What was found
PIT - DURING RON CHECK, 1.25 INCH RUNNING FORE AND AFT AT AFT PASSENGER DOOR FLOOR SILL PLATE SUPPORT ANGLE. INSTALLED DOUBLER REPAIR PER USAIR EA NR 28484A AND SRM 53-05 FIG 40. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING RON CHECK, 1.25 INCH RUNNING FORE AND AFT AT AFT PASSENGER DOOR FLOOR SILL PLATE SUPPORT ANGLE. INSTALLED DOUBLER REPAIR PER USAIR EA NR 28484A AND SRM 53-05 FIG 40. (M)