As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PAX DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED CHAFED AREA, REQUESTED NDT FOR CRACK CHECK NO DEFECTS WERE NOTED. ORIGINAL MATERIAL THICKNESS WAS 1.700". AFTER RE-WORK MATERIAL THICKNESS IS 1.665". A TOTAL LOSS OF .035. TOTAL ALLOWABLE LOSS IS .050". PAX DOOR FWD PULL-IN LEVER FOUND TO BE WITH-IN LIMITS IAW REO.