What was found
L2 DOOR SILL FR68 HAS CORROSION AROUND THE LAST TWO NUT PLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION AND FABBED REPAIR DOUBLER AND INSTALLED IAW SRM 53-41-14 PARA 5A FIG201 REPAIR PRINCIPLE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L2 DOOR SILL FR68 HAS CORROSION AROUND THE LAST TWO NUT PLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION AND FABBED REPAIR DOUBLER AND INSTALLED IAW SRM 53-41-14 PARA 5A FIG201 REPAIR PRINCIPLE 5.