What was found
DURING CHECK-C MAINT ON FWD CABIN FLOOR, THE DOOR ANGLE AT STA 160 TO 200, LBL 54, HAD CORROSION IN NUT PLATE HOLES, AND AT TWO RIVNUTS INSTALLED. FABRICATED NEW SUPPORT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT ON FWD CABIN FLOOR, THE DOOR ANGLE AT STA 160 TO 200, LBL 54, HAD CORROSION IN NUT PLATE HOLES, AND AT TWO RIVNUTS INSTALLED. FABRICATED NEW SUPPORT.