT END IN THE RADIUS OF THE BEND. / APPLIED REPAIR PLIES AND BONDED PER SRM 51-70-05 REPAIR 6.