What was found
DURING CPEP INSPECTION PER C53-224-06, IT WAS NOTED, 'R-2 DOOR THRESHOLD SILL ANGLE CORRODED AND CRACKED'. NEW PARTS WERE FABED AND INSTALLED IAW B727-SRM 51-20-01, PAGE 68.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CPEP INSPECTION PER C53-224-06, IT WAS NOTED, 'R-2 DOOR THRESHOLD SILL ANGLE CORRODED AND CRACKED'. NEW PARTS WERE FABED AND INSTALLED IAW B727-SRM 51-20-01, PAGE 68.