What was found
FUSELAGE FRAME AT FS 364.00 IS CORRODED ON FWD SIDE OF FRAME BETWEEN STRINGER 25L & STRINGER 26R. C-CHECK REPLACED FS 364.00 LOWER FRAME SECTOR BETWEEN STRINGER 25L & 26R IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT FS 364.00 IS CORRODED ON FWD SIDE OF FRAME BETWEEN STRINGER 25L & STRINGER 26R. C-CHECK REPLACED FS 364.00 LOWER FRAME SECTOR BETWEEN STRINGER 25L & 26R IAW SRM.