What was found
STRINGER 26R IS CORRODED FROM FS 333.00 TO 364.00. INSTALLED AVIONICS FLOOR PANEL IAW AMM 53-00-47-400-801. INSTALLED NEW SERVICEABLE FWD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER 26R IS CORRODED FROM FS 333.00 TO 364.00. INSTALLED AVIONICS FLOOR PANEL IAW AMM 53-00-47-400-801. INSTALLED NEW SERVICEABLE FWD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.