What was found
DURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON STRINGER 20R BETWEEN FRAME 15-16. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON STRINGER 20R BETWEEN FRAME 15-16. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21-01.