What was found
CORROSION ON STRINGER 26RH IN FS= 333 TO FS= 349 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STRINGER 26RH IN FS333 TO FS364 WAS REMOVED AND NEW STRINGER 26RH WAS INSTALLED PER CRJ900 SRM 51-42-06-001-001-A01 PAR. 6C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON STRINGER 26RH IN FS= 333 TO FS= 349 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STRINGER 26RH IN FS333 TO FS364 WAS REMOVED AND NEW STRINGER 26RH WAS INSTALLED PER CRJ900 SRM 51-42-06-001-001-A01 PAR. 6C.