What was found
DURING INSPECTION, A PREVIOUS BLEND ON THE RIGHT CENTER FUSELAGE SKIN, SECTION I BETWEEN FRAME 16-17 AND STRINGER 19R-20R, WAS FOUND TO BE OUT OF LIMITS. THE DAMAGE WAS REPAIRED 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 PREVIOUS BLEND ON THE RIGHT CENTER FUSELAGE SKIN, SECTION I BETWEEN FRAME 16-17 AND STRINGER 19R-20R, WAS FOUND TO BE OUT OF LIMITS. THE DAMAGE WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-01.