What was found
FUSELAGE FRAME AT FS310.00 IS CORRODED FROM STR 26LH TO 26RH. AND ON THE AFT VERTICAL SURFACE. -C/A-REPAIRED FUSELAGE FRAME AT FS310.00 IAW SRM 53-00-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT FS310.00 IS CORRODED FROM STR 26LH TO 26RH. AND ON THE AFT VERTICAL SURFACE. -C/A-REPAIRED FUSELAGE FRAME AT FS310.00 IAW SRM 53-00-06.